# N883FD: 2010 Boeing 777FHT - Status: Valid registration - Airframe: [Boeing 777FHT](https://openairdocs.org/model/boeing-777fht) (registry code 138527M, 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: 39285 - Year built: 2010 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 13, 2010 - Certificate issued: October 14, 2010 - Expires: October 31, 2029 - Mode S code: AC297B - 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=883FD - Page: https://openairdocs.org/aircraft/N883FD From the FAA registry file of October 21, 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 777FHT) 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 N883FD. ## FAA accident and incident reports None matched to N883FD. ## Service difficulty reports (40) As reported by operators and repair stations. - [SDR FDEA202607140922](https://openairdocs.org/sdr/FDEA202607140922), Jul 14, 2026: SKIN. DAMAGED. WHEN PERFORM EA G-5730-T0384072 P2 STEP 2, REPORT THE CURRENT AIRCRAFT CONFIGURATION TO FEDEX SERVICE ENGINEERING TO REQUEST AIRPLANE JACKING REQUIREMENTS FROM - [SDR FDEA202602260284](https://openairdocs.org/sdr/FDEA202602260284), Feb 26, 2026: SAFETY WIRE. WRONG PART. REMOVED RH DOOR SLIDE MPN 62771-128 MSN M10748 REF FEA G-2560-F0386294 REV NO. A PS P1 AND AMM 25-66-01-4 AND WRI 25-60/513. INSTALLED COPPER SAFETY WIRE (MS209 - [SDR FDEA202602260283](https://openairdocs.org/sdr/FDEA202602260283), Feb 26, 2026: SAFETY WIRE. WRONG PART. REMOVED LH SLIDE MPN 62771-127 MSN M10268 REF FEA G-2560-F0386282 REV NO. A PS P1 AND AMM 25-66-01-4 AND WRI 25-60/5712 PLACED SLIDE IN LINESHACK 380 INSTALLED - [SDR FDEA202512250013](https://openairdocs.org/sdr/FDEA202512250013), Dec 25, 2025: MODULATING VALVE. INOPERATIVE. AT FL390 WITH OAT -58C, BEGAN TO RECEIVE INTERMITTENT PACK L EICAS MESSAGE WITH CORRESPONDING CABIN TEMPERATURE DROP. COCKPIT TEMPERATURE WAS SET TO 26C AS COCK - [SDR FDEA202507111178](https://openairdocs.org/sdr/FDEA202507111178), Jul 11, 2025: SKIN. CRACKED. UT AND HFEC OPEN HOLE INSPECTION FOUND TWO CRACKS IN LH WING #5 HOLE. THE LH WING UPPER SKIN #5 HOLE TWO CRACKS REPAIRED AS PER B777 SRM51-20-07-0G REV:47.6 AND - [SDR FDEA202310041697](https://openairdocs.org/sdr/FDEA202310041697), Oct 4, 2023: SLAT. DENTED. NO .7 SLAT EXTERNAL UPR SURFACE FROM IB TO OB 74 INCH CROSS TE TO LE 2 INCH FOUND ONE DENT. EVALUATED NO.7 SLAT EXTERNAL UPR SURFACE FROM IB TO OB 74INCH CROSS - [SDR FDEA202310021685](https://openairdocs.org/sdr/FDEA202310021685), Oct 2, 2023: FLAP. DENTED. LH WING OB FLAP LOWER SURFACE FROM OB TO IB 210 INCH CROSS TE TO LE 13 INCH FOUND ONE DENT. EVALUATED LH WING OB FLAP LOWER SURFACE FROM OB TO IB 210 INCH CROSS - [SDR FDEA202310021684](https://openairdocs.org/sdr/FDEA202310021684), Oct 2, 2023: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8601-31 FOUND CRACKED,AT STA1710 RBL1. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8601-31 CRACKED AT STA1710 RBL1, DAMAGE - [SDR FDEA202310021683](https://openairdocs.org/sdr/FDEA202310021683), Oct 2, 2023: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8601-19 FOUND CRACKED,AT STA1660 RBL1. EVALUATED AND MEASURE MAIN DECK CARGO FLOOR PANEL P/N:152W8601-19 CRACKED AT STA1660 - [SDR FDEA202105281416](https://openairdocs.org/sdr/FDEA202105281416), May 28, 2021: SKIN. DAMAGED. RH ELEVATOR FWD EDGE FOUND FASTENER SINK AT ELEV STA 232.2857. REPAIRED DAMAGE ON RH ELEVATOR FWD EDGE AT ELEV STA 232.2857 AS PER B777 SRM 55-20- 01-2R REPAIR - [SDR FDEA202105281415](https://openairdocs.org/sdr/FDEA202105281415), May 28, 2021: FLOOR SUPPORT. CRACKED. FOUND BULK CARGO COMPARTMENT STRINGER CRACK AT STA1958.00 LBL8.2 BULK CARGO COMPARTMENT AT STA1958 LBL 8.2 CRACKED STRINGER REPAIRED AS PER B777 SRM 53-70-53-2R - [SDR FDEA202105241376](https://openairdocs.org/sdr/FDEA202105241376), May 24, 2021: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PNL 241QF FOUND CRACKED. REPAIRED DAMAGE ON MAIN DECK CARGO PNL 241QF AS PER B777 SRM 53-00-50-2R, REPAIR 1, REV.38. REPAIR CLASSIFIED AS - [SDR FDEA202105241370](https://openairdocs.org/sdr/FDEA202105241370), May 24, 2021: FLOOR PANEL. DAMAGED. MAIN DECK CARGO FLOOR PANEL 242PF FOUND CRACKED. REPAIRED DAMAGE ON MAIN DECK CARGO FLOOR PNL 242PF AS PER B777 SRM 53-00-50-2R, REPAIR 1,REV.38. REPAIR CLASSIF - [SDR FDEA202105241369](https://openairdocs.org/sdr/FDEA202105241369), May 24, 2021: FLOOR PANEL. DAMAGED. MAIN DECK CARGO FLOOR PNL 242LF FOUND CRACKED. REPAIRED DAMAGE ON MAIN DECK CARGO FLOOR PNL 242LF AS PER B777 SRM 53-00-50-2R, REPAIR 1,REV.38. REPAIR CLASSIFIE - [SDR FDEA202105241377](https://openairdocs.org/sdr/FDEA202105241377), May 24, 2021: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PNL 242QF FOUND CRACKED. REPAIRED DAMAGE ON MAIN DECK CARGO FLOOR PNL 242QF AS PER B777 SRM 53-00-50-2R, REPAIR 1,REV.38. REPAIR CLASSIFIE - [SDR FDEA202105151227](https://openairdocs.org/sdr/FDEA202105151227), May 15, 2021: FLOOR SUPPORT. CRACKED. FOUND BULK CARGO FLOOR SUPPORT CRACKED AT STA1958.00 LBL 8.2 . BULK CARGO AT STA1958 LBL8.2 CRACKED STRINGER REPAIRED AS PER B777 SRM 53-70-53- 2R REPAIR 2 REV3 - [SDR FDEA202105121197](https://openairdocs.org/sdr/FDEA202105121197), May 12, 2021: FITTING. DAMAGED. RHW ENG STRUT AFT FAIRING I/B AFT INSTALLATION BOLT HOLE FOUND ELONGATED RHW ENG STRUT AFT FAIRING I/B AFT SUPPORT FITTING HOLE ELONGATED REPAIRED AS PER B777 S - [SDR FDEA202105121198](https://openairdocs.org/sdr/FDEA202105121198), May 12, 2021: FITTING. WORN. RHW ENG STRUT AFT FAIRING O/B FWD INSTALLATION BOLT HOLE FOUND ELONGATED RHW ENG STRUT AFT FAIRING O/B FWD SUPPORT FITTING HOLE ELONGATED REPAIRED AS PER B777 S - [SDR FDEA202105111173](https://openairdocs.org/sdr/FDEA202105111173), May 11, 2021: SKIN. CRACKED. SURFACE HFEC INSPECTION FOUND 02EA CRACKS (FWD