N125FE

Part: WARNING MESSAGE — ILLUMINATED (ZONE 800) · airframe 19,796 hrs · 7,109 cycles

ENROUTE MAIN CARGO DOOR LIGHT ILLUMINATED. ON DESCENT PASSING 22K, LIGHT WENT OUT. RELEASED FOR SERVICE PER MEL : 52-71-01-02 CATEGORY : C. MAIN DECK CARGO DOOR INDICATION SYSTEM - INOP. VERIFY AND RECORD IN AML/EAML THAT MAIN DECK CARGO DOOR IS CLOSED, LATCHED, AND LOCKED BEFORE EACH DEPARTURE. PERFORMED OPS CHECK IAW AMM: 52-32-00-2, LOCK AND LOCK INDICATION OPERATES CORRECTLY. PERFORMED T/S IAW FIM: 52-71 FT 809 AND PSEU BITE IAW FIM:32-09 FT 803. NO FAULT FOUND. ACFT OK FOR SERVICE.

Part: ESCAPE ROPE — DISLODGED (ZONE 200) · airframe 19,613 hrs · 7,052 cycles

ESCAPE ROPE FROM MAIN ENTRY DOOR DISLODGED FROM FRAME AMM 25 61-02-2 ESCAPE ROPE REPOSITIONED IN YOUR PLACE A/C OK FOR SVC.

Part: SLAT SYSTEM — MALFUNCTIONED · airframe 19,274 hrs · 6,947 cycles

LE SLAT DISAG ON RAISING FLAPS FROM 1 TO UP. RAN QRH. DECLARED EMERGENCY, UPON ARRIVAL. RECONFIGURED SLAT/FLAP SYS TO NORMAL OPS IAW MM 27-81-00-5. PERFORMED FSEU BITETEST IAW FIM 27-51 FT 809, FAULT HISTORY SHOWED: - LEG 0 : TE FLAPS MAINT MSG 27-51104 , LE PERFORMED PSEU BITE IAW MM 31-70-04-4-99, NO BITE RECORDED FOR THE LAST 10 FLTS, IAW AHM CHECKED FLAP LEVER RDVT POSITION IAW MM 27-51-26-4. ALL CHKD OK IAW MM, RDVT 2 IS SLIGHTLY FLUCTUATING, STAYED WITHIN LIMIT RANGE (/- 0.006) OPS SLATS & FLAPS IAW MM 27-81-00-5, NO DISAGREE NOTICED & ALL CHKD NORMAL. NO HISTORY, ACFT OK TO CONTINUE

Part: FITTING — CRACKED (ZONE 200) · airframe 17,991 hrs · 6,497 cycles

MAIN CARGO COMPARTMENT BETWEEN STA 977/999 AND RBL 11/33 FLOOR FITTING BROKEN. MAIN CARGO COMPARTMENT BTWN STA 977/999 AND RBL 11/33 FLOOR FITTING WAS REPLACED IAW E.A H-2550-T0380216

Part: SKIN — BURNED (ZONE 600 AILERON) · airframe 17,991 hrs · 6,497 cycles

RH WING, OUTBOARD AILERON BETWEEN WBL 910 AND WBL 890 WITH TWO LIGHTNING STRIKE. RH WING, OUTBOARD AILERON BTW WBL 910 AND WBL 890 WAS REPAIRED IAW B767 SRM 57-60- 02-2R PAG 1 AND SRM 51-70-14-0G REP 11 PAG 17-18 REV 89 APR 15/2024

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 17,991 hrs · 6,497 cycles

MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 241WFF WITH A PUNCTURE. MAIN DECK CARGO, FLOOR PANEL 241WFF WAS REPAIRED I.A.W. B767 SRM 53-00-50-2R PAR 4.B FIG. 201 SHEET 2 REV. 89 APR 15/2024.

Part: SKIN — DENTED (NR 11 SLAT) · airframe 17,991 hrs · 6,497 cycles

SLAT 11, EXTERNAL SURFACE, UPPER WEDGE WITH DENT NEXT TO INB FRAME. SLAT 11, EXTERNAL SURFACE, UPPER WEDGE WITH DENT NEXT TO INB FRAME WAS REPAIRED IAW B767 SRM 57-43-02-2R REP 1 PAG 1-2 AND SRM 51-70-10-2R REPAIR 4 PAG 150-151 FIG 201 (SHEET 1) REV 89 APR 15/2024

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 17,991 hrs · 6,497 cycles

MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 251KFF WITH SEVERAL DENTS. MAIN DECK CARGO, FLOOR PANEL 251KFF WAS REPAIRED I.A.W. B767 SRM 53-00-50-2R PAR. 4.B FIG. 201 SHEET 2 REV. 89 APR 15/2023.

