# N892FD: 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 GE90-90B](https://openairdocs.org/engine/ge-ge90-90b) (registry code 30036)
- Data sheets: [TCDS E00049EN](https://openairdocs.org/tcds/E00049EN) (General Electric Company GE Aviation) (OpenAirDocs)
- Serial number: 38707
- Year built: 2011
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 10, 2011
- Certificate issued: September 12, 2011
- Expires: September 30, 2027
- Mode S code: AC4D43
- Registered owner: [Federal Express Cor](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20COR)
- 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=892FD
- Page: https://openairdocs.org/aircraft/N892FD

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 GE90-90B)

- [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 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 2023-05-17](https://openairdocs.org/ad/2023-05-17): Turbine Section · General Electric GE90-76B, GE90-85B, GE90-90B and 1 more. Effective May 10, 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 2018-17-12](https://openairdocs.org/ad/2018-17-12): Turbine Engine Compressor Section · General Electric GE90-76B, GE90-77B, GE90-85B and 2 more. Effective Sep 24, 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 2017-08-05](https://openairdocs.org/ad/2017-08-05): Engine Compressor Section · General Electric GE90-76B, GE90-77B, GE90-85B and 2 more. Effective May 19, 2017
- [AD 2016-19-09](https://openairdocs.org/ad/2016-19-09): High-pressure compressor (HPC) · General Electric GE90-76B, GE90-77B, GE90-85B and 2 more. Effective Nov 4, 2016
- [AD 2015-27-01](https://openairdocs.org/ad/2015-27-01): High-pressure compressor (HPC) stage 8-10 spool · General Electric GE90-76B, GE90-77B, GE90-85B and 2 more. Effective Jan 27, 2016
- [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 2011-15-06](https://openairdocs.org/ad/2011-15-06): High-pressure compressor rotor (HPCR) · General Electric GE90-76B, GE90-77B, GE90-85B and 2 more. Effective Aug 18, 2011
- [AD 2002-04-11](https://openairdocs.org/ad/2002-04-11): Life Limits Section of Instructions for Continued Airworthiness (ICA) · General Electric GE90-76B, GE90-77B, GE90-85B and 2 more. Effective Apr 8, 2002
- [AD 2002-01-12](https://openairdocs.org/ad/2002-01-12): High Pressure Turbine (HPT) Interstage Seal · General Electric GE90-76B, GE90-77B, GE90-85B and 2 more. Effective Feb 26, 2002
- [AD 2002-01-27](https://openairdocs.org/ad/2002-01-27): High Pressure Compressor Stage 2-6 Spool · General Electric GE90-76B, GE90-77B, GE90-85B and 1 more. Effective Feb 14, 2002
- [AD 2001-21-03](https://openairdocs.org/ad/2001-21-03): P3B and Ps3 Sense Lines · General Electric GE90-76B, GE90-77B, GE90-85B and 1 more. Effective Nov 26, 2001
- [AD 2000-03-02](https://openairdocs.org/ad/2000-03-02): General Electric GE90-76B, GE90-85B and GE90-90B. Effective Apr 7, 2000
- [AD 97-12-05](https://openairdocs.org/ad/97-12-05): (VSCF) Gearshaft Flange ball Bearing · General Electric GE90-76B, GE90-77B, GE90-85B and 1 more. Effective Jun 27, 1997
- [AD 97-12-04](https://openairdocs.org/ad/97-12-04): Liberated CDP Manifold Material · General Electric Aircraft Engines GE90-92B, GE90-76B, GE90-77B and 2 more. Effective Jun 27, 1997

