N942DL

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,736 hrs · 54,286 cycles

DURING A SERVICE CHECK, FOUND THE EMERGENCY LIGHTS OUT FROM ROW 31 AFT. REPLACED THE FUSE IN THE BATTERY PACK IAW AMM 33-53. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,656 hrs · 54,219 cycles

EMERGENCY LIGHTS IN FLIGHT DECK AND FWD GALLY INOPERATIVE. REPLACED THE BATTERY IAW AMM 33-53. LIGHTS TESTED GOOD. ACFT OK FOR SERVICE.

Part: COVER — LOOSE (R1 DOOR SLIDE) · airframe 72,656 hrs · 54,219 cycles

R1 DOOR SLIDE COVER LOOSE. R & R THE R1 DOOR SLIDE IAW W/C 2561-4964.

Part: STRUCTURE — CRACKED (LT WING) · airframe 72,027 hrs · 53,739 cycles

DURING WALK AROUND, FOUND A TWO INCH CRACK ON LEADING EDGE UNDER THE LT WING NR 2 SLAT OTBD END. REPAIRED.

Part: STRUCTURE — CRACKED (LT WING) · airframe 72,027 hrs · 53,739 cycles

LEFT WING L/E CRACKED INBD OF XOS 286. REPAIRED IAW SRM 57-06B, AND RI 557795-14 REV 18.

Part: SKIN — PUNCTURED (B 673) · airframe 71,146 hrs · 53,126 cycles

FOUND HOLE IN LOWER FUSELAGE AT BS 673 LONGERON 29R. REPAIRED IAW ER/A 553576-14.

Part: COMPUTER — MALFUNCTIONED (ANTI SKID SYS) · airframe 71,143 hrs · 53,124 cycles

NUMBERS 3 AND 4 MAIN TIRES BLEW ON LANDING. MAINTENANCE NOTED PRIOR ANTI-SKID COMPUTER ISSUE AND REPLACED. REPLACED ALL MAIN TIRES.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,259 hrs · 52,472 cycles

DURING SERVICE CHECK, FOUND NUMEROUS EMERGENCY LIGHTS INOPERATIVE. FOUND POWER SUPPLY B5-212 BAD. REMOVED AND REPLACED THE POWER SUPPLY IAW WDM 33-51-14.

Part: FUSE — BLOWN (BATTERY PACK) · airframe 69,893 hrs · 52,201 cycles

2L EMERGENCY DOOR EXIT LIGHT INOPERATIVE. FOUND PACK AT STA 1233R, B5-212 WITH BLOWN FUSE. REPLACED FUSE.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 69,758 hrs · 52,088 cycles

DURING DESCENT FROM FL350 TO FL240, FLOW LIGHT ILLUMINATED WITH CABIN ALT RISING RAPIDLY THROUGH 9000'. DURING EMERGENCY DESCENT AUTO INOPERATIVE. INOP 1, INOP 2 LIGHTS ILLUMINATED AND RT AC PACK PRESSURE NOTED LOW. CABIN ALT ROSE TO 16,000' AND PASSENGER OXYGEN MASKS DEPLOYED AUTOMATICALLY. ACFT PRESSURIZATION OPS CK GOOD IAW AMM 21-32. OK FOR SERVICE.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 69,758 hrs · 52,088 cycles

CABIN OXYGEN MASKS DEPLOYED. REPLACED OXYGEN CANISTER IN ROWS 10ABC TO ROWS 18ABC LT SIDE. INSTALLED OXYGEN MASK IN ROW 10ABC TO ROW 18ABC IAW MM 35-21-01. R & R OXYGEN CANISTER IN ROW 10 DE TO ROW 19DE RT SIDEPANEL. INSTALLED OXYGEN MASK IN ROWS 10 DE TO ROW 19DE RT SIDE ON PANEL IAW AMM 35-22-01. R & R REMAINING OXYGEN GENERATORS AN REPACKED MASKS. ARMED ALL OXYGEN GENERATORS IAW AMM 35-22. CLOSED ALL PANELS.

Part: COALESCER BAG — UNKNOWN · airframe 69,780 hrs · 52,109 cycles

DURING DESCENT FROM FL350 TO FL240 THE "FLOW" LIGHT ILLUMINATED WITH THE CABIN ALTITUDE RISING RAPIDLY THROUGH 9,000 FT. DURING EMERGENCY DESCENT CABIN PRESSURE, AUTO 1 INOPERATIVE, AUTO 2 INOPERATIVE AND AUTO INOPERATIVE ILLUMINATED. THE RT PACK PRESSURE WAS LOW. CABIN ALTITUDE ROSE TO 16,000 FT AND THE PASSENGER OXYGEN MASKS DEPLOYED AUTOMATICALLY. THE OXYGEN GENERATORS WERE REPLACED AND THE O2 MASK WERE RE-PACKED. MAINTENANCE PERFORMED A PRESSURIZATION OPS CHECK. THE RT PACK PRESSURE REGULATOR VALVE WAS REPLACED. THE LEFT FLOW CONTROL VALVE WAS REPLACED. THE COALESCER BAGS WERE REPLACED. HEALTH CHECKS WERE PERFORMED ON BOTH PACKS AND THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,640 hrs · 52,003 cycles

EMERGENCY LIGHTS IN TAIL COMPARTMENT INOPERATIVE. REPLACED FUSE IN BATTERY PACK, CHECKS GOOD, IAW AMM 33-53.

