N957DL

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 74,049 hrs · 55,409 cycles

FIRST CLASS EMERGENCY CEILING LIGHTS INOP. R&R BATTERY IN THE EMERGENCY BATTERY PACK B5-100 PER MM 33-53. OPS CHK - GOOD. OK FOR SVC.

Part: BATTERY — DISCHARGED (CABIN) · airframe 74,049 hrs · 55,409 cycles

AFT OVERWING EMERGENCY DOOR EXIT LIGHTS INOP. T-S AND REPLACED CABIN OVERWING EMERGENCY DOOR LIGHTS BATTERY POWER SUPPLY PER MM 33-53. MPN - 803900-1, SN OFF - 25854, SN ON - 98354. OPS CHK GOOD. OK FOR SVC.

Part: CONNECTOR — OUT OF ADJUST (CABIN) · airframe 73,929 hrs · 55,298 cycles

EMERGENCY LIGHT SEAT 15ED INOP. ADJUSTED WIRE CONNECTION. OK FOR SVC. (LP5351383)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,895 hrs · 55,267 cycles

AFT OVER WING EMERG EXIT OVHEAD SIGNS INOP. R/R BATTERY PACK B5-105 PER AMM 33-53. OPS CHK GOOD. (LP5351362)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,629 hrs · 55,020 cycles

OVERWING AFT EMERGENCY EXIT SIGNS WERE INOPERATIVE. R & R THE BATTERIES IAW AMM 33-50. OPS CHECKED NORMAL.

Part: COMPRESSOR — STALLED (RIGHT) · airframe 73,514 hrs · 54,918 cycles

FLT 2599 RETURNED TO BNA DUE TO RIGHT ENGINE FAILURE. COMPRESSOR STALL ON TAKEOFF. CREW SHUT DOWN ENGINE PER QRH. MAINTENANCE FOUND OIL IN TAIL PIPE AND TURBINE DAMAGE. THE ENGINE WAS REPLACED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,378 hrs · 54,789 cycles

EMERGENCY LIGHT BATTERY PACKS B5-104 ANDB5-105 BAD. R&R BATTERY PACKS B5-104 AND B5-105 PER WD 33-51-12. CKS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 73,378 hrs · 54,789 cycles

AFT OVERWING EMERGENCY EXIT LIGHTS INOP. R & R POWER SUPPLY EMERGENCY EXIT OVERWING PER WDM 33-51-12. OPS CK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 73,255 hrs · 54,696 cycles

CATWALK EMERGENCY LIGHT INOP. REPLACED BATTERIES AT B5-28. CHECKS GOOD. REF AMM 33-53.

Part: LIGHT — DAMAGED (CABIN) · airframe 72,591 hrs · 54,163 cycles

SEAT MOUNTED EMERGE LIGHT AT SEAT 16 IS DAMAGED. REPLACED LIGHT ASSY AT SEAT16 JAW AIM 33-50. OPS CHECK GOOD.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 71,826 hrs · 53,589 cycles

SEAT 24D ESCAPE PATH LIGHTS INOP. REPLACED SEAT WIRING HARNESS PER SWPM CHAPTER 20. OPS NORMAL.

Part: LATCH — WORN (TAILCON) · airframe 71,563 hrs · 53,376 cycles

TAILCONE LATCHES WORN AT 10 AND 2 O'CLOCK POSITIONS. REPLACED THE BARREL NUTS AND RETAINERS.

Part: FRAME — DAMAGED (BS 1117) · airframe 71,563 hrs · 53,376 cycles

AFT CARGO BAY FRAME DAMAGED BY FASTENER AT BS 1117 BETWEEN LONGERONS 29 AND 30R. REPAIRED THE FRAME IAW SRM 53-01.

Part: LIGHT — INOPERATIVE (AFT CABIN) · airframe 71,563 hrs · 53,376 cycles

LIGHT ASSEMBLY DAMAGED AT THE LT, AFT END OF THE TAIL COMPARTMENT FWD OF TAIL CONE RELEASE HANDLE. REPLACED THE EMERGENCY FLOODLIGHT IAW AMM 33-53-01.

Part: CABLE — DISCONNECTED (AFT STAIR) · airframe 70,203 hrs · 52,346 cycles

ON ARRIVAL, FOUND CABLE FOR AFT TAIL CATWALK DISCONNECTED. ATTACHED VENTRAL STAIRWAY MOVABLE CEILING LT CABLE IAW AMM 53-20. OPS CHECKED OK.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 69,300 hrs · 51,691 cycles

AFTER TAKEOFF THE AIRCRAFT WOULD NOT PRESSURIZE. ZERO PRESSURE ON BOTH PACK PRESSURE INDICATORS. NO MODE LIGHT ON TRP. AIR RETURN TO KSDF REQUIRED. WHILE AIRBORNE OUTFLOW VALVE WAS FULLY CLOSED WITH FLOW LIGHT ON PRESSURIZATION PANEL. NO FAULT LIGHTS ON EOAP. VERIFIED BOTH PACK SWITCHES WERE ON. AIR CONDITIONING SHUTOFF SWITCH TO OVERRIDE DID NOT HELP. NO AIRFOIL OR ENGINE ANTI-ICE WAS SELECTED ON. PERFORMED BOTH LEFT AND RIGHT PNEUMATIC HEALTH CHECKS PER WORK CARD 2120-2258 AND 2120-2277. ALL CHECKS WERE NORMAL. (LP# 8634350)

