# N880FD: 2009 Boeing 777F28

- Status: Valid registration
- Airframe: [Boeing 777F28](https://openairdocs.org/model/boeing-777f28) (registry code 138527E, 2 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: 32967
- Year built: 2009
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 2, 2010
- Certificate issued: March 23, 2010
- Expires: December 31, 2029
- Mode S code: AC1E56
- 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=880FD
- Page: https://openairdocs.org/aircraft/N880FD

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 777F28)

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 N880FD.

## FAA accident and incident reports

None matched to N880FD.

## Service difficulty reports (37)

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 FDEA202602170225](https://openairdocs.org/sdr/FDEA202602170225), Feb 17, 2026: SAFETY WIRE. WRONG PART. RIGHT SIDE DOOR SLIDE INSPECTION REVEALED THAT THE WRONG SAFETY WIRE WAS USED. THE WO REQUIRES REPLACING THE WIRE WITH MS20995CY16 CAD-PLATED COPPER WIRE. RH DO
- [SDR FDEA202508021365](https://openairdocs.org/sdr/FDEA202508021365), Aug 2, 2025: LIGHT. MALFUNCTIONED. EMERGENCY LIGHTS ILLUMINATED DURING BEFORE START CHECKLIST. AMM 33-51-00-5 FOUND EMERGENCY LIGHT SWITCH AT THE OVERHEAD PANEL IN THE OFF POSITION. SWITCH PUT BA
- [SDR FDEA202503140410](https://openairdocs.org/sdr/FDEA202503140410), Mar 14, 2025: SKIN. CRACKED. RH WING NO.8 SLAT OUTER SKIN FOUND CRACKED AT 51 IN TO IB EDGE. RH WING NO.8 SLAT OUTER SKIN AT 51 INCH TO I/B EDGE CRACK AREA REPAIRED AS PER B777 SRM51-10-02-
- [SDR FDEA202503050333](https://openairdocs.org/sdr/FDEA202503050333), Mar 5, 2025: SKIN. CRACKED. RH WING NO.8 SLAT OUTER SKIN FOUND CRACKED AT 39 IN TO IB EDGE. RH WING NO.8 SLAT OUTER SKIN AT 39 IN TO IB EDGE CRACK REPAIRED AS PER B777 SRM51-10- 02-0G,51-2
- [SDR FDEA202503050332](https://openairdocs.org/sdr/FDEA202503050332), Mar 5, 2025: SKIN. CRACKED. OPEN HOLE HFEC INSPECTION ON THE RH WING WBL 262 THEN FOUND HOLE #6 CRACK IN UPPER WING SKIN AS MARKED. RH WING WBL 262 UPPER SKIN #6 HOLE CRACK REPAIRED AS PER
- [SDR FDEA202503040326](https://openairdocs.org/sdr/FDEA202503040326), Mar 4, 2025: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 231RF P/N:152W8301-67 FOUND CRACKED AT STA 1014 LBL 84. MAIN DECK CARGO FLOOR PANEL 231RF P/N:152W8301-67 CRACKED AT STA 1014 LBL 84
- [SDR FDEA202410031414](https://openairdocs.org/sdr/FDEA202410031414), Oct 3, 2024: OUTFLOW VALVE. FAULTED. ON DEPARTURE, ACFT WOULD NOT PRESSURIZE. THE FWD OUTFLOW VALVE ON MEL. THE REMAINING AFT OUTFLOW VALVE INDICATED CLOSED ON DEPART BUT WOULD NOT ALLOW ACFT TO PR
- [SDR FDEA202304240753](https://openairdocs.org/sdr/FDEA202304240753), Apr 24, 2023: UNKNOWN. UNKNOWN. PDIS 880 31-50 3973 24APR23 MEM VMO GEAR DOWN STATUS MESSAGE. RETURNED TO MEM DUE TO UNABLE HIGHER ALTITUDE/AIRSPEED. AMM: 27-32-01-4 FIM: 31-51-00-810-957 TROU
- [SDR FDEA202304240752](https://openairdocs.org/sdr/FDEA202304240752), Apr 24, 2023: UNKNOWN. UNKNOWN. PDIS 880 31-50 3973 24APR23 MEM FACT U VMO GEAR DOWN STATUS MESSAGE. RETURNED TO MEM DUE TO UNABLE HIGHER ALTITUDE/AIRSPEED. FACT 24APR23 08:02 MEM U AMM: 27-32
- [SDR FDEA202209222354](https://openairdocs.org/sdr/FDEA202209222354), Sep 22, 2022: LAMP. INOPERATIVE. MDIS 880 33-50 3430 21SEP22 ANC OPEN U DURING PREFLIGHT FOUND CENTER OVERHEAD EMERGENCY LIGHT OUT DURING EMERGENCY LIGHT TEST. ALL OTHER LIGHTS OPERATE NORMALLY
