N945DL

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,437 hrs · 55,026 cycles

DURING A LINE CHECK, NOTED SIGNS ABOVE FWD EMERERGENCY EXIT DOORS INOPERATIVE. BATTERIES WERE REPLACED AND OPERATION WAS NORMAL.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 73,401 hrs · 54,990 cycles

SEAT 18D EMERGENCY LIGHT INOPERATIVE. FOUND A BROKEN WIRE. PINNED THE CONNECTOR PLUG. OP CHECKED IAW 33-50. (LP3478308)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,980 hrs · 54,632 cycles

CEILING EMERGENCY LIGHTS INOPERATIVE ROWS 1-4, AND 17-20. INSTALLED BATTERIES IN THE B5-100 & B5-102 POWER SUPPLIES IAW AMM 33-53. OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 71,994 hrs · 53,851 cycles

SEAT 29 DE, SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. FOUND A WIRE BROKEN AT CONTACT PIN IN CONNECTOR AT SEAT FRAME. TERMINATED THE WIRE IAW SWPM 20-90-03. CHECKED GOOD.

Part: STRUCTURE — DENTED (RT WING) · airframe 71,555 hrs · 53,526 cycles

DENT ON L/E VORTILON YW=85, XRS=160. REPAIRED IAW RM 57-09D PAR. 33 AND ERA 401563-14 REV. ORIGINAL.

Part: DIODE — DAMAGED (TRANSFMR RECTIFR) · airframe 71,483 hrs · 53,478 cycles

STRONG BURNING ODOR IN COCKPIT IMMEDIATELY AFTER TAKE OFF. NO SMOKE OR VISIBLE FUMES. NO ODORS IN CABIN AREA. ODOR DISSIPATED AFTER 3 OR 4 MINUTES. NO ABNORMAL COCKPIT INDICATIONS. FOUND TRANSFORMER RECITIFER DIODES DISCOLORED. REPLACED BOTH DIODES IAW AMM 24-00-00.

Part: PACKING — DAMAGED (ESCAPE SLIDE) · airframe 71,033 hrs · 53,126 cycles

DAMAGE PACKING OF TAIL CONE EVACUATION SLIDE. THE SLIDE WAS REPLACED AND WAS INSTALLED IAW CARD 5350-4644, JOB 001-0195.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,033 hrs · 53,126 cycles

CRACK ON WEB AT STA Y=1463 CANT BTW 10HRS AND 11HRS POSITION IN AFT ACCESSORY COMPARTMENT. DAMAGE AREA WAS REPAIRED PER SRM 53-03D FIG 38A, 51-30-2 & 51-30-5, 51-10-3 PAR 21 AND 14.

Part: PAN — CRACKED (BS 162) · airframe 71,033 hrs · 53,126 cycles

CRACK ON INTERNAL PAN BS 162 BTWEEN UPPER EDGE AND BEAM 1 AT MAIN ENTRANCE DOOR. HFEC INSPECTION WAS ACCOMPLISHED ON INTERNAL PAN. ONE CRACK OF 2.340 WAS FOUND. STOP DRILL WAS PERFORMED, HFEC WAS ACCOMPLISHED AFTER STOP DRILL AND NO CRACKS WERE FOUND. INTERNAL PAN AND ITEMS REMOVED WERE REPAIRED AND INSTALLED IAW SRM 51-30-1,51-30-2,51-30-4 AND 52-05 FIG 18A.

Part: ANGLE — CRACKED · airframe 71,033 hrs · 53,126 cycles

CRACK ON ANGLE BS 195 BELOW OF BEAM 1 AT FWD SERVICE DOOR. THE ANGLE WAS REPLACED IAW SRM 51-30-5 AND DWG 9911579 REV L.

Part: WEB — CRACKED (BS 192 L1 DOOR) · airframe 71,033 hrs · 53,126 cycles

CRACK ON INTERNAL WEB BS 192 OF THE L1 DOOR. THE WEB WAS REPAIRED IAW SRM 52-01 FIGURE 4.

Part: BEAM — CRACKED (PAX DOOR) · airframe 71,033 hrs · 53,126 cycles

CRACK ON BEAM NR 6 BS 177 AT MAIN ENTRANCE DOOR. THE BEAM WAS REPAIRED IAW ERA 413018-14 MA REV ORIG.

Part: LONGERON — CRACKED (BS 160) · airframe 71,033 hrs · 53,126 cycles

CRACKED LONGERON 3L BS 160. THE LONGERON WAS REPLACED IAW SRM 53-02 FIG.18.

Part: SPACER — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 71,033 hrs · 53,126 cycles

CORROSION ON SPACER OF LOWER BEAM BS 642 AT MID CARGO COMPARTMENT DOOR FRAME. THE SPACER WAS REPLACED IAW 53-05 FIG 123.

Part: BEAM — CRACKED (PAX DOOR) · airframe 71,033 hrs · 53,126 cycles

CRACK ON BEAM NR 8 (AFT EDGE) AT MAIN ENTRANCE DOOR. BEAM WAS REPAIRED IAW SRM 52-05 FIG. 95 SHEET 3.

Part: SPACER — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 71,033 hrs · 53,126 cycles

CORROSION ON SPACER AT AFT CARGO BAY LOWER DOOR FRAME. SPACER WAS REPLACED IAW SRM 53-05 FIG 123 SHEET 5 AND 51-30-5, 51-30-4.

Part: STRUT — DEFECTIVE (NLG) · airframe 70,375 hrs · 52,629 cycles

NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO DEPARTURE. MAINTENANCE FOUND THE NOSE STRUT COMPRESSED COMPLETELY. THE CREW INDICATED THE RIDE WAS HARSH DURING TAXI OUT. UPON DISASSEMBLY, THE SHOCK STRUT METERING PIN WAS DETERMINED TO BE BYPASSING. MSP MAINTENANCE REPLACED THE SHOCK STRUT ASSEMBLY IAW CMM 32-21-04. THE STRUT WAS SERVICED IAW AMM 32-21-02. THE POST SERVICE LANDING GEAR OPS CHECKS/GEAR SWING WAS ACCOMPLISHED IAW AMM 32-30-00 WITH SATISFACTORY RESULT. LEAK AND OPS CHECKS WERE ALL GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,338 hrs · 52,604 cycles

SEAT 2B AND 34E OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTER PACKS PER AMM 33-53-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,752 hrs · 52,186 cycles

FIRST CLASS CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-100.

Part: PIN — GOUGED (TAILCONE RELEASE) · airframe 69,682 hrs · 52,148 cycles

ON SHIP 945, MSP MAINTENANCE FOUND THE UPPER LT TAIL CONE RELEASE LOCK PIN GOUGED. THE LOCK PIN WAS REPLACED BY MSP MAINTENANCE.

Part: PIN — GOUGED (TAILCONE RELEASE) · airframe 69,682 hrs · 52,148 cycles

THE TAILCONE RELEASE OPS CHECK FAILED. MSP MAINTENANCE FOUND A T-PIN GOUGED AND REPLACED IT.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,775 hrs · 51,502 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN ROWS 31 THROUGH TO THE TAIL COMPARTMENT WERE INOPERATIVE. MAINTENANCE REPLACED THE FAILED FUSE AT THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,775 hrs · 51,502 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN ROWS 31 TO THE BACK OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,767 hrs · 51,498 cycles

MAINTENANCE FOUND THE EMERGENCY LIGHTS FROM SEAT ROWS 31 AND AFT TO BE INOPERATIVE. THE B5-212 POWER SUPPLY WAS REPLACED. THE LIGHTS TESTED GOOD.

