N902DE

Part: LIGHT — DAMAGED (AFT STAIRS) · airframe 71,314 hrs · 52,836 cycles

AFT STAIRS EMERGENCY LIGHT DAMAGED. REMOVED AND REPLACED AFT STAIRS EMERGENCY LIGHT PER 33-53. OP CHECK GOOD. (LP6160772)

Part: DOOR FRAME — CRACKED (LT MLG) · airframe 71,287 hrs · 52,811 cycles

FOUND CRACK LH MAIN WHEELWELL DOOR FRAME. REMOVED FRAME P/N 5930584U123 (399486). DRILLED FRAME, INSTALLED FRAME - REF BOEING DRAWING 5930584. (LP6160752)

Part: LENS — MISSING (LT WING) · airframe 71,183 hrs · 52,696 cycles

LEFT WING AFT POSITION LIGHT LENS COVER MISSING. INSTALLED LENS COVER ASSY PER MD 88 AMM 33-43. OK FOR SVC. (LP5992756)

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 71,092 hrs · 52,621 cycles

LAVATORY SMOKE DETECTOR WILL NOT TURN OFF. LOCATIONS 201. R/R LAV SMOKE DETECTOR PER AMM 26-17, OPS CHECK GOOD. (LP1277573)

Part: BATTERY — DISCHARGED (CABIN) · airframe 70,993 hrs · 52,527 cycles

INTERIOR EMERGENCY EXIT OVERWING LIGHTS INOP. R/R BATTERIES IN BATTERY PACK PER AMM 33-53. NOW OPS NML. (LP6121960)

Part: CONTROLLER — MALFUNCTIONED (WINDOW HEAT) · airframe 70,732 hrs · 52,300 cycles

CENTER WINDSHIELD ARCING DURING FLIGHT PERFORMED QRH PROCEDURE. CB X25 PULLED. R/R CENTER WINDSHIELD AND WINDOW HEAT CONTROLLER RE AMM 56-10/30-41. (LP5452398)

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,767 hrs · 51,453 cycles

PEANUT BULBS ON AFT OVERHEAD NEED TO BE RELAMPED. R/R BATTERY POWER SUPPLY B5-23 PER WDM 33-51. NO HELP. REPLACED BATTERIES ON EMERGENCY BATTERY PACK B5-23 PER AMM 33-53 OPS CKS GOOD PEANUT LIGHTS OPS GOOD. (LP5845048)

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 69,076 hrs · 50,878 cycles

FOUND CRACK IN RIGHT HYDRAULIC SERVICING HAND PUMP SUPPORT BRACKET. REPLACED CRACKED INTERCOSTAL PER DRAWING 5930584. (LP4756337)

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 69,075 hrs · 50,877 cycles

SEAT 3CD EMERGENCY LIGHTS INOP. REPAIRED WIRE HARNESS AS REQUIRED, REF. SWPM 20-93. CHECKS GOOD. (LP4756331)

Part: WIRE — DAMAGED (CABIN) · airframe 68,482 hrs · 50,364 cycles

MIDDLE FLOOR-LEVEL EMERGENCY LIGHT IN TAIL COMPARTMENT INOP. INSPECTED AND FOUND BAD SPLICE. REPAIRED WIRE AS REQ PER SWPM CH 20. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,291 hrs · 50,196 cycles

SEAT ROW 21 EMERGENCY LIGHT INOP. RELAMPED SEAT 21 EMER BULBS PER AMM 33-53-01. CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,269 hrs · 50,175 cycles

SEAT ROW 16 EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY PER AMM 33-50.

Part: LIGHT — INOPERATIVE (TAILCONE) · airframe 68,269 hrs · 50,175 cycles

EMERGENCY LIGHT IN TAIL CONE AREA INOP. RELAMPED PER 33-50. CKS OK.

Part: RIB — CRACKED (RT WING) · airframe 67,947 hrs · 49,912 cycles

RIB CRACKED ON RT WING AT IWS 63.540. REMOVED COMPLETED RIB REPAIR IAW SRM 57-02 FIG 6.

Part: SKIN — CRACKED (RT WING) · airframe 67,947 hrs · 49,912 cycles

SKIN CRACK ON RT WING AT STA XFS 63.540. REMOVED EXISTING FASTENERS AND STOP DRILLED AT EACH END OF CRACK PER MD88 SRM 57-06B FIG 33 (SHEET 2) NDT INSP OF STOP DRILLED CRACK ENDS PER SRM 57-06B 27D (1)(B) NO CRACKING BEYOND STOP DRILLED HOLES INDICTED. FABRICATED REPAIR DOUBLER FROM .063 7075-0 DOUBLER HEAT TREATED ON SHOP ORDER OF8385 INSTALLED DOUBLER PER SRM 57-06B.

Part: PIN — DISENGAGED (L1 DOOR SLIDE) · airframe 66,408 hrs · 48,656 cycles

L1 DOOR SLIDE PINS FOUND DISENGAGED. REMOVED AND REPLACED THE DOOR SLIDE IAW JIC 2561-4964. OPS CHECKED GOOD.

Part: FIRE WARNING — ILLUMINATED (RT ENGINE) · airframe 65,634 hrs · 48,024 cycles

DUE TO FIRE WARNING FOR THE NUMBER TWO ENGINE ON LOG SHEET 9493992, THE RIGHT ENGINE FIRE BOTTLE WAS DISCHARGED. MAINTENANCE REPLACED THE RIGHT ENGINE FIRE BOTTLE.

Part: DUCT — BLOWN (NR 2 ENGINE) · airframe 65,634 hrs · 48,024 cycles

PERFORMED AN IFSD AND AN ATB, DUE TO A REPORTED FIRE WARNING ON THE NR 2 ENGINE. AFTER REDUCING THE THROTTLES, THE WARNING EXTINGUISHED. VIBRATIONS WERE REPORTED IN THE AFT CABIN. IAW QRH, THE NR 2 ENGINE WAS SHUTDOWN. THE NR 2 ENGINE FIRE BOTTLE WAS DISCHARGED. MAINTENANCE FOUND THE NR 2 ENGINE 13TH STAGE DUCT BLOWN WITH DAMAGE TO THE 8TH STAGE DUCT, THE FIREWALL, AND A WIRING HARNESS. THE EGT IAW THE FLIGHT DATA RECORDER HAD REACHED 679 DEG. MAINTENANCE REPLACED BOTH NR 1 AND THE NR 2 ENGINES. THE FIRE BOTTLE WAS REPLACED.

Part: O-RING — FAILED (NLG STRUT) · airframe 65,591 hrs · 47,992 cycles

AFTER TAKE-OFF, THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH ASSOCIATED AIR NOISE FROM THE NOSE GEAR AREA. THE GEAR HANDLE WAS SELECTED DOWN AND 3 GREEN LIGHTS WERE OBSERVED. MAINTENANCE FOUND THE NOSE GEAR STRUT FLAT WITH THE SCHRADER VALVE PACKING PROTRUDING FROM THE FITTING. THE SCHRADER SERVICING VALVE O-RING WAS REPLACED, THE STRUT WAS SERVICED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (LP9493960)

Part: CABLE — FRAYED (TAILCONE RELEASE) · airframe 65,413 hrs · 47,837 cycles

RT TAILCONE RELEASE CABLE HAD BROKEN STRANDS, LT CABLE CLAMP WORN. REPLACED THE LEFT CABLE CLAMP. REPLACED THE RT RELEASE CABLE IAW 5350-01077-0101.

Part: LANYARD — MISSING (R1 DOOR) · airframe 65,022 hrs · 47,533 cycles

DOOR 1R GIRT BAR LANYARD MISSING P/N 3961899-501 REMOVED AND PINNED SLIDE. REINSTALLED 1R SLIDE AND LANYARD IAW AMDS W/C 2561-4964. SAFETY PIN REMOVED AND STOWED.

Part: SLIDE — DAMAGED (L1 DOOR) · airframe 64,683 hrs · 47,285 cycles

L1 DOOR SLIDE ENGAGEMENT PINS ARE OUT. REPLACED L1 DOOR SLIDE IAW AMDS WORK CARD 2561-4964.

Part: CABLE — DAMAGED (TAILCONE RELEASE) · airframe 64,410 hrs · 47,114 cycles

BROKEN WIRE OF TAIL CONE RELEASE CONTROL CABLE AT BS 1510. TAIL CONE RELEASE CONTROL CABLE WAS REPLACED PER MD-88 AMM 20-10-17 AND ADJUSTED PER MD-88 AMM 53-53-00-501.

Part: INTERCOSTAL — CRACKED (ENTRY DOOR) · airframe 64,410 hrs · 47,114 cycles

CRACKED INTERCOSTAL BTW BEAM 4 AND BEAM 5 CENTER SECTION AT MAIN ENTRANCE DOOR. INTERCOSTAL BTW BEAM 4 AND BEAM 5 CENTER SECTION AT MAIN ENTRANCE DOOR (L1) WAS REPLACED PER SRM 51-30-1,51-30-2 AND 51-30-5 DWG 9955763 REV K.