Part: FORMER — FAILED (UNKNOWN) · airframe 15,799 hrs · 5,746 cycles

NOSE FORMER ANGLE CRACKED AT THE RIGHT WING OSS 499.6. PER EA H-5720-T0367172 REV A VISUALLY INSPECTED FORMER AT FLE OSS 499.603 AND REPLACED FOMRER WITH ANGLE USING FEDEX DRW B67-57-002 / AND -003 REV F WITH SRM TR 57-111 AS REFERENCE.

Part: FORMER — FAILED (UNKNOWN) · airframe 15,799 hrs · 5,746 cycles

NOSE FORMER ANGLE CRACKED AT RIGHT WING OSS 565. VISUALLY INSPECTED FORMER AT FLE OSS 565 AND REPLACED FOMRER WITH ANGLE USING FEDEX DRW B67-57-002 / AND -003 REV F & A WITH SRM TR 57-111 AS REFERENCE.

Part: SKIN — WORN (LT NR 5 SLAT) · airframe 14,437 hrs · 5,297 cycles

LEFT WING OUTBOARD SLAT NO 5 TRAILING EDGE WITH WEAR (LOWER SURFACE). LEFT WING OUTBOARD SLAT NO 5 TRAILING EDGE WEDGE WAS REPAIRED IAW SRM 51-70-10-2R REPAIR 4 FIG. 202 SHEET 8 AND SRM 57-43-02-2R REP. 1 FIG. 201 PAG. 1-2 REV. 84 15-AUG-2022

Part: SKIN — WORN (RT NR 8 SLAT) · airframe 14,437 hrs · 5,297 cycles

RH WING SLAT #8 INNER SKIN WEDGE AREA TWO PREVIUS REPAIR WITH WEAR. RH WING SLAT #8 T/E WEDGE INNER SKIN, ONE PREVIOUS REPAIR WAS REPLACED AND ONE FILLER WAS REPLACED IAW B767 SRM 57-43-02-2R REP. 1 FIG. 201 PAG. 1-2 AND SRM 51-70-10-2R REP. 4 PAG. 10, 11, 98, 99, 100, 101, 150, 163, 164 FIG. 202 REV. 84 15 AUG 22

Part: WEDGE — CHAFED (RT WING SLAT) · airframe 9,259 hrs · 3,752 cycles

RW #8 SLAT TE GOUGED TWO PLACES REPAIRED #8 SLAT TRAILING EDGE WEDGE AT TWO EACH LOCATIONS BY BONDING REPAIR IAW B767 SRM 57-43-02-0I, 57-43-02-2R REPAIR 1 AND 51-70-10 REPAIR GENERAL REFINISHED REPAIR IAW B767AMM 51-21-04 AND 51-24-21. SEALED DOUBLERS IAW B767 SRM 51-20-05. PAINTED IAW B767 AMM 51-24-13 AND 51-21-01

Part: SLAT — CHAFED (ZONE 600) · airframe 9,259 hrs · 3,752 cycles

RW #8 SLAT TE GOUGED TWO PLACES REPAIRED #8 SLAT TRAILING EDGE WEDGE AT TWO EACH LOCATIONS BY BONDING REPAIR IAW B767 SRM 57-43-02-0I, 57-43-02-2R REPAIR 1 AND 51-70-10 REPAIR GENERAL REFINISHED REPAIR IAW B767AMM 51-21-04 AND 51-24-21. SEALED DOUBLERS IAW B767 SRM 51-20-05. PAINTED IAW B767 AMM 51-24-13 AND 51-21-01

Part: WEDGE — GOUGED (LE SLAT) · airframe 9,259 hrs · 3,752 cycles

RT WING NR 8 SLAT TE GOUGED TWO PLACES. REPAIRED NR 8 SLAT TRAILING EDGE WEDGE AT TWO EACH LOCATIONS BY BONDING REPAIR IAW SRM 57-43-02-0I, 57-43-02-2R REPAIR 1 AND 51-70-10 REPAIR GENERAL REFINISHED. REPAIR IAW AMM 51-21-04 AND 51-24-21. SEALED DOUBLERS IAW SRM 51-20-05. PAINTED IAW AMM 51-24-13 AND 51-21-01.

