N857FD
Registered owner: FEDERAL EXPRESS CORP, TN (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
39 reports on file, 2010-10-12 – 2026-08-22.
Part: TIRE TREAD — SEPARATED (ZONE 700) · airframe 61,966 hrs · 10,009 cycles
CHECK FOUND NR 11 TIRE TREAD SEPARATION.
Part: SAFETY WIRE — WRONG PART (ZONE 800) · airframe 59,944 hrs · 9,649 cycles
RIGHT SLIDE, REPLACE THE BREAKAWAY WIRE SECURING THE RELEASE CABLE TO THE PACKBOARD RELEASE MECHANISM ON THE PACKBOARD WITH MS20995CY16 CAD-PLATED COPPER WIRE PER SMIS 25-60/5696 (F.E.A. G-2560-F0386294 C PART 1) CMM: 25-61-31 EA: 9-2560-T0386431 FEA: G-2560-F0386294 C P1 OTHER: SMIS 25-60/5696 REMOVED AND REPLACED BREAKAWAY WIRE SECURING RELEASE CABLE AS DIRECTED WITH MS20995CY16.
Part: SKIN — DENTED (ZONE 600 FLAP) · airframe 59,912 hrs · 9,644 cycles
FOUND RT WWING T/E OTBD FLAP LOWER SURFACE DENT 1EA AT THE CROSS OTEF 335 AND T/E 2 INCHS. REPAIRED RHW T/E O/B FLAP LOWER SURFACE DENT 1EA AT THE CROSS OTEF 335 AND T/E 2 INCHES AS PER B777 SRM 57-53-01-2R-2 FIGURE 203 AND SRM 51-70-04-2R-1 REV 51.0 AND EA: G-5750-T0386221 P1, MAJOR REPAIR PER GMM 6-2-100.
Part: FITTING — CRACKED (NR 11 SLAT TRACK) · airframe 59,912 hrs · 9,644 cycles
FOUND RH WING NR 11 SLAT L/E UPPER SKIN 1 EA BULGE AT THE O/B MAIN TRACK FITTING AREA. RH WING NO.11 SLAT L/E UPPER SKIN BULGE AREA REPAIRED AS PER B777 SRM 57-43-01-2R REPAIR 9 FIG 202 REV:51.0 AND EA G-5750-T0386209 P1. TITLE:WING-FLIGHT SURFACES-RH WING #11 SLAT OUTER SKIN BULGE FORWARD OF NOSE BEAM AREA BETWEEN OSBS 915 AND OSBS 943 -SRM REPAIR-RSC TRACKING. REFER TO WRI:57505700 FOR WORK DETAILS. THIS IS A MAJOR REPAIR PER GMM 6-2-100.
Part: SKIN — CRACKED (ZONE 600) · airframe 59,912 hrs · 9,644 cycles
DURING PERFORM WORK CARD:EG-5710-E0376285E P12 STEP 3.B.& STEP5 A.(2) THEN FOUND TWO CRACKS ON RT UPPER WING SKIN FASTENER NR 5. RT WING UPPER SKIN FASTENER HOLE REPAIRED IAW SRM 51-50-02-0G, FIGURE 1, SRM 51-40-02-0G, FIGURE 12, SRM 51-20-07-0G, FIGURE 1, SRM 51-10-01-0G, FIGURE 1, SRM 51-20-06-0G, SRM 51-40-05-0G, FIGURE 4, SRM 51-20-01-0G, SRM 51-40-08-0G, FIGURE 2, SRM 51-20-05-2R, FIGURE 201 REV 51.0, AND EA G-5730-T0386190 P1. MAJOR REPAIR PER GMM6-2-100.
Part: SKIN — CRACKED (ZONE 600) · airframe 59,912 hrs · 9,644 cycles
DURING PERFORM WORK CARD:EG-5710-E0376285F P12 STEP4. B. (2). (B). THEN FOUND TWO CRACKS ON RT UPPER WING SKIN FASTENER NR 6. RT WING UPPER SKIN NR 6 CRACKED FASTENER HOLE REPAIRED IAW SRM 51-50-02-0G, FIGURE 1, SRM 51-40-02-0G, FIGURE 12, SRM 51-20-07-0G, FIGURE 1, SRM 51-10-01-0G, FIGURE 1, SRM 51-20-06-0G, SRM 51-40-05-0G, FIGURE 4, SRM 51-20-01-0G, SRM 51-40-08-0G, FIGURE 2, SRM 51-20-05-2R, FIGURE 201, REV 51.0 & EA G-5730-T0386190 P1, MAJOR REPAIR PER GMM6-2-100.