Part: PAN — CRACKED (CARGO DOOR) · airframe 64,410 hrs · 47,114 cycles

CRACK ON MID CARGO DOOR PAN BS 636 BETWEEN BEAM NR 2 AND LOWER EDGE. THE PAN WAS REPAIRED IAW ERA 551720-14 REV ORIGINAL AND ETI-88-16-424 REV 5.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 64,410 hrs · 47,114 cycles

DELAMINATED UPPER SKIN XV2= 257 ON LT WING OUTBOARD FLAP CENTER VANE. THE FLAP VANE WAS REPAIRED IAW SRM 57-03D PAR.11.

Part: CHANNEL — DAMAGED (LAVATORY) · corrosion level 2 · airframe 64,410 hrs · 47,114 cycles

CORROSION AND WEAR ON METALLIC CHANNEL AT RT & LT AFT LAVATORY FLOOR PAN 1307A AND 1307C W2. THE CHANNELS WERE REPLACED IAW SRM 51-10-4 / 51-10-3 PAR. 21, 14 / 51-30-2 / 51-30-5 AND DRAWING 9915530 REV. DA.

Part: FRAME — CRACKED (BS 1510) · airframe 64,410 hrs · 47,114 cycles

CRACKED FRAME BS 1510. THE FRAME WAS REPLACED IAW SRM 51-30-2.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 64,410 hrs · 47,114 cycles

CORROSION ON RT LOWER ACCESS PANEL CUT OUT WING LWR SKIN BETWEEN XRS =189.0 TO 214.0 . REPAIRED IAW ERA NO.551715-14AD REV. ORIGINAL AND ETI-88-16-419 REV. 2.

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 64,410 hrs · 47,114 cycles

DELAMINATED UPPER SKIN APPROX XV2= 257 AT LT WING OUTBOARD FLAP CENTER VANE. THE FLAP VANE WAS REPAIRED IAW SRM 57-03D PAR. 1.

Part: CARGO TRACK — CORRODED (BS 1007-1322) · corrosion level 2 · airframe 64,410 hrs · 47,114 cycles

CORROSION ON THE RT CARGO TRACK, BS 1007 - 1155 AND 1212 - 1322. THE CARGO TRACK WAS REPLACED IAW SRM 51-10-3 AND 51-30-1.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 64,410 hrs · 47,114 cycles

WEAR ON FWD/AFT LOWER CORNER DOUBLERS AT MID CARGO DOOR. AFT PRODUCTION DOUBLER ON LOWER CORNER WAS REPLACED PER SRM 51-30-2. FWD PRODUCTION DOUBLER ON LOWER CORNER WAS REPLACED PER SRM 51-30-2 AND 51-30-5.

Part: STRINGER — CRACKED (FUEL CELL) · airframe 64,410 hrs · 47,114 cycles

A ONE INCH CRACK ON STRINGER 16L AT XCW=12.00 INSIDE CENTER FUEL TANK. THE STRINGER WAS REPAIRED IAW ETI-88-16-398 REV 2 /ER/A 551689-14 REV A, ETI-8816-403 REV 1, ER/A 551693-14 REV ORIGINAL.

Part: FLOOR SUPPORT — CRACKED (BS 826-830) · airframe 64,410 hrs · 47,114 cycles

CRACKED ANGLE BETWEEN BS 826 - 830, LBL 44. THE ANGLE WAS REPAIRED IAW ETI-88-16-431 REV 3 AND ER/A 551735-14 REV ORIGINAL.

Part: DOUBLER — CRACKED (BS 1463) · airframe 64,410 hrs · 47,114 cycles

CRACKED INTERNAL PRODUCTION DOUBLER BS 1463, LONGERON 22L . THE DOUBLER WAS REPAIRED PER ETI-88-16-416 REV. 2 AND ER/A 551711-14 REV. ORG.

Part: BEARING — CORRODED (RT MLG) · corrosion level 2 · airframe 64,410 hrs · 47,114 cycles

CORROSION IN RETRACT ACTUATOR SUPPORT FITTING BEARING FOR RT MLG. THE BEARING WAS REPLACED IAW CMM 20-10-7.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 64,410 hrs · 47,114 cycles

ELONGATED SCREW HOLE ABOVE SPLICE ZFS= 52 AT VERTICAL STABILIZER LE.

Part: SKIN — CORRODED (LT HORIZ STAB) · corrosion level 2 · airframe 64,410 hrs · 47,114 cycles

CORROSION ON LT HORIZONTAL STABILIZER UPPER SKIN BARREL NUT HOLE NR 10 STA XH=27. THE REPAIR FOR BARREL NUT HOLE 10 WAS PERFORMED PER ER/A 551695-14 REV ORIG.

Part: VANE — WORN (TE FLAP) · airframe 64,410 hrs · 47,114 cycles

WEAR ON TRAILING EDGE AREA STA XV1=211 AT RT WING OUTBOARD FLAP INBOARD VANE. TRAILING EDGE AREA STA XV1=211 AT RT WING OUTBOARD FLAP INBOARD VANE WAS REPAIRED SRM 57-03 D.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

CRACKED CANTED FRAME STA Y 1510 REF LONG 2R AT AFT ACC COMPARTMENT. CRACKED FRAME WAS REMOVED AND REPLACED PER SRM 51-30-2 AND 51-30-5.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 64,410 hrs · 47,114 cycles

CORROSION ON SETTLEMENT AREA ON FWD FUEL BOOST PUMP SECONDARY ACCESS COVER NR 1410 AT RT WING. DUE TO EXCESSIVE CORROSION DAMAGE ACCESS COVER NR 1410 WAS REPLACED IN ACCORDING ERA 530866-14MA REV ORIGINAL.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,410 hrs · 47,114 cycles

CORROSION ON UPPER BEAM OF AFT CARGO COMPARTMENT DOOR JAMB STA Y=1160. BEAM WAS REPLACED PER SRM 51-10-4, 51-30-5 AND 53-14-3 FIG 3.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,410 hrs · 47,114 cycles

CORROSION ON BULKHEAD AND INTERCOSTALS (3EAS) ON AFT VENTRAL STAIRWAY MOVABLE CEILING INTERNAL STRUCTURE. AFT BULKHEAD WAS REPLACED PER SRM 51-30-2.

Part: VANE — CRACKED (LT WING TE FLAP) · airframe 64,410 hrs · 47,114 cycles

WEAR ON PREVIOUS REPAIR DOUBLER ON LEADING EDGE XV1=161 ON LT WING OUTBOARD FLAP INBOARD VANE. THE FLAP INBOARD VANE WAS REPLACED IAW SRM 57-03 D PAR. 11.

Part: SKIN — CORRODED (RT MLG DOOR) · corrosion level 2 · airframe 64,410 hrs · 47,114 cycles

CORROSION ON RIGHT MLG FIXED DOOR SKIN UNDER METALLIC SEAL. DUE TO EXCESSIVE CORROSION DAMAGE ON RT MLG FIXED DOOR WAS REPLACED IN ACCORDING DRAWING NUMBER 5936791 REV M.

Part: TAB — DAMAGED (RUDDER) · airframe 64,410 hrs · 47,114 cycles

DAMAGED METALLIZED COAT ON RUDDER CONTROL TAB. METALLIZED COAT ON RUDDER CONTROL TAB WAS REPAIRED PER SRM 51-70-1A PAR 23.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 64,410 hrs · 47,114 cycles

CRACKED RIB ON VERTICAL STABILIZER INTERNAL STRUCTURE STA ZFS=4.7 AND ZFS=17. RIBS WERE REPAIRED PER SRM 55-02 FIG 27, 51-30-2, 51-30-5 AND 51-10-3 PAR. 14, 21.

Part: INSERT — DAMAGED (FLOOR PANEL) · airframe 64,410 hrs · 47,114 cycles

DAMAGED FERRULES AND DELAMINATION ON FLOOR PANELS NR 1174C, 1250C. INSERTS WERE REPLACED ON FLOOR PANEL NR 1174C PER AMM 53-20-01-201 AND FLOOR PANEL NR 1250C WAS CHANGED INSERT PER AMM 53-20-01-201 AND FLOOR PANEL NR 1250 C WAS REINSPECTED AND NOT DAMAGE WAS FOUND.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 64,410 hrs · 47,114 cycles

WEAR AND BEND ON SKIN AROUND OF HANDLE HOUSING ON THE AFT CARGO DOOR. BEND ON SKIN WAS REPAIRED IAW SRM 51-10-2 PAR. 2. WEAR ON SKIN AROUND OF HANDLE HOUSING WAS BLENDED OUT IAW ERA 486446-14MA REV. ORIG.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 64,410 hrs · 47,114 cycles

CORROSION ON LT LOWER ACCESS DOOR CUT OUT WING LOWER SKIN BETWEEN XRS =189.0 TO 214.0 . REPAIRED IAW ERA NO.551715-14AD REV. ORIGINAL AND ETI-88-16-419 REV. 2.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 64,410 hrs · 47,114 cycles

CORROSION ON LT HORIZONTAL STABILIZER UPPER SKIN BARREL NUT HOLE NR 10 HSS XH=2. REPAIRED IAW ER/A 551695-14 REV ORIG.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 64,410 hrs · 47,114 cycles

CORROSION WAS FOUND ON RH HORIZONTAL STABILIZER UPPER SKIN BARREL NUT HOLES NR 3 AND 26 AT HSS XH =27. THE REPAIR FOR BARREL NUT HOLE 3 WAS PERFORMED IAW ER/A 551695-14 REV ORIG. AND FOR BARREL NUT HOLES 26 WAS PERFORMED IAW ER/A 551696-14 REV ORIG.