Part: PIN — NOT SEATED (EMERGENCY LIGHT) · airframe 68,694 hrs · 51,213 cycles

AFT EMERGENCY LIGHT AT 24DE INOPERATIVE. FOUND PIN PUSHED BACK IN SEAT CONNECTOR. REINSERTED PIN, CKS GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 68,312 hrs · 50,936 cycles

RIGHT HYDRAULIC "HOT" OAP LIGHT ON, THEN ZERO HYDRAULIC PRESSURE BOTH SYS. ACCOMPLISHED QRH PROCEDURES FOR TOTAL HYDRAULIC FAILURE. ON BASE LEG AT 3000' AGL BOTH HYDRAULIC SYSTEMS CAME BACK TO NORMAL. ACCOMPLISHED NORMAL LANDING. FOUND RT HYD SYSTEM WITH EXCESSIVE AIR. BLED BOTH SYSTEMS AND RAN ALL HYD COMPONENTS WITH ENGINES RUNNING AND ELECTRIC PUMP. NO PROBLEMS NOTED.

Part: TEE FITTING — CORRODED (BULKHEAD) · airframe 67,023 hrs · 50,058 cycles

AFT PRESSURE BULKHEAD LOWER TEE CHORD AT L26 AND L27, LT AND RT SIDES, SRM SPLICE REPAIR. COMPLIED WITH ERA/PRI 542247-14, REV 2 DATED 18DEC15 AT 0930E, PRI AND ERA MATCH.

Part: SKIN — CORRODED · corrosion level 2 · airframe 67,023 hrs · 50,058 cycles

AFT LAVATORY SERVICE PANEL HAS CORROSION, SKIN AROUND PERIMETER IS BULGED AND CRACKED. COMPLIED WITH ERA, PRI REV 1 DATED 10DEC15 AT 1550E, PRI MATCHES FINAL ERA 542209-14, REV ORIG.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,368 hrs · 48,117 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT BOTH OF THE OVERWING AFT HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: LIGHT — INOPERATIVE (TAIL) · airframe 63,222 hrs · 47,275 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. MX SECURED THE LOOSE BATTERIES IN THE CHARGER, REPLACED ONE BULB AND TERMINATED THE QUICK DISCONNECT TO THE LIGHT. THE LIGHTS RETURNED TO AN OPERATIONAL STATE.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 62,359 hrs · 46,674 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE SEAT MOUNTED EMERGENCY EXIT ROW LIGHT AT ROW 24D WAS INOPERATIVE. MAINTENANCE REPLACED THE PIG TAIL WIRES AT THE LIGHT AND THE SYS RETURNED TO NORMAL OPERATION.

Part: LONGERON — CORRODED (BS 1309-1322) · corrosion level 2 · airframe 61,961 hrs · 46,413 cycles

CORROSION ON LONGERON 22L BETWEEN BS 1309-1322. LONGERON REPLACED IAW SRM 51-30-5, 53-14-3, ITEM 22, 51-10-4 AND 53-02 FIG 18. .

Part: BULKHEAD — GOUGED (BS 1338) · airframe 61,961 hrs · 46,413 cycles

GOUGES ON LOWER AFT PRESSURE BULKHEAD BETWEEN LONGERONS 28 - 29R BS 1338 AFT CARGO BAY. REPAIRED IAW AMR 09531289 R1 AND ER/A 519155-14, REV ORIGINAL.

Part: CARGO TRACK — CORRODED (BS 332-465) · corrosion level 2 · airframe 61,961 hrs · 46,413 cycles

CORROSION ON RT CARGO TRACK BETWEEN BS 332 TO 370 & 427 TO 465 FWD CARGO BAY. CARGO TRACK WERE REPAIRED IAW SRM 53-05, FIG 4G.

Part: SKIN — CRACKED (BS 1418) · airframe 61,961 hrs · 46,413 cycles

1.906 INCH CRACK ON FUSELAGE SKIN, BS 1418 BETWEEN LONGERON 1 AND 2R. REPAIRED IAW ER/A 519149-14AD REV ORIGINAL.

Part: SKIN — DAMAGED (WINDOW BELT) · airframe 61,961 hrs · 46,413 cycles

LIGHTNING STRIKE ON WINDOW BELT LT FWD UPPER CORNER BETWEEN BS 807 TO 826. SKIN AREA WAS BLENDED, AREA WAS MEASURED AND WAS FOUND OUT OF LIMITS. REPAIR FABRICATED, TREATED , PAINTED, AND INSTALLED IAW SRM 53-05, FIG. III, 51-10-3 PAR. 21 AND 14 AND AMR 09531285 AND ER/A 519138-14 REV ORIG. SECTION III OF ER/A 519138-14, REV ORIG. (UT) WAS ACCOMPLISHED.

