# N745AM: 2006 Boeing 777-2Q8, registration cancelled 2018-04-06 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 6, 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: 32718 - Year built: 2006 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 21, 2006 - Certificate issued: February 28, 2013 - Last registry action: October 30, 2015 - Mode S code: AA0529 - 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/N745AM - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=745AM - Page: https://openairdocs.org/deregistered/N745AM-2018-04-06 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 (20) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASMF20170531005](https://openairdocs.org/sdr/ASMF20170531005), May 27, 2017: MONITOR. DAMAGED. AIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAKE OFF, CONFIGURATION STABILIZER ALARM WAS ACTIVED. MAINTENANCE PERSONNEL PERFORMED INSPECTION IAW FIM 31-43 TASK - [SDR ASMF201705002](https://openairdocs.org/sdr/ASMF201705002), May 16, 2017: PUMP. FAILED. CAPTAIN REPORTED THAT DURING CRUISE, THE FUEL QUANTITY INDICATION WAS WRONG, FUEL QUANTITY WAS VERIFIED USING FUEL DIPSTICK. OPS TESTED FOR THE SYSTEM FUEL QUAN - [SDR ASMF201602007](https://openairdocs.org/sdr/ASMF201602007), Jan 24, 2016: HYDRAULIC LINE. LEAKING. CAPTAIN REPORTED THAT DURING APPROACH, THE HYD CENTRAL SYS QTY DECREASED TO 0.14 GAL & THE MSG IN EICAS & STATUS OF AUTO BRAKE SOL VLV WAS SHOWN. PERFORMED ACFT - [SDR ASMF201503012](https://openairdocs.org/sdr/ASMF201503012), Feb 6, 2015: VALVE. LOOSE. DURING TRANSIT CHECK, IT WAS DETECTED A HYD LEAK IN THE WHEEL NR 4. DURING MX REVISION, THE WHEEL NR 4 WAS DETECTED LEAKING WITHIN LIMITS. THE BRAKES BLEED PORT - [SDR ASMF201407008](https://openairdocs.org/sdr/ASMF201407008), Jul 1, 2014: BRACKET. BROKEN. AIRCRAFT PERFORMED AN UNSCHEDULED LANDING DUE TO URGENT ATTENTION OF A SICK PAX. PERFORMED AN OVERWEIGHT LANDING INSPECTION IAW MM 05-51-35 PHASE 1, DETECTING A - [SDR ASMF2014061706010](https://openairdocs.org/sdr/ASMF2014061706010), Apr 27, 2014: SLIDE RAFT. OUT OF POSITION. DURING TRANSIT CHECK, THE LT DOOR SLIDE RAFT NR 2 WAS FOUND OUT OF POSITION ON THE ACFT FLOOR & WITH METAL SEAMS LOOSEN. ACFT WAS SENT TO THE HANGAR & SENT THE - [SDR ASMF201308008](https://openairdocs.org/sdr/ASMF201308008), Jul 12, 2013: FAIRING. DAMAGED. DURING TRANSIT CHECK, A BIRD STRIKE WAS DETECTED IN RT ENGINE. BIRD STRIKE CONDITIONAL INSPECTION WAS PERFORMED IAW MM 05-51-18, DETECTING 6 FAIRING DAMAGES AND - [SDR ASMF201211007](https://openairdocs.org/sdr/ASMF201211007), Nov 18, 2012: PROBE. MALFUNCTIONED. ACFT RETURNED TO PLATFORM DUE TO AFTER RT ENGINE START, IT WAS HAD OSCILLATIONS BETWEEN 540 AND 580 CELSIUS DEGREES OF EGT. ACFT WAS SENT TO THE HANGAR AND MX P - [SDR ASMF201106001](https://openairdocs.org/sdr/ASMF201106001), Jun 1, 2011: SENSOR. DAMAGED. AIRCRAFT RETURNED DURING CLIMB, THE EICAS MESSAGE LT PACK WAS SHOWN AND IT WAS NOT AIR ON LT DUCT. DURING MX REVISION, THE MESSAGES 21-23041 WAS SHOWN, THE