N854FD

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 52,311 hrs · 8,401 cycles

PRE-FLT MX INSP, GALLEY OVRHD (1EA) EMERGENCY LT INOP. AMM: 33-50-00-2 RELAMPED, REF B777 AMM: 33-50-00-2. EMERGENCY LT'S TEST SATIS, ITEM OK FOR SVC.

Part: NONE — UNKNOWN (N/A) · airframe 44,500 hrs · 7,050 cycles

PDIS 854 28-41 2132 08DEC21 ANC APPROX 2.5 HRS INTO FLT HAD FUEL IMBALANCE ON EICAS. AS WE RAN ECL WE NOTICED DISCREPANCIES IN TOTALIZER FUEL AND CALCULATED FUEL ON PROG P.2. THESE 2 ITEMS LED US TO RUN FUEL DISAGREE AND FUEL LEAK CHECKLISTS. AFTER ALL THIS AND CONSULTING WITH GOC, MOCC, JOHN HUNT AND DON ULSH IT WAS DECIDED TO DIVERT TO PANC. FACT 08DEC21 20:05 ANC CHECKED EXISTING FAULTS IN MAT , NOTED ONE INTERMITTENT FAULT FQPU MAINTENANCE MSG 28-20200. NO EXISTING RELATED FAULTS. CW FIM TASK 28-4100-810-824. R&R FQPU IAW M/M 28_41_01_4_0 . SOFTWARE CHK SATIS. ADJ/TEST OF FUEL QTY SATIS., VERIFIED QTY WITH STICKS, OK FOR SVC.

Part: NONE — NONE (N/A) · airframe 43,751 hrs · 6,934 cycles

MDIS 854 05-50 1962 02OCT21 KIX REPORTED FOR CAPTAIN EE# 216581 REF WRI 05-50-1960 KIX RWY 06L WIND 060 AT 5 KT MANUAL LANDING FROM RIGHT SEAT, HIGH SINK RATE LATE FLARE NO SIDE SLIP, NO DRIFT GENTLE NOSE GEAR LANDONG TOUCHDOWN FACT 02OCT21 19:54 KIX REF WRI 05-50-1960 C/W HARD LANDING PHASE 1 INSPECTION AND NO DAMAGE FOUND REF MM 05-51-01-2-2. A/C OK FOR SERVICE.

Part: SKIN — DAMAGED (ZONE 100) · airframe 41,668 hrs · 6,583 cycles

WHILE ACCOMPLISHING RIGHT HAND E.O. #G-5310-E0332629 I P6 FOUND NEW FUSELAGE SKIN DOUBLER (P/N: 143W2314Y406) EXISTING HOLE AT STATION 998 STRINGER S-35 RIGHT NEAR MILLED EDGE. COMPLIED WITH E.A.#: G-5310-T0360143 P2. TITLE: FUSELAGE- MAINFRAME- LEFT HAND AND RIGHT HAND UNDERWING LONGERON MODIFICATION PER E.O. G-5310-E0332629- DEVIATION TO TO SERVICE BULLETINS 777-53-0087 REVISION 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: SPAR — DAMAGED (LT WING) · airframe 41,668 hrs · 6,583 cycles

WHILE PERFORMING LEFT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR REPAIR (SNRM NO. N00486) FOUND 01 EACH EXISTING OVERSIZED HOLE AT LOWER CHORD THROUGH THROUGH WEB STATION 1035 LEFT BUTTOCK LINE 89. LEFT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR (01 EA) EXISTING OVERSIZED HOLE AT LOWER CHORD THROUGH WEB STATION 1035 LEFT BUTTOCK LINE 89. REPAIRED AS PER E.A. # G-5710-T0359861 P1. TITLE: FUSELAGE- MAINFRAME- DEVIATIONS TO SB-777-53-0087 AND SRM 57-10-10 REPAIR 1 Ï¿½ OVERSIZED HOLES ON WING CENTER SECTION FRONT SPAR LOWER CHORD * THIS EA DEVIATES FROM EO- 5310- E0332629 I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (SPECIAL/NON ROUTINE MAINTENANCE FORM #N00486 #N00486 AND #N00519 FOR DETAILS).

Part: SPAR — DAMAGED (LT WING) · airframe 41,668 hrs · 6,583 cycles

WHILE PERFORMING LEFT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR REPAIR (SNRM NO. N00486) FOUND 01 EACH EXISTING OVERSIZED HOLE AT LOWER CHORD STATION STATION 1035 LEFT BUTTOCK LINE 89. LEFT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR (01 EA) EXISTING OVERSIZED HOLE AT LOWER CHORD STATION 1035 LEFT BUTTOCK LINE 89. REPAIRED AS PER E.A. # G-5710-T0359861 P1. TITLE: FUSELAGE- MAINFRAME- DEVIATIONS TO SB-777-53-0087 AND AND SRM 57-10-10 REPAIR 1 Ï¿½ OVERSIZED HOLES ON WING CENTER SECTION FRONT SPAR LOWER LOWER CHORD * THIS EA DEVIATES FROM EO- 5310- E0332629 I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (SPECIAL/NON ROUTINE MAINTENANCE FORM #N00486 AND #N00521 FOR FOR DETAILS).