Part: SKIN — CORRODED (BS 200-218) · corrosion level 2 · airframe 69,539 hrs · 51,941 cycles

FORWARD ACCESSORY COMPARTMENT BS 200 TO 218 AT L28R TO L29R: FUSELAGE SKIN CORROSION AROUND THE FORWARD DRAIN MAST. COMPLIED WITH ER/A 546060-14 REF, ORIG.

Part: THRESHOLD — CORRODED (CARGO BAY) · corrosion level 2 · airframe 69,539 hrs · 51,941 cycles

LIGHT CORROSION AROUND FASTENER HOLES FOR MID CARGO DOOR SILL/THRESHOLD. COMPLIED WITH ER/A 546088-14, REV "A".

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,526 hrs · 51,931 cycles

CORROSION FOUND ON FUSELAGE SKIN AT CUTOUT FOR FWD DRAIN MAST. REPAIRED IAW ER/A 546030-14.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,918 hrs · 52,970 cycles

ANGLE CORRODED AT LOWER FWD CORNER OF R-1 DOOR OPENING UNDER THRESHOLD. REPAIRED PER ERA 546147-14 REV ORG.

Part: SCUFF PLATE — CORRODED · corrosion level 2 · airframe 69,526 hrs · 51,931 cycles

LIGHT CORROSION AROUND FASTENER HOLES FOR THRESHOLD SCUFF PLATES. REPAIRED THRESHOLD IAW SRM 53-05 FIG 123.

Part: GROUND STUD — LOOSE · airframe 69,497 hrs · 51,909 cycles

THE CREW OF FLIGHT 1302 FOUND THAT THE L2 DOOR EMERGENCY LIGHTS WILL NOT WORK WHEN TESTED. MAINTENANCE FOUND A GROUND STUD CONNECTION FOR THE BATTERY PACK LOOSE AND RETORQUED IT AND ALSO REPLACED THE BATTERY PACK POWER SUPPLY. LIGHT CHECKED OK.

Part: UNKNOWN — UNKNOWN (NLG STEERING) · airframe 69,384 hrs · 51,835 cycles

NOSEWHEEL STEERING REQUIRES EXCESSIVE FORCE ON TAXI. DURING TAKEOFF ROLL, ACFT VEERED TO THE LT AT APPROXIMATELY 80 KTS. POWER SETTING WAS EVEN AND NO TRANSWIND PRESENT. REPLACED BOTH NOSE TIRES, CHECKED SPEED BRAKES, REPLACED LT AND RT NOSE WHEEL STEERING ACTUATORS, REPLACED STEERING CONTROL VALVE AND STEERING BYPASS RELIEF VALVES, ADJUSTED CABLES. TAXIIED ACFT, CHECKED OK.

Part: CONNECTOR — FAILED (EMERGENCY LIGHT) · airframe 69,256 hrs · 51,742 cycles

THE CREW FOUND THE L-2 AND AFT CABIN DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A BAD QUICK DISCONNECT. ALSO, 3 BATTERY PACK FUSES WHERE REPLACED AND THE LIGHTS CHECKED OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,250 hrs · 51,738 cycles

FLIGHT 2461, FOUND THE EMERGENCY LIGHTS INOPERATIVE OVER COCKPIT DOOR AND L1 AND L2 DOORS. MEM MAINTENANCE REPLACED THE BATTERY BACK AND THE COCKPIT, L1, AND R1 LIGHTS CHECKED OK.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 68,871 hrs · 51,487 cycles

FAS IN AFT CABIN REPORTED POPS FROM LT ENGINE AT TAKEOFF POWER. REPLACED NR 1 ENGINE IAW 88-7110-9-0010.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,650 hrs · 51,332 cycles

MAINTENANCE FOUND THE LT AND RT AFT OVERWING EXIT SIGNS INOPERATIVE. THE EMERGENCY LIGHT BATTERIES WERE REPLACED.

Part: WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 68,499 hrs · 51,232 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE AFT EMERGENCY EXIT SIGNS WERE INOPERATIVE. MAINTENANCE ALSO FOUND THAT THE EMERGENCY LIGHTS IN ROWS 13-23 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND FUSES FOR THE EXIT SIGNS AND THEN CORRECTED A LOOSE WIRE IN A CONNECTOR, REPAIRED THE CONNECTOR PIN, AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: CONNECTOR — BURNED (CABIN LIGHTS) · airframe 68,120 hrs · 50,933 cycles

CREW NOTICED AN ELECTRIC SMOKE ODOR IN CABIN AND COCKPIT JUST BEFORE BOARDING. MAINTENANCE FOUND A BURNED LIGHT CONNECTOR OVER SEAT 28ABC AND REPLACED THE BULB, BULB HOLDER AND BALLAST ASSY.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,834 hrs · 50,747 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT ROWS 13-26 WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,559 hrs · 50,567 cycles

SEVERAL EMERGENCY LIGHTS OUT IN TAIL COMPARTMENT. RII: N ENTRY 486044 W, R & R EMERGENCY POWER SUPPLY B5-28 IAW AMM 33-53. LIGHTS CHECK GOOD. OK FOR SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 67,461 hrs · 50,497 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 15DE IN THE CABIN WAS BROKEN AND MISSING. MAINTENANCE REPLACED THE WIRE HARNESS, INSTALLED A NEW LENS COVER, AND FUNCTIONALLY CHECKED THE SYSTEM. LP 7333950.

