# N890FD: 2012 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: 41439
- Year built: 2012
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 1, 2012
- Certificate issued: August 1, 2012
- Expires: August 31, 2028
- Mode S code: AC45D5
- 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=890FD
- Page: https://openairdocs.org/aircraft/N890FD

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 N890FD.

## FAA accident and incident reports

None matched to N890FD.

## 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 FDEA202604240496](https://openairdocs.org/sdr/FDEA202604240496), Apr 24, 2026: BULB. INOPERATIVE. R1 DOOR AFT EMERGENCY EXIT SIGN LIGHT INOP (1EA BULB). REPLACED THE BULB EMERGENCY EXIT LIGHT AT R1 DOOR IAW AMM 33-51-01-2.
- [SDR FDEA202602150211](https://openairdocs.org/sdr/FDEA202602150211), Feb 15, 2026: SAFETY WIRE. WRONG PART. WRI TO REPLACE THE R1 DOOR SLIDE WIRE WITH MS20995CY16 WIRE. AMM: 25-66-01-4 REPLACED R1 DOOR SLIDE SHEAR WIRE WITH MS20995CY16 WIRE PER REF ABOVE
- [SDR FDEA202505010702](https://openairdocs.org/sdr/FDEA202505010702), May 1, 2025: SKIN. CHAFED. FWD CARGO DOOR SURROUND FWD EDGE AT 10.5" FROM BOTTOM FOUND CHAFFED. FWD CARGO DOOR SURROUND FWD EDGE AT 10.5" FROM BOTTOM CHAFFED AREA REPAIRED AS PER B777 SRM
- [SDR FDEA202505010701](https://openairdocs.org/sdr/FDEA202505010701), May 1, 2025: SKIN. DENTED. FOUND RHW T/E O/B FLAP LOWER SURFACE DENT 01 EA AT THE CROSS OTEF 263 AND T/E 4 INCHES. REPAIRED RHW T/E O/B FLAP LOWER SURFACE DENT 01 EA AT THE CROSS OTEF 263
- [SDR FDEA202505010700](https://openairdocs.org/sdr/FDEA202505010700), May 1, 2025: SKIN. DENTED. FOUND RHW T/E I/B FLAP LOWER SURFACE DENT (LENGTH 15.5 INCHES AND WIDE 13.5 INCHES) AT THE CROSS ITEF 260 AND T/E 21 INCHES. REPAIRED RHW T/E I/B FLAP LOWER SUR
- [SDR FDEA202505010698](https://openairdocs.org/sdr/FDEA202505010698), May 1, 2025: SKIN. CRACKED. OPEN HOLE HFEC INSPECTION OF #5 HOLE AT RH WING UPPER SKIN WBL 262 AND FOUND 01EA CRACK AS MARKED. RH WING UPPER SKIN WBL 262 #5 HOLE CRACKED AREA REPAIRED AS P
- [SDR FDEA202505010697](https://openairdocs.org/sdr/FDEA202505010697), May 1, 2025: SKIN. CRACKED. OPEN HOLE HFEC INSPECTION OF #5 HOLE AT LH WING UPPER SKIN WBL262 AND FOUND 01EA CRACK AS MARKED. LH WING UPPER SKIN WBL 262 #5 HOLE CRACKED AREA REPAIRED AS PE
- [SDR FDEA202412041774](https://openairdocs.org/sdr/FDEA202412041774), Dec 4, 2024: NONE. NONE. CREW WAS NOTIFIED ENROUTE THAT PER MEL RESTRICTION THE AFT BELLY POSITION A3L WAS LOADED 736 POUNDS OVER THE MEL RESTRICTION. LOWER DECK CARGO RESTRAINING SYSTE
- [SDR FDEA202210072506](https://openairdocs.org/sdr/FDEA202210072506), Oct 7, 2022: DOUBLER. MISREPAIRED. DURING PERFORMING EO G-5710-E0365655 B P8 STEP8.C.(5), FOUND 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 RHS TOO CLOSE TO EDGE OF MACHINED STE