Part: FITTING — CRACKED (PAX DOORWAY) · airframe 64,410 hrs · 47,114 cycles

CRACKED FITTING BETWEEN BEAMS 4 AND 5 CENTER SECTION AT MAIN ENTRANCE DOOR. THE FITTING WAS RELACED IAW SRM 51-30-2 AND DWG 9955763 REV K.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 64,410 hrs · 47,114 cycles

CRACK ON BEAM ANGLE AT MID CARGO DOOR BEAM NR 1 BS 636. BEAM ANGLE WAS REPLACED IAW SRM 51-30-2.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 64,410 hrs · 47,114 cycles

CRACK ON BEAM WEB AT MID CARGO DOOR BEAM NR 1 BS 637. BEAM WEB WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,410 hrs · 47,114 cycles

CORROSION ON PRODUCTION DOUBLER BTW STA 598-617 AND LONG 29L-29R AT MID CARGO COMPT. DOUBLERS WERE REPLACED PER SRM 51-30-2, 51-30-5, 51-10-3, DWG 5911412 REV DU.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 64,410 hrs · 47,114 cycles

DELAMINATED FLOOR PANEL 120C. THE FLOOR PANEL WAS FABRICATED IAW AMM 53-20-01-201.

Part: VANE — WORN (TE FLAP) · airframe 64,410 hrs · 47,114 cycles

WEAR ON TRAILING EDGE AREA STA XV2= 297 AT LT WING OUTBOARD FLAP OUTBOARD VANE. TRAILING EDGE AREA STA XV2= 297 AT LT WING OUTBOARD FLAP OUTBOARD VANE WAS REPAIRED PER SRM 57-03D PAR 11 AND ERA 492663-14MA REV ORIGINAL.

Part: BEAM — CRACKED (ENTRY DOOR) · airframe 64,410 hrs · 47,114 cycles

CRACKED BEAM 1 ON AFTER AND FWD EDGE AT MAIN ENTRANCE DOOR. CRACK ON BEAM 1 AFT AND FWD EDGE WERE REPAIRED PER SRM 52-05 FIG 97/98.

Part: SKIN — WORN (TE FLAP VANE) · airframe 64,410 hrs · 47,114 cycles

WEAR ON TRAILING EDGE AREA LOWER SURFACE STA XV2=297 AT LT WING OUTBOARD FLAP OUTBOARD VANE. TRAILING EDGE AREA LOWER SURFACE STA XV2=297 AT LT WING OUTBOARD FLAP OUTBOARD VANE WAS REPAIRED PER SRM 57- 03D PAR 11.

Part: LANYARD — DAMAGED (EVAC SLIDE) · airframe 64,410 hrs · 47,114 cycles

BROKEN WIRES ON L1 EVACUATION SLIDE LANYARD ALSO MISSING SECURITY PINS OF L1 AND R1 EVACUATION SLIDE. LANYARD WAS REPLACED PER AMM 25-62-00 AND MUST BE INSTALLED WITH CARD 5200-0654 JOB 001-0070 AND PINS WERE INSTALLED PER AMM 25-62-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,410 hrs · 47,114 cycles

CORROSION ON RT CUSP WEB X-60 TO X- 54 UPPER AND LOWER FACE BTW STA Y 503 AND 598. CUSP WEB ON STA=503 TO STA=598 WAS REPLACED AND REPAIRED PER SRM 51-10-3, 53-05 FIG 131 A, 51-30-5, 51-30-2 DWR 9930538 REV CF.

Part: SKIN — DAMAGED (RUDDER) · airframe 64,410 hrs · 47,114 cycles

DAMAGED METALLIZED COAT ON RUDDER BOTH SIDE. METALLIZED COAT ON RUDDER WAS REPAIRED AND PAINTED PER ER/AN 092613-14MA REV A.

Part: CHANNEL — CRACKED (FLOOR PANEL) · airframe 64,410 hrs · 47,114 cycles

CRACK CHANNEL ON FLOOR PANELS 769A, 769G AND P/N 9952522-445. FLOOR PANELS WERE REPAIRED PER SRM 53-05 FIG 131B AND SRM 51-20-0.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,410 hrs · 47,114 cycles

CORROSION ON RT CUSP WEB ON STA Y=763 AND Y=774 BTW X-60 TO X- 54 UPPER AND LOWER FACE. AREAS WERE REPAIRED PER SRM 53-05 FIG 131A-13/51-10-3 PAR 14, 21 /51-30-2.

Part: SKIN — DAMAGED (LT ELEVATOR TAB) · airframe 64,410 hrs · 47,114 cycles

LIGHTNING STRIKE ON TE SKIN AT LT ELEVATOR ANTI- FLOAT TAB. LT ELEVATOR ANTI- FLOAT TAB WAS REPLACED BY SRM 55-04 PAR 3.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

CRACKED LONG 17R STA Y=1309. LONGERON WAS REPLACED PER SRM 51-30-5.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 64,410 hrs · 47,114 cycles

WEAR ON FWD CARGO DOOR FWD/AFT LOWER SKIN DOUBLERS(C1). DAMAGE FWD AND AFT LOWER SKIN DOUBLERS WERE REPLACED PER ER/A 486624-14MA REV ORIGINAL.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 64,410 hrs · 47,114 cycles

CORROSION ON FUEL TANK ACCESS NR 1454C, 1409C AND 1311C AT LT/RT WING. FUEL TANK ACCESS NR 1409C, 1454C AND 1311C AT LT/RT WING WAS REPLACED PER SRM 51-22-2A.

Part: CUSP WEB — PUNCTURED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

PUNCTURE ON LT CUSP WEB BTW X=44L TO X=54L AT CPAX. CUSP WEB WAS REPAIRED PER SRM 53-05 FIG 131A -13 AND FIG 131A -20.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

CRACK ON LONG 4L BTW STA= 905 TO STA= 927 AT CABIN PASSENGER. LONGERON WAS REPAIRED PER SRM 53-02 FIG 18.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

CRACKED FRAME STA Y= 1322 AND LONG 17R AND LT SIDE AT PAX CABIN. CRACK ON STA Y:1322 LONG 17 RT WAS REPAIRED PER ER/A 493697-14MA REV B.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

CRACKED INTERCOSTAL BTW STA Y=769-788 / X=0 AND Y=1022-1041/ X=0 AT CABIN FLOOR STRUCTURE. INTERCOSTALS WERE REPLACED PER DWG 9936580 REV BW AND SRM 51-30-2 /51-30-5.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,410 hrs · 47,114 cycles

CORROSION ON FLOOR PANEL NR 160G AT W1. FLOOR PANEL WAS FABRICATED PER SRM 51-30-2 AND DWG 9957828 REV AB.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

CRACK ON LONG 4R BTW STA= 905 TO STA= 927 AT CABIN. LONGERON WAS REPAIRED PER SRM 53-02 FIG 18.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

CRACK ON FRAME BTW STA Y=1174 AND LONG 6L. FRAME WAS REPAIRED PER ER/A 495237-14 REV B.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 64,410 hrs · 47,114 cycles

PUNCTURE ON FLOOR PANEL NR 389B AT PAX CABIN. PUNCTURED AREA ON 389B FLOOR WERE REPAIRED PER AMM 25-00-00 PAR 3.

Part: CUSP WEB — CRACKED (CORRODED) · corrosion level 2 · airframe 64,410 hrs · 47,114 cycles

CORROSION ON PREVIOUS CUSP WEB REPAIR LOWER SURFACE BETWEEN BS 457 AND 465, X 54 AND X 60. REPLACED THE REPAIRE IAW SRM 53-05 FIG131A / 51-10-3-PAR 14,21 AND 38 / 51-30-5.

Part: CUSP WEB — CRACKED (BS 818) · airframe 64,410 hrs · 47,114 cycles

CRACK ON CUSP WEB BS 818, X -59. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG. 131-A AND 51-30-2.

Part: SPACER — CRACKED · airframe 64,410 hrs · 47,114 cycles

CRACKED FLOOR PANEL SPACER. THE SPACER WAS REMOVED AND A NEW SPACER WAS INSTALLED IAW AMM 53-20-01-201 PAR.5.

Part: CUSP WEB — CRACKED (BS 1240-1246) · corrosion level 2 · airframe 64,410 hrs · 47,114 cycles

CORROSION ON LT CUSP WEB X 54 TO X 60 BETWEEN BS 1240 AND 1246. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG.131A-14 AND 51-10-3.

Part: CUSP WEB — CORRODED (BS 188-196) · corrosion level 2 · airframe 64,410 hrs · 47,114 cycles

CORROSION ON DIAPHRAGM BETWEEN BS 160 TO 200 AND X 8 TO X 54. CORROSION WITHIN LIMITS IAW SRM 51-10-3 ,PAR. 14, 21,26,,38. BS 188 TO 196 BTW X=44 TO 54 OUT LIMITS. REPAIRED IAW SRM 51-70-4 FIG .1.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 64,410 hrs · 47,114 cycles

CRACK AND BENT SKIN OF MID CARGO DOOR AROUND CUT OUT OF HANDLE HOUSING. REPAIRE IAW ERA 486446-14MA.

