N135FE

Part: FLOOR PANEL — DENTED (MAIN DECK CARGO) · airframe 13,642 hrs · 6,175 cycles

MAIN DECK CARGO COMPARTMENT, STA 317, (222AFF) FLOOR PANEL WITH DENTS. MDC, FLOOR PANEL 222AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B REV. 88 DEC 15/2023

Part: FLOOR PANEL — DENTED (MAIN DECK CARGO) · airframe 13,642 hrs · 6,175 cycles

MAIN DECK CARGO COMPARTMENT, STA 317, (221CFF) FLOOR PANEL WITH DENTS. MDC, FLOOR PANEL 221CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B REV. 88 DEC 15/2023

Part: FLOOR PANEL — DENTED (MAIN DECK CARGO) · airframe 13,642 hrs · 6,175 cycles

MAIN DECK CARGO COMPARTMENT, STA 317, (221DFF) FLOOR PANEL WITH DENTS. MDC, FLOOR PANEL 221DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B REV. 88 DEC 15/2023

Part: FLOOR PANEL — DENTED (BS 317) · airframe 13,642 hrs · 6,175 cycles

MAIN DECK CARGO COMPARTMENT, STA 317, (222BFF) FLOOR PANEL WITH DENTS. MDC. FLOOR PANEL 222BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B REV. 88 DEC 15/2023

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 13,642 hrs · 6,175 cycles

MAIN DECK CARGO COMPARTMENT, STA 317, (222CFF) FLOOR PANEL WITH DENTS. MDC, FLOOR PANEL 222CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B REV. 88 DEC 15/2023

Part: SKIN — GOUGED (LE SLAT) · airframe 6,844 hrs · 2,967 cycles

RIGHT WING #8 SLAT TRAILING EDGE LOWER SURFACE GOUGED REPAIRED DAMAGE PER B767 SRM 57-43-02-2R

Part: SKIN — DENTED (LT WING SLAT) · airframe 3,515 hrs · 1,517 cycles

LEFT WING NR 5 SLAT UPPER SURFACE DENTED. REPAIRED THE DENT IAW SRM 57-43-02-2R, AND SRM 51-70-10 4. MAJOR REPAIR.

Part: WIRE — BROKEN (CARGO DOOR) · airframe 2,702 hrs · 1,155 cycles

RECEIVED "MAIN CARGO DOOR" EICAS ALERT AT CRUISE. OCCURED AT FL 370. REMOVED AND MOUNTED S892 REF B767 AMM 52-71-09-2, REQUIRES AVIONICS TO TERMINATE CONNECTION AND CHECK OUT SPLICED IN SENSOR S892 IAW B767 MM 52-71-09-2 AND SSM 52-70-01. ADDITIONAL MAINTENANCE ACTION REQUIRED. OPS CHECK GOOD. REF AMM 52-71-09-2 AND 52-71-00-5.RAN QRH AND DESCENDED TO 15,000'. PASSING APPROX 16,000' LIGHT WENT OUT. NO CHANGES IN PRESSURIZATION.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 2,167 hrs · 929 cycles

DURING TAXI IN SMELLED BURNT AIR THEN GOT "LEFT PACK TEMP EICAS" SHUT DOWN PACK AND PARKED JET. COMPLIED WITH SMOKE OR FUMES IN THE CABIN PER AMM 05-51-56-2, TASK 21-00-21-102-030, SUBTASK C (1) & (2). NO COMPONENTS WERE FOUND WITH OIL CONTAMINATION. PER FLIGHT CREW IT SMELLED LIKE AN OVERHEATED PACK. REMOVED AND REPLACED LT PACK BAY AIR CYCLE MACHINE MPN 680640-4 SN: WXP0569 REF AMM 21-51-03-4. OPS CHECK NORMAL. OK FOR SERVICE.

Part: ESCAPE ROPE — OUT OF POSITION (CABIN) · airframe 24 hrs · 16 cycles

CREW ENTRANCE DOOR ESCAPE ROPE CAUGHT IN DOOR ROLLER. REINSTALLED THE L1 DOOR EMERGENCY ESCAPE ROPE IAW AMM 25-10-00-2 & 25-61-04-2.

