# N862FD: 2011 Boeing 777-FS2

- Status: Valid registration
- Airframe: [Boeing 777-FS2](https://openairdocs.org/model/boeing-777-fs2) (registry code 138527H, 13 seats)
- Engine: [GE GE90-110B1](https://openairdocs.org/engine/ge-ge90-110b1) (registry code 30046)
- Data sheets: [TCDS E00049EN](https://openairdocs.org/tcds/E00049EN) (General Electric Company GE Aviation) (OpenAirDocs)
- Serial number: 37733
- Year built: 2011
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 14, 2011
- Certificate issued: November 16, 2011
- Expires: November 30, 2027
- Mode S code: ABD6C6
- Registered owner: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP)
- Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis)
- Owner type: Corporation
- Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=862FD
- Page: https://openairdocs.org/aircraft/N862FD

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 21 in force

### Matched by airframe (Boeing 777-FS2)

None in force.

### Matched by engine (GE GE90-110B1)

- [AD 2025-25-07](https://openairdocs.org/ad/2025-25-07): Turbine Section · General Electric Company GE GE90-90B, GE90-94B, GE90-110B1 and 1 more. Effective Feb 6, 2026
- [AD 2025-07-10](https://openairdocs.org/ad/2025-07-10): Fuel Controlling System · General Electric Company GE GE90-110B1 and GE90-115B. Effective May 21, 2025
- [AD 2024-06-15](https://openairdocs.org/ad/2024-06-15): Turbine Section · General Electric GE90-110B1 and GE90-115B. Effective May 14, 2024
- [AD 2023-26-07](https://openairdocs.org/ad/2023-26-07): Turbine Section · General Electric GE90-90B, GE90-94B, GE90-110B1 and 1 more. Effective Feb 27, 2024
- [AD 2023-04-19](https://openairdocs.org/ad/2023-04-19): Turbine Engine Compressor Section · General Electric GE90-110B1 and GE90-115B. Effective Mar 27, 2023
- [AD 2022-23-09](https://openairdocs.org/ad/2022-23-09): Turbine Engine Compressor Section, Turbine Section · General Electric GE90-90B, GE90-94B, GE90-110B1 and 1 more. Effective Jan 17, 2023
- [AD 2022-18-06](https://openairdocs.org/ad/2022-18-06): Turbine Engine Compressor Section, Turbine Section · General Electric GE90-110B1, GE90-115B, GE90-76B and 3 more. Effective Oct 26, 2022
- [AD 2021-26-06](https://openairdocs.org/ad/2021-26-06): Turbine Engine Accessory Drive · General Electric GE90-76B, GE90-85B, GE90-90B and 3 more. Effective Feb 15, 2022
- [AD 2020-21-13](https://openairdocs.org/ad/2020-21-13): Turbine Section · General Electric GE90-110B1 and GE90-115B. Effective Nov 17, 2020
- [AD 2020-18-14](https://openairdocs.org/ad/2020-18-14): Turbine Section · General Electric GE90-110B1 and GE90-115B. Effective Oct 21, 2020
- [AD 2020-10-04](https://openairdocs.org/ad/2020-10-04): Turbine Section · General Electric GE90-110B1 and GE90-115B. Effective May 27, 2020
- [AD 2020-01-55](https://openairdocs.org/ad/2020-01-55): Turbine Section · General Electric GE90-110B1 and GE90-115B. Effective Mar 2, 2020
- [AD 2018-20-23](https://openairdocs.org/ad/2018-20-23): Turbine Engine Compressor Section · General Electric GE90-110B1 and GE90-115B. Effective Nov 30, 2018
- [AD 2018-20-22](https://openairdocs.org/ad/2018-20-22): Turbine Section · General Electric GE90-110B1, GE90-113B and GE90-115B. Effective Nov 13, 2018
- [AD 2017-08-06](https://openairdocs.org/ad/2017-08-06): Engine Oil Cooler · General Electric GE90-110B1, GE90-115B, GE90-76B and 3 more. Effective May 22, 2017
- [AD 2013-23-18](https://openairdocs.org/ad/2013-23-18): Variable bypass valve (VBV) actuator fuel supply tube · General Electric GE90-110B1 and GE90-115B. Effective Jan 7, 2014
- [AD 2013-17-07](https://openairdocs.org/ad/2013-17-07): Stage 1 high-pressure turbine (HPT) stator shrouds · General Electric GE90-110B1, GE90-115B, GE90-76B and 3 more. Effective Oct 18, 2013
- [AD 2013-15-20](https://openairdocs.org/ad/2013-15-20): Transfer gearbox assembly (TGB) radial gearshafts · General Electric GE90-110B1, GE90-113B, GE90-115B and 5 more. Effective Aug 21, 2013
- [AD 2011-26-11](https://openairdocs.org/ad/2011-26-11): HPC stages 1-2 seal teeth · General Electric GE90-110B1 and GE90-115B. Effective Feb 3, 2012
- [AD 2009-25-14](https://openairdocs.org/ad/2009-25-14): Blade · General Electric GE90-110B1, GE90-113B and GE90-115B. Effective Jan 19, 2010
- [AD 2007-10-05](https://openairdocs.org/ad/2007-10-05): Turbine Center Frames (TCFs) · General Electric GE90-110B1, GE90-113B and GE90-115B. Effective Jun 14, 2007