- [SDR FDEA2022101172505](https://openairdocs.org/sdr/FDEA2022101172505), Oct 7, 2022: DOUBLER. MISREPAIRED. DURING PERFORMING EO G-5710-E0365655 B P7 STEP8.C.(5), FOUND 01EA ZLJ-8 COUNTERSUNK FASTENER AT STA 998 S35L TOO CLOSE TO EDGE OF MACHINED STEP OF DOUBLER P/N 1
- [SDR FDEA202210032455](https://openairdocs.org/sdr/FDEA202210032455), Oct 3, 2022: SKIN. DENTED. RHW T/E O/B FLAP MIDDLE LOWER SURFACE FOUND 1EA DENT AT 310" TO O/B CROSS 10" TO T/E. RHW T/E O/B FLAP MIDDLE LOWER SURFACE AT 310" TO O/B CROSS 10" TO T/E REPA
- [SDR FDEA202210032454](https://openairdocs.org/sdr/FDEA202210032454), Oct 3, 2022: SKIN. DENTED. LH WING O/B FLAP LOWER SURFACE FROM O/B TO I/B 39" CROSS AFT TO FWD 6" AREA FOUND DENTED. LH WING O/B FLAP LOWER SURFACE FROM O/B TO I/B 39" CROSS AFT TO FWD 6"
- [SDR FDEA202210022450](https://openairdocs.org/sdr/FDEA202210022450), Oct 2, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 242LF(P/N:152W8452-20) AT STA1413/RBL38.5-40 FOUND CRACK. REPAIRED MAIN DECK CARGO FLOOR PANEL 242LF(P/N:152W8452-20) AT STA1413/RBL
- [SDR FDEA202210022449](https://openairdocs.org/sdr/FDEA202210022449), Oct 2, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 242PF(P/N:152W8652-6) AT STA1439.5/RBL22-25.5 FOUND CRACK. REPAIRED MAIN DECK CARGO FLOOR PANEL 242PF (P/N:152W8652-6)AT STA 1439.5/
- [SDR FDEA202210022448](https://openairdocs.org/sdr/FDEA202210022448), Oct 2, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 242QF(P/N:152W8652-4) AT STA1445.5/RBL73-75 FOUND CRACK. REPAIRED MAIN DECK CARGO FLOOR PANEL 242QF(P/N:152W8652-4) AT STA1445.5/RBL
- [SDR FDEA202210022447](https://openairdocs.org/sdr/FDEA202210022447), Oct 2, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 241PF(P/N:152W8452-19) AT STA1388.75/LBL38.5-40 FOUND CRACK. REPAIRED MAIN DECK CARGO FLOOR PANEL 241PF(P/N:152W8452-19) AT STA1388.
- [SDR FDEA202210022446](https://openairdocs.org/sdr/FDEA202210022446), Oct 2, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 241QF(P/N:152W8452-21) AT STA1383.5/LBL43.75-45.5 FOUND CRACK. REPAIRED MAIN DECK CARGO FLOOR PANEL 241QF(P/N:152W8452-21) AT STA138
- [SDR FDEA202210022445](https://openairdocs.org/sdr/FDEA202210022445), Oct 2, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 242KF(P/N:152W8452-18) AT STA1255-1256.25/RBL87.5 FOUND CRACK. REPAIRED MAIN DECK CARGO FLOOR PANEL 242KF(P/N:152W8452-18) AT STA125
- [SDR FDEA202210022444](https://openairdocs.org/sdr/FDEA202210022444), Oct 2, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 241UF(P/N:152W8652-3) AT STA1446/LBL57-57.5 FOUND CRACK. REPAIRED MAIN DECK CARGO FLOOR PANEL 241UF(P/N:152W8652-3) AT STA1446/LBL57
- [SDR FDEA202209032157](https://openairdocs.org/sdr/FDEA202209032157), Sep 3, 2022: PUMP. FAILED. HYDRAULIC QUANTITY CENTER LOW NNC FOLLOWED BY RESERVE BRAKES STRG NNC. BOTH ECL CHECKLISTS RUN, SLOW LOSS OF CENTER HYDRAULIC QUANTITY UNTIL TOUCHDOWN. NORMAL E
