# N882FD: 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: 32969
- Year built: 2009
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Experimental, showing compliance
- Airworthiness date: July 8, 2020
- Certificate issued: April 13, 2010
- Expires: April 30, 2030
- Mode S code: AC25C4
- 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=882FD
- Page: https://openairdocs.org/aircraft/N882FD

From the FAA registry file of October 22, 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 N882FD.

## FAA accident and incident reports

None matched to N882FD.

## 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 FDEA202610051477](https://openairdocs.org/sdr/FDEA202610051477), Oct 5, 2026: HOSE. DISCONNECTED. ON POSTFLIGHT WALKAROUND FOUND NR 10 BRAKE HOSE DISCONNECTED AND HANGING. AMM: 32-45-07-4 RECONNECTED NR 10 BRAKE HOSE. REF AMM 32-45-07-4. OP'S CHECK GOOD, LEA
- [SDR FDEA202602150202](https://openairdocs.org/sdr/FDEA202602150202), Feb 15, 2026: SLIDE. NOT REPORTED. LH SLIDE ELECTRONIC CLOSURE FROM TRANSACTION MCFCTMOD, CLOSED DUE TO REMOVAL OF AFFECTED PART.
- [SDR FDEA202510222070](https://openairdocs.org/sdr/FDEA202510222070), Oct 22, 2025: SKIN. DENTED. REWORK: RH WING IB AFT FLAP LWR SURFACE FOUND DENT AT 58 INCHES TO OB EDGE AND 3 INCHES TO FWD EDGE. REPAIRED RH WING IB AFT FLAP LWR SURFACE DENT AT ITEF BS 27
- [SDR FDEA202510162033](https://openairdocs.org/sdr/FDEA202510162033), Oct 16, 2025: SKIN. DENTED. RH WING OB FLAP LWR SURFACE FOUND DENT AT 99.5 INCHES TO IB EDGE AND 11.5 INCHES TO AFT EDGE. REPAIRED RT WING OTBD FLAP LWR SURFACE DENT AT OTEF STA 99.5 IAW S
- [SDR FDEA202510152010](https://openairdocs.org/sdr/FDEA202510152010), Oct 15, 2025: SKIN. CRACKED. DURING PERFORMANCE OF WORK CARD: E G-5710-E0376285E, P12, STEP 3.B.(1), STEP 5.A.(2), & FOUND TWO CRACKS AT HOLE NR 5 OF RT UPPER WING SKIN COMMON TO FASTENERS 
- [SDR FDEA202510152009](https://openairdocs.org/sdr/FDEA202510152009), Oct 15, 2025: SKIN. CRACKED. DURING PERFORM WORK CARD:EG-5710-E0376285E P11 STEP 3.B.(1)&STEP 5.A.(2) AND FOUND TWO CRACKS AT HOLE #5 OF LH UPPER WING SKIN COMMON TO FASTENERS 0-5. LH WING 
- [SDR FDEA202501150071](https://openairdocs.org/sdr/FDEA202501150071), Jan 15, 2025: CONTROLLER. FAILED. ANTI ICE ENG L EICAS DISPLAYED IN FLIGHT. EMERGENCY DECLARED, T/S ACTIVE MX MSG 30-10291, FOUND SOLENOID ON LH ENG ANTI ICE CONTROLLER BAD, REMOVED AND REPLACED
- [SDR FDEA202405190689](https://openairdocs.org/sdr/FDEA202405190689), May 19, 2024: TIRE. LEAKING. ON CLIMB OUT GOT TIRE PRESS ALERT. RAN ECL AND TIRE PRESSURE SLOWLY DECREASED TO BELOW 50 PSI AND BEFORE DESCENT TO 7 PSI. LANDED UNEVENTFULLY 36C MEM. AIRPORT 
- [SDR FDEA202312231955](https://openairdocs.org/sdr/FDEA202312231955), Dec 23, 2023: SWITCH. FAILED. DURING POSTFLIGHT FOUND EMERGENCY LIGHT SWITCH IN THE FLIGHT DECK INTERMITTENT. AMM: 30-41-02-4 FIM: 33-51-00-2 PER ABOVE 777 FIM, REMOVED AND REPLACED WINDOW H
- [SDR FDEA202312231954](https://openairdocs.org/sdr/FDEA202312231954), Dec 23, 2023: MODULE. FAILED. DURING POSTFLIGHT FOUND EMERGENCY LIGHT SWITCH IN THE FLIGHT DECK INTERMITTENT. REMOVED AND REPLACED WINDOW HEAT/EMERGENCY LIGHTS MODULE PER ABOVE 777 AMM. OPS 
- [SDR FDEA202304210731](https://openairdocs.org/sdr/FDEA202304210731), Apr 21, 2023: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8601-31 FOUND CRACKED AT STA1780 RBL1. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8601-31 CRACK AT STA1780 RBL1. CRACK SI