Part: DOUBLER — CORRODED (BS 1336) · corrosion level 2 · airframe 64,410 hrs · 47,114 cycles

CORROSION ON PRODUCTION DOUBLER AT BS 1336 TO LONGERON 30. THE DOUBLER WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-3 PAR 21,14 AND DWG 9915561 REV: CG.

Part: DOOR FRAME — CORRODED · corrosion level 2 · airframe 64,410 hrs · 47,114 cycles

CORRODED PREVIOUS REPAIR ON LOWER AREA OF AFT VENTRAL DOOR FRAME AT W2. THE REPAIR WAS REMOVED IAW SRM 51-30-1 AND A NEW REPAIR WAS FABRICATED IAW SRM 53-05 FIG.34. 51-30-2. THE REPAIR WAS INSTALLED IAW SRM.53-05 FIG. 34.

Part: FRAME — CRACKED (BS 1485) · airframe 64,410 hrs · 47,114 cycles

CRACKED FRAME BS 1485, LONGERON 25R. THE FRAME WAS REPAIRED IAW SRM 53-03 FIG 43.

Part: FRAME — CRACKED (BS 1309) · airframe 64,410 hrs · 47,114 cycles

CRACKED FRAME ANGLE BS 1309 BETWEEN LONGERONS 15 - 16R. THE FRAME WAS REPLACED IAW DWG 9912243 REV. JS AND SRM 51-30-5, 51-30-2.

Part: FRAME — CRACKED (BS 1451) · airframe 64,410 hrs · 47,114 cycles

CRACKED FRAME BS 1451 LONGERON 3L. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5 AND DWG 9911860 REV. L.

Part: CUSP WEB — CORRODED (BS 1223-1231) · corrosion level 2 · airframe 64,410 hrs · 47,114 cycles

CORROSION ON LT CUSP WEB X 54 TO X 60 BETWEEN BS 1223 AND 1231. DAMAGE WAS REMOVED AND A REPAIR INSTALLED IAW SRM 53-05 FIG.131A, 51-10-3 PAR. 14,21,38, 51-30-2 AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 1064) · corrosion level 2 · airframe 64,410 hrs · 47,114 cycles

CORROSION ON PREVIUSLY REPAIR DOUBLER RT CUSP WEB BS 1064 BTW X -54 TO X -60 AT PAX CABIN. PREVIUSLY REPAIR DOUBLER WAS REPLACED IAW SRM 53-05 FIG 131 A.

Part: PAN — CRACKED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

CRACKED INNER PAN FWD EDGE BELOW LOWER HINGE AT FWD SERVICE DOOR. THE PAN FWD WAS REPAIRED IAW SRM 52-03 D FIG:3.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

CRACK ON LT CUSP WEB STA Y= 1184 TO BTW X=54 TO X=60 AT PAX CABIN. CUSP WEB WAS REPAIRED PER SRM 53-05 FIGURE 131A-14, 51-10-3 PARAGRAPH 21, 12, 38, 51-30-2, 51-30-5.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

CRACK ON UPPER SURFACE ALSO WEAR CHANNEL ON FLOOR PANEL P/N 9952521-449. FLOOR PANEL WAS REPAIRED PER SRM 51-10-3 SRM 53-01 AND SRM 53-05.

Part: ANGLE — CRACKED · airframe 64,410 hrs · 47,114 cycles

CRACKED ANGLE ON BEAM 1 LOWER FACE AFT SECTION AT FORWARD SERVICE DOOR. ANGLE WAS REPLACED IAW DWG 591181 REV U AND SRM 51-30-05.

Part: WEB — CRACKED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

CRACKED WEB ON STA Y=148, LONG 27L, AT E&E COMPARTMENT. CRACKED WEB WAS REPAIRED PER SRM 53-01 FIG 2 SHT3.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

CRACKED DOOR JAMB WEB STA Y=207 LONG 15L AT PAX CABIN. CRACKED DOOR JAMB WEB STA Y=207 LONG 15L AT PAX CABIN WAS REPAIRED PER SRM 53-05 FIG 142.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

CRACKED TITANIUM FRAME ON STA Y=1345 BTW LONG PROJECTION 28R TO 29R AT AFT ACCESSORIES COMPARTMENT. FRAME WAS REPAIRED PER ER/A 094719-14MA REV A.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

CRACKED STIFFENER IN AFT PRESSURE BULKHEAD 12 HRS POSITION AT CABIN PAX. STIFFENER WAS REPLACED PER SRM 51-30-5, 51-30-2, 51-10-3 PAR 14 AND 21, DWG 9915562.

Part: CHANNEL — CRACKED (FLOOR PANEL) · airframe 64,410 hrs · 47,114 cycles

CRACK CHANNEL ON FLOOR PANELS 617A, 313A AND 313E. CRACK ON CHANNEL THE FLOOR PANELS 617A, 313A AND 313E WERE REPAIR PER SRM 53-05 FIG 131B.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

DELAMINATION ON FLOOR PANEL NR 927C, 1250B, 1155B. FLOOR PANELS NR: 1250B,1155B WERE FABRICATED PER AMM 53-20-01-201 AND FERRULES WERE REPLACED PER AMM 53-20-01-201.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

CRACKED LONGERON NR 12L ON STA Y 1437 AT AFT ACC COMPARTMENT. CRACKED LONGERON WAS REMOVED AND REPLACED PER SRM 53-14-4 AND 51-30-2, 51-30-5 AND 51-10-4 AND 51-10-3 PAR 21, 14.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

CRACK ON LT CUSP WEB STA Y= 1184 TO BTW X=54 TO X=60 AT PAX CABIN. FASTENERS AND REPAIR PART WERE INSTALLED PER SRM 53-05 FIGURE 131A -14, 51-30-2.

Part: PAN — CRACKED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

CRACKED LT WINDOW RING PAN AFT/LOWER CORNER STA Y=905 AT CPAX. RING PAN WAS REPAIRED PER SRM 53-05 FIG 122, 51-30-02, 51-30-05, 51-10-03, PAR 21,14.AND ER/A 487747-14MA REV A, 493648-14MA. REV A.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

DELAMINATED FLOOR PANELS NR 148A,148B, 148C, 148D, 160 A, 160B, 160C, 160B, 160E, 200B, 200C, 200D, 200E AT W1 AREA. FLOOR PANELS NR 148A,148B, 148C, 148D, 160A, 160B, 160C, 160D, 160E, 200B, 200C, 200D AND 200E WERE FABRICATED PER AMM 53-20-01-201.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

CRACKED LONGERON 16L ON STA Y 1437 AT AFT ACC COMPARTMENT. CRACKED LONGERON WAS REMOVED AND REPLACED PER SRM 53-14-4 AND 51-30-2, 51-30-5 AND 51-10-4 AND 51-10-3 PAR 21, 14.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

DELAMINATION ON FLOOR PANEL NR 1307B. FLOOR PANEL 1307B WAS FABRICATED PER AMM 53-20-01-201.

Part: LONGERON — CRACKED (BS 1431) · airframe 64,410 hrs · 47,114 cycles

CRACKED LONGERON 9R BS 1431. THE LONGERON WAS REPAIRED IAW SRM 53-02.

Part: LONGERON — CRACKED (BS 1431) · airframe 64,410 hrs · 47,114 cycles

CRACKED LONGERON 10R BS 1431. THE LONGERON WAS REPAIRED IAW SRM 53-02 FIG 18.

Part: LONGERON — CRACKED (BS 484) · airframe 64,410 hrs · 47,114 cycles

CRACKED LONGERON 10R BS 484. THE LONGERON WAS REPAIRED IAW SRM 53-02 FIG 18, 51-10-3 PAR 14, 21, 51-30-5, 51-30-2.

Part: LONGERON — CRACKED (BS 541) · airframe 64,410 hrs · 47,114 cycles

CRACK ON LONGERON 4L AND BS 541. THE LONGERON WAS REPAIRED IAW SRM. 53-02 FIG. 18, 51-10-3 PAR. 14,21, 51-30-2 AND 51-30-5.

Part: PAN — CRACKED (BS 886) · airframe 64,410 hrs · 47,114 cycles

CRACK ON LT FWD UPPER CORNER WINDOW RING PAN BS 886. THE AREA WAS REPAIRED IAW SRM 53-05 FIG. 122, 51-30-02, 51-30-05, 51-10-03, PAR 21, 14 AND ER/A 487747-14MA REV A, 493648-14MA REV A.

Part: PAN — CRACKED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

CRACKED RT WINDOW RING PAN FWD/UPPER CORNER ON STA Y= 807 AT CPAX. AREA WAS REPAIRED PER SRM 53-05 FIG 122, 51-30-02, 51-30-05, 51-10-03, PAR 21, 14. AND ER/A 487747-14MA REV A, 493648-14MA REV A.

Part: PAN — CRACKED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

CRACKED RT WINDOW RING PAN AFT/UPPER CORNER ON STA Y= 1060, STA Y=1079, STA Y=1098 AND STA Y=1117 AT CPAX. AREAS WERE REPAIRED PER SRM 53-05 FIG 122, 51-30-02, 51-30-05, 51-10-03, PAR 21, 14 AND ER/A 487747-14MA REV A, 493648-14MA REV A.