Part: WIRE — PULLED (EMERGENCY LIGHT) · airframe 66,758 hrs · 50,032 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTS IN ROWS 13-23DEF OF THE CABIN WERE INOPERATIVE. MAINTENANCE FOUND WIRES PULLED OUT OF A SPLICE AT 13DEF. THE WIRE WAS REPAIRED WITH A NEW SPLICE AND THE SYS RETURNED TO NORMAL OPERATION.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,175 hrs · 49,624 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT ROWS 12DE-13DE WERE INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 65,690 hrs · 49,264 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT ROW 26DE WAS INOPERATIVE. MAINTENANCE FOUND A WIRE BROKEN AND REPAIRED IT. THE SYSTEM RETURNED TO NORMAL.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 65,644 hrs · 49,229 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE CABIN SERVICE DOOR EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED THE FAILED FUSE AT THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 65,644 hrs · 49,229 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT AT SEAT 34D WAS INOPERATIVE. MAINTENANCE FOUND A CONNECTOR IN THE WIRE HARNESS UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 65,644 hrs · 49,229 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT AT SEAT 24D IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A PIN PUSHED BACK INTO THE CONNECTOR, REPAIRED THE CONNECTOR PIN, AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,638 hrs · 49,224 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN FOR THE R2 DOOR AND THE AFT STAIRWAY WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 64,711 hrs · 48,554 cycles

THE PILOT DISCOVERED THAT THE GIRT BAR FOR THE EMERGENCY ESCAPE SLIDE AT R1 DOOR WOULD NOT REMAIN IN THE ARMED POSITION. RECEPTACLES WERE OBSTRUCTED ENOUGH THAT THE GIRT BAR WOULD KICK OUT OF LATCH. THE DOOR SLIDE GIRT BAR LATCHING RETAINER WAS CLEANED AND THE FOLLOW-UP FUNCTIONAL CHECK WAS GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 64,216 hrs · 48,222 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT SEAT 26DE INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE IN THE CONNECTOR, REPAIRED THE CONNECTOR PIN, AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 64,011 hrs · 48,077 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT SEAT 26DE INOPERATIVE. REPAIRED WIRING AT THE QUICK DISCONNECT AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,750 hrs · 47,905 cycles

DURING LINE CHECK, SIX OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED LAMPS AND OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,750 hrs · 47,905 cycles

DURING LINE CHECK, THE AFT THREE OVERHEAD EMERGENCY EXIT LIGHTS WERE NOTED TO BE INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY AND OPS CHECKED GOOD.

Part: SOCKET — DAMAGED (EMERGENCY LIGHT) · airframe 63,750 hrs · 47,905 cycles

DURING LINE CHECK, THE SEAT MOUNTED EMERGENCY EXIT LIGHT AT ROW 27 WAS NOTED TO BE INOPERATIVE. SOCKET ASSY REPLACED AND OPS CHECKED GOOD.

Part: LONGERON — CRACKED (BS 1250-1271) · airframe 1 hrs · 1 cycles

DURING HMV, A CRACKED WAS FOUND ON LONGERON 19RT FROM BS 1250 TO 1271 AT RT UTILITARY TUNNEL OF AFT CARGO COMPARTMENT. REMOVED LONGERON SECTION BS 1260-1279 AND INSTALLED NEW SECTION AND SPLICE IAW SRM 53-02, FIG 18.

Part: SKIN — CRACKED (FUSELAGE) · airframe 1 hrs · 1 cycles

DURING HMV, A CRACK WAS FOUND OF 0.046" OF LENGTH ON FUSELAGE SKIN OF THE FWD CARGO COMPARTMENT AT THE UPPER FWD DOOR JAMB CORNER STA Y=374 AND BTW LONGERONS 20 RT AND 21 RT. DAMAGE AREA WAS TRIMMED OUT AND FILLER, DOUBLER, AND TRIPLER WERE INSTALLED IAW ER/A 506630-14AD REV ORIG.

Part: LONGERON — CRACKED (BS 1380) · airframe 60,973 hrs · 45,908 cycles

CRACKED LONGERON 13 LT BS 1380. REPAIRED IAW SRM 53-02, FIG 18.

Part: SKIN — CRACKED (BS 1415-1421) · airframe 60,973 hrs · 45,908 cycles

CRACKED FUSELAGE SKIN AT STA Y=1418 BTW LONG 2RH-3RH. ALSO LONG 2-3L AND BTW LONG 1 AND 2R FROM STA Y=1415-1421 AT AFT ACC COMPARTMENT. REPAIRED IAW ER/A 506648-14AD, REV ORG.

