# N850FD: 2009 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: 37721
- Year built: 2009
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 24, 2009
- Certificate issued: October 1, 2009
- Expires: August 31, 2028
- Mode S code: ABA7D9
- 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=850FD
- Page: https://openairdocs.org/aircraft/N850FD

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 N850FD.

## FAA accident and incident reports

None matched to N850FD.

## Service difficulty reports (41)

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 FDEA202607120916](https://openairdocs.org/sdr/FDEA202607120916), Jul 12, 2026: LIGHT SYS. MALFUNCTIONED. CHECK FOUND WHEN THE OVERHEAD PANEL EMER LIGHTS SWITCH IN "ON" POSITION, THE EMERGENCY LIGHTS NOT ILLUMINATED. AMM: 33-51-00-5 RESET THE CB'S AND PERFORMED EMER
- [SDR FDEA202505160761](https://openairdocs.org/sdr/FDEA202505160761), May 16, 2025: FLOOR PANEL. DELAMINATED. REWORK:MAIN DECK CARGO COMPARTMENT AT STA 1940 FOUND CENTER FLOOR PANEL UPPER SURFACE HAVE SIGN OF DELAMINATED CONDITION. MEASURED MAIN DECK CARGO COMPARTMENT A
- [SDR FDEA202505010696](https://openairdocs.org/sdr/FDEA202505010696), May 1, 2025: SKIN. CRACKED. OPEN HOLE HFEC INSPECTION OF #5 HOLE AT LH WING UPPER SKIN WBL 262 AND FOUND 01EA CRACK AS MARKED. LH WING UPPER SKIN WBL 262 #5 HOLE 01EA CRACK AS MARKED REPAI
- [SDR FDEA202504240638](https://openairdocs.org/sdr/FDEA202504240638), Apr 24, 2025: SKIN. DENTED. FOUND LH WING OB FLAP LOWER SURFACE A DENT AT 226 INCH FROM IB SIDE CROSS 8 INCH FROM AFT SIDE. REPAIRED LH WING OB FLAP LOWER SURFACE A DENT AT 226 INCH FROM I
- [SDR FDEA202504240636](https://openairdocs.org/sdr/FDEA202504240636), Apr 24, 2025: SKIN. DENTED. FOUND LH WING OB FLAP LOWER SURFACE A DENT AT 198 INCH FROM IB SIDE CROSS 15 INCH FROM AFT SIDE. REPAIRED LH WING OB FLAP LOWER SURFACE A DENT AT 198 INCH FROM 
- [SDR FDEA202504230629](https://openairdocs.org/sdr/FDEA202504230629), Apr 23, 2025: SKIN. CRACKED. OPEN HOLE HFEC INSPECTION OF #5 HOLE AT RH WING UPPER SKIN WBL 262 AND FOUND 02EA CRACKS AS MARKED. RH WING UPPER SKIN WBL262 #5 HOLE 02EA CRACKS REPAIRED AS PE
- [SDR FDEA202504230628](https://openairdocs.org/sdr/FDEA202504230628), Apr 23, 2025: SKIN. BULGED. RH WING OB NO.12 SLAT OUTER SKIN FOUND BULGE AT 68 INCHES TO OB EDGE. RH WING OB NO.12 SLAT OUTER SKIN AT 68 INCHES TO OB EDGE BULGE AREA REPAIRED AS PER B777 S
- [SDR FDEA202504070586](https://openairdocs.org/sdr/FDEA202504070586), Apr 7, 2025: HYDRAULIC LINE. LEAKING. LOST ALL CENTER HYDRAULIC FLUID SHORTLY AFTER AIRBORNE. EICAS MSSG HYD PRESS SYS C APPEARED AFTER RAISING LANDING GEAR HANDLE. REMOVED AND REPLACED ELEVATOR RET
- [SDR FDEA202303300527](https://openairdocs.org/sdr/FDEA202303300527), Mar 30, 2023: PDU. UNKNOWN. EICAS FLAP DRIVE ALERT ON DEPARTURE AFTER SELECTING FLAPS UP. ECL PROCEDURES ACCOMPLISHED. RTB MEM. EMERGENCY DECLARED & CANCELED AFTER LANDING. EMERGENCY DECLA