Part: SLAT — FAILED (WING)

UPON FLAP RETRACTION NR 6 SLAT FAILED TO RETRACT.

Part: SWITCH — DIRTY (MLG DOOR)

AFT T/O WITH GEAR RETRACT AND DOOR LIGHT OUT, HANDLE WAS PLACED IN OFF POSTION, RMG DOOR ILLUM. RAN RED TABS. PLACED HANDLE IN THE UP POSITION AND LIGHT WENT OUT. LT HANDLE IN UP POSITION. NO YAW OR NOISE ASSOCIATED WITH DOOR LIGHT ON. *S/D* CLEANED SWITCH ELECTRO CONTACT CLEANER RG DOOR LIGHT, OPS CK GOOD AT THIS TIME PER 32-62-011-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 58,448 hrs · 44,127 cycles

DURING ROUTINE INSP, THE NR 1 SEAT TRACK FOUND CORRODED AT BS 783. REMOVED, REPLACED AND FAB PER IAW BAC 7S7 SRM 53-10-5, 51-30-2.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 58,448 hrs · 44,127 cycles

DURING ROUTINE INSP, THE LOWER FUSELAGE INTERCOSTAL AT RBL 23 FROM BS 1010 - 1030 FOUND CORRODED. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-4, 51-30-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 58,448 hrs · 44,127 cycles

DURING ROUTINE INSP, THE BS 344 FLOORBEAM FOUND CORRODED BETWEEN NR 3 & 5 SEAT TRACKS. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 53-10-8.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 58,448 hrs · 44,127 cycles

DURING ROUTINE INSP, THE SUPPORT BRACKET AT BS 1110, STR 19L FOUND CORRODED. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 58,448 hrs · 44,127 cycles

DURING ROUTINE INSP, THE NR 6 SEAT TRACK FROM BS 737 - 740 CORRODED. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 53-10-5.

Part: PANEL — CORRODED (FUELAGE) · airframe 58,448 hrs · 44,127 cycles

N 642-2 DURING ROUTINE INSP, THE AFT BAG BIN RIGHT TRANSISTION PANEL FOUND CORRODED AT RBL 23 FROM BS 1010-1030. R&R & FAB PER IAW BAC 7S7 SRM 51-40-2, 51-30-2.

Part: ATTACH ANGLE — CRACKED (NR 12 SPOILER) · airframe 58,448 hrs · 44,127 cycles

DURING ROUTINE INPS, THE NR 12 SPOILER O/B ATTACH ANGLE FOUND CRACKED. REMOVED AND REPLACED PER IAW BAC 727 SRM 51-30-2 & BAC SB 57-84.

Part: WEB — CORRODED (SERVICE DOOR) · airframe 58,448 hrs · 44,127 cycles

DURING ROUTINE INSP, SERVICE DOOR FOUND CORRODED INSIDE THE SECOND LIGHTENING HOLE FROM FWD, APPROX WL 232.5. REMOVED, REPLACED AND FAB WEB PER IAW BAC 727 SRM 51-20-1, 51-30-2, 52-12-00. OPS CK GOOD.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,448 hrs · 44,127 cycles

DURING ROUTINE INSP, THE LOWER FUSELAGE SHEAR TIE FROM BS 196 - 203 AT RBL 6 FOUND CORRODED. REMOVED, REPLACED AND FAB PER IAW BAC 737 SRM 51-20-1, 51-30-2.

Part: SKIN — CRACKED (RT MLG DOOR) · airframe 58,448 hrs · 44,127 cycles

DURING ROUTINE INSP, RT MAIN LANDING GEAR WING DOOR OUTER SKIN FOUND CRACKED. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 52-80-2.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 58,448 hrs · 44,127 cycles

DURING ROUTINE INSP, THE SUPPORT BRACKET ATTACHMENT FOR NOSE LANDING GEAR LOCK ACTUATOR WAS FOUND CRACKED AT BS 351.2. REMOVED AND REPLACED PER IAW BAC 727 SRM 51-30-2.

