# N840FD: 2011 Boeing 777FFX

- Status: Valid registration
- Airframe: [Boeing 777FFX](https://openairdocs.org/model/boeing-777ffx) (registry code 138527O, 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: 39682
- Year built: 2011
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 11, 2021
- Certificate issued: January 12, 2021
- Expires: January 31, 2028
- Mode S code: AB805A
- 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=840FD
- Page: https://openairdocs.org/aircraft/N840FD

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 777FFX)

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 N840FD.

## FAA accident and incident reports

None matched to N840FD.

## Service difficulty reports (31)

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 FDEA202608281245](https://openairdocs.org/sdr/FDEA202608281245), Aug 28, 2026: SKIN. DENTED. FOUND LT WING, T/E, OTBD FLAP LOWER SURFACE, HAD ONE DENT AT CROSS OTEF, 315 INCHES AND T/E 5 INCHES. REPAIRED LH WING T/E O/B FLAP LOWER SURFACE 01 EA DENT AT 
- [SDR FDEA202608261229](https://openairdocs.org/sdr/FDEA202608261229), Aug 26, 2026: SKIN. CRACKED. DURING PERFORM W/O: E G-5710-E0376285 H P14 STEP 5.A.(2) THEN FOUND TWO CRACKS AT NR 5 HOLE OF RT UPPER WING SKIN AT WBL 262. RHW UPPER SKIN OF NO.5 HOLE CRACKS
- [SDR FDEA202509011585](https://openairdocs.org/sdr/FDEA202509011585), Sep 1, 2025: BULB. FAILED. DOOR 1 L/H EXTERIOR EMERGENCY LIGHT INOP. FILAMENT REPLACED AND OPS CHECKED IAW AMM 33-51-04-02-0.
- [SDR FDEA202408301198](https://openairdocs.org/sdr/FDEA202408301198), Aug 30, 2024: WINDOW. CRACKED. POST-FLT INSP, L1 DOOR ESCAPE SLIDE BUSTLE PRESSURE GAUGE VIEWPORT WINDOW CRACKED. THE PART FINALLY SHOWED UP. REMOVED AND REPLACED L1 DOOR EMERGENCY ESCAPE SLI
- [SDR FDEA202408031080](https://openairdocs.org/sdr/FDEA202408031080), Aug 3, 2024: WINDOW. OVERHEATED. RIGHT SIDE AFT WINDOW IS VERY HOT TO THE TOUCH AND APPEARS TO HAVE SOME CHARRING AND DELAMINATION IN THE MIDDLE OF THE WINDOW ALONG THE BOTTOM EDGE. COMPLIED WI
- [SDR FDEA202403270381](https://openairdocs.org/sdr/FDEA202403270381), Mar 27, 2024: MODULE. INOPERATIVE. RECEIVED MULTIPLE EICAS ALERTS CLIMBING TO FL330. NO AUTOLAND, WNDSHEAR SYS, EEC MODE L, EEC MODE R. RAN ECL CHECKLISTS FOR EEC MODE LT & RT. ACFT CONTINUED TO 
- [SDR FDEA202403260372](https://openairdocs.org/sdr/FDEA202403260372), Mar 26, 2024: PITOT HEAD. FAILED. AUTO PILOT DISCONNECTED AFTER LEVELING FL340. ALTIMETERS LEFT AND RIGHT INDICATED 400' HIGH. MULTIPLE EICAS : "AIRSPEED UNRELIABLE" " ENG EEC MODE R" "ENG EEC M
- [SDR FDEA202402210205](https://openairdocs.org/sdr/FDEA202402210205), Feb 21, 2024: UNKNOWN. MISOVERHAULED. WHILE CARRY OUT EO E G-5710-E0366409 D PART7, FOUND FIGURE 57, SHEET 2 OF 5, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN. DISCREPANCY IN 