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

- [AD 2016-13-05](https://openairdocs.org/ad/2016-13-05) (historical): High-pressure compressor (HPC) stage 8-10 spool · General Electric GE90-76B, GE90-77B, GE90-85B and 2 more. Effective Jul 29, 2016
- [AD 2000-08-10](https://openairdocs.org/ad/2000-08-10) (historical): Life-limited Rotating Engine Parts · General Electric Aircraft Engines GE90-76B, GE90-77B, GE90-85B and 1 more. Effective Oct 23, 2000
- [AD 99-27-15](https://openairdocs.org/ad/99-27-15) (historical): Full Authority Digital Engine Control · General Electric Aircraft Engines GE90-76B, GE90-77B, GE90-85B and 17 more. Effective Jan 11, 2000
- [AD 99-08-17](https://openairdocs.org/ad/99-08-17) (historical): General Electric Aircraft Engines GE90-76B, GE90-77B, GE90-85B and 2 more. Effective May 13, 1999
- [AD 98-15-03](https://openairdocs.org/ad/98-15-03) (historical): High Pressure Compressor · General Electric Aircraft Engines GE90-76B, GE90-77B, GE90-85B and 17 more. Effective Jul 29, 1998

## Information bulletins (advisory) (1 in force)

- [SAIB NE-12-26](https://openairdocs.org/saib/NE-12-26): Fan Blade  GE90 Updated Inspections. Issued Apr 16, 2012

## NTSB investigations

None matched to N892FD.

## FAA accident and incident reports

None matched to N892FD.