Part: SPAR — CORRODED (CENTER WING) · airframe 58,448 hrs · 44,127 cycles

DURING ROUTINE INSP, CORROSION DAMAGE FOUND AT SEVERAL FASTENERS IN THE WING CENTER SECTION REAR SPAR UPPER CHORD. REMOVED AND REPLACED PER P/N 65-18538-5 IAW FEDEX EA 7-5710-53851.

Part: SWITCH — DIRTY (MLG DOOR)

AFTER T/O, RAISING GEAR HANDLE LMG DOOR AND RED DOORS LIGHT REMAINS ON. FOUND MG DOOR SWITCH SOAKED WITH OIL. CLEANED CANNON PLUG AND RECONNECTED, CYCLED LEFT GEAR DOOR 4 TIMES, CHECKS OK.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 59,420 hrs · 44,791 cycles

DURING APPROACH TO CLE, L GEAR DOWN INDICATOR LIGHT (GREEN) DID NOT ILLUMINATE; NO OTHER ABNORMAL INDICATIONS. UNABLE TO REMOVE BULBS TO REPLACE. RECEIVED VISUAL CONFORMATION FROM TOWER THAT GEAR WAS DOWN; LANDED NORMALLY. RELAMPED ANNUNCIATOR. LIGHTS TEST NORMALLY PER USE OF TEST BUTTON PER M/M 33-10-001-4. OKAY FOR SERVICE.

Part: CONNECTOR — CONTAMINATED (RT MLG DOOR)

RIGHT MAIN GEAR DOOR LIGHT CAME ON AT 12,000 FT DURING DESCENT AT 340 KIAS. CYCLED GEAR AND ALL LIGHTS WENT OUT IND NORMAL. *S/D* REMOVED WATER FROM RIGHT GEAR DOOR LOCK CONDUIT. REMOVED AND REPLACED D752 CANNON PLUG, OPER CK GOOD AS PER MM 32-62-0.

Part: ANTI-ICE DUCT — BROKEN (NR 2 ENGINE)

NR 2 ENGINE LEFT HAND ENGINE INLET ANTI-ICE DUCT BROKEN IN HALF. LOCATED JUST AFT OF ANTI-ICE VALVE. REMOVED AND REPLACED ANTI-ICE DUCT IAW FED-EX M/M 75-10-00.

Part: ANTI-ICE DUCT — DAMAGED (NR 2 ENGINE)

NR 2 ENG LEFT HAND ENGINE INLET A/I DUCT DAMAGED, LOCATED JUST FWD OF THE A/I VALVE. *S/D* REMOVED AND REPLACED ANTI-ICE DUCT PER FED-EX M/M 75-10-14.

Part: RIB — CRACKED (BS 760)

FWD UPPER HOLE AT 12 O'CLOCK ON THE RT RIB CHORD AT STA 760 IS CRACKED. REPAIRED PER EA 7-5710-25838 DATED 10-11-95.

Part: ANGLE — CRACKED (BS 760)

FWD 2 HOLES IN LT CHORD ANGLE AT STA 760 SHOW CRACKS. REPAIR COMPLETED PER EA 7-5710-25838.

Part: FITTING — CRACKED (BS 740)

LT WING FRONT SPAR FWD TERMINAL PIN JOINT HOLE CRACKED AFT END. LEVELED AND SHORED A/C IAW SRM 51-50-1, CUT LOWER CHORD ANGLE AND WEB IAW BOEING DRWG NR 65C29064, REMOVED FS 740 AFT TRUNNION AND REPLACED WITH NEW AFT TRUNNION. SPLICED WEB AND LOWER CHORD ANGLE IAW BOEING DRWG NR 65C29064.