- [SDR FDEA202402210204](https://openairdocs.org/sdr/FDEA202402210204), Feb 21, 2024: UNKNOWN. MISOVERHAULED. WHILE CARRY OUT EO E G-5710-E0366409 D PART7, FOUND FIGURE 53, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN AND THE GAP 0.60
- [SDR FDEA202402210203](https://openairdocs.org/sdr/FDEA202402210203), Feb 21, 2024: UNKNOWN. MISOVERHAULED. WHILE CARRY OUT EO E G-5710-E0366409 D PART7, FOUND FIGURE 51, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN AND THE "0.60 - 
- [SDR FDEA202402210202](https://openairdocs.org/sdr/FDEA202402210202), Feb 21, 2024: UNKNOWN. MISOVERHAULED. WHILE CARRY OUT EO E G-5710-E0366409 D PART7, FOUND FIGURE 49, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN. DISCREPANCY IN 
- [SDR FDEA202402210201](https://openairdocs.org/sdr/FDEA202402210201), Feb 21, 2024: UNKNOWN. MISOVERHAULED. WHILE CARRY OUT EO E G-5710-E0366409 D PART7, FOUND FIGURE 47, SHEET 2 OF 4, THE SECTION CUT D-D ARROW NOT MATCH THE VIEW D-D ORIENTATION SHOWN. DISCREPANCY IN 
- [SDR FDEA202402210200](https://openairdocs.org/sdr/FDEA202402210200), Feb 21, 2024: LONGERON. MISOVERHAULED. WHILE ACCOMPLISHING EO E G-5710-E0366409 D PART7,(LEFT HAND LONGERON MODIFICATION) FOUND FIGURE 44, SHEET 2 OF 2, VIEW A, CIRCLE STEP 2, THE PRINTED QUANTITY 48
- [SDR FDEA202402210199](https://openairdocs.org/sdr/FDEA202402210199), Feb 21, 2024: UNKNOWN. MISOVERHAULED. WHILE CARRY OUT EO E G-5710-E0366409 D PART8, FOUND FIGURE 120, SHEET 2 OF 5, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN. DISCREPANCY IN
- [SDR FDEA202402210198](https://openairdocs.org/sdr/FDEA202402210198), Feb 21, 2024: UNKNOWN. MISOVERHAULED. WHILE CARRY OUT EO E G-5710-E0366409 D PART8, FOUND FIGURE 116, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN AND THE 0.60 MI
- [SDR FDEA202402210197](https://openairdocs.org/sdr/FDEA202402210197), Feb 21, 2024: UNKNOWN. MISOVERHAULED. WHILE CARRY OUT EO E G-5710-E0366409 D PART8, FOUND FIGURE 114, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN AND THE "0.60 -
- [SDR FDEA202402210196](https://openairdocs.org/sdr/FDEA202402210196), Feb 21, 2024: UNKNOWN. MISOVERHAULED. WHILE CARRY OUT EO E G-5710-E0366409 D PART8, FOUND FIGURE 112, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN. DISCREPANCY IN
- [SDR FDEA202402210195](https://openairdocs.org/sdr/FDEA202402210195), Feb 21, 2024: UNKNOWN. MISOVERHAULED. WHILE CARRY OUT EO E G-5710-E0366409 D PART8, FOUND FIGURE 110 SHEET 2 OF 4, THE SECTION CUT D-D ARROW NOT MATCH THE VIEW D-D ORIENTATION SHOWN. DISCREPANCY IN 
- [SDR FDEA202402210194](https://openairdocs.org/sdr/FDEA202402210194), Feb 21, 2024: LONGERON. MISOVERHAULED. WHILE ACCOMPLISHING EO E G-5710-E0366409D PART8 (RIGHT LONGERON MODIFICATION), FOUND FIGURE 107, SHEET 2 OF 2, VIEW A, CIRCLE STEP 2, THE PRINTED QTY 48 LOCATIO
- [SDR FDEA202402180184](https://openairdocs.org/sdr/FDEA202402180184), Feb 18, 2024: STRUCTURE. UNKNOWN. WHILE ACCOMPLISHING EO # EG-5710-E0366409D-PART8, FOUND RIGHT HAND RING CHORD MODIFICATION KIT PART NUMBER 005W0129-4 SHORTAGE REPAIR ANGLE PART NUMBER 691W0017