Part: FASTENER — LOOSE (VERTICA STAB) · airframe 60,973 hrs · 45,908 cycles

LOOSE FASTENERS ON VERTICAL STAB L/E AT THE SPLICE STA ZFS=52.2, 2 ROWS OF FASTENERS ABOVE AND BELOW OF SPLICE REF OP 0501, EA 09-470871-12AD.

Part: SKIN — CRACKED (BS 304 L26L) · airframe 60,973 hrs · 45,908 cycles

DUE AT HMV/PSV SRM 53-04, FIG 12 B CLASS II AT STA 304 LONGERON 26L-28L. REPAIRED AREA IAW SRM 53-04-03.

Part: ANGLE — CORRODED (BS 200) · airframe 60,973 hrs · 45,908 cycles

CORROSION ON CUSP ANGLE BETWEEN BS 200 AND X=-54 AT CABIN FLOOR STRUCTURE. REPAIRED IAW ER/A 506639-14.

Part: LONGERON — CORRODED (BS 1287-1322) · airframe 60,973 hrs · 45,908 cycles

CORROSION ON LONGERON 22L BS 1287 TO 1322 AT AFT CARGO BAY LT UTILITARY TUNNEL. REPAIRED IAW SRM 53-02.

Part: LONGERON — CRACKED (BS 160 L2L) · airframe 60,973 hrs · 45,908 cycles

DURING HMV A CRACKED WAS FOUND ON LONGERON 2LH STA Y=160 AT PAX CABIN. LONGERON AND LONGERON END WAS REMOVED AND NEW SECTION WAS SPLICED IN AND LONGERON END INSTALLED IAW SRM 53-02 FIG18.

Part: SKIN — CORRODED (BS 769-826) · airframe 60,973 hrs · 45,908 cycles

DURING HMV, CORROSION WAS FOUND ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING STA Y=769-826 BTW LONGERONS 28 TO 30L. BLENDED AREA AND LEAVE AS IS CONDITION IAW SRM 53-04, PARA 57.

Part: CHANNEL — WORN (BS290-313 L23-24) · airframe 60,973 hrs · 45,908 cycles

DURING HMV, WEAR WAS FOUND ON LONGERON 23L AND 24L HAT SECTION BTW STA Y=290-313. DUE TO EXCESSIVE DAMAGE LONGERON SECTION WAS REMOVE STA Y=320-285 AND NEW SECTION SPLICED IN IAW SRM 53-02, FIG 18.

Part: LONGERON — CORRODED (BS 1287-1292) · airframe 60,973 hrs · 45,908 cycles

DURING HMV CORROSION WAS FOUND ON LONGERON 25L FRON STA Y=1287-1292 AT AFT CARGO COMPARTMENT. DUE TO EXCESSIVE CORROSION LONGERON SECTION WAS REMOVED STA Y=1271-1298 AND NEW SECTION SLPICED IN IAW SRM 53-02, FIG 18.

Part: SKIN — CORRODED (BS 1098-1108) · airframe 60,973 hrs · 45,908 cycles

DURING HMV, CORROSION WAS FOUND ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING BS 1098-1108 OVER LONGERON 28L BLENDED OUT AREA AND LEAVE AS IS CONDITION IAW SRM 53-04, PARA 57.

Part: SKIN — WORN (LT WING) · airframe 60,973 hrs · 45,908 cycles

DURING HMV, WEAR WAS FOUND ON LT WING LOWER SKIN AFT SECTION XRS=118 OF SETTLEMENT FAIRING AREA. BLENDED OUT AREA AND LEAVE AS IS CONDITION IAW ERA 506631-14 REV ORIG.

Part: SKIN — DAMAGED (BS 617-636) · airframe 60,973 hrs · 45,908 cycles

DURING HMV, LIGHTNING STRIKE WAS FOUND ON LT WINDOW BELT UPPER AFT CORNER BTW BS 617-636. BLENDED AREA AND LEAVE AS IS CONDITION AS TEMP REPAIR TILL 116500 TOTAL CYCLES IAW ERA 506621-14, REV ORIG.

Part: SKIN — CORRODED (BS 1079-1131) · airframe 60,973 hrs · 45,908 cycles

DURING HMV, CORROSION WAS FOUND ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING BS 1079-1131 BTW LONGERON 26 TO 30R. FUSELAGE SKIN WAS BLENDED OUT AND LEAVE AS IS CONDITION IAW SRM 53-04, PARA 57.

Part: SKIN — CRACKED (BS 197 L20-21L) · airframe 60,973 hrs · 45,908 cycles

DURING HMV, A CRACK WAS FOUND ON FUSELAGE SKIN AROUND FASTENER HEAD AT STA Y=197 BTW LONGERON 20-21L AFT LWR CORNER OF STAIR ACCESS. DAMAGE SKIN WAS TRIMMED OUT AND DOUBLER INSTALLED IAW ERA 506619-14AD, REV ORIG.

Part: LONGERON — CRACKED (BS 160 L3L) · airframe 60,973 hrs · 45,908 cycles

DURING HMV, A CRACK WAS FOUND ON LONGERON 3L BS 160 AT PAX CABIN. LONGERON AND LONGERON END WAS REMOVED AND NEW SECTION WAS SPLICED IN AND INSTALLED LONGERON END IAW SRM 53-02, FIG 18.

