# N714SA: 2012 Boeing 777FZB - Status: Valid registration - Airframe: [Boeing 777FZB](https://openairdocs.org/model/boeing-777fzb) (registry code 138527I, 11 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: 37988 - Year built: 2012 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 19, 2012 - Certificate issued: October 5, 2021 - Expires: October 31, 2028 - Mode S code: A98C7A - Registered owner: [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=714SA - Page: https://openairdocs.org/aircraft/N714SA 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 777FZB) 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 (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB DCA24WA201](https://openairdocs.org/ntsb/DCA24WA201), Jun 4, 2024: Boeing 777FZB (N714SA), Narita, Japan, incident ## FAA accident and incident reports None matched to N714SA. ## 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 P5CA2026071800028](https://openairdocs.org/sdr/P5CA2026071800028), Jul 18, 2026: FLASHLIGHT. NO TEST. F/O FLASHLIGHT TEST BUTTON INOPERATIVE. FOUND FO FLASHLIGHT POSITIONED INCORRECTLY. REPOSITIONED FLASHLIGHT & PERFORMED OPS CHECK IAW AMM 25-64-01. OPS CHECK GO - [SDR P5CA2026071600027](https://openairdocs.org/sdr/P5CA2026071600027), Jul 16, 2026: CRADLE. DAMAGED. CAPT SEAT FLASHLIGHT BROKEN SEAL. CAPTAIN'S FLASHLIGHT HOLDER WAS FOUND DAMAGED. REMOVED AND REPLACED CAPT SIDE FLASHLIGHT ASSY IAW AMM 25-64-01. OPS CHECKED GO - [SDR P5CA2026070800025](https://openairdocs.org/sdr/P5CA2026070800025), Jul 8, 2026: CONTAINER. TORN. SUPERNUMERARY POSITION 3 LIFE VEST BAG RIPPED(

REPLACED LIFE VEST AND CHECKS OK FOR SERVICE PER B777 AMM 25-62-01& IPC 25-62-01-54.

) - [SDR P5CA2026032300016](https://openairdocs.org/sdr/P5CA2026032300016), Mar 23, 2026: BATTERY. FAULTED. CAPT FLASHLIGHT BLINKS RED. REMOVED AND REPLACED CAPT FLASHLIGHT BATTERY IAW AMM 25-64-01. OPS CHK OK. - [SDR P5CA2026011500001](https://openairdocs.org/sdr/P5CA2026011500001), Jan 15, 2026: CONTROL PANEL. FAULTED. EICAS TRANSPONDER R STATUS MSG, EICAS TRANSPONDER L STATUS MSG, EICAS TCAS STATUS MSG. R & R TCAS CONTROL PANEL IAW B777 AMM 34-53-02. OPS CHECK GOOD.

) - [SDR P5CA2025091200065](https://openairdocs.org/sdr/P5CA2025091200065), Sep 12, 2025: PDU. SMOKE. MAIN DECK CARGO 45R AND 44L PDU SMOKE COMES OUT. R & R PDU 44L & 45R PER AMM 25-57-01. OPS CHK OK. DMI 238051 & 238052. - [SDR P5CA2025051900031](https://openairdocs.org/sdr/P5CA2025051900031), May 18, 2025: FLASHLIGHT. NO TEST. CAPT FLASHLIGHT WILL NOT TEST.(

REMOVED AND REPLACED CAPT FLASHLIGHT AND OPS CHECK IS GOOD IAW B777 AMM 25-64-01.

) - [SDR P5CA2025041000012](https://openairdocs.org/sdr/P5CA2025041000012), Apr 5, 2025: FILTER. ODOR. THERE IS A BURNING SMELL DUE TO PACK L (WHEN BLEED AIR DEMAND CHANGES).(

C/W CONDITIONAL INSPECTION SMOKE/ODOR IN FLIGHT DECK, FOUND CONTAMINATED RECIRCULATIN - [SDR P5CA2025022000007](https://openairdocs.org/sdr/P5CA2025022000007), Feb 20, 2025: BATTERY. DISCHARGED. AFT R4 SUPERNEMERAY EMERGENCY FLASHLIGHT BATTERY DEAD(

R/R FLASHLIGHT BATTERY IAW AMM 25-64-01. OPS CHK OK

) - [SDR P5CA2025040400011](https://openairdocs.org/sdr/P5CA2025040400011), Feb 4, 2025: UNKNOWN. ODOR. UPON STARTING LEFT ENGINE, THE CREW SMELLED A BURNING ODOR FOLLOWED BY PACK L CHECKLIST.(

