# N776AM: 2001 Boeing 777-2Q8, registration cancelled 2017-04-14 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 14, 2017 - Exported to: Austria - Status when cancelled: Valid registration - Airframe: [Boeing 777-2Q8](https://openairdocs.org/model/boeing-777-2q8) (registry code 1385238) - Engine: [GE GE90-94B](https://openairdocs.org/engine/ge-ge90-94b) (registry code 30045) - Data sheets: [TCDS E00049EN](https://openairdocs.org/tcds/E00049EN) (OpenAirDocs) - Serial number: 28692 - Year built: 2001 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 31, 2007 - Certificate issued: February 26, 2013 - Last registry action: October 30, 2015 - Mode S code: AA7F5D - Owner when cancelled: [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 was based - The mark today: https://openairdocs.org/aircraft/N776AM - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=776AM - Page: https://openairdocs.org/deregistered/N776AM-2017-04-14 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Boeing 777-2Q8: https://openairdocs.org/model/boeing-777-2q8.md ## Service difficulty reports (19) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASMF201611015](https://openairdocs.org/sdr/ASMF201611015), Sep 25, 2016: CARBON SEAL. LEAKING. CAPTAIN REPORTED THAT DURING APPROACH, THE LEFT ENGINE OIL QUANTITY DECREASED TO 3 QTS WITH ENGINE PARAMETERS NORMAL. THE AIRCRAFT WAS SENT TO THE HANGAR AND MA - [SDR ASMF20160620011](https://openairdocs.org/sdr/ASMF20160620011), May 6, 2016: TRANSCEIVER. FAILED. AIRCRAFT PERFORMED AN UNSCHEDULED LANDING DUE TO EICAS MESSAGE WXR FAIL. MAINTENANCE PERFORMED THE AIR/GROUND INTERFACE TEST IAW AMM 34-43-02, DETECTING WXR FAI - [SDR ASMF201602009](https://openairdocs.org/sdr/ASMF201602009), Feb 3, 2016: WINDSHIELD. CRACKED. AIRCRAFT RETURNED FROM FLIGHT DUE TO, DURING CLIMB THE RT WINDSHIELD GOT CRACKED. PERFORMED THE QRH 1.9 PROCEDURE, CONFIRMING THE FAILURE. ACFT WAS SENT TO THE - [SDR ASMF201511008](https://openairdocs.org/sdr/ASMF201511008), Nov 11, 2015: ACTUATOR VALVE. FAILED. AIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE RT ENG FAIL LIGHT TURNED ON WITHOUT ABNORMAL INDICATIONS & DURING THE RT ENG SHUTDOWN, THE EGT EXCEEDANC - [SDR ASMF201510028](https://openairdocs.org/sdr/ASMF201510028), Oct 9, 2015: TIRE. PUNCTURED. AIRCRAFT RETURNED TO PLATFORM DUE TO MSG IN EICAS & STATUS OF LOW PRESS IN TIRE NR 11. PERFORMED REVISION DETECTING THE TIRE NR 11 WITH PRESS DROPPED OFF TO 26 - [SDR ASMF201507018](https://openairdocs.org/sdr/ASMF201507018), Jun 29, 2015: WIRE. DAMAGED. AIRCRAFT RETURNED TO PLATFORM, DURING LT ENG START, THE FAILURE CODE 73 21 52 51 & 732 152 51 WERE SHOWED & LT ENG NOT STARTED BY TWO ATTEMPTS. PERFORMED REVISI - [SDR ASMF201310005](https://openairdocs.org/sdr/ASMF201310005), Sep 19, 2013: RADOME. DEFORMED. DURING TRANSIT CHECK, FOUND RADOME DEFORMED. FOUND OUT OF LIMITS IAW SRM 57-12-00. RADOME REPLACED IAW AMM 57-12-02. - [SDR ASMF201306003](https://openairdocs.org/sdr/ASMF201306003), Jun 2, 2013: WEDGE. CRACKED. DURING TRANSIT CHECK, THE T/E WEDGE RT OTBD FLAP WAS DAMAGED PROMOTING A CRACK OF 