Part: WIRE — CHAFED (EMERGENCY LIGHTS) · airframe 68,708 hrs · 51,453 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS FROM ROWS 30 AND AFT IN THE CABIN WERE INOPERATIVE. MAINTENANCE FOUND A WIRE CHAFING IN A SEAT TRACK, REPAIRED THE WIRE INSULATION, AND REPLACED THE BLOWN FUSE.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 68,565 hrs · 51,341 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT ALL OF THE EMERGENCY LIGHTING FROM ROW 31 AND AFT IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE FAILED FUSE AT THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,518 hrs · 51,308 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN ROWS 31-38 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,437 hrs · 51,249 cycles

MAINTENANCE FOUND AFT OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. BATTERIES WERE REPLACED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,264 hrs · 51,110 cycles

ACFT MAINTENANCE FOUND SEAT SHROUD EMERGENCY LIGHTS INOPERATIVE ON SEAT ROWS 31 AND AFT. UPPER FUSE IN EMERGENCY LIGHT BATTERY LIGHT CHARGER ABOVE SEAT ROW 35R WAS REPLACED AND NOW ALL EMERGENCY LIGHTS CK OK.

Part: WIRE — PULLED (EMERGENCY LIGHT) · airframe 68,187 hrs · 51,059 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 24DE IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND WIRES PULLED OUT OF THE CONNECTOR. THE CONNECTOR WAS REPLACED AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,109 hrs · 51,021 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT ROWS 31-35 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,060 hrs · 50,983 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE AFT CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,007 hrs · 50,941 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT ROWS 31-36 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND A FAULTY LIGHT ASSY WHICH WAS BLOWING FUSES. A SATISFACTORY FUNCTIONAL CHECK WAS PERFORMED AND THE ACFT RETURNED TO SERVICE.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,808 hrs · 50,823 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT SEAT 31DE IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED A BAD FUSE ON THE BATTERY PACK AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,735 hrs · 50,766 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT ROWS 31-36 WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,532 hrs · 49,979 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS ABOVE THE OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS. OPS CHECKED GOOD.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 66,375 hrs · 49,877 cycles

DURING INITIAL CLIMBOUT, CREW REPORTED A HOT HYDRAULIC ODOR BEING EMITTED FROM THE AIR CONDITIONING SYSTEM. BOTH THE FORWARD AND THE REAR LAVATORY SMOKE DETECTORS SOUNDED. ODOR DISSIPATED AND ALARMS SILENCED QUICKLY BUT THEN IT ALL REPEATED DURING APPROACH FOR LANDING AT DESTINATION. MAINTENANCE DISCOVERED THREE HYDRAULIC LINE LEAKS. THE A SYSTEM RETURN LINE, THE SPOILER SHUTOFF VALVE LINE, AND THE LEFT ANTI-SKID VALVE FITTING, WERE PROVIDING FLUID TO BE INGESTED BY THE APU. TWO O-RINGS AND A TEMPORARY LINE WERE INSTALLED AND THE ACFT RETURNED TO SERVICE.

Part: CONDUIT — WORN (TAILCONE RELEASE) · airframe 66,010 hrs · 49,594 cycles

MAINTENANCE DISCOVERED THAT THE LT AND RT SIDE CONDUIT FOR THE RELEASE CABLE OF THE TAILCONE WAS WORN OUT OF ALLOWABLE LIMITS. THE CONDUIT TUBE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: CAM — WORN (TAILCONE RELEASE) · airframe 66,010 hrs · 49,594 cycles

MAINTENANCE DISCOVERED THAT THE TAILCONE RELEASE MECHANISM CAM BASE WAS WORN OUT OF ALLOWABLE LIMITS. THE CAM BASE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS.

Part: RELEASE CABLE — OUT OF RIG (TAILCONE) · airframe 66,010 hrs · 49,594 cycles

MAINTENANCE DISCOVERED THAT THE TAILCONE RELEASE CABLE WAS OUT OF ALLOWABLE RIG LIMITS AS IT DID NOT CLEAR THE CONDUIT BY THE SPECIFIED .2". THE CABLE CLAMPS WERE ADJUSTED AND THE SYS WAS RIGGED BACK INTO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.

Part: FRAME — CRACKED (BS 1485) · airframe 66,010 hrs · 49,594 cycles

CANTED FRAME WEB AT BS 1485, HAS A .3750 INCH LONG CRACK AT RIVET, NEAR 8:00 O`CLOCK POSTION, WHERE TAIL INTERIOR TAIL CONE RELEASE HANDLE SUPPORT ANGLE ATTACHES. REPAIRED IAW SRM 51-70-05.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 66,010 hrs · 49,594 cycles

VERTICAL STABILIZER LT SIDE FRONT SPAR CRACKED BELOW ZFS 52.267. REPAIRED IAW ER/A 529591-14AD, REVISION ORIGINAL.

Part: SERVICE PANEL — CORRODED (LAVATORY) · corrosion level 2 · airframe 66,010 hrs · 49,594 cycles

AFT LAVATORY SERVICE PANEL HAS BULGING CORROSION AT THE LOWER FWD CORNER. CUTOUT SKIN AND INTERNAL DOUBLER TO REMOVE AREAS OF CORROSION. REPAIRED IAW PRI 529587-14, REV 0, 1, AND 2. ALL STEPS ACCOMPLISHED. COMPLIED WITH ER/A 529587-14, REV ORIG.

Part: ANGLE — DAMAGED (VERTICAL STAB) · airframe 66,010 hrs · 49,594 cycles

DURING C-CHECK, ELONGATED HOLES WERE FOUND COMMON TO THE LT ANGLE OF THE VERTICAL STABILIZER FRONT SPAR. FOUR OF THE HOLES ARE THE FIRST, FOURTH, FIFTH, AND SIXTH ABOVE ZFS=52. ONE OF THE HOLES IS THE FOURTH HOLE BELOW ZFS=52. ER/A 529591-14AD SECT I WAS ACCOMPLISHED.

Part: PANEL — OUT OF TOLERANCE · airframe 66,010 hrs · 49,594 cycles

DURING TAILCONE RELEASE FUNCTIONAL CHECK, AFT ENTRANCE DOOR ROD FAILED TO PUNCTURE DECAL AND EXTEND. FOUND INTERFERENCE FROM DECORATIVE DOOR PANEL AROUND CAM ARM ASSY. TRIMMED DECORATIVE DOOR PANEL FOR CLEARANCE. OPS CHECKED GOOD IAW AMM 53-53-00-501 AND AMDS 5350-01077-0101.