Part: SPAR — DAMAGED (RT WING) · airframe 41,668 hrs · 6,583 cycles

WHILE PERFORMING RIGHT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR (SNRM NO. N00487) FOUND 01 EACH EXISTING OVERSIZED HOLE AT LOWER CHORD THROUGH WEB STATION 1035 RIGHT BUTTOCK LINE 91.5. RIGHT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR (01 EA) EXISTING OVERSIZED HOLE AT LOWER CHORD THROUGH WEB STATION 1035 RIGHT BUTTOCK LINE 91.5. 91.5. REPAIRED AS PER E.A. # G-5710-T0359861 P1. TITLE: FUSELAGE- MAINFRAME- DEVIATIONS DEVIATIONS TO SB-777-53-0087 AND SRM 57-10-10 REPAIR 1 Ï¿½ OVERSIZED HOLES ON WING CENTER SECTION FRONT SPAR LOWER CHORD * THIS EA DEVIATES FROM EO- 5310- E0332629 I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (SPECIAL/NON ROUTINE MAINTENANCE FORM FORM #N00486, #N00487 AND #N00520 FOR DETAILS).

Part: SKIN — DAMAGED (ZONE 100) · airframe 41,668 hrs · 6,583 cycles

WHILE ACCOMPLISHING LEFT HAND E.O. #G-5310-E0332629 I P5 FOUND NEW FUSELAGE SKIN DOUBLER (P/N: 143W2314Y405) EXISTING HOLE AT STATION 998 STRINGER S-35 LEFT NEAR MILLED EDGE. COMPLIED WITH E.A.#: G-5310-T0360143 P1. TITLE: FUSELAGE-MAINFRAME- LEFT HAND AND RIGHT HAND UNDERWING LONGERON MODIFICATION PER E.O. G-5310-E0332629- DEVIATION TO SERVICE BULLETINS 777-53-0087 REVISION 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100. TO SERVICE BULLETINS 777-53-0087 REVISION 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: SPAR — DAMAGED (RT WING) · airframe 41,668 hrs · 6,583 cycles

WHILE PERFORMING RIGHT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR (SNRM NO. N00487) FOUND 01 EACH EXISTING OVERSIZED HOLE AT LOWER CHORD STATION 1035 RIGHT BUTTOCK LINE 91.5. RIGHT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR (01 EA) EXISTING OVERSIZED HOLE AT LOWER CHORD STATION 1035 RIGHT BUTTOCK LINE 91.5 REPAIRED AS PER E.A. # G-5710-T0359861 P1. TITLE: FUSELAGE- MAINFRAME- DEVIATIONS TO SB-777-53-0087 0087 AND SRM 57-10-10 REPAIR 1 Ï¿½ OVERSIZED HOLES ON WING CENTER SECTION FRONT SPAR SPAR LOWER CHORD * THIS EA DEVIATES FROM EO- 5310- E0332629 I. REPAIR CLASSIFIED AS MAJOR MAJOR PER GMM 6-2-100. SPECIAL/NON ROUTINE MAINTENANCE FORM #N00486, #N00487 AND #N00522 FOR DETAILS).

Part: SKIN — CRACKED (ZONE 100) · airframe 41,668 hrs · 6,583 cycles

DURING ACCOMPLISMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATION AROUND FASTENER HOLE AT STATION 1033 STRINGER 37 LEFT, APPROXIMATELY 0.250 INCHES IN LENGTH. COMPLIED WITH E.O.#: G-5310-E0332629 I P5. TITLE: FUSELAGE-MAINFRAME-INSPECTION AND MODIFICATION OF THE UNDERWING LONGERON AT BODY SYATION 1035- BOEING SERVICE BULLETINS 777-53A0081 AND 777-53-0087. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRUCTURE — CRACKED (BS 1035) · airframe 41,668 hrs · 6,583 cycles

DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT AS PER EO EO NO: E G-5310-E0332629 I P6 ON REMOVED FASTENER HOLES AND FOUND (01 EA) CRACK INDICATION ON RIGHT HAND SIDE VERTICAL FLANGE OF THE FRONT LOWER SPAR CHORD AT BODY STATION 1035 APPROXIMATELY RIGHT BUTTOCK LINE 81.30 LOWER OUTBOARD HOLE. WING CENTER SECTION RIGHT HAND SIDE VERTICAL FLANGE OF FRONT SPAR LOWER CHORD AT UNDERWING LONGERON LOWER WING AT STATION BODY STATION 1035 APPROXIMATELY RIGHT BUTTOCK LINE 81.30 LOWER OUTBOARD HOLE CRACKED REPAIR CARRIED OUT AS PER E.A.#G-5710-T0359861 P1 TITLE: FUSELAGE-MAINFRAME-DEVIATIONS TO SB-777-53-0087 AND SRM 57-10-10 REPAIR 1 Ï¿½ OVERSIZED HOLE ON WING CENTER SECTION FRONT SPAR LOWER CHORD *THIS EA DEVIATES FROM EO-5310-E0332629 I. REPAIR CLASSIFIED AS MAJOR PER GMM GMM 6-2-100. (SPECIAL/NON ROUTINE MAINTENANCE FORM #N00486, #N00522 AND #N00520 FOR FOR DETAILS)

Part: SKIN — CRACKED (ZONE 100) · airframe 41,668 hrs · 6,583 cycles

DURING ACCOMPLISMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND HAND FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATION AROUND AROUND FASTENER HOLE AT STATION 1026 STRINGER 37 RIGHT, APPROXIMATELY 0.500 INCHES IN LENGTH. COMPLIED WITH E.O.#: G-5310-E0332629 I P6. TITLE: FUSELAGE-MAINFRAME-INSPECTION AND MODIFICATION OF THE UNDERWING LONGERON AT BODY SYATION 1035- BOEING SERVICE BULLETINS 777-53A0081 AND 777-53-0087. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRUCTURE — CRACKED (BS 1035) · airframe 41,668 hrs · 6,583 cycles

DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT AS PER EO NO: E G-5310-E0332629 I P5 ON REMOVED FASTENER HOLES AND FOUND (01 EA) CRACK INDICATION ON LEFT HAND SIDE VERTICAL FLANGE OF THE FRONT LOWER SPAR CHORD AT BODY STATION 1035 APPROXIMATELY LEFT BUTTOCK LINE 81.30 LOWER OUTBOARD HOLE. WING CENTER SECTION LEFT HAND SIDE VERTICAL FLANGE OF FRONT SPAR LOWER CHORD AT UNDERWING LONGERON LOWER WING AT STATION BODY STATION 1035 APPROXIMATELY LEFT BUTTOCK LINE 81.30 LOWER OUTBOARD HOLE CRACKED REPAIR CARRIED OUT AS PER E.A.#G-5710-T0359861 P1 TITLE: FUSELAGE-MAINFRAME-DEVIATIONS TO SB-777-53-0087 AND SRM 57-10-10 REPAIR 1 Ï¿½ OVERSIZED HOLE ON WING CENTER SECTION FRONT SPAR LOWER CHORD *THIS EA DEVIATES FROM EO-5310-E0332629 I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (SPECIAL/NON ROUTINE MAINTENANCE FORM #N00521 AND #N00519 FOR DETAILS)

Part: SKIN — CRACKED (ZONE 100) · airframe 41,668 hrs · 6,583 cycles

DURING ACCOMPLISMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND HAND FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATION AROUND AROUND FASTENER HOLE AT STATION 1033 STRINGER 37 RIGHT, APPROXIMATELY 0.750 INCHES IN LENGTH. COMPLIED WITH E.O.#: G-5310-E0332629 I P6. TITLE: FUSELAGE-MAINFRAME-INSPECTION AND MODIFICATION OF THE UNDERWING LONGERON AT BODY SYATION 1035- BOEING SERVICE BULLETINS 777-53A0081 AND 777-53-0087. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: VALVE — FAILED (FUEL DUMP) · airframe 40,491 hrs · 6,394 cycles

PDIS 854 28-30 0702 29OCT20 ANC OPEN U. AFTER DUMPING FUEL. FUEL JET NOZZLE RIGHT ILLUMINATED AND THE RIGHT JET VALVE CONTINUED TO DUMP WHEN DUMP WAS TERMINATED. FACT 08NOV20 20:31 MEM. R & R RT FUEL JETT NOZZLE VALVE ACT, IAW AMM 28-31-03. CHECKS GOOD, OK FOR SERVICE.

