# N863FD: 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: 37734
- Year built: 2012
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 22, 2012
- Certificate issued: March 23, 2012
- Expires: March 31, 2028
- Mode S code: ABDA7D
- 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=863FD
- Page: https://openairdocs.org/aircraft/N863FD

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 N863FD.

## FAA accident and incident reports

None matched to N863FD.

## Service difficulty reports (33)

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 FDEA202602150204](https://openairdocs.org/sdr/FDEA202602150204), Feb 15, 2026: RELEASE CABLE. WRONG PART. RIGHT SLIDE PACKBOARD RELAEASE CABLE MECHANISM REQUIRES CAD PLATED COPPER BREAKAWAY WIRE. REF WRI 25-60/4116 FEA 2560-F0386282 C P1. SAFETIED RT SLIDE PACKBOARD
- [SDR FDEA202602150203](https://openairdocs.org/sdr/FDEA202602150203), Feb 15, 2026: SLIDE. FOM. L1 DOOR SLIDE REMOVED FOR F.O.M. OF F.E.A. MOD TYPE F MOD NR G-2560-F0386282 REV NR C PS P1. INSTALLED L1 DOOR SLIDE OPS CHECKS GOOD IAW AMM 25-66-01-4, & AMM 2
- [SDR FDEA202508261542](https://openairdocs.org/sdr/FDEA202508261542), Aug 26, 2025: LAMP. NO TEST. ON ARRIVAL FOUND DOOR 1L INTERIOR FWD EMERGENCY LIGHT NO FULLY ILLUMINATED DURING GROUND TEST. AMM 33-51-01-2 RELAMPED DOOR 1L INTERIOR FWD EMERGENCY EXIT SIGN 
- [SDR FDEA202502060182](https://openairdocs.org/sdr/FDEA202502060182), Feb 6, 2025: SKIN. CRACKED. UT & OPEN HOLE HFEC INSPECTION ON THE RH WING WBL 262 THEN FOUND HOLE #5 CRACKS IN UPPER WING SKIN AS MARKED. RH WING UPPER SKIN WBL 262 #5 HOLE REPAIRED AS PER
- [SDR FDEA202312111932](https://openairdocs.org/sdr/FDEA202312111932), Dec 11, 2023: LIGHT. FAILED. EMERGENCY LIGHTING LITE IN SUPERNUMERARY IS INOPERATIVE. REMOVED & REPLACED LEFT CEILING INTERIOR EMER LT ASSY AND OPS CHECKED NORMAL.
- [SDR FDEA202312051909](https://openairdocs.org/sdr/FDEA202312051909), Dec 5, 2023: UNKNOWN. UNKNOWN. EMERGENCY EXIT LIGHTS WILL NOT TEST WITH SUPERNUMERARY TEST BUTTON. HIGH RESITANCE ON PIN 8 CONNECTOR DM33093 CHECKING TO GROUND WITH BOTH POWER SUPPLY UNITS DI
- [SDR FDEA202311301900](https://openairdocs.org/sdr/FDEA202311301900), Nov 30, 2023: BATTERY. FAILED. EMERGENCY LIGHTS IN SUPERNUMERARY ILLUMINATED ON SHORT FINAL TO LANDING. STAYED ON FOR ABOUT 10 SECONDS. COMPLIED WITH OPERATIONAL CHECKS AND FUNCTIONAL CHECKS 
- [SDR FDEA202207291816](https://openairdocs.org/sdr/FDEA202207291816), Jul 29, 2022: BRACKET. ABNORMAL. DURING PERFORMING EO G-5710-E0365655 P7 STEP8.C.(8), FOUND 02EA BRACKETS P/N:675W0003-3 AND P/N:287W4908-191 SHORT EDGE MARGIN, AT STA1014-1035, STGR34-38 LHS. 
- [SDR FDEA202207251794](https://openairdocs.org/sdr/FDEA202207251794), Jul 25, 2022: FLAP. DELAMINATED. LH WING OB FLAP LWR SURFACE FOUND DELAMINATION AT OTEF STA424 LH WING OB FLAP LWR SURFACE AT OTEF STA424 REPAIRED AS PER B777F SRM 57-53-01-2R REPAIR 2 AND SRM 
