N110FE

Part: SKIN — PUNCTURED (NR 7 SLAT) · airframe 13,675 hrs · 7,082 cycles

RH WING NO.7 SLAT MID SECTION LOW SURFACE FOUND PUNCTURE, AS MARKED REPAIRED THE RH WING NO.7 SLAT MID SECTION LOW SURFACE PER B767 SRM57-43-02-2R REPAIR 1 & SRM51-70-10-2R REPAIR 4. THIS IS CAT A REPAIR. RSC TRACKING EA: H-5750-T0380979 P1 ISSUED AND COMPLETED, TITLE: WINGS - FLIGHT SURFACES - RH WING #7 SLAT TRAILING EDGE WEDGE REPAIR - RSC TRACKING. MAJOR REPAIR IAW FEDEX GMM6-2-100. SEE WRI 5750/0545 FOR WORK DETAILS.

Part: STRINGER — DAMAGED (ZONE 200) · airframe 13,675 hrs · 7,082 cycles

FUSELAGE FRAME STA1502 - STRINGER CLIP AND S-20L STRINGER 1EA FASTENER HOLE ENLARGED REPAIRED THE DISCREPANT(ENLARGED) HOLE AT FUSELAGE FRAME STA1502 - STRINGER CLIP AND S-20L STRINGER PER EA H-5310-T0380977 P1. TITLE: FUSELAGE - MAINFRAME - MISS-DRILLED FASTENER HOLE AT STA1502, S-20L STRINGER*THIS EA DEVIATES FROM EO H-5310-E0365800. THIS IS CAT A REPAIR, MAJOR REPAIR IAW FEDEX GMM6-2-100. SEE WRI 5310/0547 FOR WORK DETAILS.

Part: SKIN — DAMAGED (BS 157) · airframe 13,666 hrs · 7,081 cycles

LOWER FUSELAGE SKIN DAMAGED AT APPROX. STATION 157. FUSELAGE SKIN REPAIRED IAW FED-RE-2403203

Part: SKIN — DAMAGED (E/E BAY DOOR) · airframe 13,666 hrs · 7,081 cycles

E&E BAY DOOR AND SURROUNDING STRUCTURE DAMAGED. E&E BAY DOOR REPLACE AND SURROUNDING STUCTURES REPAIRED UNDER FED-RE-2403203 REM 97-2.

Part: ACTUATOR — FAILED (NLG) · airframe 13,666 hrs · 7,081 cycles

NLG FAILED TO EXTEND, UPON LANDING ACFT REMAINED ON CENTERLINE OF RUNWAY SURFACE. REF E.A H-5310-T0380090 P1 WORKED IN CONJUSCTION WITH 53-10/0463 COMPLETED INSTALLATION OF NOSE LANDING GEAR RETRACT ACUATOR REF B767 AMM 32-34-01-4 OPS AND LEAK CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 13,288 hrs · 6,882 cycles

WEIGHT CHECK DUE FOR THE FLIGHT DECK PORTABLE FIRE EXTINGUISHER MOUNTED IN FRONT OF RAFT STOWAGE. GMM: 9-4-404 AMM: 26-26-02-4-1 COMPLETED WEIGHT CHECK PROCEDURE PER ABOVE REFS. OK FOR SERVICE.

Part: FLAP — DAMAGED (ZONE 500) · airframe 13,091 hrs · 6,747 cycles

LH WING, INBOARD AFT FLAP LOWER SURFACE RH SIDE WITH PUNCTURE LH WING INBOARD AFT FLAP LOWER SURFACE, RH SIDE WAS REPAIRED IAW B767 SRM 57-53-01- 2R FIG 201 TABLE 1 PAG 1,4,5 AND SRM 51-70-03-0G PAR 5B FIG 15 SHEET 4 PAG 19,20,51. REV 87 AUG 15/2023