Part: BULKHEAD WEB — CRACKED (BS 1463) · airframe 66,010 hrs · 49,594 cycles

TAIL INTERIOR CANTED BULKHEAD, BS 1463, WEB CRACKED ON FWD SIDE 23" OTBD OF ACFT CENTER LINE RT SIDE- HFEC CONFIRMED ENDS MARKED. COMPLIED WITH PRI 529613-14, REV 1 AND REPAIRED IAW ER/A 529613-14, REV ORIGINAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,535 hrs · 48,604 cycles

FLIGHT CREW CONFIRMED THAT THE EMERGENCY LIGHT SYSTEM DID NOT ILLUMINATE ANY LIGHTS WHEN TESTED AND WAS INOPERATIVE WITH THE SWITCH IN ARM AND ONLY GROUND POWER AS A SOURCE DURING INITIAL POWER-UP. MAINTENANCE REPLACED ALL EMERGENCY LIGHT BATTERY PACKS AND THE SYSTEM RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,131 hrs · 48,333 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS IN ROWS 16-20 INOPERATIVE. REPLACED THE BATTERY PACK AND OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 63,545 hrs · 47,909 cycles

EMERGENCY SEAT LIGHT INOPERATIVE AT ROW 17. FOUND BROKEN WIRE IN SEAT CONNECTOR. REPLACED PIN IAW AMM 33-52, OPERATIONS CKS OK.

Part: WIRE — PULLED (EMERGENCY LIGHTS) · airframe 63,471 hrs · 47,841 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 3D IN THE CABIN WAS INOPERATIVE. MX FOUND WIRES PULLED OUT OF THE LIGHT SOCKET. THE LIGHT ASSY WAS REPLACED AND THE SYS RETURNED TO NORMAL OPERATION.

Part: O-RING — LEAKING (HYD SYSTEM) · airframe 63,035 hrs · 47,501 cycles

FLIGHT CREW AND CABIN CREW DETECTED A STRONG ODOR CIRCULATING ABOUT THE ACFT WHILE CLIMBING THROUGH FL300. CREW DESCENDED THE ACFT TO FL250 AND COMPLETED QRH PROCEDURES. ODOR DISSIPATED WITH SECURING GALLEY POWER AND THE FLIGHT CONTINUED TO SCHEDULED DESTINATION. MX FOUND AN O-RING LEAKING ON THE HYD PRESSURE RELIEF VALVE IN THE LEFT WHEEL WELL AND REPLACED IT AND ALSO CLEANED HYD FLUID RESIDUE FROM AROUND THE APU INLET. THE NR 2 COFFEEMAKER WAS REPLACED DUE TO FACT THAT THE ODOR WENT AWAY WHEN THE GALLEY POWER WAS TURNED OFF.

Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 62,982 hrs · 47,460 cycles

THE CREW DIVERTED THE ACFT AFTER SMOKE WAS REPORTED CIRCULATING IN THE CABIN. MX REPAIRED A HYD LINE LEAK IN BAG BIN TUNNEL AREA. DUCT BURN OUT PROCEDURES WERE COMPLETED.

Part: UNKNOWN — SMOKE (CABIN & COCKPIT) · airframe 62,788 hrs · 47,318 cycles

THE CREW NOTICED SMOKE IN COCKPIT AND CABIN DURING CLIMB. SMOKE COINCIDED WITH ENGINE HEAT ACTIVATION AND WAS COMING FROM VENTS. SMOKE WAS STRONG ENOUGH TO BE VISUALLY DETECTED AND SET OFF FIRST CLASS LAVATORY SMOKE DETECTOR. DETECTOR EVENTUALLY SILENCED ITSELF AND SMOKE DISSIPATED. ENGINE HEAT WAS NOT ACTIVATED AGAIN. MX INSPECTED ENGINE INLETS AND EXHAUSTS AND PULLED BLEED DUCT CAPS, NO EVIDENCE OF OIL. SLIGHT EVIDENCE OF OIL AROUND APU INLET. CLEANED APU INLET. RAN APU, NO LEAKS NOTED. NO SMOKE OR ODOR PRESENT. NO EVIDENCE OF OIL FOUND DURING BOROSCOPE INSPECTION OF NR 1 AND NR 2 ENGINES 8TH AND 13TH STAGE DUCTS.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 62,452 hrs · 47,093 cycles

DURING LINE CHECK, MX FOUND THAT THE FORWARD EMERGENCY PATHWAY LIGHT IN THE AFT STAIRWAY IN THE TAIL COMPARTMENT WAS NOT INSTALLED AND 2 AFT LIGHTS WERE NOT CONNECTED AND THEREFORE, INOPERATIVE. MX INSTALLED A NEW LIGHT ASSEMBLY IN THE AFT STAIRWELL AND ALSO CONNECTED 2 SIDEWALL EMERGENCY PATH LIGHTS. OPS CHECK WAS GOOD.

Part: COVER — INOPERATIVE (ESCAPE ROPE) · airframe 62,452 hrs · 47,093 cycles

THE CAPTAIN DISCOVERED THAT THE COCKPIT ESCAPE ROPE COMPARTMENT PANEL OVER THE CREW SEATS WOULD NOT OPEN. THIS IS CONSIDERED A DEFECT IN THE EMERGENCY ESCAPE SYS AND COULD HAVE AN ADVERSE AFFECT IN AN EVACUATION. THE PANEL WAS ADJUSTED SO IT WOULD NO LONGER BIND DURING OPERATION AND RIGGED TO MEET PUBLISHED SPECIFICATIONS.

Part: SLIDE — MISINSTALLED (TAILCONE) · airframe 62,447 hrs · 47,088 cycles

INSPECTION DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE IN THE TAILCONE WAS NO LONGER IN AN ACCEPTABLE CONFIGURATION. AN OUT OF POSITION, MISRIGGED, POOR CONDITION, OR ILL-ARRANGED SLIDE ASSY COULD PREVENT PROPER DEPLOYMENT OF THE ESCAPE SYS AND IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE TAILCONE SLIDE WAS REPLACED AND AN RII WAS COMPLETED SATISFACTORILY.

Part: ACTUATOR — CRACKED (AIRSTAIR DOOR) · airframe 62,446 hrs · 47,087 cycles

LOWER SUPPORT PLATE OF AIRSTAIR DOOR ACTUATOR IS CRACKED. REMOVED LWR SUPPORT PLATE REPAIR AIRSTAIR DOOR ACTUATOR AT BOTTOM OF RT CANTED FRAME STA.1485 FOR REPLACEMENT, FOUND MORE CRACK PAST PREVIOUS STOP DRILL, PERFORMED NEW STOP DRILL, PERFORMED HFEC INSP, NO CRACK INDICATION PASSING STOP DRILL, FABRICATED NEW LWR SUPPORT PLATE REPAIR & INSTALLED AT LWR END OF CANTED FRAME STA 1485 RT. UNDER AIRSTAIR DOOR ACTUATOR BRACKET.

Part: FRAME — CRACKED (BS 1463) · airframe 62,446 hrs · 47,087 cycles

AFT ACCESSRORY COMP CANTED FRAME 1463 WEB CRACKED AT LONG 9 LEVEL APROX AFT SIDE BRACKET CRACKED AT VENT BOX INBD ATTACH POINT AND SEVERAL SPOTS OF CORROSION ON FWD SIDE OF WEB AND FRAME BETWEEN L5LT AND L9LT. REPLACED 2 EA ANGLE BRACKETS, REWORKED AREAS FOUND WITH IN LIMITS. INSTALLED REPAIRED CANTED FRAME 1463 WEB LONG 9.