- [SDR FDEA202207141720](https://openairdocs.org/sdr/FDEA202207141720), Jul 14, 2022: BRACKET. NONE. DURING PERFORMING EO G-5710-E0365655 P8 STEP8.C.(8),FOUND 03 EA BRACKETS P/N:675W0003-4, P/N:287W4908-192 AND P/N:341W2508Y17 SHORT EDGE MARGIN, AT STA1014- 103
- [SDR FDEA202207141718](https://openairdocs.org/sdr/FDEA202207141718), Jul 14, 2022: DOUBLER. NONE. DURING PERFORMING EO G-5710-E0365655 P8 STEP8.C.(5), FOUND 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 RHS TOO CLOSE TO EDGE OF MACHINED STEP 
- [SDR FDEA202207141717](https://openairdocs.org/sdr/FDEA202207141717), Jul 14, 2022: DOUBLER. NONE. DURING PERFORMING EO G-5710-E0365655 P7 STEP8.C.(5),FOUND 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 LHS TOO CLOSE TO EDGE OF MACHINED STEP O
- [SDR FDEA202207011645](https://openairdocs.org/sdr/FDEA202207011645), Jul 1, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8452-21 FOUND CRACKED AT STA1350 LBL45. REPAIRED MAIN DECK CARGO FLOOR PANEL P/N:152W8452-21 CRACKED AT STA 1350 LBL45. AS P
- [SDR FDEA202206301624](https://openairdocs.org/sdr/FDEA202206301624), Jun 30, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8650-4 FOUND CRACKED AT STA1748 BL0. REPAIRED MAIN DECK CARGO FLOOR PANEL P/N:152W8650-4 CRACKED AT STA1748 BL0. AS PER B777
- [SDR FDEA2020070211424](https://openairdocs.org/sdr/FDEA2020070211424), Jul 1, 2020: FAN. INOPERATIVE. ARRIVED AT AIRCRAFT OBSERVED STRONG FUMES, ALERTS RECIRC FAN ANNUNCIATED. RELEASED FOR SERVICE PER MEL : 21-25-01-02 CATEGORY : C EXPIRATION : 11JUL20 "MEL 21-2
- [SDR FDEA2020012180176](https://openairdocs.org/sdr/FDEA2020012180176), Jan 18, 2020: CONTACTOR. BURNED. HYD ELEC PUMP ELCU HAS DAMAGE. INSATLLED ELCU (M29303) FOR ACMP C-1 IAW MM 24-51-05-4. OPS TESTED NORMAL IAW MM 24-51-05-4.
- [SDR FDEA2019102422725](https://openairdocs.org/sdr/FDEA2019102422725), Oct 22, 2019: FLOOR SUPPORT. CRACKED. BULK CARGO COMPARTMENT FLOOR STRINGER AT STATION 1936 RBL 49.8 FOUND CRACKED.
- [SDR FDEA2019102422724](https://openairdocs.org/sdr/FDEA2019102422724), Oct 22, 2019: FLOOR SUPPORT. CRACKED. BULK CARGO COMPARTMENT FLOOR STRINGER AT STATION 1936 RBL 41.5 FOUND CRACKED.
- [SDR FDEA201909252338](https://openairdocs.org/sdr/FDEA201909252338), Sep 25, 2019: LENS. DETACHED. POST-FLT INSP, L-1 DOOR FWD EMERGENCY EXIT LIGHT LENS DETACHED. RE-INSTALLED EMERGENCY EXIT LIGHT LENS ASSY, REF AMM: 33-50-00-2. LIGHTS TEST SATIS, ITEM OK FOR
- [SDR FDEA201907031474](https://openairdocs.org/sdr/FDEA201907031474), Jul 3, 2019: LIGHT. FAILED. POST-FLT INSP, R-1 DOOR AFT EMERGENCY EXIT LIGHT LESS THAN 10% ILLUMINATED DURING LIGHTS TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY, REF AMM: 33-50-00
- [SDR FDEA201809112442](https://openairdocs.org/sdr/FDEA201809112442), Sep 11, 2018: BATTERY PACK. DISCHARGED. LEFT HAND SIDE EMERGENCY LIGHTS ARE INOP. R&R LT BATT PACK REF MM 33-51-06-2. TEST PASS.
- [SDR FDEA201802230475](https://openairdocs.org/sdr/FDEA201802230475), Feb 23, 2018: LAMP. INOPERATIVE. POST FLIGHT INSPECTION, ONE OVERHEAD EMERGENCY LIGHT INOPERATIVE, DURING LIGHT TEST. REPLACED THE LAMP, IAW AMM 33-50-00-2. EMERGENCY LIGHTS TESTED SATISFACTORY