Part: SKIN — CRACKED (ZONE 500) · airframe 59,912 hrs · 9,644 cycles
DURING PERFORM WORK CARD:EG-5710-E0376285F P11 STEP3. B. (1). & STEP5 A. (2), THEN FOUND 02EA CRACKS ON LH UPPER WING SKIN FASTENER #5 AS MARKED. THE LEFT WING UPPER SKIN #5 FASTENER CRACKED HOLE REPAIRED IAW SRM 51-50- 02-0G, FIGURE 1, SRM 51-40-02-0G, FIGURE 12. SRM 51-10-01-0G, FIGURE 1. SRM 51-20-06-0G, SRM 51-40-05-0G, FIGURE 4, SRM 51-20-01-0G, SRM 51-40-08-0G, FIGURE 2, SRM 51-20-05-2R, FIGURE 201, REV 51, AND EA G-5730-T0386186 P1.THIS IS A MAJOR REPAIR PER GMM6-2-100.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 59,912 hrs · 9,644 cycles
FOUND MAIN DECK FLOOR PANEL 241SF (P/N 152W8601-7) DAMAGED AT STA 1450 LBL 2. MAIN DECK FLOOR PANEL 241SF (P/N 152W8601-7) CRACKED AT STA 1450 LBL 2 DAMAGE SIZE: L= 0.8" DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1 FIGURE 101-106 REV 51.0 AND REPAIRED AS PER B777 SRM 53-00-50-2R REPAIR 1 FIGURE 201-202 REV 51.0. THIS IS A MAJOR REPAIR PER GMM 6-2-100.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 59,912 hrs · 9,644 cycles
FOUND MAIN DECK FLOOR PANEL 241LF DAMAGED AT BS 1300, LBL 45. FLOOR PANEL 241LF DAMAGED: L= 1", DAMAGE OUT OF ALLOWABLE LIMIT IAW SRM 53-00-50-1A, ALLOWABLE DAMAGE 1, FIGURE 101-106, REV 51. REPAIRED IAW SRM 53-00-50-2R, REPAIR 1, FIGURE 201-202, REV 51. MAJOR REPAIR IAW GMM 6-2-100..
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 59,912 hrs · 9,644 cycles
FOUND MAIN DECK FLOOR PANEL 241QF (P/N 152W8402-21) DAMAGED AT STA 1400 LBL 45. MAIN DECK FLOOR PANEL 241QF (P/N 152W8402-21) CRACKED AT STA 1400 LBL 45 DAMAGE SIZE: L= 1.2" DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1 FIGURE 101- 106 REV 51.0 AND REPAIRED AS PER B777 SRM 53-00-50-2R REPAIR 1 FIGURE 201-202 REV 51.0. THIS IS A MAJOR REPAIR PER GMM 6-2-100.
Part: SKIN — DAMAGED (NR 7 SLAT) · airframe 59,912 hrs · 9,644 cycles
NUMBER 7 SLAT EXTERNAL UPPER SURFACE OUTER SKIN AT ISS184 SCREW HOLE FOUND ELONGATE. NR 7 SLAT EXTERNAL UPPER SURFACE OUTER SKIN AT ISS 184 ELONGATE SCREW HOLE REPAIRED IAW SRM 57-43-01-2R REPAIR 6, FIG 203, REV: 51.0 AND EA G-5750-T0386196 P1, MAJOR REPAIR IAW GMM 6-2-100.