Part: RELAY — FAILED · airframe 39,066 hrs · 6,152 cycles

AT 6000' ON DESCENT WITH AUTOPILOT ENGAGED GOT SEVERAL EICAS INDICATIONS ON NOTICEABLE "THUMP" EICAS AND STATUS MSG INCLUDED : ALT CALLOUTS, TERR POSS, SATCOM, NO LAND 3 STATUS PAGE SATCOM SYSTEM, AFDC-L, NO LAND 3 PACK L AND CAPT FSS LIGHT CAME ON FOR 2 SECONDS WENT OUT. HUD POSITION OFF LEFT 300' OF ACTUAL POSITION. AS PER FIM 24-51-00-2, LEFT GCB C24331 AMM 24-22-03-4. RAN LEFT ENGINE AS PER AMM 71-00-00-2, TEST OK. AUTOLAND SYSTEM GROUND TEST PERFORMED AS PER AMM 22-11-00-5 AND 22-31-00-5, TEST OK. EGPWS OPERATIONAL TEST PERFORMED AS PER AMM 34-46-00-5-2, TEST OK. HUD RTS TEST PERFORMED AS PER AMM 31-82-01-5-99, TEST OK. OPERATIONAL TEST OF LEFT PACK PERFORMED AS PER AMM 21-51-00-5, TEST OK. A/C OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 39,066 hrs · 6,152 cycles

AT 6000' ON DESCENT WITH AUTOPILOT ENGAGED GOT SEVERAL EICAS INDICATIONS ON NOTICEABLE "THUMP" EICAS AND STATUS MSG INCLUDED: ALT CALLOUTS, TERR POSS, SATCOM, NO LAND 3 STATUS PAGE SATCOM SYSTEM, AFDC-L, NO LAND 3 PACK L AND CAPT FSS LIGHT CAME ON FOR 2 SECONDS WENT OUT. HUD POSITION OFF LEFT 300' OF ACTUAL POSITION.

Part: SWITCH — DEFECTIVE (STOWAGE BOX) · airframe 32,797 hrs · 5,107 cycles

DURING PREFLIGHT OBSERVER SEAT OXYGEN MASK "PRESS TO TEST" SWITCH GETS STUCK IN DOWN POSITION. REMOVED AND REPLACED 1ST OBSERVER OXY STORAGE BOX, OPS CK'S NORMAL.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 215 hrs · 3,221 cycles

WHILE ACCOMPLISHING EA G-5310-T0312163 PART 2. FLOOR INTERCOSTAL DRILL HOLE DAMAGED. REPAIR CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100.

Part: SPRING — LOOSE (EMERGENCY LIGHT) · airframe 14,613 hrs · 2,087 cycles

WHEN GUARD TO EMERGENCY LIGHTS SWITCH IS CLOSED, EMERGENCY LIGHTS REMAIN IN THE OFF POSITION. FOUND SPRING OF GUARD LOOSE. SPRING REINSTALLED IN GOOD POSITION. OPERATIONS CHECKED OK IAW AMM 33-51-00-5.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,716 hrs · 1,204 cycles

ONE EMERGENCY EXIT LIGHT INOPERATIVE. DURING EMERGENCY EXIT LIGHT TEST. R & R BULB IAW SMP. OPS TEST OK IAW MM 33-51-00-5. ACFT OK FOR SERVICE.

Part: TIRE — LEAKING (NR 10) · airframe 6,913 hrs · 933 cycles

40 MINUTES AFTER REACHING CRUISE, RECEIVED TIRE PRESSURE EICAS ALERT. PRESSURE WAS LOW ON TIRE NR 10. PRESSURE WENT FROM 204 -114 OVER AN HOUR, DIVERTED. INSPECTED TIRE, NO VISUAL DEFECTS NOTED. R & R LOW NR 10 TIRE AND ADJACENT NR 9 TIRE IAW MM 32-45-01-4. INSPECTED LT GEAR FOR DAMAGE, NONE NOTED. FAILED OPS CHECK. REPLACED WITH SERVICEABLE UNIT. PREMATURE REMOVAL/INSTALLATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 2,156 hrs · 298 cycles

LT ENTRY DOOR EMERGENCY LIGHT INOP. RELAMPED, REF:B777, AMM 33-51-04-2, OPERATIONAL CHECKS GOOD. FINAL CLOSED.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 440 hrs · 86 cycles

2EA OVERHEAD EMER LIGHTS DID NOT ILLUMINATE DURING TEST IN CABIN AREA. REPLACED EMER LTS LAMP 2EA (MPN 1317)OPS CHECKED NML IAW AMM 33-51-03-20.

Part: BATTERY PACK — INOPERATIVE (R1 DOOR) · airframe 63 hrs · 28 cycles

R1 DOOR EPAS BATTERY PACK TEST LIGHT IS NOT BLINKING GREEN AS REQUIRED. REMOVED R1 EPAS BATTERY PACK AND REPLACED INTERNAL BACKUP BATTERIES IAW AMM 52-11-20-4.