Part: FITTING PIN — CORRODED (RT WING)

RIGHT WING REAR SPAR BODY FITTING FWD AND REAR BUSHINGS WORN, BODY FITTING PIN FLANGE CORRODED. INSTALLED NEW RT WING REAR SPAR BODY FITTING PIN PER SRM 51-10-1 PG 4, REPLACED FWD AND REAR BUSHINGS PER 51-10-1 PG 4, ESO 11782 AND FEDEX EA NR 7-5310-25827.

Part: SKIN — CRACKED (BS 1160)

DOUBLER CRACKED AT RIVET STA 1160 O/B OF STR 26R. REMOVED DAMAGED SKIN AT SKIN LAP STA 1149 - 1163, STR 26R PER SRM 53-30-3 FIG 5. INSTALLED REPAIR DOUBLER FROM STA 1140 - 1167 STR 26R PER SRM 53-30-3, PAGES 20-25.

Part: FLOOR BEAM — CORRODED (BS 1110)

CORROSION IN LOWER FLANGE OF FLOOR BEAM BS 1110, BL 0 - 48 RT, IN AFT CARGO COMP. REMOVED CORRODED AREA PER SRM 51-10-6, FABRICATED ANGLES AND STRAP PER ESO 11782, INSTALLED SAME PER ESO 11782, EA NR 7-5310-25188.

Part: FLOOR BEAM — CORRODED (BS 1110)

CORROSION IN AFT CARGO COMP FS 1110 FLOOR BEAM LOWER FLANGE BL 16L TO 30L. REMOVED CORRODED AREA PER SRM 51-10-6, FABRICATED FILLER AND DOUBLER PER ESO 11782, INSTALLED FILLER AND DOUBLER PER ESO 11782 AND SRM 51-10-6, 51-40-2. EA NR 7-5310-25810.

Part: FLOORBEAM — CORRODED (BS 312)

CORROSION TOP SIDE OF FLOORBEAM STA 312 LBL 35. REPAIR PER SRM 53-10-2.

Part: CASTING — CORRODED (BS 460-487)

THE 9G NET CASTING HAS HEAVY CORROSION, JUST I/B OF RBL 45 SEAT TRACK AND CRACKED STA 460 TO 487. FABRICATED NEW SUPPORT PER EA 7-5320-25815 DATED 9-25-95. INSTALLED FITTING 9G AT RBL 45 IAW ESO 11782 DATED 9-15-95 AND SRM 51-10-1.

Part: SKIN — CRACKED (PAX DOOR CUTOUT)

CRACK IN SKIN AT FWD EDGE OF ENTRY DOOR CUTOUT JUST BELOW STR 7L. REPAIRED PER ESO 11782 DATED 9-15-95 AND EA 7-5330-25765 DATED 9-18-95.

Part: SKIN — CORRODED (BS 310-318)

CORROSION BETWEEN SKINS IN CORNER OF FWD ENTRY DOOR CUTOUT, FWD UPPER CORNER APPROX STA 310 TO 318, CORNER OF DOOR AND PROCEEDS FWD TO APPROX STA 303 AREA. REPAIRED PER EA 7-5330-25765 DATED 9-18-95.

Part: CASTING — CORRODED (BS 360)

UPPER LOBE FLOOR, FOUND CORROSION ON 9G NET FLOOR ANCHOR STA 360 LT LBL 24. INSTALLED NEW NET ANCHOR CASTING PER SRM 51-10-1 EA 7-5320-25815 DATED 9-25-95.

Part: STRINGER — DAMAGED (BS 460-484)

FASTENERS PULLED THROUGH SIDE OF STR 24R STA 460 TO 484. REMOVED FASTENERS AND REPAIRED STR PER SRM 51-10-3.

Part: FRAME — CRACKED (BS 870)

BS 870 TERMINAL FITTING AFT ROW 2ND FASTENER HOLE ABOVE STR 10R HAS CRACK IND, AT 12 O'CLOCK ON O/B SIDE OF O/B FLANGE, RT SIDE FUSELAGE. CRACK IN FRAME STA 870 RT JUST ABOVE STR 10R CRACK IND IS BETWEEN THE 3RD AND 4TH FASTENER ABOVE STR 10R. INSTALLED DOUBLERS PER SB 727-53-0194-NSC2 AND NR JOB FROM NR 0724. REF NR 0724 PGS 1 AND 2 JOB PROGRESS FORMS THIS REPAIR.