Earlier reports · 2010–2025 · 28 reports
2025
Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 56,868 hrs · 9,112 cycles
DURING SERVICE CHECK, FOUND L/H SLIDE LIGHT INOP. PART 22MAR25 14:16 MC1 IDENTIFIED PARTS EMERGENCY LIGHTS. RELAMPED L/H SLIDE LIGHT PER AMM 33-51-04-2. NO HELP. REMOVED AND REPLACED L1 EMER LIGHTS POWER SUPPLY PER AMM 33-51-06-2, BUT PART BFS. SEE WRI 33-50/4783 FOR PART TRANSACTION. REINSTALLED ORIGINAL PART. NEED MORE TROUBLESHOOTING. REMOVED AND REPLACED LEFT EMER PWR SUPPLY M33093.
Part: LAMP — INOPERATIVE (ZONE 200) · airframe 56,344 hrs · 9,031 cycles
CHECK FOUND ONE EMERGENCY AREA LIGHT IS INOP. RELAMPED THE EMERGENCY AREA LIGHT REF AMM 33-51-03-2, TEST NORMAL. A/C OK TO CONTINUE.
Part: LAMP — FAILED (ZONE 200) · airframe 56,199 hrs · 8,999 cycles
LOWER RIGHT EXIT SIGN ON THE RIGHT SIDE OF ENTRY DOOR L1 HAS ONE BULB INOP. REPLACED LAMP PER AMM : 33-51-01-2. TEST PASSED.
2023
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 50,218 hrs · 7,987 cycles
MAIN DECK CARGO FLOOR PANEL 251FF(P/N:152W8601-19) AT STA1656/RBL1 FOUND A HOLE. EVALUATED MAIN DECK CARGO FLOOR PANEL 251FF(P/N:152W8601-19) AT STA1656/RBL1 A HOLE ,THE HOLE SIZE :LXW=1.8"X1.6" IN UPPER SURFACE ,WITHIN LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1,REV 43.1.REPAIRED THE HOLE AS PER B777 SRM 53-00-50-2R REPAIR 1 ,REV 43.1 .REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 50,218 hrs · 7,987 cycles
MAIN DECK CARGO FLOOR PANEL 251MF(P/N:152W8601-31) AT STA1798/LBL1.5 FOUND A HOLE. EVALUATED MAIN DECK CARGO FLOOR PANEL 251MF(P/N:152W8601-31) AT STA1798/LBL1.5 A HOLE ,THE HOLE SIZE :LXW=2.0"X1.8" IN UPPER SURFACE ,WITHIN LIMIT AS PER B777 SRM 53-00- 50-1A ALLOWABLE DAMAGE 1,REV 43.1.REPAIRED THE HOLE AS PER B777 SRM 53-00-50-2R REPAIR 1, REV 43.1 .REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
2020
Part: STRUCTURE — DAMAGED (ZONE 100) · airframe 40,257 hrs · 6,337 cycles
WHILE PERFORMING RIGHT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR (SNRM N00526) FOUND 02 EACH EXISTING OVERSIZED HOLE AT LOWER CHORD THROUGH WEB STATION 1035 RIGHT HAND BUTTLINE 88 AND RIGHT HAND BUTTLINE 90.5. RIGHT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR (02 EACH) EXISTING OVERSIZE HOLE AT LOWER CHORD THROUGH WEB STATION 1035 RIGHT HAND BUTTLINE 88 AND RIGHT HAND BUTTLINE 90.5. REPAIRED AS PER EA G-5710-T0357440 P1. TITLE: FUSELAGE MAINFRAME DEVIATIONS TO SB-777 53-0087 AND SRM 57-10-10 REPAIR 1 OVERSIZED HOLES ON WING CENTER SECTION FRONT SPAR LOWER CHORD. THIS EA DEVIATES FROM EO G-5310-E0332629 H. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. SPECIAL/NONROUTINE MAINTENANCE FORM N00526 AND N00556 FOR DETAILS.
Part: STRUCTURE — DAMAGED (ZONE 100) · airframe 40,257 hrs · 6,337 cycles
WHILE PERFORMING LEFT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR, SNRM #N00525. FOUND 01 EACH EXISTING OVERSIZED HOLE AT LOWER CHORD STATION 1035 LEFT HAND BUTTLINE 88. LEFT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR (01 EACH) EXISTING OVERSIZE HOLE AT LOWER CHORD STATION 1035 LEFT HAND BUTTLINE 88 REPAIRED, AS PER EA G-5710-T0357440 P1. THIS EA DEVIATES FROM EO G-5310-E0332629 H. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100. SPECIAL/NONROUTINE MAINTENANCE FORM N00525 AND N00554 FOR DETAILS.