Part: PAN — CRACKED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

CRACK ON LT FWD LOWER CORNER WINDOW RING PAN STA Y = 1022 AND Y = 1041 AT PAX CABIN. AREA WAS REPAIRED PER SRM 53-05 FIG 122, 51-30-02, 51-30-05, 51-10-03, PAR 21, 14 AND ER/A 487747-14MA REV A, 493648-14MA REV A.

Part: PAN — CRACKED (BS 598-845) · airframe 64,410 hrs · 47,114 cycles

CRACK ON LT FWD UPPER CORNER WINDOW RING PAN BS 598, 750 AND 845. AREA WAS REPAIRED IAW SRM 53-05 FIG. 122, 51-30-02 ,51-30-05, 51-10-03, PAR 21, 14.AND ER/A 487747-14MA REV A, 493648-14MA REV A.

Part: PAN — CRACKED (FUSELAGE) · airframe 64,410 hrs · 47,114 cycles

CRACKED RT WINDOW RING PAN AFT/UPPER CORNER ON STA Y= 1155, STA Y=1212, STA Y=1231 AND STA Y=1250 AT CPAX. AREAS WERE REPAIRED PER SRM 53-05 FIG 122, 51-30-02, 51-30-05, 51-10-03, PAR 21, 14. AND ER/A 487747-14MA REV A, 493648-14MA REV A.

Part: PAN — CRACKED (BS 886) · airframe 64,410 hrs · 47,114 cycles

CRACKED RT WINDOW RING PAN FWD & UPPER CORNER AT BS 886. REPAIRED IAW SRM 53-05 FIG. 122, 51-30-02 ,51-30-05, 51-10-03, PAR 21, 14 AND ER/A 487747-14MA REV. A, 493648-14MA REV. A.

Part: PAN — CRACKED (BS 1060-1079) · airframe 64,410 hrs · 47,114 cycles

CRACK FOUND ON THE LT FWD LOWER CORNER WINDOW RING PAN BS 1060 AND 1079. REPAIRED IAW SRM 53-05 FIG. 122, 51-30-02, 51-30-05, 51-10-03, PAR 21, 14. AND ER/A 487747-14MA, 493648-14MA.

Part: PAN — CRACKED (BS 1231-1250) · airframe 64,410 hrs · 47,114 cycles

CRACK ON THE LT AFT UPPER CORNER WINDOW RING PAN BS 1231 AND 1250. REPAIRED IAW SRM 53-05 FIG. 122, 51-30-02 ,51-30-05, 51-10-03, PAR 21,14.AND ER/A 487747-14MA REV.A, 493648-14MA REV. A.

Part: PAN — CRACKED (BS 598-1174) · airframe 64,410 hrs · 47,114 cycles

CRACKED THE RT WINDOW RING PAN FWD & LOWER CORNER AT BS 598, 788, 845 AND 1174. REPAIRED IAW SRM 53-05 FIG. 122, 51-30-02 , 51-30-05, 51-10-03, PAR 21, 14 AND ER/A 487747-14MA REV. A, 493648-14MA REV.A.

Part: PAN — CRACKED (BS 769-1231) · airframe 64,410 hrs · 47,114 cycles

CRACKED RT WINDOW RING PAN AFT & LOWER CORNER AT BS 769, 826 AND 1231. REPAIRED IAW SRM 53-05 FIG. 122, 51-30-02 ,51-30-05, 51-10-03, PAR 21,14.AND ER/A 487747-14MA, 493648-14MA.

Part: PAN — CRACKED (BS 864) · airframe 64,410 hrs · 47,114 cycles

CRACKED RT WINDOW RING PAN AFT & LOWER CORNER AT BS 864. REPAIRED IAW SRM 53-05 FIG. 122, 51-30-02, 51-30-05, 51-10-03, PAR 21, 14 AND ER/A 487747-14MA REV.A, 493648-14MA REV.A .

Part: PAN — CRACKED (BS 1003) · airframe 64,410 hrs · 47,114 cycles

CRACKED RT WINDOW RING PAN AFT & UPPER ANGLE AT BS 1003. REPAIRED IAW SRM 53-05 FIG. 122, 51-30-02 ,51-30-05, 51-10-03, PAR 21,14.AND ER/A 487747-14MA.

Part: PAN — CRACKED (BS 1117-1212) · airframe 64,410 hrs · 47,114 cycles

CRACKED RT WINDOW RING PAN FWD/LOWER CORNER AT BS 1117, 1136, 1193 AND 1212. REPAIRED IAW SRM 53-05 FIG. 122 , 51-30-02 ,51-30-05, 51-10-03, PAR 21, 14.AND ER/A 487747-14MA REV.A, 493648-14MA REV.A.

Part: PAN — CRACKED (BS 1079-1098) · airframe 64,410 hrs · 47,114 cycles

CRACK ON THE LT AFT LOWER CORNER WINDOW RING PAN BS 1079 AND 1098. REPAIRED IAW SRM 53-05 FIG. 122, 51-30-02, 51-30-05, 51-10-03, PAR 21, 14. AND ER/A 487747-14MA REV.A, 493648-14MA REV.A.

Part: PAN — CRACKED (BS 984-1098) · airframe 64,410 hrs · 47,114 cycles

CRACKED RT WINDOW RING PAN FWD & LOWER CORNER AT BS 984, 1041, 1079 AND 1098. REPAIRED IAW SRM 53-05 FIG. 122, 51-30-02, 51-30-05, 51-10-03, PAR 21, 14 AND ER/A 487747-14 MA REV.A, 493648-14MA. REV. A.

Part: VALVE — FAILED (HYD SYSTEM) · airframe 64,410 hrs · 47,114 cycles

AFT VENTRAL AIRSTAIRS WILL NOT CLOSE ALL THE WAY. CLOSED AND SECURED VENTRAL AIRSTAIRS. HYD VALVE WAS REPLACED. AND THE HYD ACTUATOR WAS REPLACED.

Part: DOOR FRAME — CRACKED (RT MLG WW) · airframe 64,317 hrs · 47,040 cycles

RIGHT MLG DOOR FWD FRAME CRACKED. REMOVED RT MLG DOOR FORWARD FRAME AND BEGAN REPLACEMENT REF SEC II PERM REPAIR INSTRUCTION ERA 551071-14 AND DWG 5930584.

Part: LIGHT — INOPERATIVE (ROW 10ED) · airframe 63,214 hrs · 46,189 cycles

MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE ON SEAT ROW 10ED. THE LIGHT ASSY WAS REPLACED.

Part: STRUCTURE — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 62,353 hrs · 45,613 cycles

AFT LAV SERVICE DOOR CORRODED.

Part: STRUCTURE — CRACKED (L1 DOOR) · airframe 62,353 hrs · 45,613 cycles

FORWARD L1 DOOR HAS A FOUR INCH CRACK VERIFIED BY EDDY CURRENT IN UPPER FWD CORNER. IAW MMB C-CHECK EMPOWER NR 213, L1 DOOR REPLACED.

Part: DOOR — CRACKED (LT MLG) · airframe 62,353 hrs · 45,613 cycles

LT MLG DOOR HAS A TWO INCH CRACK AT INBD FWD CORNER. REMOVED AND INSTALLED SERVICEABLE DOOR IAW AMM 32-12-01.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 62,353 hrs · 45,613 cycles

VERTICAL STABILIZER L/E, SKIN CRACKED AT EXISTING REPAIR, LONGERON 2R, BS 1418. CRACK PASSES THROUGH HI-LOC HOLE. REPAIR OF SKIN REPAIRED ON NR 167. L2R LONGERON REPAIRED BY SPLICE METHOD WITH SHIMMING TO ACCOMODATE SKIN REPAIR IAW SRM 53-02, FIG 18.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 62,353 hrs · 45,613 cycles

VERTICAL STABILIZER L/E, SKIN CRACKED AT BS 1418, LONGERON 3R. NR 167, SKIN CRACK AT BS 1418 AND LONGERON 3R REPAIRED BY TRIMOUT, DOUBLER INSTALLATION AND LONGERON SPLICE WITH SHIMS. ALL WORK ACCOMPLISHED AND RECORDED ON PRI 542150-14AD, REV 0 THRU REV 03 AND COMPLIES WITH FINAL ERA 542150-14AD, REV ORIGINAL RECEIVED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,071 hrs · 47,573 cycles

FUSELAGE SKIN STA 1418 BETWEEN L2R AND 3R CRACK. REPAIRED PER ERA 542150-14AD.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 62,353 hrs · 45,613 cycles

RT WING INBD FORE FLAP LOWER SURFACE HAS NUMEROUS DENTS FROM MLG DEBRIS. R & R RT INBD FORE FLAP IAW AMM 27-51-01.

Part: SCOOP — CRACKED (VERTICAL STAB) · airframe 62,353 hrs · 45,613 cycles

VERTICAL STABILIZER L/E, INLET SCOOP CRACKED TOP CENTER, NEXT TO WELD. WELDED IAW SRM 55-05.

Part: LONGERON — CRACKED (BS 1418) · airframe 62,353 hrs · 45,613 cycles

TAIL COMPARTMENT, LONGERON 2L CRACKED AT BS 1418. INSTALLED NEW LONGERON SECTION AND REPAIR SPLICE IAW SRM 53-02, FIG 18.

