N862FD
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.
28 reports on file, 2011-12-01 – 2022-07-19.
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 42,165 hrs · 6,768 cycles
MAIN DECK CABIN FLOOR PANEL 242QF FOUND CRACK. MAIN DECK CABIN FLOOR PANEL 242QF REPAIRED PER B777 SRM 53-00-50-2R . REPAIR 1, REV41.0, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 42,165 hrs · 6,768 cycles
MAIN DECK CABIN FLOOR PANEL 242PF FOUND CRACK. MAIN DECK CABIN FLOOR PANEL 242PF REPAIRED PER B777 SRM 53-00-50-2R . REPAIR 1, REV41.0, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 42,165 hrs · 6,768 cycles
MAIN DECK CABIN FLOOR PANEL 242KF FOUND CRACK. MAIN DECK CABIN FLOOR PANEL 242KF REPAIRED PER B777 SRM 53-00-50-2R . REPAIR 1, REV41.0, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 42,165 hrs · 6,768 cycles
MAIN DECK CABIN FLOOR PANEL 241MF FOUND CRACK. MAIN DECK CABIN FLOOR PANEL 241MF REPAIRED PER B777 SRM 53-00-50-2R . REPAIR 1, REV41.0, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 42,165 hrs · 6,768 cycles
MAIN DECK CABIN FLOOR PANEL 241QF FOUND CRACK. MAIN DECK CABIN FLOOR PANEL 241QF REPAIRED PER B777 SRM 53-00-50-2R . REPAIR 1, REV41.0, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 42,165 hrs · 6,768 cycles
MAIN DECK CABIN FLOOR PANEL 242LF FOUND CRACK. MAIN DECK CABIN FLOOR PANEL 242LF REPAIRED PER B777 SRM 53-00-50-2R . REPAIR 1, REV41.0, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 42,165 hrs · 6,768 cycles
MAIN DECK CABIN FLOOR PANEL 241PF FOUND CRACK. MAIN DECK CABIN FLOOR PANEL 241PF REPAIRED PER B777 SRM 53-00-50-2R . REPAIR 1, REV41.0, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 42,165 hrs · 6,768 cycles
MAIN DECK CABIN FLOOR PANEL 241UF FOUND CRACK. MAIN DECK CABIN FLOOR PANEL 241UF REPAIRED PER B777 SRM 53-00-50-2R . REPAIR 1, REV41.0, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: FLOOR PANEL — CRACKED (CABIN) · airframe 42,165 hrs · 6,768 cycles
MAIN DECK CABIN FLOOR PANEL 242PF FOUND CRACK. MAIN DECK CABIN FLOOR PANEL 242PF REPAIRED PER B777 SRM 53-00-50-2R . REPAIR 1, REV41.0, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: NONE — MECHANIC ERROR (ZONE 100) · airframe 42,165 hrs · 6,768 cycles
DURING PERFORMING EO G-5710-E0365655 P7 STEP8.C.(5), FOUND 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 LHS TOO CLOSE TO EDGE OF MACHINED STEP OF DOUBLER P/N 143W2314Y405, AND WILL RESULT IN KNIFE EDGE WITH MACHINED STEP ON AFT EDGE OF COUNTERSUNK HOLE. THE COUNTERSUNK FASTENER TOO CLOSE TO EDGE OF MACHINED STEP OF DOUBLER, REPAIRED AS PER EA: G-5310-T0369194 P1 STEP1. TITLE: FUSELAGE - MAINFRAME - LH AND RH UNDERWING LONGERON MODIFICATION PER EO G-5710-E0365655-DEVIATIONS TO SB777-57A0122 RB. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI: 53101101 FOR WORK DETAILS.
Part: FLOOR PANEL — CRACKED (CABIN) · airframe 42,165 hrs · 6,768 cycles
MAIN DECK CABIN FLOOR PANEL 241MF FOUND CRACK. MAIN DECK CABIN FLOOR PANEL 241MF REPAIRED PER B777 SRM 53-00-50-2R . REPAIR 1, REV41.0, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: NONE — MECHANIC ERROR (NONE) · airframe 42,165 hrs · 6,768 cycles
DURING PERFORMING EO G-5710-E0365655 P8 STEP8.C.(5), FOUND 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 RHS TOO CLOSE TO EDGE OF MACHINED STEP OF DOUBLER P/N 143W2314Y406, AND WILL RESULT IN KNIFE EDGE WITH MACHINED STEP ON AFT EDGE OF COUNTERSUNK HOLE. THE COUNTERSUNK FASTENER TOO CLOSE TO EDGE OF MACHINED STEP OF DOUBLER, REPAIRED AS PER EA: G-5310-T0369194 P2 STEP 1. TITLE: FUSELAGE - MAINFRAME - LH AND RH UNDERWING LONGERON MODIFICATION PER EO G-5710-E0365655-DEVIATIONS TO SB777-57A0122 RB. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI : 53101102 FOR WORK DETAILS.