- [SDR FDEA202303190469](https://openairdocs.org/sdr/FDEA202303190469), Mar 19, 2023: PDU. FAULTED. FLAPS DRIVE EICAS AFTER TAKEOFF. REF TSI 27-80/4883, PUT THE AIR/GROUND SYSTEM IN THE AIR MODE. PERFORMED STEP 7, OPS FLAPS WHEN FSEU #2 IN CONTROL, ALL OPS SAT
- [SDR FDEA202303150428](https://openairdocs.org/sdr/FDEA202303150428), Mar 15, 2023: LIGHT. FAILED. FLT CREW PRE-FLT CK REPORTED, L1 DOOR FWD EMER EXIT SIGN INDICATOR ALL OF LIGHTS INOP. ENT BY:3711964 RPT BY:3711964 R&R'D LIGHT ASSY PER MM 33-51-01-2. LIGHT F
- [SDR FDEA202209052204](https://openairdocs.org/sdr/FDEA202209052204), Sep 5, 2022: SKIN. DAMAGED. DURING PERFORMING E G-5710-E0366409 P 7 STEP7.A.(10), FOUND 02 EA HOLES OVERSIZED (DIAMETER:0.6245") ON THE SKIN AND LONGERON(P/N:140W9255Y407) AT STA993-1035 S
- [SDR FDEA202208302105](https://openairdocs.org/sdr/FDEA202208302105), Aug 30, 2022: FLOOR PANEL. NONE. MAIN DECK CARGO FLOOR PANEL AT RH STA 1476 TO STA 1790 (MPN# 152W8602-20) UNDER SIDE GUIDE ASSY FOUND DENT. REPAIRED MAIN DECK CARGO FLOOR PANEL AT RH STA 1476 
- [SDR FDEA202208302104](https://openairdocs.org/sdr/FDEA202208302104), Aug 30, 2022: FLOOR PANEL. NONE. MAIN DECK CARGO FLOOR PANEL AT RH STA 1476 TO STA 1790 (MPN# 152W8602-14) UNDER SIDE GUIDE ASSY FOUND DENT. REPAIRED MAIN DECK CARGO FLOOR PANEL AT RH STA 1476 
- [SDR FDEA202208302103](https://openairdocs.org/sdr/FDEA202208302103), Aug 30, 2022: FLOOR PANEL. NONE. MAIN DECK CARGO FLOOR PANEL BETWEEN STA 1664 TO STA 2046 (MPN# 152W8601-19) UNDER CENTERLINE RESTRAINT FOUND DENT. REPAIRED MAIN DECK CARGO FLOOR PANEL BETWEEN 
- [SDR FDEA202208302102](https://openairdocs.org/sdr/FDEA202208302102), Aug 30, 2022: FLOOR PANEL. NONE. MAIN DECK CARGO FLOOR PANEL AT LH STA 1476 TO STA 1580 (MPN# 152W8602-13) UNDER SIDE GUIDE ASSY FOUND DENT. REPAIRED MAIN DECK FLOOR PANEL AT LH STA 1476 TO STA
- [SDR FDEA202208232031](https://openairdocs.org/sdr/FDEA202208232031), Aug 23, 2022: FLOOR PANEL. NONE. MAIN DECK CARGO FLOOR PANELS AT LH STA 1476 TO STA 1580 (MPN# 152W8602-7) UNDER SIDE GUIDE ASSY AREA FOUND DENTS. REPAIRED MAIN DECK CARGO FLOOR PANELS AT LH ST
- [SDR FDEA202208232030](https://openairdocs.org/sdr/FDEA202208232030), Aug 23, 2022: FLOOR PANEL. NONE. MAIN DECK CARGO FLOOR PANELS BETWEEN STA 1664 TO STA 2046 (MPN# 152W8601-31) UNDER CENTERLINE RESTRAINT AREA FOUND DENTS. REPAIRED MAIN DECK CARGO FLOOR PANELS 
- [SDR FDEA202208232029](https://openairdocs.org/sdr/FDEA202208232029), Aug 23, 2022: FLOOR PANEL. NONE. MAIN DECK CARGO FLOOR PANELS AT RH STA 1476 TO STA 1790 (MPN# 152W8602-8) UNDER SIDE GUIDE ASSY AREA FOUND DENTS. REPAIRED MAIN DECK CARGO FLOOR PANELS AT RH ST
- [SDR FDEA202103130629](https://openairdocs.org/sdr/FDEA202103130629), Mar 13, 2021: ACTUATOR. MALFUNCTIONED. AILERON ACTUATOR REMOVED AND REPLACED RT O/B AILERON ACTUATOR REF AMM 27-11-11-4 UP TO AND INCLUDING STEP 3. H. (7). STILL REQUIRES OPS CHECK. RIG CHECK GOOD ,A
