# N746AM: 2006 Boeing 777-2Q8, registration cancelled 2018-05-24 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 24, 2018 - Exported to: Bermuda - 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: 32719 - Year built: 2006 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: April 27, 2006 - Certificate issued: November 2, 2011 - Last registry action: June 14, 2017 - Mode S code: AA08E0 - 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/N746AM - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=746AM - Page: https://openairdocs.org/deregistered/N746AM-2018-05-24 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 (15) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASMF201608008](https://openairdocs.org/sdr/ASMF201608008), Jul 5, 2016: WINDOW. CRACKED. CAPTAIN REPORTED THAT DURING CRUISE, THE RT SIDE WINDOW HEAT WITH FAULT CODE 304 022 42 DUE TO A CRACK ON THE LOWER RT CORNER WITH CORRECT CABIN PRESSURE. MAINT - [SDR ASMF201501011](https://openairdocs.org/sdr/ASMF201501011), Nov 4, 2014: GENERATOR. FAILED. CAPTAIN REPORTED THAT AFTER START ENGS APPEARED THE EICAS MSG LT BACK UP GEN OUT OF SERVICE. PERFORMED FIM 24-20 TASK 811 PROCEDURE, SHOWING FAILURE CODE 24-460 - [SDR ASMF201311223002](https://openairdocs.org/sdr/ASMF201311223002), Dec 18, 2013: WARNING SYSTEM. FALSE ACTIVATION. AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT LIM DUE TO EICAS MESSAGE WXR SYS. MX PERSONNEL PERFORMED THE AIR, GND INTERFACE TEST IAW AMM 34-43-00, NOT CONFIRMI - [SDR ASMF201312005](https://openairdocs.org/sdr/ASMF201312005), Dec 1, 2013: ENGINE. MALFUNCTIONED. CAPTAIN REPORTED THAT DURING TAKEOFF, THE RT ENG REACHED 1031 CELSIUS DEGREES OF EGT FOR AROUND 2 SECONDS. PERFORMED RT ENG INSPECTION WITH EGT PARAMETERS WITHI - [SDR ASMF201308016](https://openairdocs.org/sdr/ASMF201308016), Jul 24, 2013: FAIRING. DAMAGED. CAPTAIN REPORTED THAT DURING LANDING ROLL, ACFT HAD A BIRD STRIKE ON RT ENGINE. MX PERSONNEL PERFORMED A BIRD STRIKE CONDITIONAL INSPECTION IAW MM 05-51-18, DET - [SDR ASMF201308006](https://openairdocs.org/sdr/ASMF201308006), Jul 9, 2013: STRUCTURE. DAMAGED. DURING ROUTINE CHECK, LIGHTNING STRIKE IN NOSE AND MLG. MAINTENANCE PERSONNEL PERFORMED A LIGHTNING STRIKE INSPECTION IAW MM 05-51-19, DETECTING VHF ANTENNA NR - [SDR ASMF201303017](https://openairdocs.org/sdr/ASMF201303017), Feb 8, 2013: ACTUATOR. LEAKING. DURING TRANSIT CHECK, A HYD LEAK WAS DETECTED ON AFT REAR SPAR OF LT WING. MX PERSONNEL PERFORMED AN INSPECTION DETECTING HYD LEAK IN SPOILER ACTUATOR NR 3, SO - [SDR ASMF201207001](https://openairdocs.org/sdr/ASMF201207001), Jun 19, 2012: SKIN. PUNCTURED. DURING PUSH BACK, THE LT WING L/E WAS HIT BY A MOBILE STAIRWAY CAUSING A HOLE OF 8.0" LONG, 4.0" WIDE. INSPECTION PERSONNEL EVALUATED THE DAMAGED AND FOUND OUT - [SDR ASMF201012005](https://openairdocs.org/sdr/ASMF201012005), Dec 3, 2010: SENSOR. DAMAGED. ACFT PERFORMED AN UNSCHEDULED LANDING, DURING CRUISE THE ENG OIL FILTER RT LIGHT TURNED ON WITH AN OIL TEMP INDICATION OF 60 CENTIGRADE DEGREES AND OIL PRESSURE - [SDR ASMF201008002](https://openairdocs.org/sdr/ASMF201008002), Aug 24, 2010: PRESSURE SENSOR. DAMAGED. ACFT RETURNED OF FLIGHT DUE TO DURING CLIMB, EICAS MESSAGE AND LIGHT TURNED ON OF ENG OIL FILTER L WAS SHOWN. THE FLIGHT CREW PERFORMED THE QRH ENG OIL FILTER L - [SDR ASMF20100405](https://openairdocs.org/sdr/ASMF20100405), Apr 28, 2010: COMPRESSOR. DAMAGED. DURING A BORESCOPE INSP OF THE HPC AND HPT MODULES OF RT ENGINE WERE DETECTED 41 BLADES OF HPC 8TH STAGE AND 23 BLADES OF 9TH STAGE WITH TEARS, NICKS, BENDS AND - [SDR ASM2008F00000](https://openairdocs.org/sdr/ASM2008F00000), Aug 6, 2008: WARNING SYSTEM. MALFUNCTIONED. ACFT REJECTED TAKEOFF AT 80 KNOTS DUE TO THE E/E COMPARTMENT LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED DOOR LIGHT TEST IAW MM 62-71-00, ALL CORRECT. THE - [SDR ASMF200801003](https://openairdocs.org/sdr/ASMF200801003), Jan 23, 2008: SLAT. DAMAGED. DURING TAXING, AC HIT WITH LT SLAT NR 1 ON THE LT WING OF THE AIRCRAFT REGISTRATION N774AM. DETAILED INSPECTION WAS PERFORMED ON LT WING TIP DETECTING A STRUCTU - [SDR ASMF200711004](https://openairdocs.org/sdr/ASMF200711004), Nov 25, 2007: ENGINE. DAMAGED. CAPTAIN REPORTED THAT AT 39,000 FEET, LEFT ENGINE STALLED, DESCENDING TO 27,000 FEET WITH OSCILLATIONS IN N1 AND N2 WITH ENG CONTROL L AND ENG EEC C1 L MESSAGES - [SDR ASMF200710005](https://openairdocs.org/sdr/ASMF200710005), Oct 19, 2007: ENGINE. OVERTEMP. CAPTAIN REPORTED THAT DURING TAKEOFF RUN THE LT ENGINE EGTS INDICATION EXCEEDED RED DIAL; CAPTAIN REDUCED THE THRUST RECOVERING NORMAL INDICATIONS. AT CDG, MAIN ## Other aircraft with N746AM - [Registered now](https://openairdocs.org/aircraft/N746AM): Amazon.Com Services MK30, S/N 178650109E --- 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.