6.00" LENGTH AND 5.75" WIDE AT BS 214, ON UPPER & LOWER RT OTBD FLAP. MX PERSO - [SDR ASMF201210009](https://openairdocs.org/sdr/ASMF201210009), Sep 29, 2012: ENGINE. INTERMITTENT. ACFT REJECTED TAKE AT 70 KNOTS WITH A GROSS WEIGHT OF 268 000 KG DUE TO RIGHT ENGINE STRONG EXPLOSION WITHOUT ADVISE ON ENGINE PARAMETERS OR EXCEEDS IN CREW CAB - [SDR ASMF201207009](https://openairdocs.org/sdr/ASMF201207009), Jul 31, 2012: PANEL. PUNCTURED. DURING TRANSIT CHECK, DAMAGE WAS DETECTED IN THE NOSE COWLING SKIN ACOUSTIC PANEL OF THE LT ENGINE, A PUNCTURE 1 X 0.75 INCH BEING OUT OF LIMITS IAW SRM 54-11-0 - [SDR ASMF201110002](https://openairdocs.org/sdr/ASMF201110002), Oct 6, 2011: UNKNOWN. SMOKE. DURING CLIMB, SMOKE IN THE PASSENGER CABIN ON THE PREMIER CLASS AND THE FIRST 20 ROWS WAS VISIBLE ALONG THE CEILING; SO FLIGHT CREW ACCOMPLISHED THE QRH 8.5 PRO - [SDR ASMF201104002](https://openairdocs.org/sdr/ASMF201104002), Apr 4, 2011: PUMP. LEAKING. CAPTAIN REPORTED THAT DURING CRUISE, THE HYD QTY LOW LT AND HYD PRESS PRI LT LIGHTS TURNED ON. THE FLIGHT CREW PERFORMED THE QRH 13.3 AND 13.22 PROCEDURES, CONF - [SDR ASMF201007006](https://openairdocs.org/sdr/ASMF201007006), Jul 23, 2010: WHEEL. DAMAGED. DURING PUSH BACK THE TOW FITTING WAS BROKEN. MX PERFORMED GENERAL VISUAL INSP TO THE NLG IAW MM 05-51-01 DETECTING DAMAGE OUT OF LIMIT IN THE RT NOSE LANDING WH - [SDR ASMF201007003](https://openairdocs.org/sdr/ASMF201007003), Jul 7, 2010: ACCESS DOOR. DAMAGED. DURING TRANSIT CHECK A BIRD STRIKE WAS DETECTED BETWEEN SLAT NR 9 AND 10. MX PERFORMED A BIRD STRIKE INSP IAW 05-51-18 DETECTING DAMAGES IN ANTI ICE RELEASE ACC - [SDR ASMF201004001](https://openairdocs.org/sdr/ASMF201004001), Apr 12, 2010: BLADES. DAMAGED. DURING A BORESCOPE INSP OF THE HPC 1, 4 AND 9 STAGES BLADES OF THE RT ENGINE WAS DETECTED. 1 BLADE OF THE HPC 1ST STAGE WITH L/E TIP CURLED 90 DEGREES OUT OF LI - [SDR ASMF20090402](https://openairdocs.org/sdr/ASMF20090402), Apr 14, 2009: SKIN. DAMAGED. DURING TRANSIT CHECK, MX FOUND 3 SCRATCHES OF .5 INCHES ON THE FUSELAGE SKIN, AT THE COVER RECEPTACLE EXTERNAL POWER. A SCRATCH AT STA 342 WITH THICKNESS FOUND - [SDR ASMF 20081201](https://openairdocs.org/sdr/ASMF%2020081201), Dec 1, 2008: TIRE. SEPARATED. DURING TAKE OFF, CAPTAIN REPORTED STRONG VIBRATION IN MLG. MX PERSONNEL DETECTED TREAD LOSS IN THE WHEEL POSITION NR 1 IN THE LT MLG, CRACK IN THE LT FLAP LOWER - [SDR ASM2008F00005](https://openairdocs.org/sdr/ASM2008F00005), Sep 13, 2008: HOSE. DAMAGED. DURING TRANSIT CHECK, MAINT DETECTED DAMAGE AND HYDRAULIC LEAK ON SUPPLY HOSE ASSEMBLY TO RT ENGINE EDP. THE HOSE ASSY, PN AE70970110 WAS REMOVED AND REPLACED A - [SDR ASM2008F00001](https://openairdocs.org/sdr/ASM2008F00001), Aug 3, 2008: BLADE. BENT. DURING TRANSIT CHECK, THE MAINTENANCE PERSONNEL PERFORMED A BOROSCOPIC INSPECTION DETECTING BLADES TIP BENDED IN THE FIRST STAGE OF HIGH PRESSURE COMPRESSOR ROT ## Other aircraft with N776AM - [Registered now](https://openairdocs.org/aircraft/N776AM): Piper PA 46-350P, S/N 4636876, built 2026 --- 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.