Part: LONGERON — CRACKED (BS 1309-1322 L8R) · airframe 60,973 hrs · 45,908 cycles

DURING HMV, A CRACK WAS FOUND ON LONGERON 8R BS 1309 AND 1322 AT AFT CABIN AREA. LONGERON SECTION WAS REMOVED AND NEW SECTION WAS SPLICED IN IAW SRM 53-02, FIG 18.

Part: SKIN — CRACKED (BS 1437 L3-4L) · airframe 1 hrs · 1 cycles

DURING HMV, A CRACK WAS FOUND ON FUSELAGE SKIN AT BS 1437 BETWEEN LONGERONS 3 & 4L. DAMAGE WAS REMOVED AND FILLER DOUBLER INSTALLED IAW SRM 53-04, FIG 27.

Part: PAN — CRACKED (CARGO DOOR) · airframe 1 hrs · 1 cycles

DURING HMV, CRACKS WERE FOUND ON INNER PAN BELOW STOP FITTING NR 4 AT FWD CARGO DOOR AFT SECTION. CRACKS WERE STOP DRILLED AND DOUBLER INSTALLED IAW SRM 52-05, FIG 50.

Part: LONGERON — CRACKED (BS 541 L4R) · airframe 60,973 hrs · 45,908 cycles

DURING HMV CRACKED LONGERON WAS FOUND 4RH STA Y=541 AT INNERFUSELAGE STRUCTURE. SECTION OF LONGERON REMOVED Y=512-583 AND A NEW SECTION WAS SPLICED IN IAW SRM 53-02, FIG 18.

Part: LONGERON — CRACKED (BS 331 L3L) · airframe 60,973 hrs · 45,908 cycles

DURING HMV, A CRACK WAS FOUND ON LONGERON 3L AT BS 331. LONGERON SECTION WAS REMOVED AND NEW SECTION SPLICED IN IAW SRM 53-02, FIG 18.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 60,569 hrs · 45,613 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE OVERHEAD EMERGENCY ESCAPE LIGHTS IN THE FIRST CLASS SECTION, INOPERATIVE. REPLACED BATTERIES AND OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,834 hrs · 45,141 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 10 & 17 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLIES AT ROWS 10 & 17 AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF THEM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,011 hrs · 44,606 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING IN THE FIRST FOUR ROWS OF 1ST CLASS SEATS HAD FAILED. MAINTENANCE REPLACED THE BATTERY PACK B5-100 AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 58,893 hrs · 44,514 cycles

FLIGHT CREW REPORTED SMOKE IN CABIN ORIGINATING APPROXIMATELY MID-CABIN FROM OVERHEAD. MAINTENANCE FOUND CEILING SIDE WALL BALLAST AT ROW 21 DE BURNT. REMOVED AND REPLACED BALLAST PER MAINTENANCE MANUAL. PERFORMED OPERATION 5088. CHECKS OKAY.

Part: POWER SUPPLY — INOPERATIVE (CATWALK) · airframe 58,370 hrs · 44,120 cycles

DURING LINE CHECK MAINTENANCE FOUND 4 CATWALK EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED A BAD POWER SUPPLY (B5-212) AND THE OPERATION OF THE LIGHTS NOW CHECKS OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,937 hrs · 43,780 cycles

DURING LINE CHECK, MAINTENANCE FOUND GALLEY L2 AND AFT FLIGHT ATTENDANT EMERGENCY LIGHTS DO NOT TEST. MAINTENANCE REMOVED AND REPLACED AFT EMERGENCY LIGHT BATTERY PACK PER MAINTENANCE MANUAL. OPERATION CHECKS GOOD.

Part: LIGHT — INOPERATIVE (AFT CABIN) · airframe 57,820 hrs · 43,686 cycles

DURING SERVICE CHECK, MX FOUND AFT SECTION EMERGENCY PATHWAY LIGHTS INOPERATIVE. MX REPLACED LIGHT BASE B5-2112 AT STA 1233R. OPS CHECKS GOOD. ACFT IS OK FOR SERVICE.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 57,736 hrs · 43,622 cycles

ON 26MAR11 FOUND CORROSION AT APB CANTED BULKHEAD STA 1338 LWR T-CORD BODY LINE ZERO. REPAIRED DAMAGE PER ERA 491528-14 REV 1.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 57,736 hrs · 43,622 cycles

DURING PSV CHECK IN MSP, NOTED CORROSION COMMON TO THE AFT PRESSURE BULKHEAD ANGLE LOCATED S-28L TO S-28R. REPAIRED PER ERA 491320-14.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 57,736 hrs · 43,622 cycles

DURING MAINTENANCE VISIT FOR AFT CARGO JAMB LOWER BEAM REPLACEMENT, TOOLING DAMAGE WAS FOUND ON LONGERON 29R AT STA 1219. REPAIRED PER ERA 491438-14 REV ORIG.

Part: FRAME — DAMAGED (BULKHEAD) · airframe 57,736 hrs · 43,622 cycles

AFT PRESSURE BULKHEAD LOWER FRAME DAMAGED REPAIRED IAW PER SRM 53-03 FIG 37 AND ER/A 09-086680-12 REV EOPN 0603.

