# N884FD: 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: 37137
- Year built: 2011
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 23, 2011
- Certificate issued: February 24, 2011
- Expires: February 28, 2030
- Mode S code: AC2D32
- 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=884FD
- Page: https://openairdocs.org/aircraft/N884FD

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 N884FD.

## FAA accident and incident reports

None matched to N884FD.

## Service difficulty reports (32)

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 FDEA202606010665](https://openairdocs.org/sdr/FDEA202606010665), Jun 1, 2026: FIRE BOTTLE. FAILED. AT 2335Z (APPROX 1:15 INTO THE FLIGHT), FL340, TAT -11, .838MACH, GOT BOTTLE DISCHARGE APU CAUTION WITH LIGHT APU BTL DSCG ON OVERHEAD AND BOTTLE APU ON STATUS 
- [SDR FDEA202605030534](https://openairdocs.org/sdr/FDEA202605030534), May 3, 2026: SKIN. DENTED. FOUND LEFT WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT AT THE CROSS OTEF 127 INCHES AND T/E 10 INCHES. REPAIRED LH WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT
- [SDR FDEA202605030533](https://openairdocs.org/sdr/FDEA202605030533), May 3, 2026: SKIN. DENTED. FOUND LEFT WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT AT THE CROSS OTEF 231 INCHES AND T/E 8 INCHES. REPAIRED LH WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT 
- [SDR FDEA202604300524](https://openairdocs.org/sdr/FDEA202604300524), Apr 30, 2026: SKIN. CRACKED. DURING PERFORM WORK CARD:EG-5710-E0376285 G P12 STEP 3.B.(1) & STEP 5.A.(2) THEN FOUND 02EA CRACK AT RH WING UPPER WING SKIN COMMON TO FASTENER 5. RT WING UPPER
- [SDR FDEA202604300523](https://openairdocs.org/sdr/FDEA202604300523), Apr 30, 2026: SKIN. CRACKED. DURING PERFORM WORK CARD:EG-5710-E0376285 G P11 STEP 3.B.(1) & STEP 5.A.(2) THEN FOUND 02EA CRACK AT LT WING UPPER WING SKIN COMMON TO FASTENER 5. LT WING UPPER
- [SDR FDEA202509231776](https://openairdocs.org/sdr/FDEA202509231776), Sep 23, 2025: SPRING. DAMAGED. WHILE CLOSING DOOR 1L, AN INTERIOR SPRING BROKEN. REMOVED AND REPLACED 2 EACH SPRINGS ON VENT DOOR ASSY IAW AMM 52-11-04-4-0.
- [SDR FDEA202411231725](https://openairdocs.org/sdr/FDEA202411231725), Nov 23, 2024: MODULE. INOPERATIVE. REF MTSI 33-50/4453, EMERGENCY LIGHT SW ON OVHD PANEL FOUND TO BE INTERMITTENT INOP. R/RED WINDOW HEAT/EMER LIGHTS MODULE, INSTALLATION TEST PASSED. EMERGENCY L
- [SDR FDEA202411191687](https://openairdocs.org/sdr/FDEA202411191687), Nov 19, 2024: LIGHT. MALFUNCTIONED. EMERGENCY LIGHTS WOULD NOT SHUTOFF ON ENGINE SHUTDOWN CHECKLIST PERFORMED ENG SHUTDOWN CHKL RESET. EMER LT OPTION TURN GREEN, CHKL BACK TO NORMAL. A/C OK FOR SV
- [SDR FDEA202403200317](https://openairdocs.org/sdr/FDEA202403200317), Mar 20, 2024: POWER CABLE. CHAFED. FO EFB POWER CORD AT MAGNETIC PLUG HAD ELECTRICAL SPARKS AND ARCING IN FLIGHT. DISCONNECTED POWER CORD FROM EFB. DO NOT RECONNECT THE OLD CORD. F/O EFB POWER CO