- [SDR FDEA202207291819](https://openairdocs.org/sdr/FDEA202207291819), Jul 29, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8701-11 FOUND CRACKED AT STA1970 LBL40. REPAIRED MAIN DECK CARGO FLOOR PANEL P/N:152W8701-11 CRACKED AT STA 1970 LBL40 AS PE
- [SDR FDEA202207291818](https://openairdocs.org/sdr/FDEA202207291818), Jul 29, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8601-31 FOUND CRACKED AT STA1748 BL0. MAIN DECK CARGO FLOOR PANEL P/N: 152W8601-31 CRACKED AT STA1748 BL0 AS PER B777 SRM 53
- [SDR FDEA202207291817](https://openairdocs.org/sdr/FDEA202207291817), Jul 29, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8601-17 FOUND CRACKED AT STA1660 BL0. REPAIRED MAIN DECK CARGO FLOOR PANEL P/N:152W8601-19 CRACKED AT STA1660 BL0 AS PER B77
- [SDR FDEA202206261566](https://openairdocs.org/sdr/FDEA202206261566), Jun 26, 2022: TIRE. DELAMINATED. PDIS 880 32-41 3226 26JUN22 MEM FACT U SUSPECTED TIRE FAILURE ON TAKEOFF IN OSAKA. LANDED WITHOUT INCIDENT. TIRE DID INCUR FURTHER DAMAGE. NEED CHANGE RH NOSE W
- [SDR FDEA202106021435](https://openairdocs.org/sdr/FDEA202106021435), Jun 2, 2021: BRAKE ASSY. FIRE. AFTER BLOCK IN, #8 BRAKE CAUGHT FIRE. FIRE EXTINGUISHED BY RAMP CREW, THEN BY FIRE DEPARTMENT. REMOVED #8 BRAKE & WHEEL & PERFORMED HIGH ENERGY STOP/ HEAT DAMAG
- [SDR FDEA202009302365](https://openairdocs.org/sdr/FDEA202009302365), Sep 30, 2020: BATTERY. CORRODED. MDIS 880 52-20 1013 30SEP20 MEM. L1 EPAS BATTERY UNIT TERMINALS ARE CORRODED. FACT 30SEP20 21:38 MEM 0000086819 STEVENSON, BRIAN A-30-SEP-2020 14:10. REPLACED L
- [SDR FDEA202005291078](https://openairdocs.org/sdr/FDEA202005291078), May 29, 2020: BATTERY. DISCHARGED. POST FLIGHT INSPECTION. L-1 DOOR EPAS BATTERY PACK STATUS LIGHT NOT FLASHING. REMOVED AND REPLACED THE 2 9V BATTERIES FOR THE L-1 EPAS BATTERY PACK IAW AMM 52-1
- [SDR FDEA202002200358](https://openairdocs.org/sdr/FDEA202002200358), Feb 20, 2020: SKIN. DAMAGED. WHILE ACCOMPLISHING E.O. #G-5310-EO332629 D P5 FOUND EXISTING UNDERWING LONGERON FASTENER HOLE AT LEFT HAND STATION 1014 AND STRINGER 36 LEFT OVERSIZED TO 0.403
- [SDR FDEA202002200357](https://openairdocs.org/sdr/FDEA202002200357), Feb 20, 2020: SKIN. CRACKED. DURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND SIDE FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND 02 CRACK INDICATION AROUND F
- [SDR FDEA202002140333](https://openairdocs.org/sdr/FDEA202002140333), Feb 13, 2020: SKIN. CRACKED. DURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE UNDERWING LONGERON A
- [SDR FDEA202002140332](https://openairdocs.org/sdr/FDEA202002140332), Feb 13, 2020: SPAR. CRACKED. DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON RIGHT HAND SIDE UNDERWING LONGERON LOWER WING FRONT SPAR CHORD AND FOUND 01 EACH HOLE WIT
- [SDR FDEA2020020650268](https://openairdocs.org/sdr/FDEA2020020650268), Feb 5, 2020: LONGERON. CRACKED. DURING ULTRASONIC INSPECTION CARRIED OUT AT LEFT SIDE UNDERWING LONGERON AT BODY STATION 1035, FOUND CRACK INDICATIONS ON 02 EACH FASTENER AT VERTICAL FLANGE AN
- [SDR FDEA202002060267](https://openairdocs.org/sdr/FDEA202002060267), Feb 5, 2020: LONGERON. CRACKED. DURING ULTRASONIC INSPECTION CARRIED OUT AT RIGHT SIDE UNDERWING LONGERON AT BODY STATION 1035, FOUND CRACK INDICATIONS ON 02 EACH FASTENER AT VERTICAL FLANGE A
- [SDR FDEA2019101082496](https://openairdocs.org/sdr/FDEA2019101082496), Oct 8, 2019: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT TEST FAIL. FOUND LH SIDE EMERGENCY LIGHT BATTERY PACK UNSERVICEABLE. REPLACED BATTERY PACK ACC. AMM. 33-51-06. OPS CHECK FOUND SATISFACTORY.