Part: NONE — MECHANIC ERROR (NONE) · airframe 42,165 hrs · 6,768 cycles
DURING PERFORMING EO G-5710-E0365655 P8 STEP8.C.(5), FOUND 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 RHS TOO CLOSE TO EDGE OF MACHINED STEP OF DOUBLER P/N 143W2314Y406, AND WILL RESULT IN KNIFE EDGE WITH MACHINED STEP ON AFT EDGE OF COUNTERSUNK HOLE. THE COUNTERSUNK FASTENER TOO CLOSE TO EDGE OF MACHINED STEP OF DOUBLER, REPAIRED AS PER EA: G-5310-T0369194 P2. STEP1. TITLE: FUSELAGE-MAINFRAME-LH AND RH UNDERWING LONGERON MODIFICATION PER EO G-5710-E0365655-DEVIATIONS TO SB777-57A0122 RB. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI:53101102 FOR WORK DETAILS. NOTE :THIS ENTRY IS DUPLICATE OF SDR TRACKING #22-1586.
Part: NONE — NONE (N/A) · airframe 42,165 hrs · 6,768 cycles
DURING PERFORMING THE EO EG-5710-365655 P8 STEP 4 FOUND A EXISTING REPAIR ANGLE COMMON TO STGR36R AT STA1014 AND A COUNTERSUNK FASTENER HOLE ON THE SKIN HIDING THE REPAIR ANGLE.
Part: DOUBLER — NONE (ZONE 100) · airframe 42,165 hrs · 6,768 cycles
WHILE ACCOMPLISHING WC: E G-5710-E0365655 P8 STEP8.C.(5), FOUND 03EA HOLES AT STGR 36R SHORT EDGE MARGIN AND A HOLE DRILLED COMMON TO DOUBLER P/N:143W2314Y406, FOUND TOO CLOSE TO MACHINED EDGE. THE 03EA SHORT EDGE MARGIN HOLES AND A TOO CLOSE TO MACHINED EDGE HOLE REPAIRED AS PER EA: G-5310-T0369182 P1. TITLE : FUSELAGE-MAINFRAME DEVIATIONS CAUSED BY NCR N1760144286 FOR UNDERWING LONGERON MODIFICATION PER EO G-5710-E0365655. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI:53101103 FOR WORK DETAILS.
Part: FLOOR PANEL — CRACKED (CABIN) · airframe 42,165 hrs · 6,768 cycles
MAIN DECK CABIN FLOOR PANEL 241UF FOUND CRACK. MAIN DECK CABIN FLOOR PANEL 241UF REPAIRED PER B777 SRM 53-00-50-2R . REPAIR 1, REV41.0, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: FLOOR PANEL — CRACKED (CABIN) · airframe 42,165 hrs · 6,768 cycles
MAIN DECK CABIN FLOOR PANEL 241QF FOUND CRACK. MAIN DECK CABIN FLOOR PANEL 241QF REPAIRED PER B777 SRM 53-00-50-2R . REPAIR 1, REV41.0, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: FLOOR PANEL — CRACKED (CABIN) · airframe 42,165 hrs · 6,768 cycles
MAIN DECK CABIN FLOOR PANEL 242LF FOUND CRACK. MAIN DECK CABIN FLOOR PANEL 242LF REPAIRED PER B777 SRM 53-00-50-2R . REPAIR 1, REV41.0, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: FLOOR PANEL — CRACKED (CABIN) · airframe 42,165 hrs · 6,768 cycles
MAIN DECK CABIN FLOOR PANEL 242KF FOUND CRACK. MAIN DECK CABIN FLOOR PANEL 242KF REPAIRED PER B777 SRM 53-00-50-2R . REPAIR 1, REV41.0, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: FLOOR PANEL — CRACKED (CABIN) · airframe 42,165 hrs · 6,768 cycles
MAIN DECK CABIN FLOOR PANEL 242QF FOUND CRACK. MAIN DECK CABIN FLOOR PANEL 242QF REPAIRED PER B777 SRM 53-00-50-2R . REPAIR 1, REV41.0, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Earlier reports · 2011–2021 · 8 reports
2021
Part: NONE — LEAKING (ZONE 100) · airframe 39,788 hrs · 6,362 cycles
STATUS MSG SHOWN: "BOTTLE 2A CARGO,BOTTLE 2B CARGO, BOTTLE 2C CARGO" , MAT EXISTING FAULT MAINTENANCE MSG SHOWN:"26-40781, 26-40783, 26-40785" LOWER CARGO FIRE BOTTLE 2A, 2B&2C REMOVED,INSTALLED AND FLUSHED AS PER B777AMM 26-23-01-4 REV93.4. LOWER CARGO FIRE EXTINGUSHIING FILTER REMOVED AND REPLACED AS B777 AMM 26-23-04-4 REV 93.4. LOWER CARGO FIRE EXTINGUISHING FLOW VALVE REMOVED AND REPLACED AS PER B777 AMM 26-23-05-4 REV 93.4. CARRIED OUT CARGO FIRE EXTINGUISHING BOTTLE PRESSURE SW OPS TEST AS PER B777 AMM 26-23-00-710-801 REV 93.4. CARRIED OUT FIRE EXTINGUISHING SQUIBS OPS TEST AS PER B777 AMM 26-23-00-710-802 REV 93.4. CARRIED OUT FIRE EXTINGUISHING TUBING LEAKAGE AND BLOCKAGE FUNCTIONAL TEST AS PER B777 26-23-00-730-802 REV 93.4.ALL TEST FOUND SATISFACTORY. THE REPAIR CLASSIFIED AS MINOR PER GMM 06-2-100. NOTE: FIRE EXTINGUISHER OFF 2A P/N:473876-3, S/N: 1873BA, 2B P/N:473876-3, S/N:4180BA, 2C P/N: 473876-3, S/N:2302BA. FIRE EXTINGUISHER ON 2A P/N: 473876-3, S/N: 2303BA, 2B P/N: 473876-3, S/N: 57902EL, 2C P/N: 473876-3, S/N: 1534BA.