Part: SEAT TRACK — CORRODED (BS 828-997) · airframe 62,446 hrs · 47,087 cycles

CORROSION SEAT TRACK STA 828, 967, 997 AT LBL 54.5, REMOVED CORROSION, CHECK LIMITS IAW SRM 51-10-3-53-05. FOUND OUT OF LIMITS. REPLACED SEAT TRACK SECTIONS FROM STA 798 TO STA 1032 LBL 54.5 WITH A SPLICER. REPAIRED SEAT TRACK AT STA 916 LBL 545. IDENTIFIED REPAIR IAW PS. 900-51-1-N.4. REMOVED CORROSION ART SEAT TRACK STA 828, 967, 997 AT LBL 545.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 62,446 hrs · 47,087 cycles

LIGHTNING STRIKE ON WINDOW BELT PANEL. REPAIRED IAW ER/A 512606-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 62,446 hrs · 47,087 cycles

TWO LIGHTNING STRIKES ON WINDOW BELT. REPAIRED IAW ER/A 512605-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 62,446 hrs · 47,087 cycles

LIGHTNING STRIKE ON WINDOW BELT. REPAIRED IAW ER/A 512606-14.

Part: CUSP WEB — CRACKED (BS 788-807) · airframe 62,446 hrs · 47,087 cycles

RT CABIN FLOOR CUSP WEB HAS LIGHT CORROSION AND SCRATCHES BS 788-807 RBL 58-60. FOUND CRACKED AS WELL. REMOVED WEB AND INSTALLED NEW WEB REF SRM 51-30-01,51-30-02, 51-10-04.

Part: CUSP WEB — CRACKED (BS 1235) · airframe 62,446 hrs · 47,087 cycles

LEFT CABIN FLOOR CUSP WEB CRACKED & CORRODED AT LIGHTNING HOLE FS 1235, LBL 58. REMOVED CORROSION IAW SRM 51-10-03, FOUND OUT OF LIMITS IAW ER/A 508307-1474, FABRICATED DOUBLER AND INSTALLED DOUBLER REPAIR IAW SRM 51-30-02.

Part: FLOOR SUPPORT — CORRODED (BS 180-200) · airframe 62,446 hrs · 47,087 cycles

MAIN CABIN FLOOR SUPPORT ANGLE HAS CORROSION FROM STA 180 TO 200 AT RBL 53. REMOVED CORROSION AND FOUND OUT LIMITS IAW SRM 51-10-03 AND 53-01, FIG 1. REPLACED FLOOR SUPPORT IAW SRM 51-30-2.

Part: FLOOR SUPPORT — DAMAGED (BS 1079) · airframe 62,446 hrs · 47,087 cycles

AFT CARGO BAY FRAME BS 1079 LT FLOOR SUPPORT ANGLE BENT AND DAMAGE HOLE. REMOVED FLOOR SUPPORT ANGLE IAW SRM 51-30-5. FABRICATED AND INSTALLED NEW ANGLE SUPPORT IAW SRM 51-30-5.

Part: FLOOR SUPPORT — DAMAGED (BS 1117) · airframe 62,446 hrs · 47,087 cycles

AFT CARGO BS AT FRAME BS 1117 LT FLOOR SUPPORT ANGLE BENT, DENTED, AND DAMAGED. REMOVED DAMAGED FLOOR SUPPORT ANGLE AND INSTALLED NEW FLOOR SUPPORT ANGLE IAW ER/A 413029-14MA AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 541-560) · airframe 62,446 hrs · 47,087 cycles

LEFT CABIN CUSP WEB HAS CORROSION BS 541-560 LBL 58-60. FABRICATED AND INSTALLED REPAIR IAW SRM 53-05.

Part: FLOOR SUPPORT — DAMAGED (BS 1041) · airframe 62,446 hrs · 47,087 cycles

AFT CARGO BS AT FRAME BS 1041 FLOOR SUPPORT BENT AND DAMAGE HOLE. REMOVED FLOOR SUPPORT, FABRICATED, AND INSTALLED NEW FLOOR SUPPORT ANGLE IAW SRM 51-30-5.

Part: SUPPORT ANGLE — DAMAGED (BS 1212) · airframe 62,446 hrs · 47,087 cycles

AFT CARGO BS DOOR LOWER JAM AFT CORNER SCUFF PLATE ANGLE SUPPORT CORRODED DAMAGE AT FRAME STA 1212. REMOVED SCUFF PLATE SUPPORT ANGLE AND INSTALLED SCUFF PLATE SUPPORT ANGLE IAW SRM 51-30-5.

Part: ANGLE — CORRODED (BS 1155) · airframe 62,446 hrs · 47,087 cycles

AFT CARGO COMP AT FRAME BS 1155, SMALL A FLOOR ANGLE SUPPORT BETWEEN STR 29R AND 28R HAS SURFACE CORROSION TOP AND UNDER. REMOVED DAMAGE FLOOR ANGLE SUPPORT FOUND OUT OF LIMITS 51-30-5. LOCATED, DRILLED, AND INSTALLED NEW FLOOR ANGLE SUPPORT AT STA 1155 BETWEEN STR 29R AND 28 R IAW MD-88.

Part: FAIRING — CRACKED (HORIZONTAL STAB) · airframe 62,446 hrs · 47,087 cycles

RT UPPER BANANA FAIRING 3806 HAS 3 INCH CRACK AT FWD END. DETERMINE CRACKS LENGTH REF SPM 06-10 01-001-STOP DRILLERS ATR/UPPER BANANA FAIRING 38. NO CRACK INDICATION PAST STOP DRILLS FOUND. FABRICATED AND INSTALLED DOUBLER RT UPPER BANANA FAIRING 3806 IAW SRM 51-10-21. REPLACED SEAL.

Part: SKIN — DAMAGED (BS 1287-1309) · airframe 62,446 hrs · 47,087 cycles

ACFT DAMAGE AT RT FUS SKIN AT DRAIN OPENING BETWEEN FRAME STA 1309 & 1287 & BETWEEN LONGERON 24R & LONGERON 25R, ACCOMPLISH HIDING DAMAGE INSPECTION. CUT OUT DAMAGE AREA. NDT NO CRACK NOTED, FABRICATED SKIN DOUBLER REPAIR AND FINGER DOUBLER. INSTALLED DOUBLER AND FINGER REPAIR. INSTALLED PERMANENT REPAIR ID TAG IN REF PROCESS ST 900-5-1, NR 4.

Part: FRAME — CRACKED (BS 1485) · airframe 62,446 hrs · 47,087 cycles

AFT ACCESSORY COMPT FRAME BS 1485 RT AFT UPPER CORNER PREVIOUS REPAIR CRACK AND WEB CRACK. REMOVED PREVIOUS REPAIR. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-30-2, 53-01 FIG 2 51-10-3 & 51-30-1.

Part: SKIN — CRACKED (BS 1418) · airframe 62,446 hrs · 47,087 cycles

DURING SCHEDULED INSPECTION, THE FUSELAGE CROWN SKIN HAD A 2 INCH CRACK FS 1418, RBL 3. REPAIRED IAW SRM 53-04, FIG 40. IDENTIFIED REPAIR IAW PS 900-5-1- NR 4.

Part: ATTACH ANGLE — CORRODED (BS 1328) · airframe 62,446 hrs · 47,087 cycles

DURING SCHEDULED INSPECTION, THE RT LAVATORY AREA FS 1328 FLOOR ATTACH ANGLE HAS INTERGRANULAR CORROSION AT FUSELAGE ATTACHMENT. REPAIRED IAW SRM 53-05, FIG 24A ID REPAIR IAW PS 900-5-1 N4.