- [SDR FDEA201805241313](https://openairdocs.org/sdr/FDEA201805241313), May 24, 2018: TRANSDUCER. LEAKING. 2.5 HOURS OUT OF ANC GOT "HYD QTY LOW C" FOLLOWED BY "RESERVE BRAKE/STEERING" EICAS. HYD QTY C STARTED AT .4 WHEN GOT EICAS AND OVER 1 HOUR WENT .01. FLAPS SLOW
- [SDR FDEA201710203012](https://openairdocs.org/sdr/FDEA201710203012), Oct 20, 2017: LAMP. FAILED. FOWARD STARBOARD EMERGENCY LIGHT DOES NOT WORK. REPLACED THE LAMPS AND TESTED OK IAW AMM 33-51-03-2.
- [SDR FDEA201706091598](https://openairdocs.org/sdr/FDEA201706091598), Jun 9, 2017: SKIN. CRACKED. DURING HFEC OPEN-HOLE INSPECION ON THE RT WING LEADING EDGE INBOARD SLAT NR 8 OUTER SKIN, FASTENER HOLES FOUND TO HAVE CRACK INDICATIONS. REPAIRED IAW SRM 57-43
- [SDR FDEA201706091597](https://openairdocs.org/sdr/FDEA201706091597), Jun 9, 2017: SKIN. CRACKED. DURING HFEC OPEN-HOLE INSPECION ON THE LT WING LEADING EDGE INBOARD SLAT NR 7 OUTER SKIN, FASTENER HOLES FOUND CRACK INDICATIONS. REPAIRED IAW SRM 57-43-01-2R, 
- [SDR FDEA201510163262](https://openairdocs.org/sdr/FDEA201510163262), Oct 16, 2015: LIGHT. INOPERATIVE. EMERGENCY LIGHT OVER R1 EXIT INOPERATIVE. RELAMPED & OPERATIONS CHECKED NORMAL, OK FOR SERVICE IAW MM 33-50-00-2.
- [SDR FDEA201409272823](https://openairdocs.org/sdr/FDEA201409272823), Sep 27, 2014: BALANCE WEIGHT. OUT OF POSITION. AS THE THROTTLES DECREASED AT TOP OF CLIMB THE AIRCRAFT DEVELOPED A SIGNIFICANT VIBRATION THAT COULD BE FELT & HEARD. THE LT ENG N1 VIBRATION WAS 3.2, ALL OTHER
- [SDR FDEA201409052470](https://openairdocs.org/sdr/FDEA201409052470), Sep 5, 2014: WARNING SYSTEM. FALSE ACTIVATION. THE FSS DISCHARGE LIGHT ILLUMINATED WITH NO OTHER INDICATIONS IN THE COCKPIT. THE FSS CONTROL PANEL SHOWED SUPPRESSING FIRE WITH A FAULT ILLUMINATED IN POS 2R. 
- [SDR FDEA201309132205](https://openairdocs.org/sdr/FDEA201309132205), Sep 13, 2013: LAMP. INOPERATIVE. RT EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED LAMPS AND CHECKED OK IAW AMM 33-51-04-2.
- [SDR FDEA201301260191](https://openairdocs.org/sdr/FDEA201301260191), Jan 26, 2013: SWITCH. INOPERATIVE. EMERGENCY LIGHTS SWITCH ON OVERHEAD PANEL IS OFF IN THE ARMED POSITION. REPAIRED EMERGENCY LIGHT SWITCH GUARD, OPS CHECKED OK.
- [SDR FDEA201210053568](https://openairdocs.org/sdr/FDEA201210053568), Oct 5, 2012: LAMP. INOPERATIVE. LEFT FORWARD CEILING EMERGENCY LIGHT INOPERATIVE. LAMPED IAW MM 33-50-00-003, ACFT OK FOR SERVICE.
- [SDR FDEA201109163929](https://openairdocs.org/sdr/FDEA201109163929), Sep 16, 2011: FITTING. DAMAGED. MAIN CARGO DOOR, LOCK BAR FITTINGS DAMAGED BY CONTACT WITH LOADING BRIDGE; 3 PLACES, LOCATED AT LATCH NR 2 FWD AND LATCH NR 3 FWD AND AFT. PERFORMED INTRIM REPA
- [SDR FDEA201103281205](https://openairdocs.org/sdr/FDEA201103281205), Mar 28, 2011: SPRING. OUT OF POSITION. EMERGENCY LIGHTS SWITCH WILL NOT ARM WITH SWITCH GAURD CLOSED. REPOSITIONED RETURN SPRING ON SWITCH GAURD. COMPLETED COCKPIT EMERGENCY LIGHTS OPERATIONAL TEST R
- [SDR FDEA201008273172](https://openairdocs.org/sdr/FDEA201008273172), Aug 27, 2010: ENGINE. BIRD INGESTION. THIS FLIGHT DEPARTED. STD TAKEOFF USED AND A BIRDSTRIKE OCCURRED AT HIGH SPEED, TWO THIRDS OF THE WAY DOWN THE RUNWAY. AN IMMEDIATE ODOR OCCURRED. TOWER REPORTE

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Boeing 777F28 aircraft: https://openairdocs.org/model/boeing-777f28/aircraft.md
- The GE GE90-110B1 engine: https://openairdocs.org/engine/ge-ge90-110b1.md

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