PER MCC REQUEST, PERFORMED CONDITIONAL INSP PER AMM 05-51-50-200-801 - [SDR P5CA2025012700003](https://openairdocs.org/sdr/P5CA2025012700003), Jan 26, 2025: SKIN. CRACKED. OPEN HOLE INSPECTION CARRIED OUT AS PER WORKLOAD: SB777-57A0125 RO ON LHW UPPER SKIN COMMON TO MLG TAB OUT FASTENER HOLES 0T AND FOUND HOLE NO. 5 WITH 02EA CRAC - [SDR P5CA2025012700004](https://openairdocs.org/sdr/P5CA2025012700004), Jan 26, 2025: SKIN. CRACKED. OPEN HOLE INSPECTION CARRIED OUT AS PER WC: SB 777-57A0125 RO ON RHW UPPER SKIN COMMON TO MLG TAB OUT FASTENER HOLES 0-6 AND FOUND HOLE #5 WITH OPEN CRACK IND A - [SDR P5CA2025012800005](https://openairdocs.org/sdr/P5CA2025012800005), Jan 26, 2025: SPAR. DAMAGED. WHILE ACCOMPLISHING RH SIDE FRONT SPAR LWR CHORD FASTENER REMOVAL IAW SB 777-57A0122 REV 0 FIG 109, FOUND 1 EACH INCOMING FASTENER WITH ELONGATION(

ELONGATED - [SDR P5CA2025012800006](https://openairdocs.org/sdr/P5CA2025012800006), Jan 26, 2025: POWER SUPPLY. NO TEST. DR 1 LH EMERGENCY LIGHT FAILED OPS TEST(

T/S CARRIED OUT AS PER FIM 33-51 TASK 806 REV 103. R/R PWR SUPPLY & OPS TEST CARRIED OUT AS PER AMM 33-51-06-960- - [SDR P5CA2024060400011](https://openairdocs.org/sdr/P5CA2024060400011), Jun 4, 2024: ENGINE. FAILED. (IFSD) ON TAKEOFF, HEARD A LOUD BANG ON THE RIGHT SIDE. RH ENG N1 ROLLED BACK. CONDUCTED RIGHT ENGINE VISUAL INSPECTION AND SEVERE DAMAGE FOUND. SHUTDOWN RIGHT - [SDR P5CA2023112200115](https://openairdocs.org/sdr/P5CA2023112200115), Nov 22, 2023: UNKNOWN. UNKNOWN. RO #1 SHOULDER HARNESS MALFUNCTION.(

NO FAULT FOUND. OPS CHECKED OK PER AMM 25-11-00.

) - [SDR P5CA2023112200114](https://openairdocs.org/sdr/P5CA2023112200114), Nov 22, 2023: UNKNOWN. UNKNOWN. #1 RELIEF OFFICER INERTIAL REEL DOES NOT RETRACT.(

OBSERVER SEAT OPS CHECK GOOD IAW B777 AMM 25-11-00.

) - [SDR P5CA2023092900108](https://openairdocs.org/sdr/P5CA2023092900108), Sep 28, 2023: COVER. UNKNOWN. LAV EMERGENCY LIGHT SWITCH STUCK IN. DEFERRED LAV CAL LIGHT SWITCH LENS IAW MEL 25-20-01 NEF #6, CAT E DUE TO 27JAN24, TRANSFER TO MDDR #194249, PLACARD INSTALL - [SDR P5CA2023082800081](https://openairdocs.org/sdr/P5CA2023082800081), Aug 27, 2023: UNKNOWN. UNKNOWN. DURING CRUISE FLT LVL 320 SECONDARY ENGINE INDICATIONS APPEARED. INVERSE READING OF 4.0 ON LH ENG N1 VIBRATION. REPEATED SEVERAL TIMES(

PERFORMED #1 ENG BALAN - [SDR P5CA2022092100173](https://openairdocs.org/sdr/P5CA2022092100173), Sep 21, 2022: LIGHT. NONE. AREA EMERGENCY LT AT SUPERNUMERARY COMPARTMENT INOP(

RELAMPED AREA EMERGENCY LT ABOVE 2ND SUPERNUMERARY SEAT IAW AMM 33-51-03, CKD OK.

) - [SDR P5CA2022090800171](https://openairdocs.org/sdr/P5CA2022090800171), Sep 8, 2022: NONE. NONE. PILOT MEDICAL COMPANION KIT WARRANTY OVER EXPIRE.(

REMOVED AND REPLACED PILOT MEDICAL COMPANION KIT AND CHECK OK PER AMM 25-64-50/601.