Part: CUSP WEB — CORRODED (BS 636-656) · airframe 62,446 hrs · 47,087 cycles

LT CABIN FLOOR CUSP WEB AND DOUBLER REPAIR HAS CORROSION SPOTS FS 636-656, LBL 57"-60". (MRB 53-037-02). REMOVED CORROSION, FOUND OUT OF LIMITS; INSTALLED REPAIR IAW SRM 51-30-2, 51-30-5, 53-05- FIG 131A-6.

Part: CUSP WEB — PUNCTURED (BS 313) · airframe 62,446 hrs · 47,087 cycles

RT CABIN FLOOR CUSP WEB PUNCTURED FS 313, RBL 53. CUT OUT DAMAGE AREA FABRICATED & INSTALLED DOUBLER IAW SRM 51-10-3 51-30-2 AND 53-05 FIG 131A-23.

Part: CUSP WEB — CORRODED (BS 1098-1117) · airframe 62,446 hrs · 47,087 cycles

RT CABIN FLOOR CUSP WEB HAS CORROSION SPOTS FS 1098-1117 RBL 55-60. REMOVED CORROSION FOUND OUT OF LIMITS. REMOVED FASTENERS AND CUTOUT DAMAGE AREA. FABRICATED AND INSTALLED DOUBLER AND FILLER REPAIR IAW SRM 53-05, SRM 53-01, SRM 51-30-2, SRM 51-10-2A AND SRM 51-10-3.

Part: CUSP WEB — CORRODED (BS 1128-1155) · airframe 62,446 hrs · 47,087 cycles

RT CABIN FLOOR CUSP WEB HAS CORROSION SPOTS FS 1128-1155, RBL 55-59. CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS FROM STA 1145 TO 1166. A FILTER AND DOUBLER REPAIR WAS CARRIED OUT IAW SRM 53-05, REPAIR CONFIGURATION NR 7017. REPAIR WAS TREATED, PRIMED AND TOP COATED IAW SRM 51-10-03.

Part: CUSP WEB — CORRODED (BS 579-589) · airframe 62,446 hrs · 47,087 cycles

LT CABIN FLOOR CUSP WEB HAS CORROSION SPOTS BETWEEN FS 579 AND 598 LBL 57-60. REMOVED CORROSION AT LT CABIN FLOOR CUSP WEB UPPER SURFACE FS 579 & 598 LBL 57-60, ORIG MAT:.020", MAT. REMOVED: .004", REMAINING MAT:.016", FOUND OUT OF LIMITS IAW SRM 51-10-3 & 53-01 & ER/A 508307-14 MA. CUT OUT DAMAGE AREA AND INSTALLED REPAIR PARTS IAW SRM 53-05 FIG 131A-1 & 51-10-3. IDENTIFIED REPAIR IAW DELTA PS900-5-1-NR4.

Part: CUSP WEB — CORRODED (BS 1155-1212) · airframe 62,446 hrs · 47,087 cycles

RT CABIN FLOOR CUSP WEB HAS LIGHT CORROSION SPOTS BS 1155-1212 RBL 56-58. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS FROM BS 1145 TO 1166. A FILLER AND DOUBLER REPAIR WAS CARRIED OUT IAW SRM 53-05, REPAIR CONFIGURATION NR 7017. REPAIR AND AREAS OF CORROSION WERE TREATED, PRIMED, AND TOP COATED IAW SRM 51-10-03.

Part: CUSP WEB — CORRODED (BS 522-541) · airframe 62,446 hrs · 47,087 cycles

RT CABIN FLOOR CUSP WEB AND DOUBLER REPAIR HAS CORROSION SPOTS FS 522-541, RBL 56-60. REPLACED REPAIR DOUBLER IAW SRM 53-05.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 62,277 hrs · 46,969 cycles

DURING SVC, FOUND AFT CARGO FLOOR PANEL DAMAGED. FABRICATED NEW FLOOR PANEL AND INSTALLED.

Part: RELEASE CABLE — OUT OF RIG (TAILCONE) · airframe 60,341 hrs · 45,603 cycles

PERFORMED TAILCONE RELEASE SYSTEM OPERATIONAL CHECK 6908 AND FOUND THAT THERE WAS EXCESSIVE SLACK IN THE LOWER TAILCONE RELEASE CABLE. THE CABLE SYSTEM WAS RE-RIGGED AND THE LATCH LEVER CLAMP E WAS ADJUSTED. THE RII STEPS WERE COMPLETED AND THE FOLLOW-UP CHECK WAS SUCCESSFUL.

Part: COVER — UNSECURE (ESCAPE SLIDE) · airframe 60,341 hrs · 45,603 cycles

DURING THE PERFORMANCE OF THE TAILCONE RELEASE SYSTEM OPERATIONAL CHECK (OPN 6908), MAINTENANCE FOUND THE SLIDE COVER UNSECURED. THE COVER WAS REMOVED, THE SLIDE PACK WAS READJUSTED, AND THE COVER PROPERLY REPLACED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 59,971 hrs · 45,366 cycles

DURING INSPECTION THE EMERGENCY EGRESS AISLE LIGHTS WERE FOUND TO BE INOPERATIVE BETWEEN ROWS 31 AND 36. MAINTENANCE REPLACED THE POWER SUPPLY BATTERIES AND THE OPERATIONAL CHECK WAS GOOD.

Part: LANYARD — MISROUTED (EVAC SLIDE) · airframe 59,695 hrs · 45,180 cycles

TAIL CONE SLIDE INSTALLATION FAILED ROUTINE INSPECTION IN MSP. THE LANYARD WAS FOUND TO BE INCORRECTLY ROUTED AT THE LT AND RT ATTACH POINTS. MAINTENANCE DID CORRECT THE INSTALLATION PER ERA 493276-14, AMM 53-53-00 STEPS B-14-B18, AND OPN 7915 STEPS 3N-3P.

Part: SPAR CAP — CRACKED (HORIZ STAB) · airframe 59,628 hrs · 45,134 cycles

120911 CRACKED UPPER RIGHT SPAR HORIZONTAL STAB. REPLACED SPAR CAP.

Part: REGULATOR VALVE — MALFUNCTIONED (AC BAY) · airframe 59,569 hrs · 45,102 cycles

AS THE AIRCRAFT WAS CLIMBING THROUGH FL240, AN ELECTRICAL BURNING SMELL WAS REPORTED IN THE CABIN. CREW NOTED THAT THE OVERHEAD CIRCUIT BREAKER FOR THE LEFT AIR CONDITIONING REGULATOR VALVE (B-13) HAD TRIPPED. MAINTENANCE REPLACED THE PRESSURE REGULATOR VALVE AND ACCOMPLISHED OPN 5089, PNEUMATIC SYSTEM DUCT BURNOUT. (2011-D1373)

Part: UNKNOWN — ODOR (CABIN) · airframe 59,523 hrs · 45,067 cycles

F/A REPORT OF ELECTRICAL SMELL/ODOR. MTC PERFORMED OPN 5088, NO TROUBLE FOUND.

Part: UNKNOWN — ODOR (CABIN) · airframe 59,523 hrs · 45,067 cycles

THE AIRCRAFT RETURNED TO BWI APPROXIMATELY 15 MINUTES AFTER TAKEOFF DUE TO AN ELECTRICAL ODOR FROM THE REAR OF THE CABIN. MAINTENANCE COMPLETED A FULL DUCT BURNOUT.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 59,178 hrs · 44,831 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 31-38 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND OPERATIONALLY CHECKED THE SYSTEM.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 57,423 hrs · 43,600 cycles

DURING LINE CHECK, MX FOUND EMERGENCY EXIT LIGHT IN TAIL SECTION ABOVE CATWALK INOPERATIVE. MX RETERMINATED LIGHT ASSY IAW SWPM 20. OPERATION OF LIGHT NOW CHECKS OK.