Part: ELT — UNKNOWN (UNKNOWN) · airframe 12,667 hrs · 6,386 cycles

ELT HAS BEEN DETECTED EMITTING DURING FLIGHT. FOR INFO: IST STATION LOCAL TOWER WARNED US FOR ELT SIGNAL. RELEASED FOR SERVICE PER MEL : 25-63-10-02-A ON ARRIVAL ELT SWITCH (GUARDED) THAT IN THE OVERHEAD PANEL FOUND ARM POSITION. YESTERDAY HAPPENED ONE MORE TIME AND IST LOCAL TOWER WARNED ABOUT SAME ISSUE. FOR PRECAUTIONARY MEL APPLIED. ELECTRICAL CONNECTOR REMOVED AND STOWED. ON THE ELT TRANSMITTER, TOGGLE SWITCH SELECTED TO OFF POSITIONAS PER MEL C/7361233 REMOVED AND REPLACED FIXED ELT PER MM 23-24-01-2, PERFORMED OPERATIOAL AND SYSEM TESTS PER MM 23-24-00-5. ALL TESTS PASSED.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 12,142 hrs · 5,958 cycles

LEFT WING OUT BOARD TRAILING EDGE FLAP WITH DENT (LOWER SURFACE) LEFT WING OUTBOARD FLAP T/E, LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-53-01-2R PAG. 1-7 AND B767 SRM 51-70-03-0G PARAG. 5.A.(1) FIG. 5 PAG. 19, 36 REV. 82 DEC 15/2021

Part: WEDGE — DENTED (RT WING SLAT) · airframe 12,142 hrs · 5,958 cycles

LEFT WING SLAT NO. 6 TRAILING EDGE WEDGE WITH DENT. RH WING SLAT #6 TRAILING EDGE WEDGE UPPER SURFACE AT POSITION ISS 231-236 SKIN WAS REPAIRED IAW SRM 51-70-10-2R REP. 4 PAG. 143-154 FIG. 201, SRM 57-43-02-2R FIG. 201 PAG. 1-2 REV. 82 DEC15/2021

Part: FIRE BOTTLE — FAILED (APU) · airframe 12,018 hrs · 5,869 cycles

MDIS 110 26-11 8313 16AUG22 MXP OPEN U APU FIRE EXT. BOTTLE DISCHARGE LIGHT ILLUMINATED. MEL 16AUG22 15:22 MXP U RELEASED FOR SERVICE PER MEL : 26-22-01-B CATEGORY : B EXPIRATION : 19AUG22 "MEL 26-22-01-B: APU FIRE EXTINGUISHER - INOP. APU - INOP. REFER TO THE OPERATIONS NOTE FOR DRY ICE REST RICTIONS." THIS FLIGHT MUST REMAIN WITHIN 120 MINUTES OF LANDING AT A SUITABLE AIRPORT. DUE TO A/C DEPARTURE NO TIME FOR T/S. APU EXT SYS INOP, A/C RELEASED I.A.W MEL 26-22-001-B. A/C OK FOR SERVICE. C/7329270 FACT 17AUG22 09:34 CDG REPLACED AND TEST OK APU FIRE EXTINGUISHER BOTTLE/DISCHARGE CARTRIGE PER AMM 26-22-02-04. MEL CLOSED.

Part: INSERT — FAILED (ZONE 700) · airframe 11,820 hrs · 5,668 cycles

FOUND RH MLG FWD DOOR STOP FASTENERS TO BE LOOSE AND SHIM FASTENER HOLES TO BE ELONGATED. REMOVED INSERTS FROM RH MLG FWD DOOR STOP AND REPLACED FASTENERS REF E.A. TH- 3212-T0368483P1 AND REPLACED SHIMS REF 767 SRM 51-20-11 AND 51-20-12.

Part: INSERT — FAILED (MLG DOOR) · airframe 11,820 hrs · 5,668 cycles

FOUND LH MLG FWD DOOR STOP FASTENERS TO BE LOOSE AND SHIMS TO HAVE MIGRATED. REMOVED INSERTS FROM LH MLG FWD DOOR STOP AND REPLACED FASTENERS REF E.A. TH- 3212-T0368483P1 AND REPLACED SHIMS REF 767 SRM 51-20-11 AND 51-20-12.

Part: NONE — NONE (N/A) · airframe 11,399 hrs · 5,293 cycles

MDIS 110 33-50 7324 24NOV21 CDG FACT U EMERGENCY LIGHT GUARD IS BROKEN . FACT 24NOV21 03:19 CDG U R&R'D EMERGENCY LIGHT GUARD PER MM:33-51-08-4 , OPS CHK OK .