- [SDR FDEA202307261305](https://openairdocs.org/sdr/FDEA202307261305), Jul 26, 2023: LIGHT. INOPERATIVE. POST-FLT INSP, SUPRNMRY DIRECT CTR OVRHD EMERGENCY LT INOP. REPLACED LIGHT ASSEMBLY PER AMM 33-51-03-2 OPS CHECKES OK FOR SVC
- [SDR FDEA202212303044](https://openairdocs.org/sdr/FDEA202212303044), Dec 30, 2022: COOLING FAN. FAILED. AIRCRAFT SMELLS OF ELECTRICAL SMOKE. DURING TROUBLESHOOTING IT WAS NOTICED THAT WHEN THE L EQUIPMENT COOLING FAN WAS ISOLATED THERE WAS AN IMPROVEMENT OF THE OD
- [SDR FDEA202203290751](https://openairdocs.org/sdr/FDEA202203290751), Mar 29, 2022: NONE. NONE. PDIS 840 33-50 1107 03FEB22 CDG EMER LIGHT ARM SWITCH WIRE GUARD DOES NOT PROTECT THE SWITCH R/R THE EMERGENCY LIGHT SWITCH GUARD PER SMP.
- [SDR FDEA202202060236](https://openairdocs.org/sdr/FDEA202202060236), Feb 6, 2022: NONE. LEAKING. PDIS 840 29-11 1118 06FEB22 MEM FACT U GOT THE HYD PRESS PRI L CHECKLIST AND THE HYD QTY LOW L EICAS APPROXIMATELY 3 HOURS INTO FLIGHT FROM EGSS TO KMEM. FL340/
- [SDR FDEA202111082794](https://openairdocs.org/sdr/FDEA202111082794), Nov 8, 2021: NONE. NONE. REPEAT WRITE UP HIGH PITCH CONTINUOUS TONE, FROM CAPTAIN SIDE BELOW LEFT FOOT. CAB ALT 5800 FT DP 8.5. WENT TO MANUAL ON OUTFLOW VALVES, REDUCED CAB ALT TO 5000
- [SDR FDEA202104261044](https://openairdocs.org/sdr/FDEA202104261044), Apr 26, 2021: SKIN. DAMAGED. WHILE ACCOMPLISHING LEFT HAND E.O.#G-5310-E0332629 K P5 FOUND NEW FUSELAGE SKIN DOUBLER (PART NUMBER : 143W2314Y405) EXISTING HOLE AT STATION 998 STRINGER S-35 
- [SDR FDEA202104261043](https://openairdocs.org/sdr/FDEA202104261043), Apr 26, 2021: SKIN. DAMAGED. WHILE ACCOMPLISHING RIGHT HAND E.O.#G-5310-E0332629 K P6 FOUND NEW FUSELAGE SKIN DOUBLER (PART NUMBER : 143W2314Y406) EXISTING HOLE AT STATION 998 STRINGER S-35
- [SDR FDEA202104230985](https://openairdocs.org/sdr/FDEA202104230985), Apr 23, 2021: SKIN. CRACKED. DURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATION AROUND FASTENER
- [SDR FDEA202104230984](https://openairdocs.org/sdr/FDEA202104230984), Apr 23, 2021: SKIN. CRACKED. DURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATION AROUND FASTENER
- [SDR FDEA202104230983](https://openairdocs.org/sdr/FDEA202104230983), Apr 23, 2021: SKIN. CRACKED. DURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATION AROUND FASTENER 
- [SDR FDEA202104230982](https://openairdocs.org/sdr/FDEA202104230982), Apr 23, 2021: SKIN. CRACKED. DURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATION AROUND FASTENER 

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Boeing 777FFX aircraft: https://openairdocs.org/model/boeing-777ffx/aircraft.md
- The GE GE90-110B1 engine: https://openairdocs.org/engine/ge-ge90-110b1.md

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