Part: SKIN — CRACKED (BS 1418) · airframe 67,877 hrs · 50,608 cycles

CRACK FOUND ON FUSELAGE SKIN AT FS 1418 BETWEEN L1 AND L2R COMMON TO PREVIOUS INSTALLED REPAIR IAW SRM 53-04, FIG 40 AT L2L AND L3L. DTA, PRIOR TO 18 MONTHS SERVICE FROM SECTION I, ACCOMPLISH DTA IAW 14 CFR 25.571 AND 14 CFR 26 SUBPART E. REF SID AD 2004-11-07. ASSOCIATED ER/A 88-519149, ADDED FOR AC 0957. REMOVED INI TIME FROM MASK NOT NEEDED. REDEFERRED LOG TO QC, ESTABILISH MONITOR INSPECTION 10-0553-8-2672, SN 0957 L/L DTA. ER/A 519149-14AD REV A IS CURRENT. SUPPLEMENTAL INSPECTIONS ARE TRACKING VIA LOGPAGE 1967737. THIS LOGPAGE IS TO BE DELETED. CLOSED LOG AND REMOVED MONITOR INSPECTION IAW ALERT 30MAY15 AND LOG COMMENTS.

Part: LONGERON — DEFORMED (BS 1418) · airframe 61,961 hrs · 46,413 cycles

DEFORMED LONGERON 8R AT INTERCONECTION WITH FRAME BS 1418. DAMAGE LONGERON SECTION WAS REMOVED, NEW LONGERON AND SPLICE WERE DRILLED AND ADJUSTED AND WERE INSTALLED IAW SRM 53-02, FIG 18 51-10-4 AND 51-10-3 PAR 21/14.

Part: BEAM — CORRODED (BS 1155-1212) · airframe 61,961 hrs · 46,413 cycles

CORROSION ON LOWER DOOR FRAME BEAM BETWEEN BS 1155 TO 1166 AND BS 1201 TO 1212 AFT CARGO BAY. DUE TO EXCESSIVE CORROSION BEAM WAS REPAIRED, REPAIR PARTS WERE ADJUSTED, DRILLED, FABRICATED, TREATED, PAINTED, AND INSTALLED IAW SRM 53-05, FIG 123A, 51-10-3 PAR 21 AND 14. FOUND OUT OF LIMITS IAW SRM 53-05, FIG 123A.

Part: BULKHEAD — DAMAGED (BS 1338) · airframe 61,961 hrs · 46,413 cycles

STEP ON SPLICE REPAIR AT TEE CAP OF PRESSURE DOME, BS 1338 BETWEEN PROJECTION LONGS 26-27L AFT CARGO BAY. SHIMS WERE FABRICATED, TREATED, PAINTED, INSTALLED IAW SRM 53-03D, FIG 37A,.

Part: SEAT TRACK — CORRODED (BS 701-937) · corrosion level 2 · airframe 61,961 hrs · 46,413 cycles

CORRROSION ON SEAT TRACK RBL 54 BS 701-937. REPAIRED IAW SRM 53-05, FIG. 4A.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 61,961 hrs · 46,413 cycles

CORROSION NOTED ON HORIZONTAL STABILIZER RT UPPER SKIN. HOLES WERE REWORKED AND BUSHINGS FABRICATED AND INSTALLED IAW SRM 55-03D PAR 30 AND SRM 51-10-3, PAR 21-14.

Part: BUSHING — CORRODED (LT OVERWING) · corrosion level 2 · airframe 61,961 hrs · 46,413 cycles

CORROSION ON BUSHINGS BELOW OF LT OVERWING HEATER BLANKET AFT SIDE AT 10 LOCATIONS. BUSHINGS WERE R & R IAW SRM 51-30-10 AND EA 09-070683AD, REV L.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 61,961 hrs · 46,413 cycles

CORROSION NOTED ON HORIZONTAL STABILIZER LT UPPER SKIN. CORROSION WAS REMOVED, BUSHINGS FABRICATED AND INSTALLED IAW SRM 55-03D, PAR 30 AND SRM 51-10-3, PAR 21, 14.

Part: CUSP WEB — CORRODED (BS 581-585) · corrosion level 2 · airframe 61,961 hrs · 46,413 cycles

CORROSION ON RT CUSP WEB BS 581-585 LBL 54-60. REPAIRED IAW 53-05, FIG 131A-3, 51-10-3, FIG 14 -21, 51-30-2, 51-30-5, 51-10-3 FIG 38.

Part: FRAME — CORRODED (BS 1380) · corrosion level 2 · airframe 61,961 hrs · 46,413 cycles

CORROSION ON AFT ACCESSORY BSY FRAME BS 1380 LOWER TEE BETWEEN BL 0 TO LBL 18. FRAME REPLACED IAW 51-30-2, 51-30-5 AND DWG 9912246.