Part: ENGINE — OVERTEMP (LEFT) · airframe 10,866 hrs · 4,835 cycles

STARTED DESCENT FROM FL 310, THE OIL TEMP SPIKED UP TO 165 ON THE LT ENGINE. THROTTLE WAS PULLED TO IDLE, & CHECKLIST RUN FOR HIGH OIL TEMP, LT ENGINE. OIL QUANTITY INDICATED 0 (ZERO). AFTER 7 MINUTES OIL TEMP REDUCED BELOW AMBER BAND. ENGINE REMAINED AT IDLE, IAW CHECKLIST, UNTIL SHUTDOWN ON LANDING ROLL. A FLAPS 25 LANDING WAS PERFORMED, NO REVERSE, BRAKES 3. BRAKE TEMPS ON TAXI IN REMAINED LOW. NORMAL TAXI IN WAS ACCOMPLISHED ON ONE ENGINE. UPON BLOCK-IN ENGINE OIL QTY REMAINED REMAINED AT 0. REMOVED #1 ENGINE IAW ETOPS. REMOVE BOOTSTRAP WORK CARD 7100000-01-03, REV 14. REPLACED NR 1 ENGINE IAW ETOPS NR 1 ENGINE INSTALL BOOTSTRAP WORK CARD 7100000-01-04 REV11. A/C OK FOR SERVICE

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 10,463 hrs · 4,585 cycles

MAIN CABIN FLOOR PANEL 241YFA MISSING EDGE FILLER AT LBL 54. FABRICATED NEW FLOOR PANEL 241YFA, IAW FEDEX DWG SRZ-25-005 REV C.

Part: FLOOR SUPPORT — CRACKED (AFT CARGO BAY) · airframe 10,463 hrs · 4,585 cycles

LT AFT FUSELAGE, AFT CARGO BS 1576 LBL 78, MAIN CARGO DECK FLOOR SUPPORT CRACKED. REMOVED AND REPLACED THE LEFT AFT FUSELAGE MAIN CARGO DECK FLOOR SUPPORT SPLICE ANGLE AT STA 1576 AND LBL 78, IAW BAC DWG 146T5650, REV C AND B767 SRM 51-40-02-0G.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 10,463 hrs · 4,585 cycles

MAIN CABIN FLOOR PANEL 242TFA IS PUNCTURED TWO PLACES. FABRICATED NEW FLOOR PANEL 242TFA, IAW FEDEX DWG SRZ-25-005, REV R.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 10,463 hrs · 4,585 cycles

MAIN CABIN FLOOR PANEL 241ZFF HAS CRUSH AND DELAM DAMAGE, SEVERAL AREAS ALONG THE ENTIRE LENGTH. FABRICATED NEW FLOOR PANEL 241ZFF, IAW FEDEX DWG SRZ-25-005, REV R.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 10,463 hrs · 4,585 cycles

MAIN CABIN FLOOR PANEL 242SFF HAS SEVERAL AREAS OF DELAMINATION AND CRUSH DAMAGE AROUND FLOOR FITTING CUTOUTS. FABRICATED NEW FLOOR PANEL 241SFF, IAW FEDEX DWG SRZ-25-005, REV R.

Part: FLOOR SUPPORT — CRACKED (AFT CARGO BAY) · airframe 10,463 hrs · 4,585 cycles

RT AFT FUSELAGE, AFT CARGO BS 1576 RBL 78, MAIN CARGO DECK FLOOR SUPPORT CRACKED. REMOVED AND REPLACED THE RIGHT AFT FUSELAGE MAIN CARGO DECK FLOOR SUPPORT SPLICE ANGLE AT STA 1576 AND RBL 78, IAW BAC DWG 146T5650, REV C AND B767 SRM 51-40-02-0G.