Part: SCOOP — CRACKED (VERTICAL STAB) · airframe 62,353 hrs · 45,613 cycles

VERTICAL STABILIZER L/E, INLET SCOOP CRACKED TOP CENTER, NEXT TO WELD. WELDED IAW SRM 55-05.

Part: LANYARD — BROKEN (GIRT BAR) · airframe 61,863 hrs · 45,242 cycles

GIRT BAR LANYARD FOUND BROKEN BY FLIGHT CREW, ECP/FLT 2430. CONTRACT MAINTENANCE IN ECP REPLACED THE GIRT BAR LANYARD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,448 hrs · 44,222 cycles

MAINTENANCE FOUND MULTIPLE OVERHEAD EMERGENCY LIGHTS INOPERATIVE AFTER ROW 22. MAINTENANCE R & R BATTERY PACKS AT LOCATION 24 AND 29. OPS CHECKED OK.

Part: LIGHT — BROKEN (CABIN) · airframe 60,370 hrs · 44,169 cycles

SERVICE CHECK, MSP MAINTENANCE FOUND RED EMEGENCY LIGHT ON SIDE OF 25R BROKEN OFF AND WHITE EMERGENCY LIGHT AT ROW 30 INOPERATIVE. MSP MAINTENANCE REPLACED RED EMERGENCY LIGHT ASSY AT ROW 25 AND REINSERTED PIN FOR WHITE EMERGENCY LIGHT ASSY AT ROW 30, OPS CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 59,461 hrs · 43,531 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE ROW 10 IN SEAT EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AND THE OPS CHECK WAS GOOD.

Part: PUSHROD — DISCONNECTED (RUDDER PEDAL) · airframe 58,910 hrs · 43,117 cycles

DURING TAKEOFF ROLL, F/O COULD NOT STEER THE ACFT WITH RUDDER PEDALS. TAKEOFF ABORTED AND EXITED THE RUNWAY USING THE TILLER. MAINTENANCE FOUND THE RUDDER PEDAL STUCK AND BRAKE PUSH ROD ON THE F/O SIDE DISCONNECTED. SECURED THE ROD AND OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,736 hrs · 43,002 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN FOR BOTH OF THE AFT OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: GENERATOR — TRIPPED (LT ENGINE) · airframe 58,589 hrs · 42,911 cycles

DIVERTED DUE TO THE LT ENGINE GENERATOR TRIPPED OFF LINE AND LT CSD LOW OIL PRESSURE CAUTION ON EOAP. THE APU GENERATOR WAS ON DEFERRAL. MAINTENACE FOUND THE LT ENGINE CSD AND ENGINE COWLING COVERED WITH OIL. R & R THE LT ENGINE CSD, AIR-OIL HEAT EXCHANGER, GENERATOR, AND THE APU GENERATOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,233 hrs · 41,924 cycles

DURING LINE CHECK, THE SEAT MOUNTED EMERGENCY EXIT LIGHTS AT SEAT ROWS 10 AND 30 WERE INOPERATIVE. LIGHT ASSEMBLIES ON BOTH SEATS WERE REPLACED AND OPERATION THEN CHECKED OK.

Part: DOOR FRAME — CORRODED (FWD CARGO) · corrosion level 2 · airframe 57,193 hrs · 41,898 cycles

DURNG SCHEDULED CHECK, CORROSION WAS FOUND ON A FWD CARGO DOOR FRAME SPLICE AT THE FORWARD SEAL DEPRESSOR SEAM. REPLACED CORRODED MATERIAL AND INSTALLED SPLICE DOUBLER IAW DWG 5910142.

Part: SEAL DEPRESSOR — CRACKED (FUSELAGE) · airframe 57,193 hrs · 41,898 cycles

DURING CHECK, DOOR SEAL DEPRESSOR CRACKED APPROXIMATELY 3 INCHES LONG, AFT LOWER 6 O'CLOCK POSITION. REPAIRED IAW ER/A 520881-14.

Part: DOOR FRAME — CRACKED (RT MLG) · airframe 56,216 hrs · 41,189 cycles

DURING LINE INSPECTION, A 2 INCH CRACK WAS FOUND IN THE RT FWD MLG DOOR FRAME APPROXIMATELY 4 INCHES BELOW THE GEAR DOOR OPEN SENSOR. REPLACED DAMAGED FRAME IAW SRM 51-00 & -01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,061 hrs · 41,074 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING FOR ROWS 10-23 OF THE CABIN WERE INOPERATIVE. MX REPLACED THE BATTERIES IN THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,988 hrs · 41,029 cycles

DURING ROUTINE LINE CHECK, THE LT & RT FWD OVERWING EXIT SIGNS WERE NOTED TO BE INOPERATIVE. THE BATTERIES WERE REPLACED & OPERATION CHECKED GOOD IAW AMM 33-50.

Part: CONTAINER — OPEN (R1 DOOR SLIDE) · airframe 55,882 hrs · 40,951 cycles

PILOT REPORTED A PORTION OF THE R1 DOOR SLIDE WAS EXPOSED ON THE ACFT INTERIOR. MX OPENED THE SLIDE COVER AND, AFTER CONTACTING MX CONTROL DECIDED TO REPLACE THE SLIDE ASSY AS A PRECAUTION. THE SLIDE WAS REPLACED IAW AMM 25-62 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: LIGHT — DAMAGED (CABIN) · airframe 55,819 hrs · 40,897 cycles

FA REPORTED EMERGENCY SEAT MOUNTED LIGHTING AT ROW 32D WAS DAMAGED VIA ACARS. MA DID NOT NOTE ANY DAMAGE AT THIS LOCATION AND OPS CHECKED THE EMERGENCY EXIT LIGHTS IAW AMM 33-53 AND THE SYS CHECKED NORMALLY.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 54,687 hrs · 40,102 cycles

SEAT MOUNTED EMERGENCY PATHWAY LIGHT AT FIRST EMERGENCY EXIT ROW INOPERATIVE. FOUND BROKEN WIRE ON SEAT HARNESS. REPAIRED WIRE IAW SPWM. OPS CHECKS GOOD.

Part: LANYARD — FRAYED (R1 DOOR SLIDE) · airframe 54,476 hrs · 39,936 cycles

R1 DOOR SLIDE LANYARD FRAYED. L1 DOOR SLIDE LANYARD ROUTED IMPROPERLY. REPLACE R1 DOOR SLIDE LANYARD. REROUTED L1 DOOR SLIDE LANYARD. ALL MX IAW 25-62.

Part: PIN — UNSECURE (SLIDE) · airframe 54,217 hrs · 39,732 cycles

FLIGHT CREW FOUND PIN OUT OF DOOR SLIDE. MAINTENANCE INSPECTED SLIDE AND REINSTALLED LANYARD. OPERATION NOW CHECKS GOOD.

Part: UNKNOWN — MALFUNCTIONED (LG DOOR) · airframe 54,115 hrs · 39,662 cycles

FLIGHT HAD AN UNSAFE GEAR INDICATION DURING APPROACH, ALL 3 GEAR INDICATIONS WERE RED. CREW COMPLIED WITH THE QRH PROCEDURES AND LANDED WITH GEAR DOORS OPEN. MAINTENANCE JACKED AIRCRAFT, CYCLED GEAR SEVERAL TIMES, AND ALL CHECKS WERE NORMAL WITH ALL NORMAL INDICATIONS. MAINTENANCE REPLACED THE LEFT MLG DOOR SKID PAD AND THE RIGHT MLG DOOR ASSEMBLY DUE TO DAMAGE DURING LANDING.

Part: SKIN — CRACKED (BS 1418 L2L) · airframe 53,820 hrs · 39,457 cycles

FUSELAGE SKIN CRACKED AT BS 1418 L2L. COMPLIED WITH ERA 505035-14 REV O.

Part: SKIN — CRACKED (BS 1437 L3R) · airframe 53,823 hrs · 39,460 cycles

DURING PSV, A CRACK WAS FOUND ON THE FUSELAGE SKIN FORWARD OF BS 1437 AND JUST BELOW L3R.

Part: SKIN — CRACKED (BS 1437 L3R) · airframe 53,818 hrs · 39,456 cycles

DURING PSV, A CRACK WAS FOUND ON THE FUSELAGE SKIN JUST FORWARD OF BS 1437 AND BELOW L3R.

Part: SKIN — CRACKED (BS 1418 L2L) · airframe 53,818 hrs · 39,456 cycles

FUSELAGE SKIN CRACKED AT STA 1418 L-2L. REPAIRED WITH INTERNAL DOUBLER INSTALLATION. REF:ERA NR 505035-14 REV ORIGINAL.

Part: SKIN — CRACKED (BS 1418) · airframe 53,818 hrs · 39,456 cycles

DURING PSV, A SKIN CRACK WAS FOUND COMMON TO FUSELAGE SKIN AT BS 1418, BETWEEN L2-3L.

Part: SKIN — CRACKED (BS 1429 L3L) · airframe 53,818 hrs · 39,456 cycles

FUSELAGE SKIN CRACKED AT BS 1429 L3L. REPAIRED PER ER/A 505030-14 BY INSTALLATION OF REPAIR DOUBLER.

