# N857FD: 2010 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: 37728
- Year built: 2010
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 11, 2010
- Certificate issued: August 12, 2010
- Expires: February 29, 2028
- Mode S code: ABC1DA
- 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=857FD
- Page: https://openairdocs.org/aircraft/N857FD

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 N857FD.

## FAA accident and incident reports

None matched to N857FD.

## Service difficulty reports (39)

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 FDEA202608221219](https://openairdocs.org/sdr/FDEA202608221219), Aug 22, 2026: TIRE TREAD. SEPARATED. CHECK FOUND NR 11 TIRE TREAD SEPARATION.
- [SDR FDEA202602140193](https://openairdocs.org/sdr/FDEA202602140193), Feb 14, 2026: SAFETY WIRE. WRONG PART. RIGHT SLIDE, REPLACE THE BREAKAWAY WIRE SECURING THE RELEASE CABLE TO THE PACKBOARD RELEASE MECHANISM ON THE PACKBOARD WITH MS20995CY16 CAD-PLATED COPPER WIRE P
- [SDR FDEA202601220080](https://openairdocs.org/sdr/FDEA202601220080), Jan 22, 2026: SKIN. DENTED. FOUND RT WWING T/E OTBD FLAP LOWER SURFACE DENT 1EA AT THE CROSS OTEF 335 AND T/E 2 INCHS. REPAIRED RHW T/E O/B FLAP LOWER SURFACE DENT 1EA AT THE CROSS OTEF 33
- [SDR FDEA202601220078](https://openairdocs.org/sdr/FDEA202601220078), Jan 22, 2026: FITTING. CRACKED. FOUND RH WING NR 11 SLAT L/E UPPER SKIN 1 EA BULGE AT THE O/B MAIN TRACK FITTING AREA. RH WING NO.11 SLAT L/E UPPER SKIN BULGE AREA REPAIRED AS PER B777 SRM 57-
- [SDR FDEA202601210077](https://openairdocs.org/sdr/FDEA202601210077), Jan 21, 2026: SKIN. CRACKED. DURING PERFORM WORK CARD:EG-5710-E0376285E P12 STEP 3.B.& STEP5 A.(2) THEN FOUND TWO CRACKS ON RT UPPER WING SKIN FASTENER NR 5. RT WING UPPER SKIN FASTENER HOL
- [SDR FDEA202601210076](https://openairdocs.org/sdr/FDEA202601210076), Jan 21, 2026: SKIN. CRACKED. DURING PERFORM WORK CARD:EG-5710-E0376285F P12 STEP4. B. (2). (B). THEN FOUND TWO CRACKS ON RT UPPER WING SKIN FASTENER NR 6. RT WING UPPER SKIN NR 6 CRACKED FA
- [SDR FDEA202601200074](https://openairdocs.org/sdr/FDEA202601200074), Jan 20, 2026: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL 241SF (P/N 152W8601-7) DAMAGED AT STA 1450 LBL 2. MAIN DECK FLOOR PANEL 241SF (P/N 152W8601-7) CRACKED AT STA 1450 LBL 2 DAMAGE SIZE
- [SDR FDEA202601200073](https://openairdocs.org/sdr/FDEA202601200073), Jan 20, 2026: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL 241LF DAMAGED AT BS 1300, LBL 45. FLOOR PANEL 241LF DAMAGED: L= 1", DAMAGE OUT OF ALLOWABLE LIMIT IAW SRM 53-00-50-1A, ALLOWABLE DAM
- [SDR FDEA202601200072](https://openairdocs.org/sdr/FDEA202601200072), Jan 20, 2026: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL 241QF (P/N 152W8402-21) DAMAGED AT STA 1400 LBL 45. MAIN DECK FLOOR PANEL 241QF (P/N 152W8402-21) CRACKED AT STA 1400 LBL 45 DAMAGE 
- [SDR FDEA202601200071](https://openairdocs.org/sdr/FDEA202601200071), Jan 20, 2026: SKIN. DAMAGED. NUMBER 7 SLAT EXTERNAL UPPER SURFACE OUTER SKIN AT ISS184 SCREW HOLE FOUND ELONGATE. NR 7 SLAT EXTERNAL UPPER SURFACE OUTER SKIN AT ISS 184 ELONGATE SCREW HOLE 
- [SDR FDEA202601200070](https://openairdocs.org/sdr/FDEA202601200070), Jan 20, 2026: SKIN. CRACKED. DURING PERFORM WORK CARD:EG-5710-E0376285F P11 STEP3. B. (1). & STEP5 A. (2), THEN FOUND 02EA CRACKS ON LH UPPER WING SKIN FASTENER #5 AS MARKED. THE LEFT WING 
- [SDR FDEA202503220473](https://openairdocs.org/sdr/FDEA202503220473), Mar 22, 2025: POWER SUPPLY. INOPERATIVE. DURING SERVICE CHECK, FOUND L/H SLIDE LIGHT INOP. PART 22MAR25 14:16 MC1 IDENTIFIED PARTS EMERGENCY LIGHTS. RELAMPED L/H SLIDE LIGHT PER AMM 33-51-04-2. NO HELP
