# N804AM: 1994 Boeing 757-2Q8, registration cancelled 2006-03-27 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 27, 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: 26271 - Year built: 1994 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 7, 1994 - Certificate issued: August 12, 2003 - Last registry action: August 12, 2003 - Mode S code: AAF0C5 - Owner when cancelled: [Castle 2003-1a LLC](https://openairdocs.org/faa-owner/CASTLE%202003-1A%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/N804AM - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=804AM - Page: https://openairdocs.org/deregistered/N804AM-2006-03-27 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 (15) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASMF200601006](https://openairdocs.org/sdr/ASMF200601006), Jan 12, 2006: O-RING. LEAKING. DURING OVERNIGHT CHECK, THE RIGHT ENGINE WAS REPLACED FOR MAINTENANCE CONVENIENCE AND DURING TESTS WAS DETECTED FUEL LEAK AT FLOW TRANSMITTER. THE TRANSMITTER O - [SDR ASMF200510011](https://openairdocs.org/sdr/ASMF200510011), Oct 16, 2005: START VALVE. MALFUNCTIONED. AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING LEFT ENGINE START, THE STARTER VALVE LIGHT TURNED ON AND EICAS MESSAGES, L ENG STARTED. DISPLAYED WITH - [SDR ASMF200510003](https://openairdocs.org/sdr/ASMF200510003), Oct 3, 2005: BLADE. DAMAGED. DURING TRANSIT CHECK, DETECTED A BLADE DAMAGED, LT ENGINE LPC 1ST STAGE. THE BLADE WAS OUT OF LIMITS WITH A DAMAGE OF 4 X 0.750 AT LEADING EDGE. DURING OVERNIGH - [SDR ASMF200510002](https://openairdocs.org/sdr/ASMF200510002), Oct 3, 2005: IDG. FAILED. AIRCRAFT RETURNED TO PLATFORM DURING TAXING. THE LT GENERATOR SHUTDOWN AND EICAS MESSAGES (RUDDER PCU, R ELEV PCU, L ELEV PCU, EQPT CLG TEST) WERE SHOWN. THE LT - [SDR ASMF200509013](https://openairdocs.org/sdr/ASMF200509013), Sep 22, 2005: VALVE. MALFUNCTIONED. AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING ENGINES START, APU SHUT DOWN, FAULT LIGHT TURNED ON AND EICAS MESSAGE APU FAULT WAS DISPLAYED. THE FIM - [SDR ASMF200509001](https://openairdocs.org/sdr/ASMF200509001), Sep 1, 2005: ACM. FAILED. AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING PUSHBACK, THE AIR CONDITION PACKAGE FAILED WITH EICAS MESSAGES OF RIGHT ENGINE PURGE VALVE DID NOT OPER - [SDR ASMF200507016](https://openairdocs.org/sdr/ASMF200507016), Jul 21, 2005: ELEVATOR. OUT OF RIG. CAPTAIN REPORTED THAT THE MESSAGE -ELEV ASYM- WAS SHOWN IN EICAS. THE FIM 27-09-00 FIG. 106 PROCEDURE WAS PERFORMED AND DURING CONTROLS TESTS REPEATED THE MESSA - [SDR ASMF200506021](https://openairdocs.org/sdr/ASMF200506021), Jun 19, 2005: STARTER. FAILED. ACFT RETURNED TO PLATFORM. DURING RT ENGINE STARTING, N2 INDICATION REACHED 23 PERCENT AND WENT TO ZERO. PNEUMATIC STARTER AND PNEUMATIC STARTER VALVE REPLACED - [SDR ASMF200501015](https://openairdocs.org/sdr/ASMF200501015), Jan 19, 2005: VALVE. FAILED. DURING TRANSIT CHECK WAS DETECTED A HYDRAULIC LEAK IN THE LEFT ENGINE FILTERS MODULE TUBE, TUBE WAS TIGHTENED AND ENGINE WAS MOTORIZED, BUT DURING THE PROCESS A - [SDR ASMF200412009](https://openairdocs.org/sdr/ASMF200412009), Dec 22, 2004: PUMP. DAMAGED. CAPT REPORTED LT HYD SYSTEM LOST, LT HYD QTY AT EICAS FAULT CODE 291106-01, LT HYD ELECTRIC PUMP FAULT CODE 291133-01, PTU FAULT CODE 292201-00 AND RT ELECTRIC - [SDR ASMF200404024](https://openairdocs.org/sdr/ASMF200404024), Apr 29, 2004: TUBE. DAMAGED. DURING TRANSIT CHECK AN HYDRAULIC LEAK WAS DETECTED ON LT ENGINE. DURING MAINTENANCE REVISION AN HYDRAULIC TUBE (P/N 316N3100-28) WAS DETECTED WITH DAMAGE. PROV - [SDR MEX2003405](https://openairdocs.org/sdr/MEX2003405), Aug 31, 2003: WARNING LIGHT. ILLUMINATED. AIRCRAFT ARRIVED WITH CAPTAIN REPORT OF EICAS MESSAGE FLAP-SLAT ELEC. ONCE WE HAVE ADDITIONAL INFORMATION WE WILL SEND YOU AS SUPPLEMENT TO THIS REPORT.(K) - [SDR MEX2003408](https://openairdocs.org/sdr/MEX2003408), Aug 31, 2003: WIRE. LOOSE. AIRCRAFT ARRIVED WITH CAPTAIN REPORT OF (WARN ELEX/ SLAT FLAP ELEC STATUS) MESSAGE IN EICAS. DURING REVISION WAS DETECTED BCPU POPPED DUE TO LOOSE OF WIRE NUMBE - [SDR MEX2003237](https://openairdocs.org/sdr/MEX2003237), Jun 18, 2003: INDICATOR. FAILED. AIRCRAFT RETURN TO PLATFORM DUE TO TCAS NR 1 BLOCKED WITH INDICATION IN DISPLAY. THE INDICATOR VSI/TRA DISPLAY WAS REPLACED IAW 34-22-06, ALL TEST CORRECT. - [SDR MEX2002300](https://openairdocs.org/sdr/MEX2002300), Sep 17, 2002: WARNING SYSTEM. FALSE ACTIVATION. AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF THE LIGHT (OIL FILTER CLOGGING) TURNED ON DURING LT ENGINE STARTING. TECH PERFORMED AN ERASER PROCEDURE AND THE ## Other aircraft with N804AM - [Registered now](https://openairdocs.org/aircraft/N804AM): Boeing 737-9, S/N 68151, built 2025 - [Cancelled 2020-03-13](https://openairdocs.org/deregistered/N804AM-2020-03-13): Early Aeroplane Manufactory LL BEAVER RX 550 PLUS, S/N 4000AM, built 2016. Sale reported, canceled. Owner: [Sugar Land, TX](https://openairdocs.org/faa-place/TX/Sugar%20Land) --- 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.