- [SDR FDEA202010302719](https://openairdocs.org/sdr/FDEA202010302719), Oct 30, 2020: LAMP. INOPERATIVE. POST-FLT INSPECTION, R-1 OVERHEAD EMERGENCY LIGHT INOPERABLE ON LIGHTS TEST. RE-LAMPED, REF B777 AMM: 33-51-03-2. EMERGENCY LIGHTS TEST SATISFACTORY. ITEM OK FO
- [SDR FDEA202001020002](https://openairdocs.org/sdr/FDEA202001020002), Jan 2, 2020: SKIN. CRACKED. DURING ACCOMPLISHMENT OF HFEC INSPECTION ON FUSELAGE SKIN OF LEFT HAND UNDERWING LONGERON FOUND 02 EACH CRACKS INDICATION AT STATION 1024 AND STATION 1035 STRIN
- [SDR FDEA201912233282](https://openairdocs.org/sdr/FDEA201912233282), Dec 23, 2019: SKIN. CRACKED. HFEC SURFACE INSPECTION CARRIED OUT ON THE RIGHT HAND SIDE OF THE FUSELAGE SKIN COMMON TO THE UNDERWING LONGERON WITHIN A 2 INCHES RADIUS OF THE FASTENER HOLES 
- [SDR FDEA2019122093263](https://openairdocs.org/sdr/FDEA2019122093263), Dec 19, 2019: FLOOR SUPPORT. CRACKED. BULK CARGO COMPARTMENT FLOOR PANEL SUPPORT STRINGER STATION 1980.5 RBL 40 FOUND CRACKED. REFER SNRM N00384 FOR WORK DETAIL CARRIED OUT AT BULK CARGO COMPARTMENT
- [SDR FDEA2019122093262](https://openairdocs.org/sdr/FDEA2019122093262), Dec 19, 2019: FLOOR SUPPORT. CRACKED. BULK CARGO COMPARTMENT FLOOR SUPPORT STRINGER STATION 1937 RBL 16 FOUND CRACKED. BULK CARGO COMPARTMENT FLOOR SUPPORT STRINGER STATION 1937 RBL 16 SECTION STRIN
- [SDR FDEA2019122093261](https://openairdocs.org/sdr/FDEA2019122093261), Dec 19, 2019: FLOOR SUPPORT. CRACKED. BULK CARGO COMPARTMENT FLOOR PANEL SUPPORT STRINGER STATION 1931 RBL 40 FOUND CRACKED. BULK CARGO COMPARTMENT FLOOR PANEL SUPPORT STRINGER AT STATION 1931 RBL 4
- [SDR FDEA201912193260](https://openairdocs.org/sdr/FDEA201912193260), Dec 19, 2019: FLOOR SUPPORT. CRACKED. BULK CARGO COMPARTMENT FLOOR PANEL SUPPORT STRINGER STATION 1958 RBL 49.8 FOUND CRACKED. BULK CARGO COMPARTMENT FLOOR PANEL SUPPORT STRINGER STATION 1958 RBL 49
- [SDR FDEA201912173255](https://openairdocs.org/sdr/FDEA201912173255), Dec 17, 2019: STRUCTURE. CRACKED. DURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON RIGHT HAND UNDERWING LONGERON AT BODY STATION 1035, FOUND CRACK INDICATION ON FRONT
- [SDR FDEA201912173254](https://openairdocs.org/sdr/FDEA201912173254), Dec 17, 2019: LONGERON. CRACKED. ULTRASONIC INSPECTION CARRIED OUT ON LEFT HAND UNDERWING LONGERON AT BODY STATION 1035 AND CRACK INDICATION FOUND AT 01EACH FORWARD INBOARD FASTENER HOLE AND 02
- [SDR FDEA201912173253](https://openairdocs.org/sdr/FDEA201912173253), Dec 17, 2019: LONGERON. CRACKED. ULTRASONIC INSPECTION CARRIED OUT ON THE RIGHT HAND SIDE UNDERWING LONGERON AT BODY STATION 1035 AND CRACK INDICATION FOUND AT 02EACH FORWARD FASTENER HOLES AND
- [SDR FDEA201902170442](https://openairdocs.org/sdr/FDEA201902170442), Feb 17, 2019: SUPPORT BRACKET. CRACKED. LEFT HAND ENGINE: INBOARD T/R LATCH STRAP SUPPORT BRACKET BROKEN. REPLACED DAMAGED BRACKET IRW SRM 51-40-02-0G.