Part: FRAME — CORRODED (BS 1271) · corrosion level 2 · airframe 61,961 hrs · 46,413 cycles

CORROSION FOUND ON FRAME BS 1271 L28L-28R. FRAME WAS REPLACED DUE TO BEING OUT OF LIMITS. REPAIRED IAW SRM 53-03, FIG 2A.

Part: SEAT TRACK — CORRODED (BS 670-829) · corrosion level 2 · airframe 61,961 hrs · 46,413 cycles

CORROSION LT SEAT TRACK RBL 22 BS 670-898. SEAT TRACK REPAIRED IAW SRM 53-05, FIG 4A, 51-10-3, PAR 14,21,38 & 51-20-0.

Part: LONGERON — CORRODED (BS 1250-1259) · corrosion level 2 · airframe 61,961 hrs · 46,413 cycles

DURING CHECK, CORROSION FOUND ON LONGERON 23LT BETWEEN BS 1250 TO 1259 AFT CARGO BAY. REPLACED LONGERON IAW SRM 51-30-2.

Part: LONGERON — CORRODED (BS 1193-1212) · corrosion level 2 · airframe 61,961 hrs · 46,413 cycles

DURING CHECK, CORROSION FOUND ON LONGERON 29L, REPAIR SPLICE BETWEEN BS 1193 TO 1212 AFT CARGO BAY. REPLACED LONGERON SECTION IAW SRM 51-10-3 & -4.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,961 hrs · 46,413 cycles

DURING CHECK, CORROSION ON AFT LAVATORY SERVICE PANEL. FOUND OUT OF LIMITS. REPLACED LAVATORY SERVICE PANEL IAW SRM 53 & 51.

Part: CUSP WEB — CORRODED (BS 896-897) · corrosion level 2 · airframe 61,961 hrs · 46,413 cycles

DURING CHECK, CORROSION FOUND ON RT CUSP WEB LBL 54 - 60 BETWEEN BS 896 - 897. REPAIRED IAW SRM 53-05, FIG 131A-4, 51-30-2, 51-10-3 PAR. 14, 21, 38 AND PS-900-5-1 NR 4.

Part: CUSP WEB — CORRODED (BS 765) · corrosion level 2 · airframe 61,961 hrs · 46,413 cycles

DURING CHECK, CORROSION FOUND ON RT CUSP WEB X=-54 TO X=-60 AT BS 765. REPAIRED IAW SRM 53-05 FIG 131A-9.

Part: LONGERON — CRACKED (BS 845) · airframe 61,961 hrs · 46,413 cycles

CRACKED LONGERON 1 BS 845. LONGERON WAS TRIMED OUT AND NEW SECTION OF LONGERON WAS DRILLED ADJUSTED AND REPAIR SPLICES WERE FABRICATED, REPAIR PARTS WERE TREATED PAINTED AND INSTALLED IAW SRM 53-02, FIG 18 AND AMR 09531284, REV 1 AND ER/A 519135-14 REV, ORIG.

Part: SKIN — DAMAGED (RUDDER) · airframe 61,961 hrs · 46,413 cycles

DAMAGE METALLIZED COAT ON LT & RT RUDDER SURFACE. RUDDER REPAIRED IAW SRM 51-70-1A PARAGRAPH 23A, FIGURES 58 AND 59.

Part: INTERCOSTAL — CORRODED (BS 1309-1322) · corrosion level 2 · airframe 61,961 hrs · 46,413 cycles

CORROSION ON INTERCOSTAL BS 1309 - 1322 AND L27-28L . CORROSION REMOVED IAW SRM 51-10-3 PAR 26. FOUND OUT OF LIMITS IAW SRM 53-01 FIG 1. INTERCOSTAL REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: LONGERON — CRACKED (BS 1380) · airframe 61,961 hrs · 46,413 cycles

CRACKED LONGERON 14L BS 1380. DAMAGE REMOVED, REPAIR INSTALLED IAW SRM 53-02 FIG. 18, 51-30-5, 51-10-4, 51-10-3 PAR 14 AND 21.

Part: LONGERON — CRACKED (BS 1380) · airframe 61,961 hrs · 46,413 cycles

CRACKED LONGERON 11L BS 1380. DAMAGE REMOVED, NEW SECTION OF LONGERON AND NEW UNION SPLICE ADJUSTED, DRILLED, TREATED, PAINTED, INSTALLED, IAW SRM 53-02 FIG 18, 51-30-2, 51-30-5, 51-10-4, 51-10-3 PAR 21-14 AND PS 900-5-4 NR 4.

Part: INTERCOSTAL — CRACKED (BS 1271-1287) · airframe 61,961 hrs · 46,413 cycles

CRACK ON INTERCOSTAL BS 1271 - 1287 AND X=-22 TO X=22. INTERCOSTAL STOP DRILLED AND REPAIR DOUBLER INSTALLED IAW ER/A 380524-14 MA.