## Service difficulty reports (26)

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 FDEA202512052223](https://openairdocs.org/sdr/FDEA202512052223), Dec 5, 2025: LAMP. NO TEST. PRE-FLT MX INSP, L1 DOOR OVRHD EMERGENCY LIGHT INOP. REPLACED THE LAMP, IAW AMM 33-50-00-2. EMERGENCY LIGHTS TEST SATIS, ITEM OK FOR SVC.
- [SDR FDEA202412301855](https://openairdocs.org/sdr/FDEA202412301855), Dec 30, 2024: HINGE. BINDING. CREW ENTRY DOOR 1L IS DIFFICULT TO OPEN. INSTALLED NEW HINGE MECHANISM ON L1 DOOR PER AMM 52-11-06-4 THROUGH COMPLETION OF STEP 3.D,
- [SDR FDEA202408051087](https://openairdocs.org/sdr/FDEA202408051087), Aug 5, 2024: LANDING GEAR. MALFUNCTIONED. AFTER TAKEOFF LFPG RWY 09R, NOSE GEAR FAILED TO RETRACT. RESULTING IN GEAR DISAGREE EICAS MESSAGE AND CHECKLIST POPULATING WITH GEAR HANDLE UP, NOSE GEAR DOWN I
- [SDR FDEA202405280738](https://openairdocs.org/sdr/FDEA202405280738), May 28, 2024: SKIN. DELAMINATED. NO. 7 SPOILER LWR SURFACE FROM OB TO IB 17 INCH CROSS TE TO LE 29.5 INCH FOUND DELAMINATION.` EVALUATED NO .7 SPOILER LOWER SURFACE FROM OB TO IB 17 INCH CROSS 
- [SDR FDEA202312261958](https://openairdocs.org/sdr/FDEA202312261958), Dec 26, 2023: SMOKE DETECTOR. FAILED. MAIN DECK AND LWR AFT CARGO FIRE LIGHT ILLUMINATED DURING COCKPIT SETUP. MX WAS CALLED AND SYSTEM CHECKED OK. BOTH LIGHTS AGAIN ILLUMINATED AFTER CLOSING THE EN
- [SDR FDEA202110012438](https://openairdocs.org/sdr/FDEA202110012438), Oct 1, 2021: DOUBLER. UNKNOWN. REQUEST BY CUSTOMER TO CREATE A SDR FOR EA G-5310-T0364043 P1 STEP 3 REPAIR FASTENER INTERFERENCE WITH LH LONGERON NEW DOUBLER (143W2314Y405) TRAILING EDGE DURI
- [SDR FDEA202109132294](https://openairdocs.org/sdr/FDEA202109132294), Sep 13, 2021: BEAM. CRACKED. FOUND FWD CARGO DOOR INNER SKIN CRACK AT STA 521 UPPER CARGO DOOR INNER SKIN CRACK REPAIRED AS PER EA: G-5230-T0364041 P1 TITLE: DOORS- CARGO DOOR 1 HYD SYS-HEA
- [SDR FDEA202109062227](https://openairdocs.org/sdr/FDEA202109062227), Sep 6, 2021: FLOOR PANEL. CRACKED. MAIN DECK CARGO STA 1397 RBL 38 FLOOR PANEL P//N:152W8452-20 FOUND CRACK MAIN DECK CARGO STA 1397 RBL 38 FLOOR PANEL P/N: 152W8452-20 REPAIRED AS PER B777 SRM 5
- [SDR FDEA202109062226](https://openairdocs.org/sdr/FDEA202109062226), Sep 6, 2021: FLOOR PANEL. CRACKED. MAIN DECK CARGO STA 1434 RBL 61 FLOOR PANEL P//N:152W8652-4 FOUND CRACK MAIN DECK CARGO STA 1434 RBL 61 FLOOR PANEL P/N: 152W8652-4 REPAIRED AS PER B777 SRM 53-
- [SDR FDEA202109062225](https://openairdocs.org/sdr/FDEA202109062225), Sep 6, 2021: FLOOR PANEL. CRACKED. MAIN DECK CARGO STA 1281 RBL 109 FLOOR PANEL P//N:152W8452-18 FOUND CRACK MAIN DECK CARGO STA 1281 RBL 109 FLOOR PANEL P/N: 152W8452-18 REPAIRED AS PER B777 SRM
- [SDR FDEA202109062224](https://openairdocs.org/sdr/FDEA202109062224), Sep 6, 2021: FLOOR PANEL. CRACKED. MAIN DECK CARGO STA 1455 RBL21 FLOOR PANEL P/N:152W8652-6 FOUND CRACK MAIN DECK CARGO STA 1455 RBL 21 FLOOR PANEL P/N: 152W8652-6 REPAIRED AS PER B777 SRM 53-00
- [SDR FDEA202109062222](https://openairdocs.org/sdr/FDEA202109062222), Sep 6, 2021: FLOOR PANEL. CRACKED. MAIN DECK CARGO STA 1405 LBL51 FLOOR PANEL P/N:152W8452-21 FOUND CRACK MAIN DECK CARGO STA 1405 LBL 51 FLOOR PANEL P/N: 152W8452-21 REPAIRED AS PER B777 SRM 53-
- [SDR FDEA202109042214](https://openairdocs.org/sdr/FDEA202109042214), Sep 4, 2021: FRAME. DAMAGED. FOUND 01EA LOWEST O/B HOLE WITH CRACK INDICATION ON LHS VERTIACL FLANGE OF THE SPAR CHORD AT UNDERWING LONGERON LOWER WING,BS1035 LBL82 AS PER W/C EG-5310- E033