Part: SKIN — CHAFED (RT WING SLAT 9) · airframe 10,463 hrs · 4,585 cycles

RIGHT WING NR 9 SLAT LOWER TRAILING EDGE WEDGE SKIN CHAFED. REPAIRED NR 9 SLAT RIGHT WING LOWER TRAILING EDGE WEDGE 33.75" FROM INBOARD END BY BONDING FILLER SKIN, INTERNAL DOUBLER, CORE, FIBERGLASS WEDGE AND EXTERNAL DOUBLER, IAW B767 SRM: 57-43-02-2R REPAIR 1 FIG 201 AND 57-43-02-0I AND 51-70-10 REPAIR GENERAL AND 51-70-10 REPAIR 4 PARA 3 FIG 202. APPLIED FINISH, IAW B767 AMM 51-21-04-7 AND 51-21-10. APPLIED FILLET SEAL TO REPAIR DOUBLER, IAW B767 SRM 51-20-05-0G. MAJOR REPAIR.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 10,463 hrs · 4,585 cycles

MAIN CABIN FLOOR PANEL 241JFF HAS CRUSH AND DELAMINATION DAMAGE ALONG THE LBL 55 SIDE, ENTIRE LENGTH. FABRICATED NEW MAIN CABIN FLOOR PANEL 241JFF, IAW FEDEX DWG SRZ-25-005, REV R.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 10,463 hrs · 4,585 cycles

MAIN CABIN FLOOR PANEL 241WFF HAS THREE SEPARATE AREAS OF DAMAGE. REPAIRED 3 EA DAMAGE AREAS ON FLOOR PANEL 241WFF, IAW B767 SRM 53-00-50-2R, PARA 4C.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 10,463 hrs · 4,585 cycles

MAIN CABIN FLOOR PANEL 241NFF HAS BROKEN INSERTS AND DELAMINATION DAMAGE ALONG THE FORWARD EDGE. FABRICATED NEW MAIN CABIN FLOOR PANEL 241NFF, IAW FEDEX DWG SRZ-25-005 REV R.

Part: BEAM — DAMAGED (NR 2 NACELLE) · airframe 10,463 hrs · 4,585 cycles

NR 2 PYLON INBOARD SKIRT BEAM FWD FLANGE HAS ELONGATED HOLES. REPAIRED ELONGATED HOLES ON NR 2 PYLON INBOARD SKIRT BEAM FWD FLANGE, IAW FEDEX EA H-5450-T0358609-P1.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 10,463 hrs · 4,585 cycles

MAIN CABIN FLOOR PANEL 241HFF HAS MISSING EDGE FILLER SEVERAL AREAS. REPAIRED EDGE FILLER ON FLOOR PANEL 241HFF, IAW B767 SRM 53-00-50-2R PARA 4G (2).

Part: ANGLE — CRACKED (FLOORBEAM) · airframe 10,463 hrs · 4,585 cycles

FWD LT FRAME STA 246 LBL 50 BELOW FLOOR INTERCOSTAL ANGLE CRACKED. REMOVED AND REPLACED ANGLE P/N 141T5146-16, IAW B767 SRM 51-40-02 AND BAC DWG 141T5600 REV-.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 10,463 hrs · 4,585 cycles

MAIN CABIN FLOOR PANEL 241LFF PUNCTURED TWO PLACES AND HAS MISSING EDGE FILLER. REPAIRED DAMAGES TO FLOOR PANEL 241LFF, IAW B767 SRM 53-00-50-2R, PARA 4C AND 4G (2).

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 10,463 hrs · 4,585 cycles

MAIN CABIN FLOOR PANEL 242BFA IS PUNCTURED TWO PLACES. REPAIRED DAMAGES TO FLOOR PANEL 242BFA, IAW B767 SRM 53-00-50-2R, PARA 4C.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 10,463 hrs · 4,585 cycles

MAIN CABIN FLOOR PANEL 242HFF IS PUNCTURED, MARKED. REPAIRED FLOOR PANEL 242HFF, IAW B767 SRM 53-00-50-2R, PARA 4C.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 10,463 hrs · 4,585 cycles

MAIN CABIN FLOOR PANEL 241KFF IS DAMAGED AT 3 SEPARATE AREAS, MARKED. REPAIRED 3 EA DAMAGES ON FLOOR PANEL 241KFF, IAW B767 SRM 53-00-50-2R, PARA 4C AND 4D.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 10,463 hrs · 4,585 cycles

MAIN CABIN FLOOR PANEL 242VFF HAS A PUNCTURE. REPAIRED FLOOR PANEL 242VFF, IAW B767 SRM 53-00-50-2R, PARA 4D.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 10,463 hrs · 4,585 cycles

MAIN CABIN FLOOR PANEL 241QFF HAS PUNCTURE DAMAGE, MARKED. REPAIRED FLOOR PANEL 241QFF, IAW B767 SRM 53-00-50-2R, PARA 4D.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 10,463 hrs · 4,585 cycles

MAIN CABIN FLOOR PANEL 241FFF PUNCTURED THREE PLACES. REPAIRED DAMAGES TO FLOOR PANEL 241FFF, IAW B767 SRM 53-00-50-2R, PARA 4D AND 4E.