Part: O2 GENERATOR — MISINSTALLED (AFT CABIN) · airframe 53,818 hrs · 39,456 cycles

DURING A PSV-Q CHECK, AFT FLIGHT ATTENDANT OXYGEN GENERATOR AT THE LEFT SERVICE DOOR AND THE AFT FLIGHT ATTENDANT CEILING MOUNTED OXYGEN GENERATOR WERE FOUND WITH THE SAFETY CAPS INSTALLED. REMOVED THE SAFETY CAPS.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 52,435 hrs · 38,506 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN AT ROW 24DE WAS INOPERATIVE. MAINTENANCE FOUND A CONNECTOR IN THE WIRE HARNESS UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 52,335 hrs · 38,444 cycles

EMERGENCY SLIDE LIGHTING DID NOT ILLUMINATE AT ALL DURING PLANNED SLIDE DEPLOYMENT.

Part: PIN — LOOSE (CONNECTOR) · airframe 51,971 hrs · 38,167 cycles

DURING LINE CHECK, MAINTENANCE FOUND ROW 1 EMERGENCY PATHWAY LIGHT INOPERATIVE. MAINTENANCE FOUND PIN LOOSE AT FLOOR CONNECTOR. MAINTENANCE RE-INSERTED PIN PER SWPM. OPERATION CHECKS NORMAL. AIRCRAFT OKAY FOR SERVICE.

Part: PIN — PULLED (CABIN) · airframe 50,662 hrs · 37,250 cycles

DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY PATHWAY LIGHT INOPERATIVE AT ROW 16DE. MAINTENANCE FOUND PIN PULLED FROM CONNECTOR. MAINTENANCE RE-SECURED THE PIN AND THE OPERATION OF LIGHT NOW CHECKS GOOD. AIRCRAFT IS OK FOR SERVICE.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,711 hrs · 36,631 cycles

AFT CARGO BETWEEN STA 1287 AND 1309 LONGERON 22L CORRODED. REPLACED SECTION OF LONERON PER SRM 53-02 FIG 1B. (DLM88102935)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,711 hrs · 36,631 cycles

MAIN CABIN STA 905 TO 1003 LEFT I/B SEAT TRACK CORRODED. REPLACED DAMAGED SECTION OF TRACK PER SRM 53-05 FIG 4F AND DRAWING 5930961. (DLM88102934)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,711 hrs · 36,631 cycles

MAIN CABIN STA 1244 TO 1249 LEFT O/B CENTER OF SEAT TRACK CORRODED. REPLACED SEAT TRACK FROM STA 1174 TO 1308 LBL 56 PER SRM 53-05 FIG 4, 51-30-1, AND 51-30-5. (DLM88102929)

Part: FRAME SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,711 hrs · 36,631 cycles

AFT CARGO STA 1231 FRAME SPLICE AT LONGERON 29RT TO 30RT HAS CORROSION. REPLACED FRAME SPLICE PER SRM 53-14-3 FIG 3A, 53-01 FIG 1, AND DRAWING 9919603. (DLM88102925)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,711 hrs · 36,631 cycles

AFT CARGO COMPARTMENT AFT OF STA 1320 BETWEEN L29L AND L30L SHEAR TIE IS CORRODED. REPLACED SHEAR TIE PER SRM 53-03D FI 3. (DLM88102926)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,711 hrs · 36,631 cycles

MAIN CABIN CUSP WEB AT STA 522-541 HAS CORROSION AROUND LIGHTENING HOLE. REMOVED DAMAGE AND REPAIRED PER ERA 398191-14MA. (DLM88102924)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,711 hrs · 36,631 cycles

MAIN CABIN STA 1155 TO 1193 CUSP WEB HAS CORROSION. REPLACED CUSP WEB FROM STA 1098 TO 1174 AND 1174 TO 1250 PER SRM 51-30-5, 51-10-1, 51-10-2, AND 51-10-4. (DLM88102932)

Part: SKIN — CHAFED (CARGO DOOR) · airframe 49,711 hrs · 36,631 cycles

AFT CARGO DOOR OUTER SKIN AFT LOWER CORNER DOUBLER CHAFED. REPLACED DOUBLER PER SRM 51-10-04. (DLM88102918)

Part: SKIN — CHAFED (CARGO DOOR) · airframe 49,711 hrs · 36,631 cycles

AFT CARGO DOOR OUTER SKIN FWD LOWER CORNER DOUBLER IS CHAFED. REPLACED DOUBLER PER SRM 51-30-2 AND 51-10-4. (DLM88102928)

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,711 hrs · 36,631 cycles

STA 1380 LONGERON 28L FUSELAGE SKIN CRACKED. REPLACED SKIN PER SRM 51-10-4, 51-30-2, 51-30-5, AND 53-34-0 FIG 4. (DLM88102933)

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 49,711 hrs · 36,631 cycles

MAIN CABIN RT CUSP WEB BETWEEN STA 218 AND 237 CRACKED AT LIGHTNING HOLE. INSTALLED CUSP WEB PER SRM 51-10-2, 51-30-2, AND ERA398191-14MA. (DLM88102931)

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,711 hrs · 36,631 cycles

AFT ACCESSORY O/B OF RT VERT STAB DORSEL FIN ATTACH FITTING SHEAR TIE CRACKED. REPLACED SHEAR TIE PER SRM 51-10-02, 51-30-05, AND DRAWING 9953016. (DLM88102917)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,711 hrs · 36,631 cycles

MAIN CABIN STA 1003 TO 1095 LT OUTBOARD SEAT TRACK LBL 56 CORRODED. REPLACED SEAT TRACK PER SRM 53-24-0. (DLM88102930)

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 49,711 hrs · 36,631 cycles

MAIN CABIN STA 731 TO 826 LBL 44 SEAT TRACK I/B EDGE CHAFED SEVERAL PLACES AT SCREW HOLES. REPLACED SEAT TRACK FROM STA 800 TO 840 LBL 44 PER SRM 51-30-1, 51-30-5, AND 53-05 PAGE 32. (DLM88102927)

Part: LONGERON FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,711 hrs · 36,631 cycles

AFT CARGO COMP BETWEEN STA 1338 AND 1330 AT LONGERON 28L END CAP CORRODED. REMOVED AND REPLACED LONGERON END FITTING IAW MD88 SRM 53-01 FIG 1, 51-30-5, 51-30-2, 51-10-4 AND DRAWING 5936667. (DLM88102908)

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,711 hrs · 36,631 cycles

DURING HMV AT PEMCO DHN FOUND CORRODED FRAME AT STA 1309 BETWEEN L28L AND L28R. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW 53-01 FIG 1. CUT OUT DAMAGE SECTION, OBTAINED NEW FRAME, LOCATED, DRILLED AND INSTALLED FRAME, REPAIR ANGLES, SPLICE PLATES IAW MD88 SRM 53-03D FIG 2A. (DLM88102894)

Part: DOUBLER — DENTED (FUSELAGE) · airframe 49,711 hrs · 36,631 cycles

DENT ON EXISTING EXTERIOR REPAIR STA 241 BETWEEN L17L AND L18L. INSTALLED NEW REPAIR PER SRM 53-04D FIG 12B AND DRAWING SG09530002. (DLM88102913)

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 49,711 hrs · 36,631 cycles

AFT CARGO COMPARTMENT LT TIE DOWN TRACK HAS CORROSION AROUND FASTENER HOLES FROM STA 1098 TO FWD SIDE OF APB. REPLACED TIE DOWN TRACK PER SRM 51-30-1 AND 53-01 FIGURE 1. (DLM88102897)

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,711 hrs · 36,631 cycles

AFT CARGO STA 1214 TIE DOWN TRACK SUPPORT HAS CORROSION BETWEEN LONGERON 27L AND 28L. REPLACED TIEDOWN TRACK IAW DRAWING 5956034. (DLM88102895)

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,711 hrs · 36,631 cycles

AFT ACC COMP STA 1380, FRAME CORRODED IN SEVERAL PLACES FROM LONGERON 24L TO 24R. REMOVED AND REPLACED FRAME IAW MD88 SRM 51-30-2 AND DRAWING 5911429. (DLM88102907)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,711 hrs · 36,631 cycles

MAIN CABIN STA 160-168 LBL 53 FLOOR SUPPORT CORRODED. INSTALLED NEW FLOOR SUPPORT PER SRM 53-01 FIG 1, 53-14-01 FIG 11, 51-30-05, 51-30-02. (DLM88102901).