Part: UNKNOWN — SMOKE (AFT CABIN) · airframe 57,358 hrs · 43,379 cycles

DURING TOUCHDOWN, THE F/A REPORTED BLUE SMOKE WITH AN OIL ODOR IN THE AFT SECTION OF CABIN THAT REMAINED VISIBLE FOR 5 MINUTES. MX INSPECTED ACFT AND APU INLET FOR OIL OR HYD CONTAMINATION AND NONE WAS FOUND. PERFORMED OPN 588 AND OPN 5089, DUCT BURNED OUT WITH COALESCER BAG CHANGE. ACFT IS OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,262 hrs · 43,332 cycles

DURING LINE CHECK, MX FOUND ALL FIRST CLASS CEILING EMERGENCY LIGHTS INOPERATIVE. MX REPLACED BATTERY AND BATTERY PACKS. AFTER CHARGING BATTERY, LIGHTS OPERATED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,589 hrs · 42,899 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHTS IN AFT SERVICE DOOR, AFT AIRSTAIRS, AND AIRSTAIRS PATHWAY INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK B5-212, POWER SUPPLY, AND RE-LAMPED. OPERATION OF LIGHTS NOW CHECK OK. (2010-D1257) (DLM88102866)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,589 hrs · 42,899 cycles

DURING LINE CHECK MAINTENANCE FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK B5-211 AND CHARGER FOR COCKPIT LIGHTS. OPERATION OF LIGHTS NOW CHECK OK. (2010-D1259) (DLM88102868)

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 56,344 hrs · 42,740 cycles

DURING LINE CHECK MX FOUND EMERGENCY LIGHT AT 2C INOPERATIVE. MX SECURED PULLED WIRES FROM CONNECTOR AND REPLACED LIGHT ASSY IAW AMM 33-53-01. OPS OF LIGHT NOW CHECK OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,178 hrs · 42,607 cycles

MX FOUND THE FWD ESCAPE PATH LIGHTING TO BE INOPERATIVE. MX REPLACED THE POWER SUPPLY AND THE F/A EMERGENCY LIGHT SWITCH. AN OPS TEST WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,107 hrs · 42,554 cycles

THE PILOTS FOUND THAT THE RIGHT AND LEFT AFT OVERWING EXIT IDENTIFIERS REMAINED ON WITH THE AIRCRAFT POWERED DOWN AND THE EMERGENCY LIGHT SWITCH IN THE OFF POSITION. MAINTENANCE REPLACED THE NI-CAD BATTERIES IN THE BATTERY PACK SERIAL NUMBER 22757 IN OVERHEAD BIN ABOVE AFT OVERWING EXIT. AN OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE (2010-D0963)(DLM88102083).

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,102 hrs · 42,551 cycles

THE CABIN CREW REPORTED THAT THE LEFT AND RIGHT AFT EMERGENCY EXIT OVERWING IDENTIFIERS REMAINED ON WITH POWER REMOVED FROM THE AIRCRAFT. MAINTENANCE REMOVED THE BATTERIES FROM THE POWER SUPPLY AND RESET THE EMERGENCY LIGHTS WITH THE SHIP'S BATTERY ON AND RE-INSTALLED THE BATTERIES. AN OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE (2010-D0964)(DLM88102084).

Part: FUSE — BLOWN (BATTERY PACK) · airframe 56,092 hrs · 42,547 cycles

MAINTENANCE FOUND THE L2 EMERGENCY DOOR WALL LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED THE 5 AMP FUSE IN BATTERY PACK B5-212. AN OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE (2010-D0965)(DLM88102085).

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 55,955 hrs · 42,468 cycles

ON LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY PATH LIGHTS FROM 31D TO 38D TO BE INOPERATIVE. MAINTENANCE REPLACED THE FUSE ON THE POWER SUPPLY. AN OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE (2010-D0861)(DLM88101933).

Part: BEAM — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 55,654 hrs · 42,269 cycles

THE AFT CARGO LOWER DOOR BEAM HAD CORROSION TH AT EXCEEDED 50 PERCENT OF THE ORIGINAL THICKNESS. DAMAGE WAS CUT OUT AND REPAIRS WERE INSTALLED IAW SRM 53-05 FIG 123 AND ER/A 482970-14. (DLM88101452)

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 55,654 hrs · 42,269 cycles

MX SET UP FOR INSP OF ALL EMERGENCY EXIT SIGN DUE TO FAA FINDINGS. MX REPLACED SEVERAL BROKEN EMERGENCY EXIT SIGNS AND REPLACED BATTERY PACKS FOR LT & RT OVERWING EMERGENCY EXIT SIGNS IAW AMM 33-53-00. OPERATION OF LIGHTS NOW CHECKS GOOD.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,654 hrs · 42,269 cycles

ON 30MAY10, THE AFT CARGO LWR DOOR SILL BEAM WAS CORRODED BEYOND SRM LIMITS. REPAIRED IAW ER/A 482970-14 REV3

Part: STOP FITTING — BULGED (DOOR FRAME) · corrosion level 2 · airframe 55,654 hrs · 42,269 cycles

ON 26MAY10, THE FWD CARGO COMPT HAD BULGED MATERIAL ON THE LWR AFT STOP FITTING & CORROSION ON THE DOOR JAMB. FAB'D FWD SPLICE HALVES IAW SRM 53-05D. (DLM88101637)

