# N774AM: 2001 Boeing 777-2Q8, registration cancelled 2019-01-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 3, 2019 - 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: 28689 - Year built: 2001 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 17, 2006 - Certificate issued: February 27, 2013 - Last registry action: September 20, 2018 - Mode S code: AA77EF - 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/N774AM - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=774AM - Page: https://openairdocs.org/deregistered/N774AM-2019-01-03 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 (27) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASMF201801007](https://openairdocs.org/sdr/ASMF201801007), Dec 2, 2017: SEAL. LEAKING. DURING A TRANSIT CHECK, FOUND A HYDRAULIC LEAK IN THE NOSE LANDING GEAR. THE NOSE LANDING GEAR SHOCK STRUT HYDRAULIC LEAK OUT OF LIMITS. THE SEALS WERE REPLACED - [SDR ASMF20170911009](https://openairdocs.org/sdr/ASMF20170911009), Aug 28, 2017: PCU. LEAKING. DURING TRANSIT CHECK, DETECTED EVIDENCE OF A HYDRAULIC LEAK IN THE LEFT MAIN LANDING GEAR. MAINTENANCE PERSONNEL PERFORMED INSPECTION IAW AMM 27-61-00, DETECTIN - [SDR ASMF201608002](https://openairdocs.org/sdr/ASMF201608002), Jun 19, 2016: COUPLER. LEAKING. DURING TRANSIT CHECK, A WATER LEAK WAS DETECTED IN THE LOWER FUSELAGE. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING WATER LEAK IN THE LT AFT CARGO COMPART - [SDR ASMF201606003](https://openairdocs.org/sdr/ASMF201606003), Apr 17, 2016: BRAKE ASSY. OVERHEATED. AIRCRAFT REJECTED TAKEOFF AT 100 KNOTS DUE TO AN EVENT OF 1023 DEGREES CELSIUS OF EGTS EXCEEDANCE IN THE FELT ENGINE AND BY NOTIFICATION OF THE AIR TRAFFIC CONT - [SDR ASMF201602001](https://openairdocs.org/sdr/ASMF201602001), Dec 20, 2015: SLIDE RAFT. STUCK. DURING TRANSIT CHECK, THE LT DOOR SLIDE, RAFT NR 1 WAS FOUND STUCK & OUT OF POSITION. REMOVED THE LT DOOR SLIDE, RAFT NR 1 IAW AMM 25-66-01 & DEFERRED THE LT DO - [SDR ASMF201511009](https://openairdocs.org/sdr/ASMF201511009), Nov 12, 2015: ACTUATOR VALVE. FAILED. AIRCRAFT RETURNED TO PLATFORM DUE TO DURING LT ENG START THE MSG IN EICAS & STATUS OF ENG FUEL VLV LT, SPAR VLV LT & LIGHTS TURNED ON. PERFORMED FIM 28-20 TASK - [SDR ASMF201506012](https://openairdocs.org/sdr/ASMF201506012), May 15, 2015: RADOME. OUT OF LIMITS. AIRCRAFT PERFORMED AN UNSCHEDULED LANDING DUE TO DURING CLIMB EICAS MSG WXR FAIL & BOTH WX RADARS DID NOT SHOW INDICATIONS CORRECT. PERFORMED A BIRD & HAIL STRI - [SDR ASMF201409009](https://openairdocs.org/sdr/ASMF201409009), Aug 27, 2014: IDG. LEAKING. CAPTAIN REPORTED THAT AFTER START