- [SDR FDEA202309271662](https://openairdocs.org/sdr/FDEA202309271662), Sep 27, 2023: POWER SUPPLY. FAILED. EMERGENCY LIGHTS WILL NOT EXTINGUISH WHEN TESTED. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLIES ABOVE L1 DOOR AND R1 DOOR REF. AMM 33-51-06-2. ALL LIGHTS 
- [SDR FDEA202308171453](https://openairdocs.org/sdr/FDEA202308171453), Aug 17, 2023: SKIN. BENT. RH WING NO.10 SLAT OUTER SKIN FOUND BULGE AT WS 657-661 AND 19.5 IN AWAY FROM AFT EDEG. RH WING NO.10 SLAT OUTER SKIN BULGE AREA AT WS 657-661 AND 19.5 IN AWAY 
- [SDR FDEA202308161448](https://openairdocs.org/sdr/FDEA202308161448), Aug 16, 2023: SKIN. DENTED. LH OB FLAP LOWER SURFACE FROM IB TO OB 15.5 INCH CROSS TE TO LE 4 INCH FOUND ONE DENT. EVALUATED LH OB FLAP LOWER SURFACE FROM IB TO OB 15.5 INCH CROSS TE TO LE
- [SDR FDEA202104090855](https://openairdocs.org/sdr/FDEA202104090855), Apr 9, 2021: SKIN. CRACKED. FUSELAGE LEFT HAND BILGE AREA AT STATION 1685 AREA FOUND WITH EXISTING BLENDOUT . FUSELAGE LEFT HAND BILGE AREA AT STATION 1685 AREA STRINGER-47 LEFT EXISTING B
- [SDR FDEA202104010805](https://openairdocs.org/sdr/FDEA202104010805), Apr 1, 2021: FLOOR SUPPORT. CRACKED. BULK CARGO - FLOOR PANEL STRINGER AT RBL 41.5 FOUND 02 EA CRACKS AT STA 1937 AND STA 1958 AS MARKED. BULK CARGO FLOOR PANEL STRINGER AT RBL 41.5 AT STA 1937 AND
- [SDR FDEA202103300798](https://openairdocs.org/sdr/FDEA202103300798), Mar 30, 2021: DOUBLER. MISALIGNED. WHILE ACCOMPLISHING LH E.O.#G-5310-E0332629 K P5 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STA 998 STR S-35L NEAR MILLED EDGE. COMPLIED WITH E.A.# G-5310
- [SDR FDEA202103300797](https://openairdocs.org/sdr/FDEA202103300797), Mar 30, 2021: DOUBLER. MISALIGNED. WHILE ACCOMPLISHING RH E.O.#G-5310-E0332629 K P6 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STA 998 STR S-35R NEAR MILLED EDGE. COMPLIED WITH E.A.# G-5310
- [SDR FDEA202103290793](https://openairdocs.org/sdr/FDEA202103290793), Mar 29, 2021: FITTING. CRACKED. DURING HFEC OPEN HOLE INSPECTION CARRIED OUT AS PER EO NO: E-G-5310-E0332629 K P5 ON REMOVED FASTENER HOLES AND FOUND 01 EA CRACK INDICTION ON LHS VERTICAL FLAN
- [SDR FDEA202103290792](https://openairdocs.org/sdr/FDEA202103290792), Mar 29, 2021: FITTING. CRACKED. DURING HFEC OPEN HOLE INSPECTION CARRIED OUT AS PER EO NO: E-G-5310-E0332629 K P6 ON REMOVED FASTENER HOLES AND FOUND 01 EA CRACK INDICATION ON RHS VERTICAL FLA
- [SDR FDEA201908211991](https://openairdocs.org/sdr/FDEA201908211991), Aug 21, 2019: LAMP. INOPERATIVE. POST-FLT INSP, ONE OVERHEAD SUPRNMRY EMERGENCY LIGHT INOPERATIVE DURING A LIGHTS TEST. REPLACED THE LAMP, IAW AMM: 33-51-04-2. LIGHT TESTED SATIS, OK FOR SERVIC
- [SDR FDEA201705041358](https://openairdocs.org/sdr/FDEA201705041358), May 4, 2017: LATCH. DAMAGED. PREFLIGHT MX CHECK, FOUND THE L1 DOOR EMERGENCY ESCAPE SLIDE COVER SHROUD FWD LATCH DEFORMED AND NOT RETAINING SHROUD ASSY. REMOVED AND REPLACED L1 DOOR BUSTLE 
- [SDR FDEA201702220625](https://openairdocs.org/sdr/FDEA201702220625), Feb 22, 2017: LAMP. INOPERATIVE. DURING A POST FLIGHT INSPECTION, ONE OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-50-00-2. LIGHTS TESTED GOOD, OK FOR SERVICE.