Part: SLIDE — MISRIGGED (L2 DOOR) · airframe 57,390 hrs · 43,574 cycles

DURING LINE CHECK, MX FOUND L2 DOOR SLIDE LANYARD INSTALLED IMPROPERLY. MX REPOSITIONED L2 DOOR SLIDE LANYARD IAW MM.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 54,825 hrs · 41,518 cycles

DURING LAYOVER, MX FOUND THE NR 10 SEAT EMERGENCY LIGHT WIRE BROKEN MX REWIRED THE NR10 SEAT EMERGENCY LIGHT WIRE. OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,296 hrs · 42,832 cycles

MAINTENANCE FOUND THE EMERGENCY TRACK LIGHT AT SEAT 22D TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY TRACK LIGHT ASSEMBLY AT 22D. AN OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE (ODI2010-D0942)(DLM88102029).

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 55,888 hrs · 42,546 cycles

DURING LINE CHECK, MX FOUND EMERGENCY LIGHT AT 3CD INOP. MX REPAIRED CONNECTOR AT SEAT 3CD. OPS OF LIGHT NOW CHECKS GOOD.

Part: PAN — CORRODED (BS 422) · corrosion level 2 · airframe 55,888 hrs · 42,546 cycles

ON 02JUN10, THE FWD CARGO DOOR SILL LOWER PAN WAS CORRODED BEYOND SRM LIMITS AT STA 422 FWD OF THE AFT CORNER ALSO, JAMB CORRODED BEYOND LIMITS UNDER THRESHOLD AT STA 370. REPAIRED SILL AND JAMB IAW ER/A 09-482741-14 REV ORIG

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,888 hrs · 42,546 cycles

ON 02JUN10, THE MID CARGO DOOR SILL PAN WAS CORRODED BEYOND SRM LIMITS BETWEEN THE FWD AND AFT DOOR STOPS. REPAIRED IAW SRM 53-05, FIG 123. (DLM88101651)

Part: PAN — CORRODED (BS 417) · corrosion level 2 · airframe 55,888 hrs · 42,546 cycles

ON 02JUN10, THE FWD CARGO DOOR SILL PAN AT STA 417 WAS CORRODED BEYOND SRM LIMITS. REPLACED PAN IAW ER/A 09-482741-14 REV ORIG. (DLM88101650)

Part: THRESHOLD — CORRODED (BS 636-693) · corrosion level 2 · airframe 55,888 hrs · 42,546 cycles

ON 02JUN10, THE MID CARGO DOOR THRESHOLD HAD CORROSION BEYOND SRM LIMITS AT ALONG THE EDGE FROM STA 636-693. REPAIRED IAW SRM 53-05, FIG 123.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,888 hrs · 42,546 cycles

ON 02JUN10, THE MID CARGO LOWER DOOR SILL PAN, LOWER FLANGE WAS CORRODED BEYOND SRM LIMITS AT THE AFT DOOR STOP FTG. REPAIRED IAW SRM 53-05 P.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,823 hrs · 42,509 cycles

MX FOUND THE AFT CABIN EMERGENCY FLOOR LIGHTS TO BE INOPERATIVE. MX REPLACED THE AFT CABIN EMERGENCY FLOOR LIGHTS POWER SUPPLY B5-212. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — BROKEN (EMERGENCY LIGHTS) · airframe 55,776 hrs · 42,477 cycles

MX NOTICED THAT THE EMERGENCY LIGHT AT 14DE WAS FOUND TO BE INOPERATIVE. MX FOUND A BROKEN HARNESS AND INSTALLED A SPLICE. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,507 hrs · 42,292 cycles

MX FOUND THE AFT SEAT MOUNTED EMERGENCY LIGHTS TO BE INOPERATIVE. MX REPLACED THE AFT POWER SUPPLY FOR THE EMERGENCY PATH LIGHTS. AN OPS CHECK WAS GOOD AND THE ACFT WAS RETURNED TO SERVICE. INVESTIGATOR E23309.

Part: SOCKET — SHORTED (EMERGENCY LIGHT) · airframe 55,477 hrs · 42,268 cycles

WORKING MSU FOR INTERMITTENT AFT EMERGENCY LIGHT BATTERY CHARGER BLOWING PICO FUSE. FOUND SHORT IN SEAT 31 EMERGENCY LIGHT SOCKET. REPLACED SAME AND TESTED. CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,342 hrs · 42,179 cycles

EMERGENCY LIGHTS IN AFT CABIN INOP. REPLACED EMERGENCY LIGHTS POWER SUPPLY-LIGHTS CK GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,289 hrs · 42,144 cycles

EMERGENCY LIGHTS FROM 31 BACK AND TAIL COMP ARE INOPERATIVE. INSPECTED UNDER SEAT WIRES AND TAIL COMP NO TROUBLE FOUND. REPLACED POWER SUPPLY CHARGER PER M/M LIGHTS OPS GOOD

Part: FUSE — OPEN (EMERGENCY LIGHTS) · airframe 55,261 hrs · 42,121 cycles

EMERGENCY LIGHT OUT FROM ROW 31ED. FOUND AFT BATT PATH FUSE OPEN. REPLACED IAW AMM. OP CK NML. OK FOR SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 47,759 hrs · 37,327 cycles

REPAIR ON FUSELAGE SKIN BETWEEN STA 180-207 AND LONGERONS 19-22L - TEMPORARY REPAIR. TEMPORARY REPAIR REMOVED AND PERMANENT REPAIR INSTALLED PER SRM 53-05D, FIG 57A.

Part: FRAME — CORRODED (FUSELAGE) · airframe 47,759 hrs · 37,327 cycles

EXFOLIATION CORROSION ON LOWER SECTION OF FRAME STA 1380. DAMAGED TEE REMOVED AND NEW SECTION INSTALLED PER DOUGLAS DRAWING 9912246.

Part: FITTING — CORRODED (LT MLG) · airframe 47,759 hrs · 37,327 cycles

LT MAIN LANDING GEAR SUPPORT FITTING, EXFOLIATION CORROSION ON INNER BORE OF BUSHING. CORROSION REMOVED, PERMANENT REPAIR PERFORMED FOLLOWING INSTRUCTIONS AND RECOMMENDATIONS CONTAINED IN THE BCAG SR09570087 AND BCAG SR-ID 1-301794190.

Part: TEE FITTING — DAMAGED (FUSELAGE) · airframe 47,751 hrs · 37,322 cycles

TOOLING MARKS ON LOWER T-CAP CHORD OF AFT PRESSURE BULKHEAD AT STA 1338 BETWEEN LONGERONS 28L-28R. SKIN P/N 5911429-151 TRIMMED FOR ACCESS. CHORD P/N SR09530001-33 SPLICED PER EA 09-086680-12 REV E, OPN 0603. SKIN REPAIRED PER SRM 53-03 FIG 37.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,751 hrs · 37,322 cycles

CRACKS ON FUSELAGE SKIN BETWEEN LONGERONS 2R AND 3R AT STA 1437. PERMANENT REPAIR INSTALLED IAW SRM 53-04 FIG 27.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,751 hrs · 37,322 cycles

FUSELAGE SKIN REPAIR AT STA 379.5 TO 389 BETWEEN LONGERONS 27R AND 29R - SCRATCH AND TWO CRACKS. PERMANENT REPAIR INSTALLED PER AMX REPAIR DRAWING AMR0953593 R1 AND ERA 460140-14.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,751 hrs · 37,322 cycles

REPAIR OF CRACKS IN STA 1446 UPPER CANTED FRAME. FRAME OUTER CAP P/N 9911859-121 REMOVED. NEW CAP INSTALLED PER SRM 53-03D FIG 30.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,736 hrs · 37,308 cycles

CRACK ON FUSELAGE SKIN AT THE STA 175 ON RT UPPER FWD CORNER. DAMAGE REMOVED AND PERMANENT REPAIR INSTALLED PER SRM 53-05D, FIG 112, SH 3.