Part: STRUCTURE — DAMAGED (ZONE 100) · airframe 40,257 hrs · 6,337 cycles
WHILE PERFORMING RIGHT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR (SNRM N00526) FOUND 02 EACH EXISTING OVERSIZED HOLE AT LOWER CHORD STATION 1035 RIGHT HAND BUTTLINE 88 AND RIGHT HAND BUTTLINE 90.5. RIGHT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR (02 EACH) EXISTING OVERSIZE HOLE AT LOWER CHORD STATION 1035 RIGHT HAND BUTTLINE 88 AND RIGHT HAND BUTTLINE 90.5 REPAIRED, AS PER EA G-5710-T0357440 P1. TITLE: FUSELAGE MAINFRAME DEVIATIONS TO SB-777 53-0087 AND SRM 57-10-10 REPAIR 1 OVERSIZED HOLES ON WING CENTER SECTION FRONT SPAR LOWER CHORD. THIS EA DEVIATES FROM EO G-5310-E0332629 H. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100. SPECIAL /NONROUTINE MAINTENANCE FORM N00526 AND N00553 FOR DETAILS.
Part: STRUCTURE — DAMAGED (ZONE 100) · airframe 40,257 hrs · 6,337 cycles
WHILE PERFORMING LEFT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR. SNRM N00525 FOUND 01 EACH EXISTING OVERSIZED HOLE AT LOWER CHORD THROUGH WEB STATION 1035 LEFT HAND BUTTLINE 88. LEFT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR (01 EACH) EXISTING OVERSIZE HOLE AT LOWER CHORD THROUGH WEB STATION 1035 LEFT HAND BUTTLINE 88. REPAIRED AS PER EA G-5710-T0357440 P1 TITLE: FUSELAGE MAINFRAME DEVIATIONS TO SB-777-0087 AND SRM 57-10-10 REPAIR 1 OVERSIZED HOLES ON WING CENTER SECTION FRONT SPAR LOWER CHORD. THIS EA DEVIATES FROM EO G-5310-E0332629 H. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100. SPECIAL/NONROUTINE MAINTENANCE FORM #N00525 AND N00555 FOR DETAILS.
Part: STRUCTURE — CRACKED (BS 1035) · airframe 40,257 hrs · 6,337 cycles
DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON REMOVED FASTENER HOLES ON RIGHT HAND SIDE VERTICAL FLANGE OF THE SPAR CHORD AT UNDERWING LONGERON LOWER WING BODY STATION 1035 APPROXIMATELY RIGHT HAND BUTTLINE 82AND FOUND 01 EACH LOWEST OUTBOARD HOLE WITH CRACK INDICATION. WING CENTER SECTION RIGHT HAND SIDE VERTICAL FLANGE OF FRONT SPAR LOWER CHORD AT UNDERWING LONGERON LOWER WING AT BODY STATION 1035 APPROXIMATELY RIGHT BUTTLINE 82, 01 EACH LOWEST OUTBOARD HOLE CRACKED REPAIRED, AS PER EA G-5710-T0357440 P1. TITLE: FUSELAGE MAINFRAME DEVIATIONS TO SB-777 53-0087 AND SRM 57-10-10 REPAIR 1 OVERSIZED HOLES ON WING CENTER SECTION FRONT SPAR LOWER CHORD. THIS EA DEVIATES FROM EO G-5310-E0332629 H. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100. (SNRM N00533, N00556 FOR DETAILS)
Part: DOUBLER — OUT OF ALIGNMENT (ZONE 100) · airframe 40,257 hrs · 6,337 cycles
WHILE ACCOMPLISHING EO G-5310-E0332629 H PART 6 FOUND 3 EACH PILOT HOLES AT NEW FUSELAGE SKIN DOUBLER MISALIGNED WITH THE LONGERON FITTING BETWEEN BODY STATION 993 TO BODY STATION 1008 BETWEEN STRINGER 35 RIGHT TO STRINGER 36 RIGHT. DOUBLER WITH MISALIGNED HOLES REPLACED WITH NEW PART 143W2314Y406 AND INSTALLED, AS PER EO G5310 E0332629 H P6. TITLE: FUSLAGE-MAINFRAME INSPECTION AND MODIFICATION OF THE UNDERWING LONGERON AT BODY STATION 1035 BOEING SERVICE BULLETINS 777-53A0081 AND 777-53-0087. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.