Part: LONGERON — CRACKED (BS 160) · airframe 61,961 hrs · 46,413 cycles

LONGERON 3L BS 160 CRACKED. LONGERON REMOVED, NEW SECTION LONGERON AND SPLICE DRILLED IAW SRM 53-02 FIG 18 AND 51-10-2. NEW LONGERON AND SPLICE TREATED AND PAINTED IAW SRM 51-10-3 PAR 14, 21. INSTALLED IAW SRM 53-02 FIG. 18 AND PS 900-5-1 NO.04.

Part: CUSP WEB — CORRODED (CABIN) · corrosion level 2 · airframe 61,961 hrs · 46,413 cycles

CORROSION ON RT CUSP WEB FROM X=-54 TO X=-60 Y=1015 TO 1016. CORROSION REMOVED, REPAIR PARTS FABRICATED, AND INSTALLED IAW SRM 51-10-3 PART 14, 21, 38, SRM 51-30-2, 53-05 FIG 131A-1, PS-900-5-1.

Part: SKIN — CORRODED (BS 780) · corrosion level 2 · airframe 61,961 hrs · 46,413 cycles

DURING SCHEDULED CHECK, CORROSION FOUND ON FUSELAGE SKIN BS 780 BETWEEN L28 - 29R. REPAIRED IAW SRM 53-04D, FIG. 57, 51-30-5.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,897 hrs · 46,378 cycles

DURING LINE CHECK, OVERHEAD EMERGENCY EXIT LIGHTS BETWEEN ROWS 27 & 31 WERE INOPERATIVE. REPLACED POWER SUPPLY IAW AMM 33-53 AND OPS CHECKED OK.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LGHT) · airframe 61,897 hrs · 46,378 cycles

DURING LINE CHECK, SEAT MOUNTED EMERGENCY ESCAPE LIGHT AT SEAT 4R WAS INOPERATIVE. REPLACED SEAT HARNESS IAW AMM 33-53 AND OPS CHECKED OK.

Part: WIRE — SHORTED (EMERGENCY LIGHTS) · airframe 59,765 hrs · 44,799 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT ROWS 27-31 WERE INOPERATIVE. MX FOUND A WIRE SHORTED AND REPOSITIONED IT ALONG WITH REPLACING THE BATTERIES. THE SYS RETURNED TO NORMAL.

Part: FRAME — CRACKED (BS 1485) · airframe 59,765 hrs · 44,799 cycles

FUSELAGE FRAME CRACKED BS 1485. REPAIRED CRACKED FUSELAGE FRAME IAW SRM 53-03D, FIG 47.

Part: FRAME — CRACKED (BS 864) · airframe 59,765 hrs · 44,799 cycles

LEFT OVERWING FRAME AT BS 864, CRACKED, HFEC VERIFIED. BLENDED FRAME TO LIMITS IAW AMDS CARD 5310-01415-0201. REMOVED FRAME DRILLED NEW FRAME, INSTALLED IAW AMDS 5310-01415-301 POS 11.

Part: UNKNOWN — ODOR (CABIN) · airframe 59,535 hrs · 44,644 cycles

SHORTLY AFTER TAKEOFF, THE F/A REPORTED AN ELECTRICAL ODOR WITH NO VISIBLE SMOKE. FLIGHT CREW SECURED POWER TO THE GALLEY IN COMPLIANCE WITH THE QRH. ODOR SUBSIDED WITH GALLEY POWER OFF, UNTIL LANDING WHEN IT OCCURRED AGAIN. MX INSPECTED THE GALLEY, COFFEEMAKERS, OVEN, APPLIANCE CONTROL PANELS, AND BEHIND CEILING PANELS. NO PROBLEM WAS FOUND AND NO OBVIOUS SOURCE OF ODOR WAS IDENTIFIED. A DUCT BURNOUT PROCEDURE WAS COMPLIED WITH AND THE ACFT HAS RETURNED TO SERVICE.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 59,754 hrs · 44,790 cycles

VERTICAL STABILIZER FRONT SPAR, RT CHORD ZFS=52 / CRACKED.

Part: LIGHT — INOPERATIVE (ROW 20) · airframe 59,137 hrs · 44,357 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 20 IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF THE SYSTEM.

Part: SKATE ANGLE — LOOSE (FUSELAGE) · airframe 56,218 hrs · 42,417 cycles

TWO SMOKING WORKING FASTENERS IN LEFT SKATE ANGLE, STA CANT 1474. REPAIRED PER ERA 494213-14.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 56,218 hrs · 42,417 cycles

DURING PSV IN MSP CRACKS WERE FOUND ON THE 5912141-85 FUSELAGE TO VERT STABILIZER ATTACH ANGLE NEAR STATION 1465. THE 5912141-85 ANGLE IS MADE FROM 0.080 IN THICK A286 CRES. REPAIRING PER ERA 494213-14, WORK IN CURRENTLY IN PROGRESS.