Part: BRAKE — DAMAGED (NR 8) · airframe 8,057 hrs · 3,316 cycles

PDIS 125 32-43 4006 12NOV19 CDG OPEN U LOGPAGES:2841209 ON LANDING ROLLOUT APPLIED BRAKES MANUALLY FELT VIBRATION. ON SHUTDOWN BRAKE TEMP LIGHT IS ON BRAKE TEMPS 4435 WITH LIGHT BRAKING SHGN 12NOV19 20:11 CDG U UPON CAPTAIN'S FEEDBACK DECIDED TO CHECK FOR HISTORY AND FOUND SAME WRITE UP FROM THE 8TH OF NOVEMBER. ON VISUAL OUTSIDE INSPECTION WE HAD NO FINDINGS BUT DUE TO PREVIOUS HISTORY WE DECIDED TO REMOVE THE WHEEL AS PER AMM 32_41_08_4_4. AFTER REMOVING THE WHEEL FOUND BRAKE THRUST PLATE RUBING ON THE INNER SIDE OF THE WHEEL AS WELL AS THE BRAKE INNER HEAT SHIELD BROKEN LOOSE. BRAKE ASSY REMOVED FOR FURTHER INSPECTION AS PER AMM 32_41_08_4_4 AND FOUND BRAKE ASSY INNER OUTBOARD BEARING LOOSE. ALL PARTS THOUROGLY CLEANED FOR INSPECTION AND AXLE SLEEVE INSPECTED AS PER AMM 32-11-26-6 AND ALL FOUND TO BE IN GOOD CONDITION. R/RD OF BRAKE ASSEMBLY #8 DONE IAW AMM 32-41-08-4-4 TEST OK

Part: SENSOR — FOD (CARGO DOOR) · airframe 5,572 hrs · 2,342 cycles

1.25 HOURS INTO FLIGHT, RECEIVED A MAIN CARGO EICAS. COMPLIED WITH QRH. INDICATOR WENT OUT. DECENDING THRU FL220. PRESSURIZATION NORMAL THOUGHOUT. FOUND DEBRIS ON THE SENSOR TARGET S892. REMOVED THE DEBRIS. INSPECTION CHECKED GOOD. PERFORMED PSEU BITE, ALL MAIN CARGO DOOR SYSTEM TESTS GOOD. NO FAULTS, NO STATUS MESSAGE, ANNUNCIATOR LIGHT TESTED GOOD IAW FIM 32-09, FT 809. OKAY FOR SERVICE.

Part: SMOKE BARRIER — DAMAGED (CREW REST) · airframe 5,439 hrs · 2,275 cycles

CREW REST SMOKE CURTAIN HAS HOLE IN IN LEFT PLASTIC WINDOW. INSTALLED NEW CURTAIN PER IPC 26-29-01-01.

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 1,769 hrs · 788 cycles

FLAPS STOPPED BETWEEN 20 AND 25 FLAPS ON INITIAL CONFIGURATION FOR LANDING WITH T/E FLAP DISAGREE. COMPLIED WITH QRH FOR REF FLAP 20 LANDING. VERIFIED OVERLOAD TRIP INDICATORS ON LT & RT WINGS AND VERIFIED FLAP TRANSMITTERS TO BE GOOD FOR SERVICE. PERFORMED FSEU BITE PROCEDURE, NO FAULTS FOUND. REF FIM 27-51/810. R & R FSEU AS PRECAUTION. REF AMM 27-51-01-4, VERIFIED ALL TRANSMITTER VALUES ARE WITHIN LIMITS. REF 27-51-45-2, FLAP SYS OPS IS GOOD, ACFT OK FOR SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · 8 cycles

AT FL 360 GOT A CABIN ALTITUDE MASTER WARNING. CABIN WAS SHOWING JUST OVER 10,000 FT WITH A 200 FT PER MIN CLIMB. WE WENT TO AUTO 2 BUT CABIN CONTINUED TO CLIMB, COMPLIED WITH QRH. ON DESCENT WE TRIED MANUAL & WERE ABLE TO CONTROL THE CABIN ALTITUDE. TROUBLESHOOTING IAW FIM 21-31 FAULT TREE 803 BITE. CHECKED LT & RT AUTOMATIC PRESS CONTROLLERS, BOTH CONTROLLERS SHOWED AC POWER OFF ON LAST FLIGHT. BITE & PRESS TEST ON LT & RT CONTROLLERS SHOWED NO INFLOW ON PREVIOUS FLIGHT. CONTROLLERS TEST NORMAL WITH NO CURRENT FAULTS. CABIN PRESS CONTROL SYS ADJUSTMENT & TEST IAW AMM 21-31-00-5, SATISFACTORY. AWAITING PARTS. R & R CABIN PRESS SELECTOR IAW AMM 21-31-01-4. OPERATIONS CHECKED GOOD. R & R AUTOMATIC CABIN PRESS CONTROLLER NR 1 IAW AMM 21-31-02-4. R & R CABIN PRESS OUTFLOW VLV IAW AMM 21-31-03-2. ACCOMPLISHED CABIN CONTROL SYS ADJUSTMENT & TEST IAW AMM 21-31-00-5. OK FOR SERVICE.