Part: SKIN — CRACKED (ZONE 100) · airframe 40,257 hrs · 6,337 cycles
HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON RIGHT HAND SIDE EXTERNAL SURFACE OF THE FUSELAGE SKIN WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE UNDERWING LONGERON AND THE FUSELAGE SKIN AND FOUND 1 EACH CRACK APPROXIMATELY 0.5 INCHES LENGTH, AS MARKED ON THE FUSELAGE SKIN OF THE UNDERWING LONGERON AT BODY STATION 1029, STRINGER 37 RIGHT. COMPLIED WITH EO: G-5310-E0332629 H (P6). TITLE: FUSELAGE MAINFRAME-INSPECTION AND MODIFICATION OF THE UNDERWING LONGERON AT BODY STATION 1035 BOEING SERVICE BULLETINS 777-53A0081 AND 777-53-0087. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100. REFER TO WRI: 53100168 FOR WORK DETAIL.
Part: DOUBLER — OUT OF ALIGNMENT (ZONE 100) · airframe 40,257 hrs · 6,337 cycles
WHILE ACCOMPLISHING LEFT HAND EO G-5310-E0332629 H PART 5 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STATION 998 STRINGER S-35 LEFT NEAR MILLED EDGE. COMPLIED WITH EA G-5310-T0357565 P1. TITLE: FUSELAGE MAINFRAME-DEVIATION TO SB-777-53-0087 R1-LT AND RT UNDERWING LONGERON MODIFICATION. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.
Part: DOUBLER — OUT OF ALIGNMENT (ZONE 100) · airframe 40,257 hrs · 6,337 cycles
WHILE ACCOMPLISHING EO G-5310-E0332629 H PART 6 FOUND NEW FUSELAGE SKIN DOUBLER PART NUMBER 143W2314Y406 PILOT HOLES MISALIGN WITH EXISTING FUSELAGE SKIN HOLES BETWEEN BODY STATION 993 TO BODY STATION 1008 BETWEEN STRINGER 35 RIGHT TO STRINGER 36 RIGHT. DOUBLER WITH MISALIGNED HOLES REPLACED WITH NEW PART 143W2314Y406 AND INSTALLED, AS PER EO G5310 E0332629 H P6. TITLE: FUSLAGE-MAINFRAME INSPECTION AND MODIFICATION OF THE UNDERWING LONGERON AT BODY STATION 1035 BOEING SERVICE BULLETINS 777-53A0081 AND 777-53-0087. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100. REFER TO WRI: 53100168 FOR WORK DETAIL.
Part: DOUBLER — OUT OF ALIGNMENT (ZONE 100) · airframe 40,257 hrs · 6,337 cycles
WHILE ACCOMPLISHING RIGHT HAND EO G-5310-E0332629 H PART 6 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STATION 998 STRINGER S-35 RIGHT NEAR MILLED EDGE. COMPLIED WITH EA G-5310-T0357565 P2. TITLE: FUSELAGE MAINFRAME-DEVIATION TO SB-777-53-0087 R1-LT AND RT UNDERWING LONGERON MODIFICATION. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.