- [SDR FDEA202304210730](https://openairdocs.org/sdr/FDEA202304210730), Apr 21, 2023: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8407-34 FOUND CRACKED AT STA1245 RBL55. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8407-34 CRACKED AT STA1245 RBL55.CRACK
- [SDR FDEA202304210729](https://openairdocs.org/sdr/FDEA202304210729), Apr 21, 2023: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8601-9 FOUND CRACKED AT STA1555 RBL1. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8601-9 CRACKED AT STA1555 RBL1.CRACK SIZ
- [SDR FDEA202201270753](https://openairdocs.org/sdr/FDEA202201270753), Jan 27, 2022: LAMP. FAILED. PDIS 882 33-50 2851 27JAN22 DXB STARBOARD CEILING EMERGENCY LIGHT IN SUPERNUMERARY INOP. RELAMPED STARBOARD SIDE AREA LIGHT & OPS CHK SATISFACTORY IAW AMM REF 3
- [SDR FDEA202008071783](https://openairdocs.org/sdr/FDEA202008071783), Aug 7, 2020: FLOOR SUPPORT. CRACKED. BULK CARGO COMPARTMENT BS 1937, RBL 49.8 ON REMOVAL OF FLOOR SUPPORT FOUND EDGE CRACKED. STRINGER REPAIRED AS PER B777 SRM 53-70-53-2R FIGURE 202 REPAIR 2 FROM 
- [SDR FDEA2020081821747](https://openairdocs.org/sdr/FDEA2020081821747), Aug 2, 2020: SKIN. CRACKED. 02 EACH CRACK FOUND APPROXIMATE 0.6" IN LENGTH FOR BOTH CRACK DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND SIDE FUSELAGE SKIN BETWEEN STATION 103
- [SDR FDEA2020081402747](https://openairdocs.org/sdr/FDEA2020081402747), Aug 2, 2020: SKIN. CRACKED. 02 EACH CRACK FOUND APPROXIMATE 0.6" IN LENGTH FOR BOTH CRACK DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND SIDE FUSELAGE SKIN BETWEEN STATION 103
- [SDR FDEA2020081421746](https://openairdocs.org/sdr/FDEA2020081421746), Aug 2, 2020: SKIN. CRACKED. CRACK FOUND APPROXIMATE 0.7" IN LENGTH DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND SIDE FUSELAGE SKIN AT APPROXIMATELY STATION 1030, STRINGER STR
- [SDR FDEA2020080321747](https://openairdocs.org/sdr/FDEA2020080321747), Aug 2, 2020: SKIN. CRACKED. TWO CRACKS FOUND APPROXIMATE 0.6" IN LENGTH FOR BOTH CRACKS FOUND DURING HIGH FREQUENCY EDDY CURRENT INSPECTION FUSELAGE SKIN BETWEEN BS 1030 AND 1035, STRINGER
- [SDR FDEA2020080321746](https://openairdocs.org/sdr/FDEA2020080321746), Aug 2, 2020: SKIN. CRACKED. CRACK FOUND APPROXIMATE 0.7" IN LENGTH, DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON THE FUSELAGE SKIN AT BS 1030, STRINGER 37L.
- [SDR FDEA2020080321745](https://openairdocs.org/sdr/FDEA2020080321745), Aug 2, 2020: SKIN. DAMAGED. WHILE ACCOMPLISHING EO G-5310-E0332629 G P6, FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT BS 998, STRINGER 35R NEAR MILLED EDGE.
- [SDR FDEA2020080321744](https://openairdocs.org/sdr/FDEA2020080321744), Aug 2, 2020: SKIN. DAMAGED. WHILE ACCOMPLISHING EO G-5310-E0332629 G P5 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT BS 998, STRINGER 35L NEAR MILLED EDGE.
- [SDR FDEA202007301725](https://openairdocs.org/sdr/FDEA202007301725), Jul 30, 2020: FLOOR SUPPORT. CRACKED. LOWER BULK CARGO COMPARTMENT BS 1916, RBL 49.8 FLOOR SUPPORT FOUND CRACKED. REPAIRED AS PER B777 SRM 53-70-53-2R FIGURE 202 REPAIR 2 FROM EXISTING SPLICE STATIO
- [SDR FDEA2020081421648](https://openairdocs.org/sdr/FDEA2020081421648), Jul 25, 2020: LONGERON. CRACKED. DURING ULTRASONIC INSPECTION CARRIED OUT AT LEFT HAND SIDE UNDERWING LONGERON AT BODY STATION 1035 AND STRINGER 36 FOUND 02 EA FASTENER HOLES WITH CRACK INDICAT