- [SDR FDEA202501210113](https://openairdocs.org/sdr/FDEA202501210113), Jan 21, 2025: LAMP. INOPERATIVE. CHECK FOUND ONE EMERGENCY AREA LIGHT IS INOP. RELAMPED THE EMERGENCY AREA LIGHT REF AMM 33-51-03-2, TEST NORMAL. A/C OK TO CONTINUE.
- [SDR FDEA202501020002](https://openairdocs.org/sdr/FDEA202501020002), Jan 2, 2025: LAMP. FAILED. LOWER RIGHT EXIT SIGN ON THE RIGHT SIDE OF ENTRY DOOR L1 HAS ONE BULB INOP. REPLACED LAMP PER AMM : 33-51-01-2. TEST PASSED.
- [SDR FDEA202305260943](https://openairdocs.org/sdr/FDEA202305260943), May 26, 2023: FLOOR PANEL. DAMAGED. MAIN DECK CARGO FLOOR PANEL 251MF(P/N:152W8601-31) AT STA1798/LBL1.5 FOUND A HOLE. EVALUATED MAIN DECK CARGO FLOOR PANEL 251MF(P/N:152W8601-31) AT STA1798/LBL1.
- [SDR FDEA202305260942](https://openairdocs.org/sdr/FDEA202305260942), May 26, 2023: FLOOR PANEL. DAMAGED. MAIN DECK CARGO FLOOR PANEL 251FF(P/N:152W8601-19) AT STA1656/RBL1 FOUND A HOLE. EVALUATED MAIN DECK CARGO FLOOR PANEL 251FF(P/N:152W8601-19) AT STA1656/RBL1 A 
- [SDR FDEA202010232615](https://openairdocs.org/sdr/FDEA202010232615), Oct 23, 2020: STRUCTURE. DAMAGED. WHILE PERFORMING RIGHT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR (SNRM N00526) FOUND 02 EACH EXISTING OVERSIZED HOLE AT LOWER CHORD THROUGH WEB STA
- [SDR FDEA202010232614](https://openairdocs.org/sdr/FDEA202010232614), Oct 23, 2020: STRUCTURE. DAMAGED. WHILE PERFORMING LEFT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR. SNRM N00525 FOUND 01 EACH EXISTING OVERSIZED HOLE AT LOWER CHORD THROUGH WEB STATI
- [SDR FDEA202010232613](https://openairdocs.org/sdr/FDEA202010232613), Oct 23, 2020: STRUCTURE. DAMAGED. WHILE PERFORMING RIGHT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR (SNRM N00526) FOUND 02 EACH EXISTING OVERSIZED HOLE AT LOWER CHORD STATION 1035 RI
- [SDR FDEA202010232611](https://openairdocs.org/sdr/FDEA202010232611), Oct 23, 2020: STRUCTURE. DAMAGED. WHILE PERFORMING LEFT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR, SNRM #N00525. FOUND 01 EACH EXISTING OVERSIZED HOLE AT LOWER CHORD STATION 1035 LE
- [SDR FDEA202010152502](https://openairdocs.org/sdr/FDEA202010152502), Oct 15, 2020: DOUBLER. OUT OF ALIGNMENT. WHILE ACCOMPLISHING EO G-5310-E0332629 H PART 6 FOUND 3 EACH PILOT HOLES AT NEW FUSELAGE SKIN DOUBLER MISALIGNED WITH THE LONGERON FITTING BETWEEN BODY STATION 
- [SDR FDEA202010152501](https://openairdocs.org/sdr/FDEA202010152501), Oct 15, 2020: DOUBLER. OUT OF ALIGNMENT. WHILE ACCOMPLISHING EO G-5310-E0332629 H PART 6 FOUND NEW FUSELAGE SKIN DOUBLER PART NUMBER 143W2314Y406 PILOT HOLES MISALIGN WITH EXISTING FUSELAGE SKIN HOLES 
- [SDR FDEA202010152500](https://openairdocs.org/sdr/FDEA202010152500), Oct 15, 2020: SKIN. CRACKED. HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON RIGHT HAND SIDE EXTERNAL SURFACE OF THE FUSELAGE SKIN WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE UN
- [SDR FDEA202010152499](https://openairdocs.org/sdr/FDEA202010152499), Oct 15, 2020: SKIN. CRACKED. HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON LEFT HAND SIDE EXTERNAL SURFACE OF THE FUSELAGE SKIN WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE UND
- [SDR FDEA202010152503](https://openairdocs.org/sdr/FDEA202010152503), Oct 15, 2020: DOUBLER. OUT OF ALIGNMENT. WHILE ACCOMPLISHING LEFT HAND EO G-5310-E0332629 H PART 5 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STATION 998 STRINGER S-35 LEFT NEAR MILLED EDGE. COMP
