# N803AM: 1994 Boeing 757-2Q8, registration cancelled 2006-11-14 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 14, 2006 - Exported to: Turkey - Status when cancelled: Valid registration - Airframe: [Boeing 757-2Q8](https://openairdocs.org/model/boeing-757-2q8) (registry code 1384972) - Engine: [Pratt & Whitney PW2037](https://openairdocs.org/engine/pratt-whitney-pw2037) (registry code 52117) - Data sheets: [TCDS E17NE](https://openairdocs.org/tcds/E17NE) (OpenAirDocs) - Serial number: 26268 - Year built: 1994 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 9, 1994 - Certificate issued: December 29, 2003 - Last registry action: December 29, 2003 - Mode S code: AAED0E - Owner when cancelled: [Castle 2003-2a LLC](https://openairdocs.org/faa-owner/CASTLE%202003-2A%20LLC) - 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/N803AM - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=803AM - Page: https://openairdocs.org/deregistered/N803AM-2006-11-14 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 757-2Q8: https://openairdocs.org/model/boeing-757-2q8.md ## Service difficulty reports (18) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASMF200607008](https://openairdocs.org/sdr/ASMF200607008), Jul 10, 2006: SLIDE. INCORRECT. AIRCRAFT RETURNED TO PLATFORM, RT DOOR NR 1 SLIDE WAS NOT ARMED CORRECTLY. SLIDE WAS ARMED IAW MM 25-66-01 AND DOOR WAS VERIFIED BY CONDITION, BEING ALL CORRECT - [SDR ASMF200606017](https://openairdocs.org/sdr/ASMF200606017), Jun 28, 2006: ENGINE. FAILED. AIRCRAFT RETURNED TO PLATFORM, (L ENG REV CONT) AND (L ENG PRI CONT) MESSAGES WERE SHOWN IN EICAS. FIM 78-34-00, FIGURE 112 PROCEDURE WAS PERFORMED AND LT ENGIN - [SDR ASMF200606008](https://openairdocs.org/sdr/ASMF200606008), Jun 12, 2006: ENGINE. LEAKING. ON ARRIVAL, CAPTAIN REPORTED AIRCRAFT FLEW WITH REDUCED THRUST 1.5 HRS DUE TO LOW OIL QUANTITY INDICATION (3QTS) IN LT ENG. MX DETECTED AN OIL LEAK THRU OIL PRE - [SDR ASMF200604008](https://openairdocs.org/sdr/ASMF200604008), Apr 16, 2006: WHEEL. DAMAGED. AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING TAXIING SPOILERS LIGHT AND EICAS MESSAGE WERE SHOWN. BITE TO SPOILERS MODULE WAS PERFORMED CONTINUING T - [SDR ASMF200601004](https://openairdocs.org/sdr/ASMF200601004), Jan 10, 2006: IDG. FAILED. DURING TRANSIT CHECK, CAPTAIN REPORTED THAT APU OIL LIGHT TURNED ON. THE APU REPORT WAS DEFERRED IAW MEL 49-11-1 CAT C AND AIRCRAFT WAS DISPATCHED. LATER, AIRCR - [SDR ASMF200502005](https://openairdocs.org/sdr/ASMF200502005), Feb 5, 2005: CONTROL MODULE. FAILED. AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF AFTER ENGINES STARTED, EICAS MESSAGES STAB TRIM" WAS SHOWN. REPORT WAS DEFERRED IAW MEL 27-41-2. DURING TRANSI - [SDR ASMF200502002](https://openairdocs.org/sdr/ASMF200502002), Feb 5, 2005: CONTROL MODULE. FAILED. AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF AFTER ENGINES STARTED, EICAS MESSAGES "STAB TRIM" WAS SHOWN. REPORT WAS DEFERRED IAW MEL 27-41-2. DURING TRANS - [SDR ASMF200501014](https://openairdocs.org/sdr/ASMF200501014), Jan 23, 2005: A/C PACK. INOPERATIVE. AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF LT AIR CONDITIONING PACK WAS OUT OF SERVICE. AT PLATFORM, BOTH AIR CONDITIONING SYSTEMS WERE CHECKED BEING COR - [SDR ASMF200411004](https://openairdocs.org/sdr/ASMF200411004), Nov 5, 2004: BLADE. NICKED. DURING OVERNIGHT SERVICE, BOROSCOPE INSPECTION WAS PERFORMED ON RIGHT ENGINE AND NICKS WERE DETECTED ON ONE BLADE OF 11TH STAGE, OUT OF LIMITS IAW MM 72-00-00. - [SDR ASMF200407015](https://openairdocs.org/sdr/ASMF200407015), Jul 11, 2004: BLEED VALVE. FAILED. CAPTAIN REPORTED WHEN STARTING CLIMB FROM FL350 TO FL390 THE RT ENGINE EPR'S INDICATION FLUCTUATE SEVERALLY AND ENGINE PANCAKING AND NOT CLIMBING. AIRCRAFT WAS - [SDR ASMF200405010](https://openairdocs.org/sdr/ASMF200405010), May 6, 2004: PROXIMITY SENSOR. DAMAGED. DURING TRANSIT CHECK, (LANDING GEAR) AND (MAINTENANCE GEAR DOOR) LIGHTS TURNED ON. DURING MAINTENANCE REVISION, PSEU WAS DETECTED WITH DAMAGE ON SENSOR 076. PRO - [SDR MEX2003539](https://openairdocs.org/sdr/MEX2003539), Nov 28, 2003: PUMP. FAILED. AIRCRAFT RETURNED TO GATE DUE TO LOW OIL PRESSURE INDICATION ON NR 2 ENGINE DURING STARTING. SYSTEM WAS VERIFIED AND THE OIL PUMP WAS REPLACED IAW MM 79-21-04, - [SDR MEX2003387](https://openairdocs.org/sdr/MEX2003387), Aug 23, 2003: SHUTOFF VALVE. MALFUNCTIONED. DURING PUSH BACK AND LEFT ENGINE STARTING, ENGINE VALVE LIGHTS TURNED ON, SPAR VALVE DID NOT GO OFF AND N2 WAS BETWEEN 25 PERCENT AND 30 PERCENT WITHOUT EGT INC - [SDR MEX2003236](https://openairdocs.org/sdr/MEX2003236), Jun 18, 2003: PACKING. FAILED. AIRCRAFT ARRIVED WITH CAPTAIN REPORT WITH 1 QUART OF OIL IN ENGINE NR 2. DURING REVISION WAS DETECTED LEAK IN RIGHT HYDRAULIC PUMP. THE RIGHT HYDRAULIC PUMP PAC - [SDR MEX2002299](https://openairdocs.org/sdr/MEX2002299), Sep 16, 2002: FUEL CONTROL. FAILED. FLT 600 - MEX-ATL - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF AN STARTING FAILED OF THE RIGHT ENGINE. AT POSITION 24, TECHNICIANS TRIED STARTING AGAIN AND - [SDR ASM2002F00002](https://openairdocs.org/sdr/ASM2002F00002), May 18, 2002: ACTUATOR. FAILED. DURING INSPECTION, DETECTED A LEAK IN THE RIGHT FUEL TANK. THE LEAK WAS AT THE RIGHT SHUTOFF VALVE. RIGHT TANK WAS SEALED. DURING OVERNIGHT SERVICE THE O-RINGS - [SDR MEX2002105](https://openairdocs.org/sdr/MEX2002105), Apr 10, 2002: PROBE. FAILED. FLT 404 - MEX-JFK - AIRCRAFT WAS SENT TO THE HANGAR FOR HIGH EGT ON NR 2 ENGINE (930 GRADES). PERFORMED A FIM PROCEDURE DETECTED THE PROBES T/C 2 T/C 6 OUT OF L - [SDR MEX2002015](https://openairdocs.org/sdr/MEX2002015), Jan 18, 2002: WIRE HARNESS. DAMAGED. FLT 239 - GDL-MEX - CREW REPORTED THAT DURING THE ENGINE STARTING, THE ENGINE 1 WAS NOT STABILIZED, THE RPM'S REMAINED AT 42 PERCENT AND MAINTENANCE AREA REPORT ## Other aircraft with N803AM - [Cancelled 2019-12-02](https://openairdocs.org/deregistered/N803AM-2019-12-02): DJI PHANTOM 3 PROFESSION, S/N P76DCD26012518. Registration expired, pending cancellation. Owner: [Cinch Stephen E](https://openairdocs.org/faa-owner/CINCH%20STEPHEN%20E), [Clevland Heights, OH](https://openairdocs.org/faa-place/OH/Clevland%20Heights) --- 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.