Part: SKIN — MISMFG (BS 1130)

TWO FASTENERS INSTALLED IN ONE HOLE, THROUGH SHEAR TIE STA 1130, O/B OF STR 29L. REMOVED DAMAGE FROM FASTENERS AT STA 1130 O/B OF STR 29L. INSTALLED DOUBLER OF AFT FUSE BELLY SKIN PER SRM 53-30-3.

Part: FLOOR BEAM — CORRODED (BS 360)

CORROSION OF FLOOR TRACK AT LBL 45 AT BS 360, 400-420 AND 380. REMOVED SECTION OF FLOOR BEAM STATION 360 - 420 AND INSTALLED NEW FLOOR TRACK FROM STA 360-420 PER SRM 51-10-5.

Part: SKIN — MISMFG (BS 1150)

AFT CARGO BELLY SKIN AT STA 1150, STA 29 - 2 EA HOLES HAVE 2 FASTENERS IN ONE HOLE. REMOVED DAMAGED FASTENERS, INSTALLED DOUBLER ON SKIN PER SRM 53-30-3.

Part: FLOOR BEAM — CORRODED (BS 640)

STA 640, RBL 5 UPPER FLANGE OF FLOOR BEAM HAS EXFOLIATION CORROSION PILLOWED AND BLOWN OUT - REMOVED CORROSION AND INSTALLED DOUBLER REPAIR WITH 7075-T6 EXTRUSIONS AND A 15-5 STAINLESS STEEL STRAP, CAD PLOTED AND HEAT TREATED TO 180-200 RSI, TREATED AND PRIMED ALL SURFACES AS REQ'D. INSTALLED WITH FASTENERS AND FAYING SURFACE SEALER PER SRM 53-10-8.

Part: FLANGE — CORRODED (BS 480)

UPPER MAIN CARGO, CORROSION ON BOTTOM SIDE OF THE FWD FLANGE STA 480 RBL 5. REMOVED CORROSION AT LOCATIONS PER SRM 51-10-01, INSTALLED REPAIR IAW SRM 53-10-8 FIG 5 AND 51-40-2.

Part: FLOOR BEAM — CORRODED (BS 480)

CORROSION BOTTOM OF FLOOR BEAM JUST I/B OF RBL 25 SEAT TRACK STA 480. REMOVED PORTION OF CORRODED BEAM - FABRICATED AND INSTALLED DOUBLER PER 53-10-8 FIG 5 OF SRM.

Part: FLOORBEAM — CORRODED (BS 480)

UPPER LOBE FLOOR, CORROSION ON UNDERSIDE OF FLOORBEAM LT STA 480 BETWEEN BL 0 AND LBL 24. CORROSION REMOVAL WAS BEYOND LIMITS. INSTALLED REPAIR IAW 53-10-8 FIG 5 AND 51-40-2.

Part: FLOOR BEAM — CORRODED (BS 400)

HEAVY CORROSION AT F/B SCREW HOLES STA 400, LBL 35 ON FLOOR BEAM TOP SIDE. REMOVED CORROSION BY CUTTING OUT DAMAGED AREA PER SRM 53-10-8. INSTALLED FLOOR BEAM REPAIR PER SRM 53-10-8, PG 45 - 48.

Part: FLOOR BEAM — CORRODED (BS 480)

UPPER LOBE FLOOR STA 480 LT CORROSION ON UNDERSIDE OF FLOOR BEAM BETWEEN LBL 24 AND LBL 45 AROUND FASTENER HOLES. REMOVED CORROSION NR 7 ABOVE LOCATION PER SRM 51-10-06. CORROSION REMOVED BEYOND LIMITS, REPAIRED CORRODED FLOOR BEAM PER 53-10-8 FIG 5.