- [SDR FDEA201802190434](https://openairdocs.org/sdr/FDEA201802190434), Feb 19, 2018: PUMP. CRACKED. RAT PUMP CRACKED AND LEAKED DURING MOTORING TEST. OPEN
- [SDR FDEA201705281533](https://openairdocs.org/sdr/FDEA201705281533), May 28, 2017: FLOOR SUPPORT. PUNCTURED. BULK CARGO BAY RT FLOOR SUPPORT BS 1935, RBL 49.8 FOUND PUNCTURED. REPAIRED IAW SRM 53-70-53-2R, FIGURE 202, REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-10
- [SDR FDEA201705281532](https://openairdocs.org/sdr/FDEA201705281532), May 28, 2017: FLOOR SUPPORT. PUNCTURED. BULK CARGO BAY RT FLOOR SUPPORT, BS 1972, RBL 32, FOUND PUNCTURED. REPAIRED IAW SRM 53-70-53-2R, FIGURE 202, REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-10
- [SDR FDEA201609053118](https://openairdocs.org/sdr/FDEA201609053118), Sep 5, 2016: PUMP. SHEARED. HYDRAULIC QUANTITY LOW RT, EICAS ALERT MESSAGE FOLLOWED BY HYDRAULIC QUANTITY LOW CHECKLIST. R & R RT ENGINE EDP IAW MM 29-11-05-4-2 AND CHECK VALVE IAW MM 29-1
- [SDR FDEA201609043116](https://openairdocs.org/sdr/FDEA201609043116), Sep 4, 2016: SENSOR. FALSE INDICATION. ENGINE OIL FILTER SENSOR RT ON STATUS PAGE FOLLOWED BY ENGINE OIL FILTER BYPASS RT, ALERT ON EICAS. PERFORMED CHIP CHECK ANALYSIS AND NO M50 MATERIAL FOUND IN T
- [SDR FDEA201512043906](https://openairdocs.org/sdr/FDEA201512043906), Dec 4, 2015: STATIC WICK. MISSING. ON CLIMB, LIGHTNING STRIKE ON NOSE OF ACFT. WX FAIL THEN DISPLAYED. VIBRATION OF ACFT, NOISE FOLLOWED. PERFORMED LIGHTNING INSPECTION IAW MM 05-51-19-2, FOUND O
- [SDR FDEA201508042468](https://openairdocs.org/sdr/FDEA201508042468), Aug 4, 2015: GUARD. BROKEN. EMERGENCY LIGHTS SAFETY GUARD IS BROKEN. FOUND GUARD FOR EMER LIGHTS, SWITCH WILL NOT STAY IN THE UP, GUARDED POSITION. DOES NOT HAMPER WITH NORMAL OPERATIONS O
- [SDR FDEA201507272420](https://openairdocs.org/sdr/FDEA201507272420), Jul 27, 2015: BOTTLE. LOW PRESSURE. L1 DOOR SLIDE PACK INFLATION CYLINDER PRESSURE IS IN RED BAND. R & R LT SLIDE ASSEMBLY IAW AMM 25-66-01-4.
- [SDR FDEA201505011354](https://openairdocs.org/sdr/FDEA201505011354), May 1, 2015: STOWAGE BOX. FAILED. CAPTAINS OXYGEN MASK RESET BUTTON DOES NOT WORK WHEN PUSHED. R & R CAPTAINS OXYGEN MASK BOX IAW MM 35-11-18-2. OPS CHECKED SATISFACTORY. ACFT OK FOR SERVICE.
- [SDR FDEA201306071222](https://openairdocs.org/sdr/FDEA201306071222), Jun 7, 2013: WIRE. DAMAGED. RELAY K24051, THREE SOCKET BASE WIRES INSULATION COLOR CHANGED TO BROWNISH COLOR. RELAY K24051, SOCKET BASE AND WIRES W3135-0004-12, W3135-0005-12, W3135-0018-1
- [SDR FDEA201208263181](https://openairdocs.org/sdr/FDEA201208263181), Aug 26, 2012: SPRING. OUT OF POSITION. COVER ON THE EMERGENCY LIGHTS SWITCH IS BROKEN. FOUND SPRING INSIDE GUARDED SWITCH IS MISALIGNED, POSITONED SPRING, AND OPS CHECKED OK IAW SMP.

## 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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