) - [SDR P5CA2022071100146](https://openairdocs.org/sdr/P5CA2022071100146), Jul 11, 2022: SWITCH. OUT OF POSITION. EMERGENCY LIGHTS SWITCH MUST BE SLIGHTLY FORWARD TO OFF IN ORDER TO DISARM LIGHTS(PERFORMED OPS TEST IAW AMM 33-51-00-710-803, TEST PASSED) - [SDR P5CA2022062500145](https://openairdocs.org/sdr/P5CA2022062500145), Jun 25, 2022: DRIVE UNIT. INOPERATIVE. WX RADAR INOP(REMOVED& AND REPLACED WXR ANTENNA DRIVE UNIT PER AMM 34-43-03 / 401. THEN WEATHER RADAR SYSTEM OPERATIONAL. TEST OK PER AMM 34-43-00-710-804-002. - [SDR UIEA2022060700572](https://openairdocs.org/sdr/UIEA2022060700572), Jun 6, 2022: LIGHT. ILLUMINATED. AFTER SECURE CHECKLIST EMERGENCY LIGHTS REMAINED ILLUMINATED WITH SWITCH OFF. PERF EMERG LT OPS TEST EXCERCISED SW ASSY ALL OPS FND SATIS AMM 33-51-00 - [SDR UIEA2022030900194](https://openairdocs.org/sdr/UIEA2022030900194), Mar 9, 2022: FLASHLIGHT ASSY. FAILED INSP. FO SIDE FLASHLIGHT DOES NOT TEST(

TRANSFERRED TO MDDR 162327 IAW MEL 25-64-02, CAT C.

/

LP 1598900- REMOVED AND REPLACED FIRST OFFICER FLASHLIGHT IAW A - [SDR Q2SA20210826454](https://openairdocs.org/sdr/Q2SA20210826454), Aug 26, 2021: LINE. LEAKING. WHILE EN-ROUTE (ANC-JFK) RECEIVED CAUTION "RESERVE BRAKES/STRG" + "HYD QTY LOW C" FOLLOWEED BY "HYD PRESS SYS CÏ¿½. PERFORMED CHECKLIST AND SHUTDOWN ELECT C2 PU - [SDR P5CA2022071800148](https://openairdocs.org/sdr/P5CA2022071800148), May 27, 2021: GUARD. OUT OF POSITION. EMERGENCY LIGHT GUARD KEEPS TURNING SWITCH OFF(FIXED EMER LIGHTS GUARD PER AMM 33-51-00. CONDITION OK) - [SDR Q2SA20200706433](https://openairdocs.org/sdr/Q2SA20200706433), Jul 6, 2020: TIRE. SEPARATED. AIRCRAFT GROUNDED. DURING T/O ROLL EXPERIENCED NOSE GEAR SHIMMY. DEPARTURE CONTROL ADVISED THAT TIRE DEBRI WAS REPORTED ON RUNWAY. AFTER LANDING INSPECTION OF N - [SDR Q2SA20200506430](https://openairdocs.org/sdr/Q2SA20200506430), May 6, 2020: LINE. LEAKING. AIRCRAFT GROUNDED. AFTER T/O "HYD SYS C QUANTITY LOW". CREW DECLARED EMERGENCY. DETERMINED RIGHT MAIN GEAR STEERING LINE LEAKING , INSTALLED TEMP LINE IAW AMM 3 - [SDR Q2SA20180114387](https://openairdocs.org/sdr/Q2SA20180114387), Jan 14, 2018: WIRE. DAMAGED. NO SIDEWALL LIGHTS ON LEFT AND RIGHT SIDE OF MAIN CARGO DECK DO NOT ILLUMINATE. AIRCRAFT GROUNDED. SIGN OF BURN WITH CONNECTED WIRES DISCOLORED AND BURNED AS WE - [SDR Q2SA20170513382](https://openairdocs.org/sdr/Q2SA20170513382), May 13, 2017: TURBINE BLADES. SEPARATED. LEFT ENGINE INDICATED A VIBRATION OF 5.2 AFTER TAKE OFF AIRFRAME VIBRATION WAS FELT UNTIL POWER PULLED BACK. VIBRATION REMAINED AT 4.6 UNTIL ENGINE SHUT DOWN. A - [SDR Q2SA20130528203](https://openairdocs.org/sdr/Q2SA20130528203), May 28, 2013: SKIN. DAMAGED. LEFT WING L/E OTBD OF ENGINE PANEL, OPEN. DURING INVESTIGATION FOUND APPROX 11 X 7 INCH SECTION OF SKIN DETACHED FROM RIVET ROW ON NR 5 SLAT STA 711.5 ACCOMPLIS - [SDR Q2SA2012071671401](https://openairdocs.org/sdr/Q2SA2012071671401), Jul 16, 2012: GUARD. BROKEN. EMERGENCY LIGHT CONTROL SWITCH GUARD BROKEN. REMOVED AND REPLACED SWITCH GUARD PER AMM 33-51-00, PAGE 501. ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Earlier aircraft with N714SA The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N714SA before. - [Cancelled 2007-03-01](https://openairdocs.org/deregistered/N714SA-2007-03-01): Cessna A185F, S/N 18504416, built 1984. Exported to Brazil. Owner: [Southern Cross Aircraft LLC](https://openairdocs.org/faa-owner/SOUTHERN%20CROSS%20AIRCRAFT%20LLC), [Ft Lauderdale, FL](https://openairdocs.org/faa-place/FL/Ft%20Lauderdale) ## Related - Other Boeing 777FZB aircraft: https://openairdocs.org/model/boeing-777fzb/aircraft.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.