Part: SKIN — CORRODED (FUSELAGE) · airframe 47,736 hrs · 37,308 cycles

CORROSION AT FUSELAGE SKIN STA 260 BETWEEN LONGERONS 30 AND 29L. CORROSION REMOVED AND PERMANENT REPAIR INSTALLED IAW REPAIR DRAWING AMR0953595 R2 DATED 03APR07 AND ERA 460861-14.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 47,735 hrs · 37,307 cycles

CARGO DOOR JAMB BEAM REPAIR - CORROSION ON BOTTOM OF AFT CARGO COMPARTMENT DOOR JAMB BEAM BETWEEN STA 1175 AND 1195. CORROSION REMOVED AND PERMANENT REPAIR INSTALLED PER SRM 53-05, FIG 63.

Part: SKIN — DAMAGED (T/E FLAP) · airframe 47,735 hrs · 37,307 cycles

LT INBOARD FLAP LOWER SKIN REPAIR BETWEEN STA XW=47 AND XIFO=64.7248 - TEMPORARY REPAIR INSTALLED. TEMPORARY REPAIR REMOVED, DAMAGED SKIN TRIMMED OUT AND NEW SECTION WAS SPLICED PER AM REPAIR DWG AMR0957194 R01 DATED 14MAR07 AND ERA 460139-14.

Part: BALANCE WEIGHT — CORRODED (LT ELEVATOR) · airframe 47,735 hrs · 37,307 cycles

EXFOLIATION CORROSION ON BALANCE TIP OF LEFT ELEVATOR INBOARD FACE. PERMANENT REPAIR ACCOMPLISHED BY REPLACING THE BALANCE TIP FOLLOWING INSTRUCTIONS AND RECOMMENDATIONS CONTAINED IN DWG 5910412.

Part: FITTING — CORRODED (MLG) · airframe 47,731 hrs · 37,305 cycles

DURING CURRENT VISIT, CORROSION WAS FOUND AT THE LHS MLG SUPPORT FITTING AT THE BORE FOR THE RETRACT CYLINDER. THE CORROSION WAS REMOVED BY OVERSIZING THE HOLE AND INCREASING THE DEPTH OF THE BORE, AND WAS APPROVED BY BOEING, WHO ISSUED AN AMOC FAA FORM 8100. REPAIR IS DOCUMENTED IN ERA 460860-14AD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 47,731 hrs · 37,305 cycles

LT FUSELAGE SKIN FS 260 BETWEEN LONGERONS 29L AND 30 CORROSION. ISSUED ER/A 460861-14 WHICH DOCUMENTED SKIN REPAIR. TCAS INTERNAL DOUBLER WAS EXTENDED AND AN EXTERNAL REPAIR DOUBLER WAS ADDED. ER/A REFERS TO AMX REPAIR DWG AMR0953595 WHICH ACCOMPLISHED THE REPAIR. REPETITIVE INSPECTIONS INITIATED AT 8000 HR INTERVALS.

Part: SKIN — CRACKED (FS 382 L29R) · airframe 47,731 hrs · 37,305 cycles

DURING CURENT HMV, A SCRATCH WITH TWO CRACKS WERE FOUND ON THE RHS FUSELAGE SKIN NEAR THE FORWARD CARGO DOOR CUTOUT. THE SUBJECT CRACKS WERE TRIMMED OUT, AND A BOEING APPROVED REPAIR INSTALLED PER 460140-14.

Part: GASKET — LEAKING (APU OIL CAP) · airframe 46,597 hrs · 36,531 cycles

CABIN FILLED UP WITH SMOKE AFTER LEFT ENGINE WAS STARTED. BOTH FIRE DETECTORS WENT OFF IN AFT LAVS. RAN APU. FOUND OIL CAP LEAKING. REPLACED OIL CAP WITH NEW GASKET. LEAK CHECK IS GOOD. CLEANED APU INLET. C/W OPN 5089

Part: SKIN — DENTED (BS 207-S18-19L) · airframe 46,418 hrs · 36,397 cycles

SRM 53-04D FIG 38 TABLE C. DENT IS CONDITION 1B, BUT OUT OF LIMITS DUE TO CREASE AND DISTANCE TO FRAME. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS, TREATED AND PAINTED REPAIR PARTS IAW DRD 53-04D FIG 12B. INITIAL WRITE UP--DENT AFT OF L1 DOOR AT F.S. 207 BETWEEN STR L18 AND L19.

Part: WIRE HARNESS — BROKEN (NLG) · airframe 45,899 hrs · 36,027 cycles

AFTER TAKEOFF WITH GEAR HANDLE IN UP POSITION NOSE GEAR UNSAFE LIGHT ILLUMINATED INTERMITTENTLY FOR REMAINDER OF FLIGHT-GEAR EXTENDED NORMALLY FOR LANDING WITH ALL INDICATIONS GREEN. REPAIRED BROKEN WIRES ON D1-32 NOSE GEAR UPLOCK SENSOR. SWUNG GEAR, ALL OPS AND INDICATIONS NORMAL. C/W OPN 50006 NOSE GEAR SERVICE OPERATION, ALL CHECKS GOOD.

Part: TRANSMITTER — LEAKING (HYD SYSTEM) · airframe 40,343 hrs · 32,103 cycles

WHILE CONFIGURING THE AIRCRAFT FOR APPROACH, THE LEFT HYDRAULIC QUANTITY DECREASED TO 3 QUARTS. SERVICED SAME TO FULL. FOUND HYD PRESS TRANSMITTER LEAKING. REPLACED TRANSMITTER, RAN HYD AND NO LEAKS FOUND PER M/M. OPS CKS GOOD.

Part: PUMP — MALFUNCTIONED (NR 2 ENGINE) · airframe 38,877 hrs · 31,171 cycles

AT LEVEL OFF (FL230) RT ENG FLAMED OUT, LT ENGINE BECAME UNSTABLE, BUT RECOVERED. RIGHT ENG FAILED COMPLETELY. NO VIBES NOTED. REPLACED FUEL PUMP AND CONTROL.