### Historical (superseded or no longer in force)

- [AD 2021-15-05](https://openairdocs.org/ad/2021-15-05) (historical): Engine Controls · General Electric GE90-110B1 and GE90-115B. Effective Sep 13, 2021
- [AD 2020-20-17](https://openairdocs.org/ad/2020-20-17) (historical): Engine Controls · General Electric GE90-110B1 and GE90-115B. Effective Oct 23, 2020
- [AD 2017-07-04](https://openairdocs.org/ad/2017-07-04) (historical): Compressor Section · General Electric GE90-110B1 and GE90-115B. Effective Apr 21, 2017
- [AD 2013-24-17](https://openairdocs.org/ad/2013-24-17) (historical): High pressure compressor (HPC) rotor stage 2-5 spools · General Electric GE90-110B1 and GE90-115B. Effective Dec 31, 2013
- [AD 2013-14-51](https://openairdocs.org/ad/2013-14-51) (historical): Failure of a transfer gearbox assembly radial gearshaft · General Electric GE90-110B1 and GE90-115B
- [AD 2013-10-52](https://openairdocs.org/ad/2013-10-52) (historical): Transfer gearbox assemblies (TGBs) · General Electric GE90-110B1 and GE90-115B. Effective Jun 26, 2013

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N862FD.

## FAA accident and incident reports

None matched to N862FD.