Part: BLKHD WEB — CORRODED (BS 950)

AFT CARGO COMP FS 950 BLKD UPPER FLANGE AND WEB CORRODED BETWEEN RBL 24 - 54. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-10-9 FIG 2, SRM 51-10-9.

Part: SPAR — CORRODED (BS 870)

RIVET HEAD POPPED AND CORROSION ON OUTSIDE OF CENTER TANK REAR SPAR JUST FWD OF STA 870 RT, RBL 50. REMOVED CORR - MATERIAL THICKNESS BEYOND MM LIMIT. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER PER AA ESO 11782. AWAITING FEDEX EA.

Part: FLOOR BEAM — CORRODED (BS 420)

ON NR 0234, CORROSION ON FLOOR BEAM IN MAIN CARGO STA 420 RBL 20. CORROSION REMOVED BEYOND LIMITS. CUT OUT AREA AND INSTALLED .090 INCH DOUBLERS AND FILLER PER SRM 53-11-8, FIG 8.

Part: RIB — CRACKED (RUDDER)

UPPER RUDDER THRUST HINGE, LOWER LT SIDE. RIB IS CRACKED BETWEEN FASTENERS. REMOVED 6 EACH FASTENERS - HFEC CHECKED. VERIFIED CRACK FROM HOLE-TO-HOLE, AFT ROW. INSTALLED DOUBLER PER FEDEX EA 7-5510-25773 DATED 9-15-95. PAINTED ALL AREAS EFFECTED FOR WATER-TIGHT SEAL.

Part: AFT TRUNNION — DAMAGED (FS 740)

LEFT WING FRONT SPAR FORWARD TERMINAL PIN JOINT HOLE CRACKED AFT FORWARD. LEVELED AND SHORED A/C IAW SRM 51-50-1. CUT LOWER CHORD ANGLE AND WEB IAW BOEING DWG 65C29064. REMOVED FS 740 AFT TRUNNION AND REPLACED WITH NEW AFT TRUNNION. SPLICED WEB AND LOWER CHORD ANGLE IAW BOEING DWG 65C29064.

Part: FLOOR — DAMAGED (BS 344)

UNAUTHORIZED REPAIR INSTALL ON FLOOR, BS 344 LBL 38. REMOVED AND REPLACED REPAIR PER DRAWING NR SR27-53-007, NR O857.

Part: FLOORBEAM — CORRODED (BS 400)

CORROSION ON MAIN CABIN FLOORBEAM STA 400 AT LBL 35.

Part: SKIN — DAMAGED (BS 1138)

HOLE IN STR 9R AND CRACKED AT STA 1138, CUT OUT DAMAGED PART OF STR 9R AND FUSE SKIN THAT WAS DAMAGED ALONG WITH STR. INSTALLED FLUSH DOUBLER AND STR REPAIR PER 53-30-8. ARRIVED IN TUL IN THIS CONDITION.

Part: SKIN — CORRODED (BS 440)

OUTSIDE FUSELAGE STA 440 STR 17R THERE IS A BULGE IN THE SKIN NR 00073. LFEC SHOWS CORROSION IN EXCESS OF 20 PERCENT MATERIAL LOSS. REMOVED CORROSION AND FABRICATED DOUBLER PER SRM 53-30-3.

Part: SKIN — DAMAGED (FUSELAGE)

STR 9R HAD HOLE AND CRACK AND ONE FAST HOLE WITH EXISTING MISDRILL CAUSED DAMAGE IN FUSELAGE SKIN (A/C CAME IN WITH THIS COND). STR DAMAGE AND FUSELAGE SKIN DAMAGE WAS CUT OUT AND STR SPLICE 9 .050 INCH DOUBLER ON SKIN WAS INSTALLED, PER SRM 53-30-3, FIG 9, NR 0224.

Part: CASTING — CORRODED (CARGO DOOR)

CORROSION ON MAIN CARGO DOOR CASTING, 7 PLACES LOCATED BETWEEN 6TH AND 7TH LATCHES.