ENGS, THE EICAS MSG ELEC GEN SYS R WAS SHOWN & THE RT DRIVE LIGHT TURNED ON. DURING MAINTENANCE REVISION, AN OIL LEAK WAS DETE - [SDR ASMF201407003](https://openairdocs.org/sdr/ASMF201407003), Jun 15, 2014: SKIN. DENTED. DURING OVERNIGHT CHECK, DETECTED A BIRD STRIKE ABOVE FUSELAGE WINDSHIELD, SO BIRD STRIKE CONDITIONAL INSPECTION WAS PERFORMED IAW MM 05-51-18, DETECTING A DENT - [SDR ASMF201407001](https://openairdocs.org/sdr/ASMF201407001), Jun 1, 2014: STATIC PORT. DAMAGED. DURING TRANSIT CHECK DETECTED EVIDENCE OF A LIGHTNING STRIKE IN THE RT ENG STATIC PORT. PERFORMED A LIGHTNING STRIKE INSPECTION IAW MM 05-51-19 DETECTING THE ST - [SDR ASMF201311011](https://openairdocs.org/sdr/ASMF201311011), Nov 5, 2013: SHUTOFF VALVE. MALFUNCTIONED. DURING FUELING FOR PUMP JETTISON TEST, A FUEL SPILLAGE IN THE RT TANK OCCURRED DUE TO THE SHUTOFF VLV DID NOT CLOSE. THE PLATFORM WAS CLEANED BY FIREMEN & MX PE - [SDR ASMF20130531012](https://openairdocs.org/sdr/ASMF20130531012), May 15, 2013: LINE. LEAKING. CAPTAIN REPORTED THAT DURING LANDING, A HYD LEAK WAS DETECTED IN THE RT HYD SYS WITH INDICATION OF 30 PERCENT. MX PERSONNEL PERFORMED REVISION DETECTING HYD LEA - [SDR ASMF201211006](https://openairdocs.org/sdr/ASMF201211006), Nov 16, 2012: BYPASS VALVE. FAILED. ACFT RETURNED TO PLATFORM DUE TO DURING TAXING THE NOSE WHEEL STEERING WAS STUCK. MX PERSONNEL PERFORMED THE FIM 32-51 TASK 808 PROCEDURE, DETECTING THE BY PASS - [SDR ASMF201205001](https://openairdocs.org/sdr/ASMF201205001), Apr 27, 2012: CONNECTOR. DAMAGED. DURING OVERNIGHT CHECK, THE EMERGENCY LOCATOR TRANSMITTER ACTIVATED INTERMITTENTLY WITH ELT SWITCH IN OFF POSITION. MX PERSONNEL REMOVED THE EMERGENCY LOCATOR T - [SDR ASMF201105001](https://openairdocs.org/sdr/ASMF201105001), Apr 28, 2011: O-RING. CRACKED. DURING TRANSIT CHECK, TECH PERSONNEL DETECTED A FUEL LEAK IN RT WING DUE TO A CRACK IN THE FUEL PUMP O-RING NR 3; SO THE RT FUEL PUMP O-RING WAS REPLACED IAW MM - [SDR ASMF20110322001](https://openairdocs.org/sdr/ASMF20110322001), Mar 22, 2011: BOLT. LOOSE. CAPTAIN REPORTED DURING THE DESCENT, THE RT ENGINE VIBRATION REACHED 4.7 OF N2. ACFT WAS SENT TO THE HANGAR AND MX PERFORMED A TRIM BALANCE IAW MM 71-00-00 TASK - [SDR ASMF201102003](https://openairdocs.org/sdr/ASMF201102003), Feb 14, 2011: BLADES. DAMAGED. DURING A BORESCOPE INSPECTION OF THE HPC 1ST STAGE BLADES OF RIGHT ENGINE WAS DETECTED FOUR BLADES OF THE HPC 1ST STAGE WITH LEADING EDGE TIP CURLED 45 DEGREES - [SDR ASMF201012009](https://openairdocs.org/sdr/ASMF201012009), Dec 17, 2010: TIRE. DAMAGED. DURING TOWING TO PLATFORM, THE TOW TRACTOR DRIVER WAS EXCEEDING