- [SDR FDEA202109042213](https://openairdocs.org/sdr/FDEA202109042213), Sep 4, 2021: SKIN. CRACKED. SURFACE HFEC INSPECTION FOUND 02EA CRACKS(FWD CRACK APPROX 0.700INCH IN LENGTH AND AFT CRACK APPOX 0.950INCH IN LENGTH)ON THE EXTERNAL SURFACE OF THE FUSELAGE S
- [SDR FDEA202109042211](https://openairdocs.org/sdr/FDEA202109042211), Sep 4, 2021: SKIN. CRACKED. SURFACE HFEC INSPECTION FOUND 02EA CRACKS(FWD CRACK APPROX 0.900INCH IN LENGTH AND AFT CRACK APPROX 0.700INCH IN LENGTH) ON THE EXTERNAL SURFACE OF THE FUSELAGE
- [SDR FDEA202107201824](https://openairdocs.org/sdr/FDEA202107201824), Jul 20, 2021: TIRE. LOW PRESSURE. ENROUTE RECEIVED ALERT TIRE PRESS. TIRE 10 LOWEST PRESSURE 157. TIRE 9 LOWEST PRESSURE 198. EMERGENCY DECLARED. THE #10 TIRE WAS OUT OF LIMT, REPLACED #9 TIRE A
- [SDR FDEA202009162227](https://openairdocs.org/sdr/FDEA202009162227), Sep 16, 2020: LENS. DETACHED. MDIS 892 33-50 9488 16SEP20 MEM POST-FLT INSP, L-1 AFT EMERGENCY LT LENS DETACHED. FACT 16SEP20 06:49 MEM INSPECTEDD LT ASSY, FOUND RETAINING SET SCREW STAND-OF
- [SDR FDEA2018092522655](https://openairdocs.org/sdr/FDEA2018092522655), Sep 22, 2018: SLIDE. UNWANTED DEPLOY. PDIS 892 25-60 7128 21SEP18 ANC OPEN U LOGPAGES:2935476 SLIDE DOOR 1L DEPLOYED DURING DOOR CLOSING PRIOR TO BLOCK OUT NEW DOOR ESCAPE SLIDE FITTED I.A.W.B777 AM
- [SDR FDEA201710233030](https://openairdocs.org/sdr/FDEA201710233030), Oct 23, 2017: LINE. LEAKING. APPROACHING 50 FT CALL, DURING LANDING HYD QTY LOW C ANNUNCIATED. LANDED, STOPPED AT HIGH SPEED. FOUND HYD LEAKS FROM THE PRESSURE LINE OF THE LT PCU. R & R THE
- [SDR FDEA201709142551](https://openairdocs.org/sdr/FDEA201709142551), Sep 14, 2017: SIGN. INOPERATIVE. L1 DOOR FWD EMERGENCY EXIT SIGN HAS HALF BULBS BURNED OUT. REPLACED L1 DOOR FWD EMER EXIT SIGN IAW AMM 33-51-01-2 AND OPS CHECK GOOD. PN 702409-1001 CPN 3312328
- [SDR FDEA201701070076](https://openairdocs.org/sdr/FDEA201701070076), Jan 7, 2017: CTC. INOPERATIVE. LEFT PACK EICAS ILLUMINATED DURING DESCENT, PASSING FL240. RAN CHECKLIST, RESET THE LT PACK AND DID NOT RESET PROPERLY. TURNED THE LT PACK OFF AND RECIRCULATION
- [SDR FDEA201612284570](https://openairdocs.org/sdr/FDEA201612284570), Dec 28, 2016: BEAM. GOUGED. LOWER FORWARD LARGE CARGO DOOR HINGE ADJACENT AREA MID INNER SURFACE FOUND WITH DEEP GOUGE. LOWER FORWARD LARGE CARGO DOOR HINGE ADJACENT AREA MID INNER SURFACE
- [SDR FDEA201605121541](https://openairdocs.org/sdr/FDEA201605121541), May 12, 2016: LIGHT. INOPERATIVE. OVERHEAD EMER LIGHT NEXT TO 1L DOOR INOPERATIVE. RELAMPED OVERHEAD EMER LT IAW MM 33-51-03-2. OPERATIONS CHECKED SATISFACTORY. ACFT OK FOR SERVICE.
- [SDR FDEA201304290886](https://openairdocs.org/sdr/FDEA201304290886), Apr 29, 2013: TIRE. FAILED. DURING MX POST FLIGHT INSPECTION, NR 12 TIRE TREAD MISSING. R & R WHEEL IAW MM 32-45-01-4.
- [SDR FDEA201209073250](https://openairdocs.org/sdr/FDEA201209073250), Sep 7, 2012: SLIDE. UNWANTED DEPLOY. L1 ESCAPE SLIDE BLOWN. L1 DOOR SLIDE/RAFT REMOVED. REPLACED L1 DOOR SLIDE ASSY AND EPAS RESEVOIR IAW MM 25-66-01-4 AND 52-11-22-4.
- [SDR FDEA201203160969](https://openairdocs.org/sdr/FDEA201203160969), Mar 16, 2012: LAMP. INOPERATIVE. R2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED R2 DOOR EMERGENCY LIGHT. OPS CHECKED GOOD.

## 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 GE90-90B engine: https://openairdocs.org/engine/ge-ge90-90b.md

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