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,711 hrs · 36,631 cycles

MAIN CABIN CUSP WEB STA 560-579 RT CORRODED. REPAIRED CUSP WEB IAW ERA 398191-14MA. (DLM88102904)

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,711 hrs · 36,631 cycles

AFT CARGO SKIN FWD OF FS 1212 HAS CORROSION AT DRAIN AREA FROM L29L TO L29R. INSTALLED REPAIR FILLER AND DOUBLER IAW ERA486148-14 REV ORIG. (DLM88102900)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,711 hrs · 36,631 cycles

MAIN CABIN RT CUSP WEB BETWEEN STA 655 AND 674 HAS CORROSION. REPLACED CUSP WEB PER DRAWING 9910151. (DLM88102898)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,711 hrs · 36,631 cycles

AFT CARGO BETWEEN STA 1136-1155 BOTTOM SIDE LT CUSP WEB CORRODED. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-14-03 FIG 12, 53-01 AND ERA 398191-14MA. (DLM88102912)

Part: PAN — GOUGED (CARGO BAY) · airframe 49,711 hrs · 36,631 cycles

FWD CARGO DOOR PAN HAS 4 GOUGES AROUND CORE NUTS STA 410 L28R. REPLACED LOWER PAN SECTION PER SRM 53-01- FIG 1, 53-14-02 FIG 2, AND 53-05 FIG 44. (DLM88102909)

Part: STIFFENER — DAMAGED (FLOOR PANEL) · airframe 49,711 hrs · 36,631 cycles

FLOOR PANEL 826D STIFFENER HAS HOLE, CRACKS, AND CHAFING. REPLACED CHANNEL PER SRM 51-10-04. (DLM88102903)

Part: A/C PACK — ODOR · airframe 48,112 hrs · 35,549 cycles

REPEAT WRITE UP. AFTER T/O AND CLIMB F/AS REPORTED ODOR AND RT AFT LAV SMOKE DETECTOR BEEPING. HOT PACK ODOR DETECTED IN COCKPIT. RAN BOTH PACKS ON MANUAL TO GET RID OF ODOR. SMOKE DETECTOR SILENCED AFTER A FEW MINUTES. CA-C/W OPN 5088 CABIN SMOKE /ODOR TROUBLESHOOTING. NO DEFECTS NOTED. C/W OPN 5089 DUCT BURNOUT. NO ODORS DETECTED. REPLACED COLESTER BAGS. DUCTS LEAK CK OK. ACFT OK FOR SVC.

Part: WIRE — CHAFED (AUTOTHROTTLES) · airframe 41,620 hrs · 31,300 cycles

WKG MCO - AUTOTHROTTLES DISCONNECTED. DURING T/S FOUND CHAFED WIRES AT AUTOTHROTTLE SERVO. CUT BACK ALL A/T SERVOMOTOR WIRES PRIOR TO DAMAGED AREA AND REPLACED A/T SERVOMOTOR C/P P10-430. MADE REPAIR TO DAMAGED SYSTEM WIRES PER MM. RTS ON DFGC 1 AND 2 GOOD. PERFORMED TESTS ON ALL AFFECTED SYSTEMS ASSOCIATED WI DAMAGED WIRING ALL A/C SYSTEMS TEST GOOD. A/T CHKS GOOD, CLEARED MCO AND REMOVED PLACARD.

Part: SPAR CAP — DAMAGED (VERTICAL STAB) · airframe 34,275 hrs · 26,224 cycles

VERTICAL STABILIZER HORIZONTAL STABILIZER HINGE PLATES HAD THREE HOLES WITH DAMAGE. REPAIRED IAW ERA 093177-14AD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 33,566 hrs · 25,727 cycles

SEVERAL EMERGENCY SEAT LIGHTS INOP AFTER ROW 17. SECURED LOOSE CONNECTOR AT ROW 17.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,406 hrs · 25,622 cycles

CABIN SEAT EMERGENCY LIGHTING INOP ROW 18 THRU 23. REPLACED BATTERY PACK AND BATTERIES AT ROW 18.

Part: BULB — BURNED OUT (MLG INDICATOR) · airframe 32,507 hrs · 25,026 cycles

RIGHT MAIN LANDING GEAR LIGHT BURNED OUT. GEAR INSPECTION VIEWING PORT DIRTY AND DIFFICULT TO SEE THROUGH. RELAMPED RT MLG INDICATOR CAPSULE AND CLEANED VIEWING PRISM.

Part: ODOR — DETECTED (COCKPIT) · airframe 32,434 hrs · 24,977 cycles

ON CLIMBOUT STRONG ELECTRICAL BURNING ODOR IN COCKPIT AND FORWARD CABIN. PERFORMED OPN 5088, NO PROBLEMS FOUND. RAN ENGINES AT POWER WITH PACKS ON, WING AND ENGINE ANT-ICE ON AND OFF. NO PROBLEMS FOUND.

Part: COMPRESSOR — DAMAGED (NR 1 ENGINE) · airframe 31,499 hrs · 24,366 cycles

LT ENGINE SLOW TO ACCEL ON GROUND. ENGINE DID PRODUCE T/O POWER TO MATCH RT ENGINE HOWEVER LT N1 94 PERCENT AND RT N1 90 PERCENT LT EGT 600 RT 560. UPON SELECTION OF CLIMB POWER 3 COMPRESSOR STALLS NOTED. LT ENGINE PULLED BACK TO IDLE STALLS STOPPED. COMPRESSOR STALL CHECK LIST WAS RUN AND THROTTLE ADVACED TO 80 PERCENT NO MORE STALLS HOWEVER LT EPR 20 PERCENT LESS THAN RT WITH THROTTLES MATCHED. FOUND DAMAGE IN COLD STREAM AT BLEED VALVES. ENGINE REPLACED

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,805 hrs · 23,862 cycles

EMERGENCY LIGHTS OUT AT ROW 17 THRU ROW 23. REPLACED BATTERY CHARGER

Part: BEARING — NOISY (NLG WHEEL) · airframe 30,788 hrs · 23,852 cycles

LOUD NOISE IS COMING FROM THE NOSE WHEEL AREA. FOUND LT NOSE WHEEL BEARING FAILED. REPLACED WHEEL ASSY

Part: OVEN — OVERHEATED (GALLEY) · airframe 30,435 hrs · 23,591 cycles

FWD GALLEY OVEN OVERHEATS AND SMOKES. REPLACED SAME.

Part: HOSE — RUPTURED (NBR 1 ENG) · airframe 26,586 hrs · 20,767 cycles

LT HYD PRESS LOW LIGHT ILLUMINATED ON OAP HYD PRESS WAS ZERO///FOUND PRESS LINE ON LT ENG LEAKING. REPLD LINE

Part: COVER — BROKEN (PAX DOOR SLIDE) · airframe 24,360 hrs · 19,140 cycles

WHEN OPENING L1 DOOR, THE SLIDE ASSY FELL OFF OF THE DOOR AND ON TO THE RAMP. THE SLIDE WAS NOT ARMED AND DID NOT DEPLOY. THE SLIDE''S PLASTIC COVER WAS DAMAGED SO IT WAS REPLACED. S/N OFF 0382, S/N ON 1145, P/N 259001365.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 23,484 hrs · 18,503 cycles

ON LAYOVER FOUND BATTERY PACK ABOVE SEATS 17-18 EF INOP. REPLACED BATTERIES INSIDE PACK AND TESTED REF M/M OPS CK OK.

Part: SENSOR — INOPERATIVE (NOSE GEAR) · airframe 22,937 hrs · 18,086 cycles

AFTER T/O ON GEAR RETRACTION, NOSE GEAR UNSAFE LIGHT. LIGHT REMAINED ON. RECYCLED GEAR RAN CHECK LIST AND LIGHT REMAINED ON. WHEN GEAR LOWER FOR LANDING ALL IND NORMAL. REPLACED NOSE GEAR POSITION SENSOR, NOSE GEAR LOCK SENSOR AND R2-252 SWUNG GEAR SEVERAL TIMES. GEAR IND NOW NORMAL.

Part: ENGINE — FAILED (NR 2)

NR 2 ENG FAILED AFTER T/O. RETURNED TO LAND. REPLACED ENGINE.

Part: SOCKET — FAILED (CABIN)

AIRCRAFT RETURN TO BLOCK WITH ELECTRICAL SMELL AND SMOKE FROM FIRST CLASS NUMBER 4 FLUORESCENT LIGHT ARCING. REPLACED BULB HOLDER ASSY.

Part: PACK — MALFUNCTIONED (LEFT)

FUME/ODOR FROM A/C ON GRD, THOUGHT IT WAS TUG DID NOT GO AWAY IN FLT LT PACK RUNS 250 PSI RT PACK RUNS 350 PSI. FOUND LT PACK PUTTING OUT ODOR DISCONNECTED RAM SENSE LINE FROM FLOW CONTROL VALVE LT SIDE. FWD TO MCO/PLACARD PER MEL 21-00-01A.

Part: ENGINE — BIRD STRIKE (NR 1)

AFTER TAKEOFF GOT STRONG SMOKE ODOR THROUGHOUT CABIN FRONT TO AFT. ACFT INJUSTED BIRD IN NR 1 ENGINE AFTER TAKEOFF. EVIDENCE SHOWS IT WENT THROUGH COMPRESSOR. BORO, OK.

Part: BATTERY — DISCHARGED (CABIN)

REPORTS OF LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INTERMITTENT OR INOPERATIVE. REPLACED BATTERY PACKS FOR OVERWING EMERGENCY EXIT SIGNS. OPERATION CHECKS GOOD.

Part: FAN — FAILED (RADIO RACK)

STRONG ELECT SMELL AND SMOKE AT PUSHBACK. FOUND RADIO RACK FAN FAILED. REPLACED FAN, OPS NORMAL.

Part: CROSS OVER RIB — CRACKED (LWR FUS)

FOUND DURING C-2 LETTER CHECK, CROSS OVER RIB BETWEEN MLG WHEEL WELL DOORS AFT SIDE CRACKED ON LT SIDE OF RIB AND RT SIDE 1 INCH EACH. REPAIRED PER SRM 53-05 FIG 101.