THE MAXIMUM NLG TOWING ANGLE TO LT SIDE AND TOW BAR WAS BROKEN. MX PERFORMED THE MAXIMUM NLG TOW - [SDR ASMF201009001](https://openairdocs.org/sdr/ASMF201009001), Sep 1, 2010: SKIN. DAMAGED. CAPTAIN REPORTED A LIGHTNING STRIKE IN THE LT SIDE LOWER FUSELAGE SKIN. MX PERFORMED A LIGHTNING STRIKE INSPECTION IAW MM 05-51-19, NO DAMAGES WERE DETECTED. - [SDR ASMF201008004](https://openairdocs.org/sdr/ASMF201008004), Jul 3, 2010: SKIN. DAMAGED. DURING TRANSIT CHECK WAS DETECTED A LIGHTNING STRIKE IN THE FUSELAGE SKIN. MX PERFORMED A LIGHTNING STRIKE INSP IAW MM 05-51-19 DETECTING RIVETS WITH HEAD BURNE - [SDR ASMF201006004](https://openairdocs.org/sdr/ASMF201006004), Jun 27, 2010: FLAP SYSTEM. MALFUNCTIONED. ACFT REJECTED TAKEOFF AT 65 KNOTS, DURING TAKEOFF ACCELERATION A FLAP CONFIGURATION ALARM WITH RED ANNOUNCEMENT TURNED ON. MX PERSONNEL VERIFIED FOR FAILURE DET - [SDR ASMF201006002](https://openairdocs.org/sdr/ASMF201006002), Jun 8, 2010: SEAL. OUT OF POSITION. ACFT RETURNED TO DEPARTURE, DURING CLIMB WAS DETECTED A LOAD COMPARTMENT PRESSURIZATION LEAK NOISE. MX FOUND THE FWD ACCESS ELEC DOOR SEAL, UPSIDE DOWN, THE DOO - [SDR ASMF20090704](https://openairdocs.org/sdr/ASMF20090704), Jul 29, 2009: SKIN. DAMAGED. DURING OVERNIGHT CHECK SEVERAL LIGHTNING STRIKES IN FUSELAGE SKIN BS 340.5 / S39L; STA368.5 / S39L; STA 410.5 / S-40L; STA411.5 / S-39L; STA 421.5 / S-39L; STA - [SDR ASMF200802007](https://openairdocs.org/sdr/ASMF200802007), Feb 24, 2008: SKIN. DEFORMED. DURING TAXING, THE AC LT SLATS NR 2 AND 3 STRUCK AGAINST A LAMPPOST OF TAXIWAY. DETAILED INSP WAS PERFORMED ON LT WING DETECTING STRUCTURAL DAMAGE ON SLATS NR 2 - [SDR ASMF200801004](https://openairdocs.org/sdr/ASMF200801004), Jan 23, 2008: LIGHT. DAMAGED. THE LT SLAT NR 1 OF THE AC REGISTRATION N746AM HIT AC LT WING TIP. DETAILED INSPECTION WAS PERFORMED ON LT WING TIP DETECTING CRACKED THE LENS OF THE LT REAR PO - [SDR ASMF200707008](https://openairdocs.org/sdr/ASMF200707008), Jul 11, 2007: SLAT SYSTEM. MALFUNCTIONED. AIRCRAFT RETURNED TO PLATFORM, EICAS SHOWS SLATS PRIMARY FAIL MESSAGE. MAINTENANCE PERSONNEL CHECKED THE MAT AND IT SHOWED THE FAILURE CODE 27-20962 (LATCHED); - [SDR ASMF200706001](https://openairdocs.org/sdr/ASMF200706001), Jun 8, 2007: BYPASS VALVE. UNLOCKED. AIRCRAFT REJECTED TAKEOFF AT 50 KTS, STARTED THE TAKEOFF RUN, THE MAIN GEAR STEERING CONFIGURATION LIGHT TURNED ON AND THE ALARM WAS ACTIVATED. MAINTENANCE PERS ## Other aircraft with N774AM - [Registered now](https://openairdocs.org/aircraft/N774AM): Amazon.Com Services MK30, S/N 178650109H --- 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.