Part: SILL — CORRODED (BS 636-693) · airframe 59,776 hrs · 44,809 cycles

SRM D/R 53-05, FIG 123, CORROSION AT FS 636-693 DOOR SILL, STRINGER R28 AT NUT PLATES FOR SCUFF PLATE. REPAIR SRM 53-05, FIG 123, REPAIR 3202, NO INSPECTION REQUIRED, NO INSPECTION NEEDED.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 56,218 hrs · 42,417 cycles

DURING PSV IN MSP, CRACKS WERE FOUND ON THE 5912141-86 FUSELAGE TO VERT STAB ATTACH ANGLE NEAR STATION 1465. THE 5912141-86 ANGLE IS MADE FROM 0.080 IN THICK A286 CRES. REPAIRING PER ERA494212-14, WIP IN PROGRESS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,788 hrs · 40,733 cycles

THE EMERGENCY FLOOR LIGHT AT SEAT 3C WAS FOUND TO BE INOPERATIVE. MX REPLACED THE EMERGENCY LIGHT ASSY AT SEAT 3C. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.

Part: WINDOW FRAME — DAMAGED (FS 522-541) · airframe 53,134 hrs · 40,272 cycles

DURING ACCOMPLISHMENT OF PERM REPAIR TO LIGHTNING STRIKE DAMAGE AT STA 292 FOUND ADDITIONAL LIGHTNING DAMAGE TO WINDOW BELTS BTWN 522-544 AND 541-560

Part: WIRE HARNESS — FAULTY (CABIN) · airframe 53,086 hrs · 40,237 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT 15DE TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE LIGHT ASSEMBLY HARNESS. AN OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — UNSECURE (EMERGENCY LIGHTS) · airframe 52,531 hrs · 39,877 cycles

EMERGENCY EXIT ROW LIGHTS AT ROW 10 AND 20 INOP. SECURE CONTACT. OPS CK NML.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 52,508 hrs · 39,862 cycles

THE FIRST FASTENER HOLE BELOW ZFS-52 ON THE RT CHORD OF VERTICAL STABILIZER FRONT SPAR WAS FOUND WITH A CRACK INDICATION. THE INSP IS BEING ACCOMPLISHED IAW EO 09-470871-12. REPAIRED IAW ER/A 479449-14 REV ORIG.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 52,376 hrs · 39,782 cycles

PASSENGER SEAT 27D EMERGENCY LIGHTING FLOOR LIGHTS INOP/ DAMAGED RESET CONNECTOR. OPS GOOD.

Part: BULB — BURNED OUT (MLG INDICATOR) · airframe 50,117 hrs · 38,298 cycles

ON GEAR HANDLE DOWN LT MG AND NOSE GEAR WERE GREEN RT MG DID NOT ILLUMINATE PRESSED ON W/O SUCCESS ELECTED TO GO AROUND. TOWER VISUALLY CONF ALL GEAR DOWN, ATTEMPTED TO RELAMP LMG AND NLG LTS WITH RMG W/O SUCCESS, F/O VISUALLY CONFIRMED MLG WITH PERISCOPE IAW QRH. DECLARED EMERGENCY GEAR PINS INSTALLED AFTER LANDING. VERIFIED ALL BULBS BURNED OUT RT MG POSITION LIGHT. RELAMPED WITH SAME TEST OK ON GEAR POSITION LIGHT TEST. PER AMM 32-60-03-201. PERFORMED PSEU BITE AND SENSOR TEST OF RT MG DOWN AND LOCKED SENSOR. ALL PASS/NO FAULT/GEARPINS REMOVED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,431 hrs · 36,600 cycles

EXFOLIATION CORROSION ON PAX CABIN FLOORBEAM FOR GIRT BAR AT R1 LOWER DOOR JAMB. NEW FLOOR SUPPORT INSTALLED IAW SRM 51-30-1.

Part: CUSP WEB — CORRODED (PAX CABIN) · airframe 47,431 hrs · 36,600 cycles

EXFOLIATION CORROSION ON RT CUSP WEB AT PAX CABIN STA Y=507 TO 508. REPAIRED CUSP WEB IAW ERA 398191-14MA REV A.

Part: CUSP WEB — CORRODED (BS 897) · airframe 47,431 hrs · 36,600 cycles

EXFOLIATION CORROSION ON LT CABIN CUSP WEB AT STA Y=897. REPAIRED IAW ERA 398191-14MA REV A.

Part: CUSP WEB — DENTED (BS 766) · airframe 47,431 hrs · 36,600 cycles

FOUND DENT ON LT CABIN CUSP WEB AT STA Y=766.5. REPAIRED IAW ERA 398191-14MA REV A.

Part: CUSP WEB — CORRODED (BS 737) · airframe 47,431 hrs · 36,600 cycles

EXFOLIATION CORROSION ON LT CABIN CUSP WEB Y=737. REPAIRED CUSP WEB IAW ERA 398191-14 MA REV A.

Part: CUSP WEB — CORRODED (BS 598-712) · airframe 47,431 hrs · 36,600 cycles

EXFOLIATION CORROSION ON RT CUSP WEB AT PAX CABIN AT STA Y=598 TO 712, NEW CUSP WEB WAS INSTALLED IAW DOUGLAS DWG 9930538.