FIM - [SDR ASMF201010007](https://openairdocs.org/sdr/ASMF201010007), Oct 20, 2010: SENSOR. DAMAGED. ACFT PERFORMED AN UNSCHEDULED LANDING, DUE TO DURING CLIMB THE ENG OIL FILTER SENSOR AND ENG OIL FILTER LIGHTS TURNED ON AND DURING CRUISE THE EICAS MESSAGE ENG - [SDR ASMF201008001](https://openairdocs.org/sdr/ASMF201008001), Aug 19, 2010: TIRE. DETACHED. DURING TAKEOFF RUN; A STRONG NOISE WAS HEARD, IECAS MESSAGE OF TIRE PRESS WAS SHOWN AND TIRE PRESS LIGHT TURNED ON, THE TIRE NR 1 WAS DEFLATED AND THE FLIGHT CO - [SDR ASMF201004002](https://openairdocs.org/sdr/ASMF201004002), Mar 21, 2010: BLADES. DAMAGED. DURING A BOROSCOPIC INSP OF THE HPC 1ST STAGE BLADES, VSV AND IGV SYSTEMS OF LT ENGINE WAS DETECTED THE HPC 1ST STAGE WITH A TIP CURLED BROKEN, CAUSING DAMAGES - [SDR ASMF20100321001](https://openairdocs.org/sdr/ASMF20100321001), Mar 21, 2010: BLADE. DAMAGED. DURING A BOROSCOPIC INSP OF THE HPC 1ST STAGE BLADES, VSV AND IGV SYSTEMS OF LT ENG WAS DETECTED THE HPC 1ST STAGE WITH A TIP CURLED BROKEN, CAUSING DAMAGES IN - [SDR ASMF200911001](https://openairdocs.org/sdr/ASMF200911001), Nov 11, 2009: BRAKE ASSY. LEAKING. DURING TRANSIT CHECK, A HYD LEAK WAS DETECTED ON THE RT MLG BRAKE NR 8. MX REPLACED THE BRAKE ASSY NR 8 IAW MM 32-45-07, TESTED CORRECT. - [SDR MAS2008F00062](https://openairdocs.org/sdr/MAS2008F00062), Aug 21, 2008: THRUST REVERSER. DAMAGED. DURING TRANSIT CHECK WAS DETECTED THE OUTBOARD REVERSER OF THE RT ENGINE WITH EXTENDED DAMAGE ON FAN DUCT INNER WALL WITH MATERIAL MISSING OF 70 X 60 INCH BY IM - [SDR 2008FA0000472](https://openairdocs.org/sdr/2008FA0000472), Jun 6, 2008: ENGINE. FAILED. DURING TRANSIT CHECK, THE RT ENGINE WAS DETECTED WITH DAMAGES. MAINT PERFORMED BOROSCOPIC INSPECTION, DETECTING DAMAGES OUT OF LIMITS, SO RT ENGINE WAS REPLACED - [SDR 2008FA0000471](https://openairdocs.org/sdr/2008FA0000471), Jun 1, 2008: SENSOR. FAILED. AC RETURNED TO DEPARTURE DUT TO RT ENGINE STALLED. MAINT PERFORMED FIM 75-21 TASK 822 AND STALL INSPECTION IN 1ST, 5TH AND 9TH HPC STAGES. NO DAMAGES WERE DETEC - [SDR ASMF200806001](https://openairdocs.org/sdr/ASMF200806001), Jun 1, 2008: SENSOR. FAILED. AIRCRAFT RETURNED OF FLIGHT DUE TO RIGHT ENGINE STALLED. MAINTENANCE PERSONNEL PERFORMED FIM 75-21 TASK 822 AND STALL INSPECTION IN 1ST, 5TH AND 9TH HPC STAGES, - [SDR ASMF200710004](https://openairdocs.org/sdr/ASMF200710004), Oct 18, 2007: ENGINE. OVERTEMP. AIRCRAFT REJECTED TAKEOFF AT 101 KNOTS DUE TO HIGH TEMPERATURE INDICATION ON THE LT ENGINE, REACHING 1035 CELSIUS DEGREES MOMENTARY AND 1015 DURING 11 SECONDS. - [SDR ASMF200607003](https://openairdocs.org/sdr/ASMF200607003), Jul 2, 2006: SCUFF PLATE. GROUND DAMAGE. DURING TRANSIT CHECK, AIRCRAFT WAS HIT BY A BAGGAGE CONVEYOR PROMOTING A DENT OF 3 INCHES LONG, 1 INCH WIDE AND .2500 INCH DEPTH IN THE SCUFF PLATE OF THE ACCES ## Other aircraft with N745AM - [Registered now](https://openairdocs.org/aircraft/N745AM): Cirrus Design SR22T, S/N 11597, 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.