2020
Part: GUARD — BROKEN (LIGHT SWITCH) · airframe 34,668 hrs · 5,492 cycles
WITH EMERGENCY LIGHTS SWITCH CLOSED IT SHOWS OFF INSTEAD OF ARMED FOUND EMERGENCY LIGHTS SWITCH GUARD BROKEN, REMOVED AND REPLACED EMERGENCY LIGHTS SWITCH GUARD REF B777 C.M.M. 30-41-13, OPS CK NORMAL. A/C OK TO CONTINUE.
2017
Part: LINE — CHAFED (RT ENGINE) · airframe 23,436 hrs · 3,676 cycles
AT 6 30 INTO FLIGHT, RIGHT ENGINE OIL QTY DROPPED TO 4 AND STATUS ALERT. OIL CONTINUED TO DROP TO ZERO AND THEN OIL PRESSURE STARTED TO FLUCTUATE AND DROP. ALERTED GOC AND COORDINATED DIVERT TO PACD. SHUT DOWN RIGHT ENGINE WHEN "ENG OIL PRESS R" CAME ON AT 10 PSI. FOUND OIL LEAK ON OIL LINE P/N 2034M68G01. R & R SAME OIL LINE TURBINE CENTER FRAME (TCF) OIL SUPPLY TUBE, NO LEAKS.
Part: SKIN — DAMAGED (LE SLAT) · airframe 22,145 hrs · 3,463 cycles
LEFT HAND WING NR 7 SLAT ASSEMBLY CENTER LEADING EDGE SURFACE FOUND DAMAGED AT ISS 264.620. SLAT SURFACE REPAIRED AS PER EA G-5750-T0332638 P1 REPAIR FOR 01 EA BULGE FOUND COMMON LT WING NR 7 SLAT ASSY CENTER LE OUTER SKIN AT ISS 264.620. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
2015
Part: SMOKE DETECTOR — FAILED (NOT REPORTED) · airframe 152 hrs · 2,286 cycles
AT LEVEL OFF AT FL 340, RECEIVED A MOMENTARY MASTER CAUTION & EICAS MESSAGS, FOR SMOKE. AFTER RESEARCH DETERMINED FAULTY SMOKE DETECTOR. TROUBLESHOT FIM 26-16-00-810 836. R & R SMOKE DETECTOR NR 1 M26564 IAW AMM 26-16-01-4-1.
2013
Part: COVER — DAMAGED (LIGHT SWITCH) · airframe 7,893 hrs · 1,119 cycles
EMERGENCY LIGHT SWITCH COVER BROKEN. REPLACED EMERGENCY LIGHT MODULE REF SMP. ACCOMPLISHED ADJUSTMENT TEST OF EMERGENCY LIGHT IAW AMM 33-51-00-5 AND SMP.
Part: BATTERY — INOPERATIVE (L1 DOOR ASSIST) · airframe 6,477 hrs · 918 cycles
L1 DOOR EMERGENCY POWER ASSIST SYS (EPAS) STATUS LIGHT NOT BLINKING. R & R 2 EA, 9 VOLT BATTERIES IAW AMM 52-11-20-4, OK FOR SERVICE.
2011
Part: CONNECTOR — DAMAGED · airframe 54 hrs · 17 cycles
GATE POWER FLUXED AND DROPPED OFF LINE AT GATE 393 CAUSING THE CARGO BOTTLE 2 A, B, &C TO FAULT, AND WILL NOT RESET WITH OPS TEST OF CARGO SQUIBS. LATCHED FAULT WITH MX MESSAGE'S 26-40781, 26-40783, AND 26-40785. FOUND 1 CONNECTOR PLUG RETAINER MISSING AND 1 READY TO FALL APART. ALL 3 SUIBS ARE BAD. REPLACED SQUIB CONNECTOR PLUGS ON 2A, 2B, AND 2C IAW FEC 777 SWPM 20-63-00. R & R 2A, 2B, AND 2C FIRE EXT BOTTLES W/REF TO 26-23-01. ALSO IAW AMM 26-23-01 HAD TO REPLACE LWR FIRE EXT FILTER/REGULATOR W/REF TO AMM 26-23-04. ALL MSG'S CLEARED AND TESTS PASSED. ACFT OK FOR SVC. FINAL CLOSED.