Part: DRIVE UNIT — MALFUNCTIONED (WX RADAR) · airframe 10,139 hrs · 4,333 cycles

WX FAIL ON EITHER SELECTED ON LT OR RT CTR CONTROL PANEL ON CENTER PEDESTAL. WINDSHEAR SYS EICAS LT WAS ALSO PRESENT DURING ENROUTE PHASE OF FLIGHT. R & R THE WEATHER RADAR ANTENNA DRIVE UNIT IAW AMM 34-43-05-47. A/C OK FOR SERVICE

Part: LAMP — INOPERATIVE (MLG INDICATOR) · airframe 6,691 hrs · 2,603 cycles

DURING APPROACH, THE LEFT LANDING GEAR LIGHT DID NOT ILLUMINATE. ACCOMPLISHED GO AROUND, QRH AND MOCC/GOC. GEAR CYCLED, DID NOT HELP. NO SECONDARY OR TERTIARY WARNING. NO EICAS WARNINGS. LANDING UNEVENTFUL. REPLACED THE LAMP IN THE INDICATOR IAW AMM 33-16-02-2. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 5,434 hrs · 2,126 cycles

INCOMING DISCREPANCY WRI 53-21/2521, AFT PIT FLOOR PANEL STA 1197 DAMAGED. REMOVED AND REPLACED FLOOR BOARD ON WORK ORDER 00069928 SEQ 000807.

Part: FLOORBOARD — GOUGED (ZONE 100) · airframe 5,434 hrs · 2,126 cycles

IN LOWER AFT CARGO FOUND DAMAGE ON CARGO FLOOR BOARD AT STATION 1197 70 MEASURING 3 1/2" LONG X 3/4" WIDE. REMOVED DAMAGED AFT PIT FLOORBOARD PER SRM 51-40-02-06. FABRICATED NEW PANEL ON T17/1299248 PER SRZ-25-005. MAJOR REPAIR CAT A. INSTALLED FLOOR PANEL PER SRM 51-40-02-006.

Part: FLOORBOARD — CRACKED (ZONE 200) · airframe 5,434 hrs · 2,126 cycles

FLOORBOARD 145T5876-94 CRACKED EDGES. FABRICATED FLOORBOARD 242FF 145T5876-94 ON T17/1299306 PER SRZ-25-005 REV M MAJOR REPAIR CAT A.

Part: FLOOR PANEL — GOUGED (ZONE 100) · airframe 5,434 hrs · 2,126 cycles

LOAD CREW REPORTS A GOUGE IN THE FIBERGLASS FLOOR PANEL OF THE AFT PIT AT STA 1197, ON THE OUTBOARD EDGE OF THE RIGHT SIDE PANEL. GOUGE IS APPROX 1 INCH LONG AND LESS THAN ONE INCH ACROSS. REMOVED DAMAGED FLOOR PANEL PER SRM 51-40-02-06. FABRICATED NEW PANEL ON T17/1299249 PER SRZ-25-005. MAJOR REPAIR CAT A. INSTALLED FLOOR PANEL PER SRM 51-40-02-06.

Part: LATCH — DAMAGED (ZONE 200) · airframe 3,055 hrs · 1,185 cycles

ON PREFLIGHT, FOUND LATCH HANDLE ON EMERGENCY RAFT LOCKER JAMMED, PREVENTING ACCESS. COMPLIED WITH EA H-2560-T0326232 REV NO A POS P3, R&R THE LATCH ON THE LIFE RAFT STORAGE COVER PER SMP.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19 hrs · 746 cycles

FUSELAGE MOUNTED EMER EXIT LIGHT INOPERATIVE. RELAMPED FUSELAGE MOUNTED EMER EXIT LIGHT. OPERATIONS CHECKED OK.