CRACK APPROX.0.700 INCH IN LENGTH AND AFT CRACK APPROX.0.650 INCH IN LENGTH) ON THE EXTERNAL SUR FACE OF THE FUSE - [SDR FDEA202105111172](https://openairdocs.org/sdr/FDEA202105111172), May 11, 2021: SKIN. CRACKED. SURFACE HFEC INSPECTION FOUND 01EA CRACK APPROX.0.650 INCH IN LENGTH ON THE EXTERNAL SURFACE OF THE FUSELAGE SKIN AROUND THE 01EA HOLE COMMON TO THE RIGHT SIDE - [SDR FDEA202105071149](https://openairdocs.org/sdr/FDEA202105071149), May 7, 2021: DOUBLER. DAMAGED. ELONGATE HOLE FOUND ON THE DOUBLER AT STA993 STGR34LH-35LH DURING PERFORMING EO EG-5310-E0332629 K P5 STEP 11.P . REPAIR CARRIED OUT TO THE ENLONGATED HOLE ON T - [SDR FDEA202105071148](https://openairdocs.org/sdr/FDEA202105071148), May 7, 2021: LONGERON. DAMAGED. DURING PERFORMING EO EG-5310-E0332629K P6 STEP 13.H, 11EA YYT-10 FASTENER HOLES WERE 1ST OVERSIZED AT STA993-1003 STGR35RH-36RH, 3EA YLK-16 FASTENER HOLES WERE - [SDR FDEA202105071147](https://openairdocs.org/sdr/FDEA202105071147), May 7, 2021: SKIN. DAMAGED. DURING PERFORMING EO EG-5310-EO332629K P6 STEP 11.P,FOUND 01EA ZLJ-8 (BACB30NY8K*) COUNTERSUNK FASTENER AT STA 998 STGR 35R NEAR THE EDGE OF MACHINED STEP OF DO - [SDR FDEA202105071145](https://openairdocs.org/sdr/FDEA202105071145), May 7, 2021: FITTING. DAMAGED. DURING PERFORMING EO EG-5310-EO332629K P5 STEP 11.P,FOUND 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA 998 STGR35L NEAR THE EDGE OF MACHINED STEP OF DOUB - [SDR FDEA202105071143](https://openairdocs.org/sdr/FDEA202105071143), May 7, 2021: FITTING. DAMAGED. DURING PERFORMING EO EG-5310-EO332629K P6 STEP 13.H, 11 EA YYT-10 FASTENER HOLES WERE 1ST OVERSIDED AT STA 993-1003 STGR35RH-36RH, 3EA YLK-16 FASTENER HOLES WER - [SDR FDEA202105071150](https://openairdocs.org/sdr/FDEA202105071150), May 7, 2021: SKIN. GOUGED. DURING PERFORMING EO G-5310-EO332629 K P6 STEP 9A FOUND SOME GOUGES ON THE EXTERNAL SURFACE OF THE FUSELAGE SKIN COMMON TO LONGERON FITTING AFTER REMOVAL OF THE - [SDR FDEA202105071146](https://openairdocs.org/sdr/FDEA202105071146), May 7, 2021: FITTING. DAMAGED. DURING PERFORMING EO EG-5310-EO332629K P6 STEP 11.M, FOUND 01 EA EXISTING HOLES OVERSIZED (DIAMETER:0.434") ON THE SKIN AT STA 993 - STA1035,STGR 35R - 37R. THE - [SDR FDEA202105071144](https://openairdocs.org/sdr/FDEA202105071144), May 7, 2021: FITTING. DAMAGED. DURING PERFORMING EO EG-5310-EO332629K P5 STEP 11.M,FOUND 01EA EXISTING HOLES OVERSIZED (DIAMETER:0.434") ON THE SKIN AT STA 993-STA 1035 STGR 35L-37L. THE BOEI - [SDR FDEA202012033018](https://openairdocs.org/sdr/FDEA202012033018), Dec 3, 2020: NONE. NONE. R/H HORIZONTAIL STAB TIP T/E DAMAGED BY A/C STRIKE ALL WORK COMPLETED ON R/H HORIZONTAL STAB FAIRING. PART INSTALLED MADE SERVICABLE BY COMPLETION OF EA G-5510- - [SDR FDEA2020062311304](https://openairdocs.org/sdr/FDEA2020062311304), Jun 21, 2020: BRACKET. CRACKED. WHEN OPENING NR 2 ENGINE T/R FOUND