Part: LONGERON — CORRODED (BS 640-690) · corrosion level 2 · airframe 55,654 hrs · 42,269 cycles

ON 26MAY10, THE C2 DOOR SILL LONGERON WAS FOUND TO BE CORRODED BEYOND SRM LIMITS FROM BS 640-690. INSTALLED -15 DOUBLER IAW SRM 53-05 SHT 2. (DLM88101636)

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 55,430 hrs · 42,104 cycles

MX FOUND THE EMERGENCY ESCAPE PATH LIGHTS AT SEATS 31-38 INOP. MX REPLACED THE FUSES IN THE CHARGER AND CLEANED THE CONNECTOR FROM THE WALL AT SEAT 35. AN OPS CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FUSE — OPEN (EMERGENCY LIGHTS) · airframe 54,992 hrs · 41,830 cycles

DURING LAYOVER CHECK, MX FOUND THE EMERGENCY LIGHTS AT SEAT 31 AND AFT INOPERATIVE. MX REPLACED THE BATTERY PACK, NO HELP. THE ORIGINAL BATTERY PACK WAS RE-INSTALLED. THE F1 FUSE IN THE BATTERY PACK POWER SUPPLY WAS REPLACED. THEN THE SYS CHECKED NORMALLY.

Part: INDICATOR — STUCK (ENGINE EPR) · airframe 54,952 hrs · 41,812 cycles

2H EPR STUCK AT APPROX 1.5 ON T/O ROLL- RTO AT 30 KTS. FLIGHT CREW PLACARD INSTALLED IAW MEL 77-00-01A.

Part: LIGHT — INOPERATIVE (SEAT 23DEF) · airframe 54,854 hrs · 41,753 cycles

PAX SEAT 23DEF EMERGENCY PATH LIGHT INOP. REMOVED AND REPLACED CLEAR PATH LIGHT KIT. OPS CHK GOOD.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 53,549 hrs · 40,933 cycles

RIGHT UPPER AFT STABILIZER SKIN CRACKED. C/W ERA 460477-14 REV A CODE 9-55-11. PERM REPAIR RT HORIZ STAB / UPPER AFT SKIN PNL / INBOAD END CRACK ON NR 1 EO CARDS 1-3 09-460214-12AD REV D ME 08.

Part: UNKNOWN — ODOR (CABIN) · airframe 50,591 hrs · 39,021 cycles

SMELLED SMOKE IN MID CABIN. NO OTHER INDICATIONS. SMELL WENTAWAY. CABIN LIGHTS WERE OFF.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 47,410 hrs · 36,947 cycles

FOUND HORIZONTAL STABILIZER/RT/UPPER AFT SKIN PANEL, CRACK REPAIR. THE UPPER AFT SKIN PANEL OF THE RT HORIZONTAL STABILIZER WAS FOUND WITH A 1.85" CRACK NEAR THE INBD AFT END OF THE PANEL. THE CRACK WAS STOP DRILLED ON A TIME LIMITED BASIS. THE PERMANENT REPAIR WILL REPLACE THE SKIN PANEL WITH A NEW PANEL. THE REPAIR IS DOCUMENTED PER ER/A 460477-14.

Part: SKIN — DAMAGED (BS 207 L20R) · airframe 46,800 hrs · 36,593 cycles

THE FUSELAGE SKIN WAS FOUND DAMAGED AT STA 207 BETWEEN LONGERON 20R AND 21R. DAMAGED SKIN WAS CUT OUT AND AN EXTERNAL REPAIR DOUBLER WAS INSTALLED.

Part: SKIN — DENTED (FS 118 L28-29L) · airframe 46,800 hrs · 36,593 cycles

THE FUSELAGE SKIN HAS A DENT BEYOND ALLOWABLE LIMITS BETWEEN L28L-29L AT FS 118. THE DAMAGED SECTION OF SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.

Part: SKIN — CORRODED (BS 798-812) · airframe 46,800 hrs · 36,593 cycles

CORROSION FOUND ON FUSELAGE SKIN FROM FS 798 TO 812 AT THE RT FILLET FARING RUB STRIP. THE DAMAGED SECTION OF SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.

Part: SKIN — DAMAGED (FS 598 L29-30R) · airframe 46,800 hrs · 36,593 cycles

THE FUSELAGE SKIN WAS CREASED AT STA 598 FROM L29R TO L30. THE DAMAGED SECTION OF SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.

Part: SKIN — GOUGED (LWS 59) · airframe 46,800 hrs · 36,593 cycles

THE LT INBOARD FLAP, OUTBOARD TE WEDGE LOWER SKIN IS GOUGED AT STATION W 59.450. THE DAMAGED SKIN WAS CUT OUT AND NEW SECTION OF SKIN WAS SPLICED IN.