- [SDR FDEA202010152498](https://openairdocs.org/sdr/FDEA202010152498), Oct 15, 2020: STRUCTURE. CRACKED. DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON REMOVED FASTENER HOLES ON RIGHT HAND SIDE VERTICAL FLANGE OF THE SPAR CHORD AT UNDERWING 
- [SDR FDEA202010152497](https://openairdocs.org/sdr/FDEA202010152497), Oct 15, 2020: STRUCTURE. CRACKED. DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON REMOVED FASTENER HOLES ON LEFT HAND SIDE VERTICAL FLANGE OF THE SPAR CHORD AT UNDERWING L
- [SDR FDEA202010152504](https://openairdocs.org/sdr/FDEA202010152504), Oct 15, 2020: DOUBLER. OUT OF ALIGNMENT. WHILE ACCOMPLISHING RIGHT HAND EO G-5310-E0332629 H PART 6 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STATION 998 STRINGER S-35 RIGHT NEAR MILLED EDGE. CO
- [SDR FDEA202010082435](https://openairdocs.org/sdr/FDEA202010082435), Oct 8, 2020: FLOOR SUPPORT. CRACKED. LOWER BULK CARGO COMPARTMENT FLOOR STRINGER FOUND CRACK AT STATION 1958 RBL 41.5. LOWER BULK CARGO COMPARTMENT AT STATION 1958 RBL 41.5 CRACKED FLOOR STRINGER R
- [SDR FDEA2019111532940](https://openairdocs.org/sdr/FDEA2019111532940), Nov 13, 2019: NONE. NONE. PDIS 857 05-50 9138 13NOV19 SEA OPEN U LOGPAGES:3182688 FLEW INTO A VERY THIN, RAGGED VOLCANIC ASH CLOUD @ FL340 AT APPROX 2350Z NOTICED A SMALL, BUT STEADY EGT
- [SDR FDEA201705021333](https://openairdocs.org/sdr/FDEA201705021333), May 2, 2017: LAMP. INOPERATIVE. RT AFT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMP AND OPS CHECKED GOOD IAW AMM 33-51-00-5. ACFT OK FOR SERVICE.
- [SDR FDEA201508182609](https://openairdocs.org/sdr/FDEA201508182609), Aug 18, 2015: BATTERY. DAMAGED. L1 DOOR EMER POWER ASSIST SYS STATUS LIGHT FOUND NOT BLINKING. FOUND LOWER EPAS BACKUP BATTERY SOCKET DEFORMED & NOT FULLY INSERTED INTO EPAS PACK. R & R BOTH E
- [SDR FDEA201508182608](https://openairdocs.org/sdr/FDEA201508182608), Aug 18, 2015: BATTERY. DAMAGED. L1 DOOR EMER POWER ASSIST SYS STATUS LIGHT FOUND NOT BLINKING. FOUND LOWER EPAS BACKUP BATTERY SOCKET DEFORMED & NOT FULLY INSERTED INTO EPAS PACK. R & R BOTH E
- [SDR FDEA201508182602](https://openairdocs.org/sdr/FDEA201508182602), Aug 18, 2015: BATTERY. DAMAGED. L1 DOOR EMER POWER ASSIST SYS STATUS LIGHT FOUND NOT BLINKING. FOUND LOWER EPAS BACKUP BATTERY SOCKET DEFORMED & NOT FULLY INSERTED INTO EPAS PACK. R & R BOTH E
- [SDR FDEA201307111543](https://openairdocs.org/sdr/FDEA201307111543), Jul 11, 2013: UNKNOWN. ODOR. ON ENTERING COCKPIT, FAINT ODOR SIMILAR TO A BURNED ELECTRICAL WAS PRESENT. SWITCHED AIR CONDITION CART AIR TO APU AIR, ODOR STOPPED IAW FIM 21-00-00-2, CHECKED
- [SDR FDEA201307101520](https://openairdocs.org/sdr/FDEA201307101520), Jul 10, 2013: BULB. INOPERATIVE. FOUND RT OVERWING SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED BULB IAW MM33-51-04-2. TEST PASSED.
- [SDR FDEA201210213709](https://openairdocs.org/sdr/FDEA201210213709), Oct 21, 2012: SLIDE. FAILED. MAIN CABIN DOOR SLIDE ACTIVATED. CAPT/FO, BOTH VERIFIED DOOR(S) WERE DISARMED BUT SLIDE ACTIVATED, DOOR SYNOPSIS INDICATED "M" ON BOTH DOORS. REMOVED LT DOOR MO
- [SDR FDEA201103130949](https://openairdocs.org/sdr/FDEA201103130949), Mar 13, 2011: SLIDE. UNWANTED DEPLOY. L1 SLIDE DEPLOYED ON ARRIVAL. R&R L1 DOOR MOUNTED ESCAPE SLIDE PACK IAW AMM 25-66-01-4 AND R&R L1 EPAS RESERVOIR IAW AMM 52-11-22-4, ACFT OK FOR SERVICE.
- [SDR FDEA201010124015](https://openairdocs.org/sdr/FDEA201010124015), Oct 12, 2010: LINE. LEAKING. HYD QTY LOW CTR (LOST ALL HYD FLUID IN CTR) SVC'D HYD FLUID TO CTR HYD SYS TO PROPER LEVEL IAW AMM 12-12-01-3-0, PERF CTR HYD SYS LEAKS FOUND. NO EXTERIOR LEAKS

## 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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