Part: STRUCTURE — CRACKED (BS 1035) · airframe 40,257 hrs · 6,337 cycles
DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON REMOVED FASTENER HOLES ON LEFT HAND SIDE VERTICAL FLANGE OF THE SPAR CHORD AT UNDERWING LONGERON LOWER WING BODY STATION 1035 APPROXIMATELY LEFT HAND BUTTLINE 82 AND FOUND 01 EACH LOWEST OUTBOARD HOLE WITH CRACK INDICATION. WING CENTER SECTION LEFT HAND SIDE VERTICAL FLANGE OF FRONT SPAR LOWER CHORD AT UNDERWING LONGERON LOWER WING AT BODY STATION 1035 APPROXIMATELY LEFT HAND BUTTLINE 82, 01 EACH LOWEST OUTBOARD HOLE CRACKED REPAIRED, AS PER EA G-5710-T0357440 P1. TITLE: FUSELAGE MAINFRAME DEVIATIONS TO SB-777 53-0087 AND SRM 57-10-10 REPAIR 1 OVERSIZED HOLES ON WING CENTER SECTION FRONT SPAR LOWER CHORD. THIS EA DEVIATES FROM EO G-5310-E0332629 H. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100. (SNRM N00554, N00555 AND N00526 AND WRI: 57-10/0255 FOR ADDITIONAL DETAILS).
Part: SKIN — CRACKED (ZONE 100) · airframe 40,257 hrs · 6,337 cycles
HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON LEFT HAND SIDE EXTERNAL SURFACE OF THE FUSELAGE SKIN WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE UNDERWING LONGERON AND THE FUSELAGE SKIN AND FOUND 1 EACH CRACK APPROXIMATELY 0.75 INCHES LENGTH, AS MARKED ON THE FUSELAGE SKIN OF THE UNDERWING LONGERON AT BODY STATION 1029 STRINGER 37 LEFT. COMPLIED WITH EO G-5310-E0332629 H (P5). TITLE: FUSELAGE MAINFRAME-INSPECTION AND MODIFICATION OF THE UNDERWING LONGERON AT BODY STATION 1035 BOEING SERVICE BULLETINS 777-53A0081 AND 777-53-0087. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.
Part: FLOOR SUPPORT — CRACKED (BULK CARGO) · airframe 40,257 hrs · 6,337 cycles
LOWER BULK CARGO COMPARTMENT FLOOR STRINGER FOUND CRACK AT STATION 1958 RBL 41.5. LOWER BULK CARGO COMPARTMENT AT STATION 1958 RBL 41.5 CRACKED FLOOR STRINGER REPAIRED, AS PER B777 SRM 53-70-53-2R FIGURE 202 REPAIR 2. REPAIR STRINGER 01 EACH AND REPAIR ANGLE 04 EACH (ZEE SECTION) FABRICATED, AS PER B777 SRM 53-70-53-2R FIGURE 202 REPAIR 2. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.
2019
Part: NONE — NONE (NONE) · airframe 37,114 hrs · 5,780 cycles
PDIS 857 05-50 9138 13NOV19 SEA OPEN U LOGPAGES:3182688 FLEW INTO A VERY THIN, RAGGED VOLCANIC ASH CLOUD @ FL340 AT APPROX 2350Z NOTICED A SMALL, BUT STEADY EGT CLIMB AT A FIXED N1. EGT MAXED OUT AT 710 DEGREES BEFORE MAEUVERING OUT OF CLOUD. EVERYTHING RETURNED TO NORMAL SHORTLY THERE AFTER. NO ALERTS WERE NOTED. COMPLIED WITH PHASE IA GENERAL VISUAL INSPECTION IAW AMM 05-51-31-2 AND AMM 71-00-00-6. NO DEFECTS NOTED. A/C OK FOR SERVICE. FACT 13NOV19 06:24 SEA MAINT MANUAL UPDATE.
2017
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,546 hrs · 4,220 cycles
RT AFT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMP AND OPS CHECKED GOOD IAW AMM 33-51-00-5. ACFT OK FOR SERVICE.
2015
Part: BATTERY — DAMAGED (L1 DOOR) · airframe 209 hrs · 3,066 cycles
L1 DOOR EMER POWER ASSIST SYS STATUS LIGHT FOUND NOT BLINKING. FOUND LOWER EPAS BACKUP BATTERY SOCKET DEFORMED & NOT FULLY INSERTED INTO EPAS PACK. R & R BOTH EPAS BATTERIES & TESTED OK IAW AMM 52-11-20.