- [SDR FDEA2020081451647](https://openairdocs.org/sdr/FDEA2020081451647), Jul 25, 2020: LONGERON. CRACKED. DURING ULTRASONIC INSPECTION CARRIED OUT AT RIGHT HAND SIDE UNDERWING LONGERON AT BODY STATION 1035 AND STRINGER 36 FOUND 01EA FASTENER HOLES WITH CRACK INDICAT
- [SDR FDEA2020072751648](https://openairdocs.org/sdr/FDEA2020072751648), Jul 25, 2020: STRINGER. CRACKED. DURING ULTRASONIC INSPECTION CARRIED OUT AT LEFT HAND SIDE UNDERWING LONGERON AT BODY STATION 1035 AND STRINGER 36 FOUND 04EA FASTENER HOLES WITH CRACK INDICATI
- [SDR FDEA2020072751647](https://openairdocs.org/sdr/FDEA2020072751647), Jul 25, 2020: STRINGER. CRACKED. DURING ULTRASONIC INSPECTION CARRIED OUT AT RIGHT HAND SIDE UNDERWING LONGERON AT BODY STATION 1035 AND STRINGER 36 FOUND 03EA FASTENER HOLES WITH CRACK INDICAT
- [SDR FDEA201901110098](https://openairdocs.org/sdr/FDEA201901110098), Jan 11, 2019: SLEEVE. MISSING. FOUND DURING REMOVAL OF MAIN WHEEL NR 10 BRAKE SLEEVE ASSY MISSING. ADDITIONALLY FOUND CHARFING DAMAGE ON MAIN WHEEL ASSY AND BRAKE ASSY. C/W E.A. G-3242-T03445
- [SDR FDEA201710263059](https://openairdocs.org/sdr/FDEA201710263059), Oct 26, 2017: FLOOR SUPPORT. CRACKED. BULK CARGO FLOOR SUPPORT AT BS 1915 - 1920, RBL 42 FOUND CRACKED. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 53-70-53-2R, FIG 202, REPAIR 2. THE REPAIR WAS CLASSIFI
- [SDR FDEA201703220970](https://openairdocs.org/sdr/FDEA201703220970), Mar 22, 2017: SWITCH. BENT. ON ARRIVAL, DURING CONNECT FLT INTERPHONE FOUND EMER EXIT LIGHT TEST SWITCH BENT ON NLG. REPLACED THE TEST SWITCH.
- [SDR FDEA201605271742](https://openairdocs.org/sdr/FDEA201605271742), May 27, 2016: FMS. OUT OF DATE. REJECTED ON TAKEOFF DUE TO A FMC RNWY DISAGREE, CAUTION MSG ON EICAS. REJECT WAS AT 30 KT, ON RNWY 04 WINDS WERE 050 - 10 KTS. THE FMC IS AN MEL 34-61-01-03, RE
- [SDR FDEA201501030014](https://openairdocs.org/sdr/FDEA201501030014), Jan 3, 2015: LIGHT. INOPERATIVE. EMERGENCY CEILING LIGHT AT L1 DOOR IS INOPERATIVE. RELAMPED L1 DOOR AREA EMER LIGHT IAW AMM 33-50-00-2. OPERATIONS CHECKED NORMAL.
- [SDR FDEA201307221671](https://openairdocs.org/sdr/FDEA201307221671), Jul 22, 2013: SLIDE. LOW PRESSURE. R1 DOOR EMERGENCY SLIDE OUT OF GREEN BAND. R & R R1 DOOR EMERGENCY SLIDE IAW AMM 25-66-01-4. ACFT OK FOR SERVICE.
- [SDR FDEA201303120551](https://openairdocs.org/sdr/FDEA201303120551), Mar 12, 2013: BOTTLE. LOW PRESSURE. FOUND R1 DOOR SLIDE INDICATOR NEEDLE IN RED. R & R R1 DOOR SLIDE RAFT ASSY PER MM 25-66-01-4.
- [SDR FDEA201302210389](https://openairdocs.org/sdr/FDEA201302210389), Feb 21, 2013: LINE. LEAKING. F/O O2 MASK DOES NOT INFLATE CORRECTLY WHEN DONNING. F/O OXYGEN MASK HARNESS PIPE WAS LEAKING. R & R F/O OXYGEN MASK IAW MM 35-11-18-2.
- [SDR FDEA201109013627](https://openairdocs.org/sdr/FDEA201109013627), Sep 1, 2011: SPRING. OUT OF ADJUST. GUARD ON EMERGENCY LIGHTS SWITCH HAS MALFUNCTIONED; DOES NOT ARM SOMETIMES WHEN CLOSED. ADJUSTED SPRING ON SWITCH GUARD; SWITCH CHECKS GOOD REF AMM 33-51-00-5-0
- [SDR FDEA201105231930](https://openairdocs.org/sdr/FDEA201105231930), May 23, 2011: WARNING LIGHT. ILLUMINATED. AFTER LANDING DURING RUNWAY TURNOFF AT LESS THAN 10 KNOTS F/O SELECTED SPEED BRAKES UP ENGINES WENT TO MAX POWER ON GROUND. WITH ALERTS CONFIG GEAR/CONFIG FLAPS

## 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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