BIFURICATION BRACKET ON PYLON CRACKED. REMOVED AND REPLACED NR 2 ENG T/R BIFURICATION BEACKET IN REF TO 777 SRM 51-40-02, JOB - [SDR FDEA201807111662](https://openairdocs.org/sdr/FDEA201807111662), Jul 11, 2018: SKIN. DAMAGED. LT WING SLAT NR 7 L/E FOUND WRINKLE AT FROM O/B TO I/B 23IN POS. COMPLIED WITH EA G-5750-T0340942 P1, REPAIRED THE LT WING NR 7 SLAT L/E WRINKLE. MAJOR REPAIR I - [SDR FDEA201710213019](https://openairdocs.org/sdr/FDEA201710213019), Oct 21, 2017: LAMP. FAILED. RIGHT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-04-2. - [SDR FDEA201411193807](https://openairdocs.org/sdr/FDEA201411193807), Nov 19, 2014: LIGHT. INOPERATIVE. ONE EMER LIGHT INOPERATIVE. RELAMPED EMER LIGHT AT 1R. EMER LIGHTS CHECKED GOOD IAW AMM SMP. - [SDR FDEA201411153722](https://openairdocs.org/sdr/FDEA201411153722), Nov 15, 2014: UNKNOWN. MALFUNCTIONED. UNCOMMANDED TURN, DURING CRUISE PHASE OF FLIGHT WITH LNAV & VNAV SELECTED, THE ACFT STARTED A RANDOM TURN TO THE LEFT. SWITCHED TO HEADING SELECT TO TURN BACK T - [SDR FDEA201408092126](https://openairdocs.org/sdr/FDEA201408092126), Aug 9, 2014: MODULE. MALFUNCTIONED. LOSS OF MULTIPLE SYS DURING CLIMB OUT. ACFT WAS LOADED DURING HEAVY RAIN, DURING LAST PART OF LOADING SECONDARY EXTERNAL POWER CYCLED OFF & ON RAPIDLY SEVERAL T - [SDR FDEA201311062694](https://openairdocs.org/sdr/FDEA201311062694), Nov 6, 2013: CIRCUIT CARD. FAILED. "DET FIRE ENG RT" EICAS MESSAGE 230 INTO FLIGHT. INTERROGATED MATERIAL, FOUND MAINT MESSAGE 26-10012 NOT ACTIVE. TROUBLESHOT IAW FIM 26-11 TASK 805, R & R ENGIN - [SDR FDEA201306171317](https://openairdocs.org/sdr/FDEA201306171317), Jun 17, 2013: SCAVENGE PUMP. FAILED. RT ENGINE APPEARED TO BE LOOSING OIL BEFORE START, LEFT 24 QTS, RIGHT 23 QTS. AFTER 3 HOURS OF FLIGHT RT ENG SLOWLY DECREASED TO 14 QTS WHILE LT ENG REMAINED AT - [SDR FDEA201305291119](https://openairdocs.org/sdr/FDEA201305291119), May 29, 2013: CIRCUIT BREAKER. TRIPPED. DURING ACFT POWER UP, FOUND P320 PANEL, RELAY K24050, CTRL (F1) CIRCUIT BREAKER TRIPPED. RELAY, CONNECTOR, AND WIRES REMOVED AND REPLACED AS PER SWPM 20-10-11 R - [SDR FDEA201212184316](https://openairdocs.org/sdr/FDEA201212184316), Dec 18, 2012: LAMP. BURNED OUT. EMERGENCY LIGHT LAMP BURNED OUT. REPLACED LAMP IAW AMM 33-51-03-2. EMERGENCY LIGHT TESTED SATISFACTORY. - [SDR FDEA201108313594](https://openairdocs.org/sdr/FDEA201108313594), Aug 31, 2011: BALLAST. FAILED. LIGHT OVER LEFT ENTRY DOOR COMES ON IF YOU CYCLE EMERGENCY LIGHT SWITCH IT GOES OFF. AFTER A PERIOD OF TIME COMES BCACK ON. TROUBLESHOT TO A BAD ENTRY DOOR LIGH ## Related - Other Boeing 777FHT aircraft: https://openairdocs.org/model/boeing-777fht/aircraft.md - STCs for the Boeing 777FHT: https://openairdocs.org/model/boeing-777fht/stcs.md - The GE GE90-110B1 engine: https://openairdocs.org/engine/ge-ge90-110b1.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.