Part: BATTERY — DISCHARGED (ENTRY) · airframe 36,673 hrs · 29,589 cycles

COCKPIT AND ENTRY OVERHEAD EMERGENCY LIGHTS INOP REPLD BATTERY PACK IN CEILING PWR SUPPLY ABOVE NEON AISLE LIGHT

Part: ACTUATOR — FAILED (NLG DOOR) · airframe 36,591 hrs · 29,536 cycles

SEVERE VIBRATION FROM NOSE GEAR AFTER GEAR RETRACTION. GEAR WAS LOWERED AND ALL INDICATIONS WERE NORMAL. FOUND RT GEAR DOOR RETRACTION ACTUATOR FAILED TO LOCK UP. REPLACED GEAR DOOR RETRACTION ACTUATOR PER MM. JACKED NOSE GEAR AND RETRACTED 3 TIMES. OPS CHECK NORMAL

Part: BATTERY — INOPERATIVE (EXTERIOR LIGHTS) · airframe 36,569 hrs · 29,523 cycles

OUTSIDE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERT PACK. OPERATES NORMALLY

Part: SOCKET — BROKEN (CABIN) · airframe 34,328 hrs · 27,856 cycles

PASSENGER SEAT 30D EMERGENCY TRACK LIGHTS INOP. REPLACED SOCKET ASSY, OPS CHECKS NORMAL.

Part: UNKNOWN — ODOR (CABIN) · airframe 31,707 hrs · 25,930 cycles

SHORTLY AFTER TAKEOFF AND THROUGHOUT CLIMB THRU APPROXIMATELY 18,000 FEET PASSENGERS AND FLIGHT ATTENDANTS REPORTED ODORS IN CABIN AROUND THE AFT GALLEY AREA. SMELLS DESCRIBED AS BURNING SMELLS SIMILAR TO BURNING ELECTRICAL OR RUBBER. CK''D OVENS, COFFEEMAKERS, WATER COMPRESSOR, INTERNAL AND EXTERIOR LIGHTS, RECIRC FANS, PACK OPERATION. RAN AIRCRAFT AT TAKEOFF POWER THEN AT 1.8 EPR WITH NO ODORS PRESENT. ALSO RAN APU WITH PACK, OPS STILL WITH NO ODORS. FOUND NO C/B''S POPPED, NO SMELL COMING FROM TIRES AFTER TAXIING. UNABLE TO DUPLICATE.

Part: ELT — TORN (CABIN) · airframe 31,676 hrs · 25,906 cycles

DURING L/O CK, FOUND ELT AUTO RELEASE TAPE TORN AND MISSING. REMOVED AND REPLACED ELT IAW MM.

Part: BRACKET — BROKEN (AIRSTAIR DOOR) · airframe 30,311 hrs · 24,878 cycles

ON CLIMBOUT THROUGH FL 260 FT LOUD POP FOLLOWED BY RAPID DECOMPRESSION. FLIGHT CREW MANUALLY DEPLOYED THE OXYGEN MASKS. REPLACED BROKEN BRACKET ON FWD AIRSTAIR DOOR. DOOR OPENED IN FLIGHT.

Part: SKIN — GOUGED (BS 370)

FUSELAGE/SKIN ASSY, FS 370 STRINGER 20R, REPAIR FOR GOUGE. THE FUSELAGE SKIN WAS BADLY GOUGED AT THE UPPER FWD CORNER OF THE C1 DOOR. THE DAMAGED AREA OF SKIN WAS ROUTED OUT OVER A 3 BY 1 AT THE DOOR CORNER AND OVER A 2 BY 36 AREA OVER STRINGER 20R. THE SKIN CUTOUTS WERE REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER INSTALLED PER ER/A 366297-14, REV B.

Part: BATTERY — DISCHARGED (CABIN)

AFT JUMPSEAT CENTER FLASHLIGHT RED LIGHT NOT FLASHING. REPLACED AFT JUMPSEAT AFT FLASHLIGHT, CKS OK.

Part: ACTUATOR — FAILED (OUTFLOW VALVE)

AFTER T/O, BOTH AUTO PRESS CONTROLLERS FAILED COULD NOT PRESSURIZE A/C IN AUTO. A/C ATB-RETURNED TO STL. REPLACE OUTFLOW VALVE ACTUATOR PER M/M CKS NML.

Part: OIL SYST — LEAKING (APU)

AT CRUISE, CABIN AND COCKPIT NOTED SMOKE. DIVERTED CHA. FOUND APU LEAKING OIL CONTAMINATING PACKS. REPLACED APU.

Part: PACK — MALFUNCTIONED (RIGHT)

ON T/O, THE SMOKE DETECTORS IN THE AFT LAVS SOUNDED THEN QUIT AFTER POWER REDUCTION. AT CRUISE FLIGHT THE FLIGHT ATTN REPORTED AN ODOR FROM THE AIRCOND SYS AT THAT TIME THE ODOR BECAME NOTICEABLE IN THE COCKPIT AND A HAZE WAS NOTICED IN THE CABIN. AN EMERGENCY WAS DECLARED AND THE FLIGHT DIVERTED TO CHA. CONTRACT MTC VERIFIED THE OIL LEVEL IN THE ACMS AND FOUND THE RT PACK WAS PRODUCING THE SMOKE. DEACTIVATED THE PACK PER MEL 21-00-01A.

Part: DUCT — RUPTURED (NR 2 ENGINE)

RT ENG FIRE INDICATION ON CLIMBOUT. FIRE INDICATION EXTINGUISHED WHEN THROTTLE WAS RETARDED. ALL OTHER ENG INDICATIONS NML. FOUND RUPTURED 13TH STAGE DUCT WITH LINER DAMAGE. REPLACED ENGINE.

Part: HYDRAULIC LINE — LEAKING (FUSELAGE)

SMOKE IN CABIN DURING T/O, SMOKE DETECTORS WENT OFF AND SMOKE DISAPPEARED DURING T/O THRUST. REPLACED HYD LINE IN 48 SECTION DROPPING FLUID INTO APU INLET.

Part: TEMP CONTROLLER — MALFUNCTIONED (E/E COMP)

ON TAKEOFF, A STRONG ACRID SMELL FILLED THE CABIN IMMEDIATELY FOR APPROX 4-5 MINUTES. BEFORE CLEARING ODOR, RETURNED WHEN GEAR EXTENDED FOR LANDING. TEMP IN COCKPIT INCREASED, SMOKE DET. ACTIVATED. FOUND RT AUTO TEMP CONT HAD VALVE FULL OPEN, RAN FULL COLD IN MANUAL, RAN BOTH ENGINES AND OPERATED BOTH PACKS. NO PROBLEMS FOUND. FWD. RT. AUTO TEMP. CONTROLLER TO MCO AND PLAC. PER. MEL 21-00-30A.

Part: LIGHT SOCKET — SHORTED (CABIN)

CREW REPORTS, BURNED ODOR AT SEAT ROW 30 TO 31. FOUND SIDEWALL LIGHT SOCKET AND BULB BURNED. REMOVED AND DISCONNECTED BALLAST FWD TO MCO AND PLAC PER MEL 33-00-02. REPLACED LIGHT SOCKET AND OPERATION NORMAL.

Part: THERMOSTAT — MALFUNCTIONED (LT ANTI-ICE)

BURNING ODOR, NO VISIBLE SMOKE ON SHORT FINAL. SMOKE ALARMS IN AFT LAVS ACTIVATED. ANTI-ICE IN USE, ODOR DISSIPATED WHEN ANTI-ICE SHUT OFF. REPLACED ANTICIPATORS AND THERMOSTATS L/R SIDE. NO SMOKE OR ODOR NOTED DURING ENGINE RUN WITH ANTI-ICE ON.

Part: DOOR — CRACKED (CARGO DOOR)

FOUND DURING LETTER CHECK, AFT CARGO DOOR HANDLE CUTOUT CRACKED REPAIRED DOOR HANDLE PER SRM 52-05.