## Service difficulty reports (28)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR FDEA202207191765](https://openairdocs.org/sdr/FDEA202207191765), Jul 19, 2022: FLOOR PANEL. CRACKED. 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 MAJ
- [SDR FDEA202207181761](https://openairdocs.org/sdr/FDEA202207181761), Jul 18, 2022: FLOOR PANEL. CRACKED. 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 MAJ
- [SDR FDEA202207181759](https://openairdocs.org/sdr/FDEA202207181759), Jul 18, 2022: FLOOR PANEL. CRACKED. 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 MAJ
- [SDR FDEA202207181758](https://openairdocs.org/sdr/FDEA202207181758), Jul 18, 2022: FLOOR PANEL. CRACKED. 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 MAJ
- [SDR FDEA202207181757](https://openairdocs.org/sdr/FDEA202207181757), Jul 18, 2022: FLOOR PANEL. CRACKED. 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 MAJ
- [SDR FDEA202207181756](https://openairdocs.org/sdr/FDEA202207181756), Jul 18, 2022: FLOOR PANEL. CRACKED. 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 MAJ
- [SDR FDEA202207181755](https://openairdocs.org/sdr/FDEA202207181755), Jul 18, 2022: FLOOR PANEL. CRACKED. 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 MAJ
- [SDR FDEA202207181754](https://openairdocs.org/sdr/FDEA202207181754), Jul 18, 2022: FLOOR PANEL. CRACKED. 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 MAJ
- [SDR FDEA202206281598](https://openairdocs.org/sdr/FDEA202206281598), Jun 28, 2022: FLOOR PANEL. CRACKED. 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 MIN
- [SDR FDEA202206281597](https://openairdocs.org/sdr/FDEA202206281597), Jun 28, 2022: FLOOR PANEL. CRACKED. 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 MIN
- [SDR FDEA202206281596](https://openairdocs.org/sdr/FDEA202206281596), Jun 28, 2022: FLOOR PANEL. CRACKED. 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 MIN
- [SDR FDEA202206281595](https://openairdocs.org/sdr/FDEA202206281595), Jun 28, 2022: FLOOR PANEL. CRACKED. 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 MIN
- [SDR FDEA202206281594](https://openairdocs.org/sdr/FDEA202206281594), Jun 28, 2022: FLOOR PANEL. CRACKED. 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 MIN
- [SDR FDEA202206281593](https://openairdocs.org/sdr/FDEA202206281593), Jun 28, 2022: FLOOR PANEL. CRACKED. 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 MIN
- [SDR FDEA202206281592](https://openairdocs.org/sdr/FDEA202206281592), Jun 28, 2022: FLOOR PANEL. CRACKED. 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 MIN
- [SDR FDEA202206281587](https://openairdocs.org/sdr/FDEA202206281587), Jun 28, 2022: NONE. MECHANIC ERROR. 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 
- [SDR FDEA202206281586](https://openairdocs.org/sdr/FDEA202206281586), Jun 28, 2022: NONE. MECHANIC ERROR. 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 
- [SDR FDEA202206281585](https://openairdocs.org/sdr/FDEA202206281585), Jun 28, 2022: NONE. MECHANIC ERROR. 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 
- [SDR FDEA202206281584](https://openairdocs.org/sdr/FDEA202206281584), Jun 28, 2022: DOUBLER. NONE. 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, 
- [SDR FDEA202206281583](https://openairdocs.org/sdr/FDEA202206281583), Jun 28, 2022: NONE. NONE. 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 
- [SDR FDEA202111082795](https://openairdocs.org/sdr/FDEA202111082795), Nov 8, 2021: NONE. LEAKING. 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 
- [SDR FDEA202007310731](https://openairdocs.org/sdr/FDEA202007310731), Jul 30, 2020: GUARD. BROKEN. WITH EMERGENCY LIGHTS SWITCH CLOSED IT SHOWS OFF INSTEAD OF ARMED FOUND EMERGENCY LIGHTS SWITCH GUARD BROKEN, REMOVED AND REPLACED EMERGENCY LIGHTS SWITCH GUARD
- [SDR FDEA201708222331](https://openairdocs.org/sdr/FDEA201708222331), Aug 22, 2017: LINE. CHAFED. 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. ALER
- [SDR FDEA201704121139](https://openairdocs.org/sdr/FDEA201704121139), Apr 12, 2017: SKIN. DAMAGED. 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 
- [SDR FDEA201507092184](https://openairdocs.org/sdr/FDEA201507092184), Jul 9, 2015: SMOKE DETECTOR. FAILED. AT LEVEL OFF AT FL 340, RECEIVED A MOMENTARY MASTER CAUTION & EICAS MESSAGS, FOR SMOKE. AFTER RESEARCH DETERMINED FAULTY SMOKE DETECTOR. TROUBLESHOT FIM 26-16-0
- [SDR FDEA201309162238](https://openairdocs.org/sdr/FDEA201309162238), Sep 16, 2013: COVER. DAMAGED. 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.
- [SDR FDEA201305281108](https://openairdocs.org/sdr/FDEA201305281108), May 28, 2013: BATTERY. INOPERATIVE. 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.
- [SDR FDEA201112015102](https://openairdocs.org/sdr/FDEA201112015102), Dec 1, 2011: CONNECTOR. DAMAGED. 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

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Boeing 777-FS2 aircraft: https://openairdocs.org/model/boeing-777-fs2/aircraft.md
- The GE GE90-110B1 engine: https://openairdocs.org/engine/ge-ge90-110b1.md

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