Part: BATTERY — DAMAGED (L1 DOOR) · airframe 209 hrs · 3,066 cycles
L1 DOOR EMER POWER ASSIST SYS STATUS LIGHT FOUND NOT BLINKING. FOUND LOWER EPAS BACKUP BATTERY SOCKET DEFORMED & NOT FULLY INSERTED INTO EPAS PACK. R & R BOTH EPAS BATTERIES & TESTED OK IAW AMM 52-11-20.
Part: BATTERY — DAMAGED (L1 DOOR) · airframe 209 hrs · 3,066 cycles
L1 DOOR EMER POWER ASSIST SYS STATUS LIGHT FOUND NOT BLINKING. FOUND LOWER EPAS BACKUP BATTERY SOCKET DEFORMED & NOT FULLY INSERTED INTO EPAS PACK. R & R BOTH EPAS BATTERIES & TESTED OK IAW AMM 52-11-20.
2013
Part: UNKNOWN — ODOR (COCKPIT) · airframe 12,773 hrs · 1,740 cycles
ON ENTERING COCKPIT, FAINT ODOR SIMILAR TO A BURNED ELECTRICAL WAS PRESENT. SWITCHED AIR CONDITION CART AIR TO APU AIR, ODOR STOPPED IAW FIM 21-00-00-2, CHECKED MEC COMP'T NORMAL. ACFT OK FOR SERVICE. FINAL CLOSED.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,756 hrs · 1,735 cycles
FOUND RT OVERWING SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED BULB IAW MM33-51-04-2. TEST PASSED.
2012
Part: SLIDE — FAILED (PAX DOOR) · airframe 9,875 hrs · 1,318 cycles
MAIN CABIN DOOR SLIDE ACTIVATED. CAPT/FO, BOTH VERIFIED DOOR(S) WERE DISARMED BUT SLIDE ACTIVATED, DOOR SYNOPSIS INDICATED "M" ON BOTH DOORS. REMOVED LT DOOR MOUNTED ESCAPE SLIDE IAW AMM 25-66-00 201, AND LT CREW DOOR CLOSED EASILY. INSTALLED LT ENTRY DOOR ESCAPE SLIDE PACK PER MM 25-66-01-4. R & R LT EPAS RESERVOIR AND OPS CHECKED OK PER MM 52-11-22-4.
2011
Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 2,565 hrs · 343 cycles
L1 SLIDE DEPLOYED ON ARRIVAL. R&R L1 DOOR MOUNTED ESCAPE SLIDE PACK IAW AMM 25-66-01-4 AND R&R L1 EPAS RESERVOIR IAW AMM 52-11-22-4, ACFT OK FOR SERVICE.
2010
Part: LINE — LEAKING (HYD SYSTEM) · airframe 580 hrs · 99 cycles
HYD QTY LOW CTR (LOST ALL HYD FLUID IN CTR) SVC'D HYD FLUID TO CTR HYD SYS TO PROPER LEVEL IAW AMM 12-12-01-3-0, PERF CTR HYD SYS LEAKS FOUND. NO EXTERIOR LEAKS CAN BE FOUND. SUMP DRAINED LT FUEL TK & RT FUEL TK, FOUND HYD CONTAMINATED IN RT FUEL TK FUEL SAMPLE. SUSPECTED HYD LEAKS FROM THE CTR HYD SYS HEAT EXCHANGER OR PIPING INSIDE THE RT FUEL TK. REQUIRED RT FUEL TK ENTRY TO LOCATE THE LEAKS. FOUND HYDRAULIC LEAK INSIDE RT SIDE FUEL TANK, UNDERWING ACCESS PANEL 633EB, ONE HYD PIPE ISOLATED FROM THE SLEEVE. REPAIRED PIPING PER AMM 20-10-09-8, PERF. LEAKS CHECK SATISFACTORY. PERF. CTR HYD SYS FLUSHING PER AMM 29-11-00-2 REPLACED THE PRESSURE AND CASE DRAIN AC MOTOR PUMP FILTER PER AMM 29-11-41-4-0. SERVICED THE HYDRAULIC TO PROPERLY LEVEL,PERFORMED PRIMARY FLT CONTROL OPERATION PER AMM 27-00-00.