- [SDR FDEA202209022146](https://openairdocs.org/sdr/FDEA202209022146), Sep 2, 2022: PUMP. LEAKING. PDIS 890 29-02 0368 02SEP22 KIX HYDRAULIC QUANTITY CENTER LOW NNC FOLLOWED BY RESERVE BRAKES STRG NNC. BOTH ECL CHECKLISTS RUN, SLOW LOSS OF CENTER HYDRAULIC QU
- [SDR FDEA2020061091156](https://openairdocs.org/sdr/FDEA2020061091156), Jun 9, 2020: SKIN. PUNCTURED. LT WING NR 5 SPOILER UPPER SURFACE FOUND PUNCTURE DAMAGE AT WS722. LEFT HAND WING NR 5 SPOILER UPPER SURFACE PUNCTURE DAMAGE AT WING STATION 717 TO WING STATION
- [SDR FDEA202006051132](https://openairdocs.org/sdr/FDEA202006051132), Jun 5, 2020: SKIN. PUNCTURED. LT WING NR 5 SPOILER UPPER SURFACE FOUND PUNCTURE DAMAGE AT WS 717. LEFT HAND WING NR 5 SPOILER UPPER SURFACE AT WING STATION 717 TO WING STATION 722. REPAIRED 
- [SDR FDEA202006051131](https://openairdocs.org/sdr/FDEA202006051131), Jun 5, 2020: SKIN. PUNCTURED. LT WING NR 3 SPOILER UPPER SURFACE FOUND PUNCTURE DAMAGE AT WS907. LEFT HAND WING NR 3 SPOILER UPPER SURFACE PUNCTURE DAMAGE AT WING STATION 907. REPAIRED AND S
- [SDR FDEA202005221030](https://openairdocs.org/sdr/FDEA202005221030), May 22, 2020: SKIN. CRACKED. DURING ACCOMPLISHMENT OF MEDIUM FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND WING SLAT NR 5 OUTER SKIN FOUND 01 EACH CRACK. INDICATION AT FASTENER HOLE AT STA
- [SDR FDEA201907041482](https://openairdocs.org/sdr/FDEA201907041482), Jul 4, 2019: COOLING FAN. JAMMED. FUMES IN COCKPIT NO CAUTION OR WARNING DISPLAYED FUMES DETECTED BY SMELL-DISIPATED AFTER RIGHT EQUIP COOLING FAN WAS DEACTIVATED. FLIGHT SAFETY REPORT FILED. DE
- [SDR FDEA201804281140](https://openairdocs.org/sdr/FDEA201804281140), Apr 28, 2018: SLIDE. LOW PRESSURE. L1 SLIDE RAFT PRESSURE LOW. R/RD L1 SLIDE RAFT PER AMM 25-66-01-4. REMOVED SLIDE RAFT.
- [SDR FDEA201702090493](https://openairdocs.org/sdr/FDEA201702090493), Feb 9, 2017: COVER. MISSING. COVER FOR EXIT LIGHT ON LEFT SIDE OF L1 DOOR IS MISSING, INSTALLED A NEW EMERGENCY EXIT LIGHT COVER.
- [SDR FDEA201702090492](https://openairdocs.org/sdr/FDEA201702090492), Feb 9, 2017: COVER. MISSING. COVER FOR THE EXIT LIGHT ON THE LT SIDE OF THE L1 DOOR IS MISSING. INSTALLED THE EXIT SIGN ASSY AND COVER SMP. LIGHT CHECKED OK.
- [SDR FDEA201503050686](https://openairdocs.org/sdr/FDEA201503050686), Mar 5, 2015: HANDLE. OUT OF POSITION. HAD TO OPEN LT WINDOW TO MAKE TURN INTO GATE. WINDOW WILL NOT LOCK CLOSED. FOUND LT WINDOW LOCKING HANDLE IN THE INCORRECT POSITION. OPENED & CLOSED LT WINDOW S
- [SDR FDEA201410042965](https://openairdocs.org/sdr/FDEA201410042965), Oct 4, 2014: GIRT BAR. OUT OF ADJUST. L1 DOOR WILL NOT ARM. ADJUSTED GIRT BAR, OPS CHECKED GOOD IAW MM 52-11-00-5.
- [SDR FDEA201409122603](https://openairdocs.org/sdr/FDEA201409122603), Sep 12, 2014: SPRING. MISSING. EMERGENCY LIGHTS SWITCH IS MISSING INTERNAL SPRING CLIP, DOES NOT DISARM OR ARM EMER LIGHTS WHEN COVER IS POSITIONED DOWN OR WHEN SELECTED TO OFF. R & R EMER LI

## 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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