- [SDR FDEA201601210273](https://openairdocs.org/sdr/FDEA201601210273), Jan 21, 2016: SKIN. PUNCTURED. FORWARD LOWER FUSELAGE SKIN AT STATION 630, BETWEEN STRINGER 34R - 35R, FOUND A 2" PUNCTURE HOLE. REPAIR IDENTIFIED AS MAJOR REPAIR BY ENGINEERING. EA G-5330-T0
- [SDR FDEA201506101753](https://openairdocs.org/sdr/FDEA201506101753), Jun 10, 2015: BULB. INOPERATIVE. ONE OVERHEAD EMERGENCY EXIT LIGHT DID NOT ILLUMINATE DURING CABIN INSPECTION. R & R THE OVERHEAD EMERGENCY EXIT LIGHT & OPS CHECKED NORMAL IAW AMM 33-51-03-2.
- [SDR FDEA201501130144](https://openairdocs.org/sdr/FDEA201501130144), Jan 13, 2015: LIGHT. INOPERATIVE. POST FLIGHT CHECK FOUND 1 SUP AREA EMER LT INOPERATIVE. RELAMPED IAW AMM 33-51-03-2. EMER LIGHTS TESTED NORMAL. ITEM OK FOR SERVICE.
- [SDR FDEA201407041627](https://openairdocs.org/sdr/FDEA201407041627), Jul 4, 2014: BATTERY PACK. DISCHARGED. ON POST FLIGHT CHECK FOUND L1 DOOR EMER ASSIST BATTERY PACK GREEN TEST LIGHT NOT FLASHING. R & R L1 DOOR ASSIST BATTERY PACK TEST LIGHT 9V BACK UP BATTERIES TWO
- [SDR FDEA201405110984](https://openairdocs.org/sdr/FDEA201405110984), May 11, 2014: SLIDE. DEPLOYED. DOOR L1 SLIDE DEPLOYED. REMOVED L1 DOOR MOUNTED SCAPE SYS IAW MM 25-66-00-2. RESTORED DOOR MOUNTED ESCAPE SLIDE SYS AFTER SLIDE DEPLOYMENT. 2 SLIDE SAFETY PINS,
- [SDR FDEA201307231644](https://openairdocs.org/sdr/FDEA201307231644), Jul 23, 2013: TIRE. LEAKING. TIRE PRESSURE EICAS MESSAGE. NR 3 MLG TIRE PRESSURE 180 PSI DECREASED TO 160 PSI. REMAINED AT 160 PSI AFTER LANDING. VERIFIED NR 3 TIRE PRESSURE IS LOW. R & R N
- [SDR FDEA201306151305](https://openairdocs.org/sdr/FDEA201306151305), Jun 15, 2013: AUTOPILOT SYS. MALFUNCTIONED. ACFT WENT INTO AN UNCOMMANDED RIGHT TURN. NOTICED IT HAD GONE INTO HDG MODE AND THE HDG WAS APPROX 112 DEGREES (VS. 030) F/O DISCONNECTED AUTOPILOT AND BANKS 30
- [SDR FDEA201211224125](https://openairdocs.org/sdr/FDEA201211224125), Nov 22, 2012: INTERFACE UNIT. INOPERATIVE. APPROX 2.5 HRS INTO FLIGHT, RECIEVED HYD QTY LOW R CAUTION MESSAGE. OBSERVED CONTINUOUS DROP IN RIGHT HYD QTY THROUGHOUT REMAINDER OF FLIGHT, DIVERTED. R & R RT
- [SDR FDEA201203281167](https://openairdocs.org/sdr/FDEA201203281167), Mar 28, 2012: COMPUTER. MALFUNCTIONED. FLIGHT PLAN WAS LOADED VIA UPLINK. FLIGHT PLAN WAS CHECKED IN CAPTAINS PREFIGHT ON PLAN PAGE FOR PROPER SEQUENCING AND VERIFIED WITH F/O THROUGH CFM PROCEDURES.
- [SDR FDEA201110074382](https://openairdocs.org/sdr/FDEA201110074382), Oct 7, 2011: BATTERY. INOPERATIVE. FOUND R1 DOOR EPAS POWER GREEN LIGHT DOES NOT COMES ON. REPLACED EPAS POWER PACK BACKUP BATT AND CHECK OK IAW MM52-11-20-4-2, 52-11-20-5-2. ACFT OK FOR SERVICE.
- [SDR FDEA201103150981](https://openairdocs.org/sdr/FDEA201103150981), Mar 15, 2011: LIGHT. INOPERATIVE. R-1 DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE R1 DOOR EMERGENCY EXIT LIGHT.

## 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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