- [SDR FDEA2018092512656](https://openairdocs.org/sdr/FDEA2018092512656), Sep 21, 2018: SKIN. CRACKED. MDIS 850 27-80 9729 21SEP18 ANC POST FLT LEFT WING SLAT #5 ZONE 2, UPPER SKIN SURFACE 10 INCH CRACK. FACT 22SEP18 23:11 ANC REPLACED LEFT WING #5 SLAT REF MM 27
- [SDR FDEA201712183405](https://openairdocs.org/sdr/FDEA201712183405), Dec 18, 2017: COVER. OUT OF POSITION. L1 DOOR AFT COVER WILL NOT CLOSE FLUSH WITH FORWARD. REPOSITIONED THE AFT HINGE DOOR COVER, IAW AMM 52-11-25-2. OK FOR SERVICE.
- [SDR FDEA201709262723](https://openairdocs.org/sdr/FDEA201709262723), Sep 26, 2017: HANDLE. BINDS. L1 DOOR HANDLE BINDING DURING DOOR OPENING & CLOSING. INSTALLED A MISSING SPACER RING IAW AMM 52-11-01-4.
- [SDR FDEA201707031843](https://openairdocs.org/sdr/FDEA201707031843), Jul 3, 2017: DOOR. BINDING. DURING PREFLIGHT, FLIGHT CREW WAS UNABLE TO OPEN THE L1 DOOR. PERFORMED INSPECTION AND CHECK OF THE L1 DOOR IAW AMM 52-11-00-6, STEPS 1 & 2. A NEW ESCAPE SLIDE 
- [SDR FDEA201706291785](https://openairdocs.org/sdr/FDEA201706291785), Jun 29, 2017: TIRE. LEAKING. NR 10 TIRE PRESSURE INDICATED 194 PSI. TIRE PRESSURE 171PSI. EICAS EVENT RECORED. NINE HOURS LATER, 94 PSI. LANDING NORMAL IAW QRN, NO VIBRATION OR DAMAGE NOTED
- [SDR FDEA201706241755](https://openairdocs.org/sdr/FDEA201706241755), Jun 24, 2017: GIRT BAR. OBSTRUCTED. DURING BLOCK IN, UNABLE TO OPEN THE LT DOOR. FOUND FLAP OF GIRT MATERIAL LOOSE ON BOTTOM OF DOOR-MOUNTED SLIDE INTERFERING WITH GIRT RELEASE. RESTOWED GIRT MATE
- [SDR FDEA201506111766](https://openairdocs.org/sdr/FDEA201506111766), Jun 11, 2015: WARNING MESSAGE. ILLUMINATED. ON DES, ON MAGENTA LINE, SPEED BRAKES MID, A/C DID UNCOMMAMDED RT ROLL 35DEG BANK. A/P DISCONNECTED NOOTHER PROB. PERFORMED AUTOPILOT FLIGHT DIRECTOR SYSTEM. GR
- [SDR FDEA201210033553](https://openairdocs.org/sdr/FDEA201210033553), Oct 3, 2012: BULB. INOPERATIVE. THE F/O NOTICED THAT THE DOOR 1L AFT OVERHEAD EMERGENCY LIGHT WAS NOT ILLUMINATED. REPLACED BULB IAW MM 33-51-03-2 , ALL TEST OK. FINAL CLOSED.
- [SDR FDEA201112035134](https://openairdocs.org/sdr/FDEA201112035134), Dec 3, 2011: TIRE. DAMAGED. ON POST FLIGHT, FOUND NR 7 MAIN TIRE MISSING, TIRE RECAP. REPLACED NR7 WHEEL ASSY REF MM 32-45-01-4. PREMATURE REMOVAL/INSTALLATION. FINAL CLOSED.
- [SDR FDEA201110194588](https://openairdocs.org/sdr/FDEA201110194588), Oct 19, 2011: UNKNOWN. FUMES. ON DESCENT BETWEEN FL250-FL200 THERE FUMES SIMILAR TO ACETONE IN THE COCKPIT. FINISH DESCENT AND LANDING ON O2. AT BLOCK-IN THERE WERE NO FUMES. CHECKED ALL ARE

## 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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