Part: LOCK — MALFUNCTIONED (MLG) · airframe 43,754 hrs · 34,487 cycles

AIRCRAFT DEPARTED HARD SURFACE OF RUNWAY AND TAXIED MOMENTARILY THROUGH GRASS AREA. ALL ENGINE INDICATIONS NORMAL. ON LANDING ROLLOUT, BRAKING SEEMED INEFFECTIVE. CLEANED NLG AND FUSELAGE. PERFORMED HIGH ENERGY INSP. NO EVIDENCE OF HIGH ENERGY STOP CONDITION NOTED. PERFORMED HIGH DRAG/SIDE LOAD INSP PER M/M. NO ITEMS NOTED. FURTHER CHECKS AND TROUBLESHOOTING CURRENTLY IN PROGRESS.

Part: MANIFOLD — FAILED (BRAKES) · airframe 40,037 hrs · 31,806 cycles

AFTER TOUCHDOWN THE CREW APPLIED MAX BRAKES WITH NO A BRAKE PRESSURE AVAILABLE. REPLACED BRAKE MANIFOLD AND VALVE.

Part: B-NUT — LOOSE (HYDRAULIC SYS) · airframe 33,984 hrs · 27,468 cycles

LT HYD QTY W/HYD QTY LOW IND. FOLLOWED CK LIST PROCEDURES AND LOST LT HYD PRESSURE W/GOOD QTY. ZERO LEFT HYD PRESSURE W/GOOD RIGHT HYD PRESSURE AND GOOD QUANTITIES. WHEN XFER PUMP TURNED ON PER MCC. QTY RETURNED TO 19 QTS WITHOUT PRESSURE. FWD B-NUT LOOSE AT LT THRUST RVSR CONTROL VALVE. REPLACED HYD PRESS LINE THAT RUNS FROM ACCUMULATOR TO CONTROL VALVE. CHECK OF EDP CKS GOOD, LEAK CKS GOOD.

Part: TRANSFORMER — OVERHEATED (E/E BAY) · airframe 33,453 hrs · 27,068 cycles

FWD E/E ABOVE TR L-2 HAS EVIDENCE OF HIGH HEAT TEMPERATURE DUE TO INSULATION BLANKET DAMAGE AND WORN FRAME AT STA 48 LBL 2D. REMOVED AND REPLACED L-2 TRANSFORMER RECTIFIER, OPS CHECK GOOD PER M/M.

Part: STARTER — SPARKS (NR 1 ENGINE) · airframe 33,453 hrs · 27,068 cycles

NR 1 ENGINE STARTER EMITTING SPARKS DURING ENGINE SPIN. REPLACED STARTER PER M/M 80-10-01-2. REINSTALLED START VALVE.

Part: TRANSFORMER — DAMAGED (E/E BAY) · airframe 33,453 hrs · 27,068 cycles

FWD E/E ABOVE TR L-2 HAS EVIDENCE OF HIGH HEAT TEMPERATURE DUE TO INSULATION BLANKET DAMAGE AND WORN FRAME AT STA 48 LBL 20. REPAIRED DAMAGE.

Part: HARNESS — BROKEN (CABIN) · airframe 32,765 hrs · 26,561 cycles

A 17D EMERGENCY LIGHT INOP. REPLACED WIRE ASSY, OPS CKS NORMAL.

Part: SKIN — DAMAGED (FUSELAGE)

THE LT FUSELAGE WINDOW BELT SKIN AT WINDOWS 11, 13 AND 15 SUFFERED LIGHTNING DAMAGE TO THE UPPER CORNERS OF THE WINDOW CUTOUTS. THE DAMAGES WERE REPAIRED WITH A ONE-PIECE DOUBLER PER THE GUIDLINES OF DAC SRO9530053 AND ER/A 360060-14, REV F.

Part: PACK — OIL LEAK (TAIL COMP)

AFTER LIFTOFF, HOT SMELL LIKE HOT A/C PACK IN AFT CABIN. FOUND RT PACK CAUSING SMELL IN CABIN. RENDERED PACK INOPERABLE. FWD TO MCO/PLAC .

Part: LIGHT ASSY — FAILED (CABIN)

F/A'S AND PAX REPORT SMELL OF BURNING RUBBER OR ELECTRICAL SMELL IN REAR OF A/C, SMELL PRESENT IN ALL PHASES OF FLT. NO SMOKE PRESENT. C/A FOUND CEILING LIGHT FIXTURE AT SEAT ROW 36AB SMOLDERING. REMOVED LAMP AND DISCONNECTED BALLAST FWD TO MCO/PLAC MEL 33-00-2. LIGHT ASSY WILL BE REPLACED.

Part: EMER POWER SW — INOPERATIVE (COCKPIT)

DURING IDLE DESCENT THROUGH 8,000, CBS K7 AND L8 POPPED OPEN, RESULTING IN LOSS OF A/C EMERGENCY BUS. EMERGENCY POWER ON, WORKED OK. REPLACED EMERGENCY POWER SWITCH.

Part: ANGLE — CRACKED (WW KEEL BEAM)

DURING G-1 LTR CHECK, FOUND KEEL BEAM AFT CROSSOVER ANGLE CRACKED. ACCOMPLISHED REPAIRS PER SRM 53-05 FIG 101.

Part: ACTUATOR ARM — BROKEN (RT TE FLAP)

FOUND ON ARRIVAL FOR LETTER CHECK, THE RIGHT SIDE INBOARD FLAP INBOARD DRIVE ACTUATOR CASTING CRACKED. REPLACED CASTING ARM AND ACTUATOR.