Part: FLOORBEAM — CRACKED (BS 965) · airframe 47,431 hrs · 36,600 cycles

CRACKED FLOORBEAM ON PAX CABIN AT STA Y=965 AND X=0. NEW FLOOR SUPPORT INSTALLED IAW DOUGLAS DRW 5930544.

Part: CHANNEL — DEFORMED (HORIZONTAL STAB) · airframe 47,431 hrs · 36,600 cycles

DEFORMED "C" CHANNEL ON RT HORIZONTAL STABILIZER REAR SPAR AT STA XHS=207. INSTALLED NEW "C" CHANNEL IAW SRM 51-30-2, SRM 51-30-5 AND DOUGLAS DWG 9918401.

Part: CUSP WEB — CORRODED (BS 566) · airframe 47,431 hrs · 36,600 cycles

EXFOLIATION CORROSION ON LT CABIN CUSP WEB AT STA Y=566. REPAIRED CUSP WEB IAW ERA 398191-14MA REV A.

Part: FLOORBEAM — CRACKED (BS 984) · airframe 47,431 hrs · 36,600 cycles

CRACKED FLOORBEAM AT PAX CABIN BTW STA Y=984 X=0,11. NEW FLOOR SUPPORT INSTALLED IAW SRM 51-30-5.

Part: FLOOR SUPPORT — CORRODED (BS 150-200) · airframe 47,431 hrs · 36,600 cycles

EXFOLIATION CORROSION ON PAX CABIN FLOOR SUPPORT BTW STA Y=150 AND 200 RBL 7. NEW FLOOR SUPPORT INSTALLED IAW SRM 51-30-1.

Part: CUSP WEB — CORRODED (BS 817) · airframe 47,431 hrs · 36,600 cycles

EXFOLIATION CORROSION ON RT CUSP WEB AT PAX CABIN STA Y=817. REPAIRED CUSP WEB IAW ERA 398191-14MA REV A.

Part: SEAT TRACK — CORRODED (BS 1141-1168) · airframe 47,431 hrs · 36,600 cycles

EXFOLIATION CORROSION ON LT GENERATION FLOOR SUPPORT AT STA 1141, 1168. INSTALLED NEW SECTION OF TRACK IAW SRM 53-05D FIG 4F.

Part: SEAT TRACK — CORRODED (BS 896) · airframe 47,431 hrs · 36,600 cycles

GENERAL SURFACE CORROSION ON RT SEAT TRACK X=54 AT STA 896. REPAIRED IAW SRM 53-05D FIG 4A.

Part: ISOLATOR — CORRODED (LT ENGINE) · airframe 47,431 hrs · 36,600 cycles

RUST ON AFT VIBRATION ISOLATOR AT LT ENGINE. VIBRATION ISOLATOR REPLACED AND WILL BE INSTALLED WITH OPN 7151 RC 805.

Part: CUSP WEB — CORRODED (PAX CABIN) · airframe 47,431 hrs · 36,600 cycles

EXFOLIATION CORROSION ON LT CABIN WEB AT STA Y=546. REPAIRED CUSP WEB IAW ERA 398191-14MA REV A.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,761 hrs · 34,810 cycles

EMERGENCY TRACK LIGHTING INOP AFT OF ROW 30. REMOVED AND REPLACED BATTERY PACK ASSY OPS CHECK NORMAL

Part: CHARGER — FAILED (EMERGENCY LIGHT) · airframe 44,451 hrs · 34,586 cycles

EMERGENCY LIGHTS FROM SEAT 31 AFT INOP. REPLACED BATTERY PACK NO HELP. REPLACED CHARGER AND BATTERY PACK LIGHTS, OPS CK GOOD.

Part: GEARBOX — LEAKING (APU) · airframe 42,838 hrs · 33,468 cycles

F/A REPORTED SMOKE IN CAPT'S SIDE AFT LAV CLIMBING THRU 9000 FT. F/A DISCHARGED HALON FIRE EXT IN LAV. A/C RETURNED TO GATE, ON ARRIVAL FOUND APU GEARBOX OIL LEAK AT FITTING FOR CHIP DETECTOR. OIL CONTAMINATED APU AIR INLET. REPAIRED SAME.

Part: FLUID — DETECTED (APU BAY) · airframe 40,521 hrs · 31,835 cycles

AFTER TAKEOFF FLIGHT ATTENDANTS REPORTED SMOKE/FUMES AFT CABIN. FOUND FLUID IN APU COMP. CLEANED SAME, PERFORMED DUCT BURNOUT.

Part: CABLE — UNSERVICEABLE (TAILCONE) · airframe 38,185 hrs · 30,172 cycles

WORKING MSU TO VERIFY TAILCONE RELEASE SYSTEM LOCKING CABLE FOUND ONE CABLE BROKEN REF IPC 53-50-00-25A REPLACED CABLE

Part: ODOR — DETECTED (CABIN) · airframe 35,395 hrs · 28,260 cycles

STRONG BURNING RUBBER ODOR IN CABIN AFTER T/O AND LANDING. PERFORMED DUCT BURNOUT, NO ODOR NOTED

Part: SEAL — WORN (APU OIL CAP) · airframe 34,161 hrs · 27,380 cycles

AFTER TAKEOFF EXPERIENCED A ODOR CONSISTANT WITH A WARM DUCT THE AFT LAV SMOKE DETECTORS SOUNDED AND F/A'S REPORT A SLIGHT HAZE IN CABIN. AT FL 9000 FT. ODOR CEASED AND SMOKE DETECTORS STOPPED. FOUND APU OIL CAP SEAL DETERIORATED. REPLACED OIL CAP CLEANED AREA AND PERFORMED DUCT BURN OUT PER AMM

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 33,087 hrs · 26,637 cycles

99525-71, -76 FLOOR PANELS WERE FOUND DISBONDED AND CRACKED. REPAIR PER ER/A 417223-14.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,087 hrs · 26,637 cycles

THE AFT C1 DOOR JAMB SKIN AND DOUBLER WERE FOUND CRACKED AT FS 427, L23R. DAMAGE WAS CUT OUT AND REPAIRED PER ERA 413035-14.

Part: BEAM — CORRODED (FUSELAGE) · airframe 29,679 hrs · 24,080 cycles

FUSELAGE / C2 DOOR OPENING / LOWER SILL BEAM : BEAM REPLACEMENT. THE LOWER SILL BEAM OF THE C2 DOOR CUTOUT WAS FOUND CORRODED AND HAD NUMEROUS MISDRILLED AND DAMAGED HOLES FROM A PREVIOUS REPAIR AND SCUFF PLATE INSTALLATION. THE DAMAGED BEAM WAS REMOVED AND A NEW BEAM INSTALLED PER B/P. THE REPAIR IS DOCUMENTED PER ER/A 379537-14.

Part: SEAL — BROKEN (FIRE EXTINGUISH) · airframe 28,984 hrs · 23,568 cycles

FIRST CLASS WATER FIRE EXTINGUISHER SEAL FAILED. REPLACED FIRST CLASS WATER FIRE EXTINGUISHER.

Part: ENGINE — MALFUNCTIONED (NR 1)

NR 1 ENGINE FAILED TO ACHIEVE FULL THRUST (ONLY 90 PERCENT AND 1.90 EPR). REPLACED ENGINE FOR CRACKED FUEL MANIFOLD.

Part: BATTERY — DISCHARGED (CABIN)

FLASHLIGHT AFT OF FLIGHT ATTENDANT, FWD LIGHT RED LIGHT DOES NOT BLINK. REPLACED BATTERY PER M/M. OPS CHECKS GOOD.

Part: BLKHD TEE CAP — DAMAGED (BS 1338)

THE LOWER TEE CAP SECTION OF THE AFT PRESSURE BULKHEAD AT FS 1338 WAS FOUND DAMAGED AND REQUIRED REPLACEMENT. THE DAMAGED TEE CAP WAS REMOVED AND REPLACED PER DL ERA 273379-14.

Part: FRAME — DAMAGED (BS 1382)

THE LOWER LOBE OF THE FS 1382 FRAME WAS DAMAGED FROM A TAIL STRIKE BETWEEN L-21L AND L-24L. ALSO, BETWEEN L-18R AND L-21R. THE DAMAGE WAS REPLACED WITH FABRICATED PARTS PER DL ERA 273498-14.

Part: SKIN — DENTED (FS 1315-1338)

FUSELAGE SKIN BETWEEN FS 1315 AND FS 1338 AND BETWEEN STR 25L AND STR 25R WAS FOUND DAMAGED AFTER THE A/C EXPERIENCED A TAIL STRIKE. ACCOMPLISHED REPAIRS PER DL ERA 273253-14 REV A.

Part: BLKHD WEB — DAMAGED (BS 1338)

THE P-DOME LOWER WEB AT STA 1338 WAS DAMAGED DURING A TAIL STRIKE INCIDENT. THE DAMAGE IN THE LOWER WEB WAS SPLICED PER DL ERA 273378-14.

Part: POWER SUPPLY — INOPERATIVE (AFT CABIN)

ON PREFLIGHT, AFT CABIN EMERGENCY FLOOR TRACK LIGHTS INOP. REPLACED POWER SUPPLY AND OPERATION NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

ON THRU SVC CK, FOUND AFT SECTION ROW 29 AND AFT EMERGENCY PATH LIGHTS INOP. C/A REPLACED BATTERY PACK, NO HELP. REPLACED FUSES. OPS NORMAL.

Part: RIB — CRACKED (KEEL BEAM)

FOUND DURING F-1 LETTER CHECK, KEEL BEAM CROSS OVER RIB CRACKED AFT OF LT GEAR DOOR. REPAIRED PER SRM 53-05 FIG 101.