# N805AM: Boeing 757-2Q8, registration cancelled 2012-07-31 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 31, 2012 - Status when cancelled: N-number assigned, not yet registered - 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: 26272 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Experimental, showing compliance - Airworthiness date: April 27, 2004 - Last registry action: July 31, 2012 - Mode S code: AAF47C - The mark today: https://openairdocs.org/aircraft/N805AM - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=805AM - Page: https://openairdocs.org/deregistered/N805AM-2012-07-31 From the FAA registry file of October 28, 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 (21) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASMF200707009](https://openairdocs.org/sdr/ASMF200707009), Jul 13, 2007: LANDING GEAR. INOPERATIVE. AIRCRAFT RETURNED, NOSE LANDING GEAR DID NOT RETRACT. DURING CHECK, TECH DETECTED THE LOCK PIN OF THE NOSE LANDING GEAR INSTALLED, SO IT WAS REMOVED AND AIRCRAF - [SDR ASMF200703004](https://openairdocs.org/sdr/ASMF200703004), Mar 12, 2007: IDG. LEAKING. AIRCRAFT REJECTED TAKEOFF AT 80 KNOTS DUE TO (L GEN) LIGHT TURNED ON IN EICAS. DURING MAINTENANCE CHECK, THE LT IDG WAS DETECTED WITH LOW OIL LEVEL. FAILURE WAS - [SDR ASM200608020](https://openairdocs.org/sdr/ASM200608020), Aug 27, 2006: ACTUATOR. LEAKING. DURING OVERNIGHT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE RIGHT RUDDER ACTUATOR. RUDDER ACTUATOR WAS REPLACED IAW MM 27-21-20, TESTED CORRECT. - [SDR ASMF200607017](https://openairdocs.org/sdr/ASMF200607017), Jul 23, 2006: PDU. MALFUNCTIONED. CAPTAIN REPORTED THAT DURING APPROACH THE LT FLAP/SLAT SYSTEM DID NOT OPERATE HYDRAULICALLY IN NORMAL MODE PROCEEDING TO THE ALTERNATE MODE AND FLAPS DISAGREE M - [SDR ASMF200512015](https://openairdocs.org/sdr/ASMF200512015), Dec 16, 2005: IRU. FAILED. DURING TRANSIT CHECK, THE LT RDMI SHOWED HDG AND VOR FLAGS. THE SENSORS WERE CHECKED IN FMC SHOWING THAT THE THREE INERTIAL UNITS WERE CORRECT; THE LT AND CENTR - [SDR ASMF200511009](https://openairdocs.org/sdr/ASMF200511009), Nov 23, 2005: STARTER. DAMAGED. DURING LT ENGINE STARTING, THE PNEUMATIC STARTER FAILED. DURING MAINTENANCE REVISION WAS DETECTED THE PNEUMATIC STARTER WITH DAMAGE, SO IT WAS REPLACED IAW MM 8 - [SDR ASMF200506013](https://openairdocs.org/sdr/ASMF200506013), Jun 10, 2005: IDG. FAILED. AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING THE LEFT ENGINE STARTED, THE N2 REACHED 30 PERCENT AND IT DID NOT INCREASE. THE LEFT ENGINE WAS STARTED - [SDR ASMF200506003](https://openairdocs.org/sdr/ASMF200506003), Jun 2, 2005: IDG. FAILED. AIRCRAFT RETURNED, LT GENERATOR FAILURE, APU DID NOT START AT 35 000 FT, 24 22 25 EICAS MESSAGES, 01 GEN OFF DISPLAYED AND 01 AS BUSS OFF REMAINED ILLUMINATED. - [SDR ASMF200505027](https://openairdocs.org/sdr/ASMF200505027), May 24, 2005: ENGINE. FAILED. CAPTAIN REPORTED THAT DURING DESCENT AT 18500 FEET, THE LEFT ENGINE OIL FILTER LIGHT CAME ON. THE ABNORMAL PROCEDURE 05-14 WAS PERFORMED AND THE A/T ARMED SWITC - [SDR ASMF200409004](https://openairdocs.org/sdr/ASMF200409004), Sep 11, 2004: HEAT EXCHANGER. LEAKING. DURING TRANSIT CHECK, A LEAK WAS DETECTED ON OIL TANK TUBE SCUPPER AND FUEL/OIL HEAT EXCHANGER. LT ENGINE WAS STARTED AND LEAK INCREASED. FUEL/OIL HEAT EXCHANGE - [SDR ASMF200405027](https://openairdocs.org/sdr/ASMF200405027), May 28, 2004: VALVE. FAILED. AIRCRAFT RETURNED TO PLATFORM, LT ENGINE WAS SHUTDOWN AND (FUEL CONT) AND (SPAR VALVE) LIGHTS TURNED ON. STATUS DISPLAY MESSAGES, APU PERFORMANCE AND ABNORMAL S - [SDR MEX2004019](https://openairdocs.org/sdr/MEX2004019), Jan 15, 2004: THRUST REVERSER. FAILED. DURING TRANSIT REVISION, THE LT REVERSER WAS OPEN AND LIGHT AND MESSAGE WAS IN DISPLAY. THE REVERSER WAS REVISED AND ICE AND SNOW WAS DETECTED INTO THE REVERSE. - [SDR MEX2003560](https://openairdocs.org/sdr/MEX2003560), Dec 23, 2003: INDICATOR. LEAKING. FLT 494 - MEX-LAX - AIRCRAFT PERFORMED AN UNSCHEDULED LANDING IN GDL AS CONSEQUENCE OF THE RIGHT QUANTITY INDICATION DECREASE TO .08 QUARTS. AT PLATFORM, THE HY - [SDR MEX2003534](https://openairdocs.org/sdr/MEX2003534), Nov 25, 2003: PITOT TUBE. DAMAGED. AIRCRAFT RETURNED TO GATE DUE TO (R AUX PITOT) LIGHT WAS TURNED ON AND THE CABIN TEMPERATURE CONTROL HAD A FAILURE, TEMP REACHED 37 DEGREES CELSIUS. AIRCRAFT WA - [SDR MEX2003273](https://openairdocs.org/sdr/MEX2003273), Jul 7, 2003: ANTENNA. FAILED. AIRCRAFT ARRIVED WITH CAPTAIN REPORT RADAR OUT OF SERVICE. DURING REVISION WAS DETECTED WAVE GUIDE WITH DAMAGE. AIRCRAFT WAS SENT TO THE HANGAR, AND THE WAVE GU - [SDR MEX2003150](https://openairdocs.org/sdr/MEX2003150), May 1, 2003: CONTROL UNIT. FAILED. DURING TRANSIT CHECK CAPTAIN REPORTED NORM ANTI-SKID AND ALTN ANTI-SKID MESSAGES IN EICAS. MESSAGE APPEARED EVERY TIME THAT THE PARKING BRAKES WERE USED. FIM PR - [SDR MEX2003016](https://openairdocs.org/sdr/MEX2003016), Jan 29, 2003: WARNING SYSTEM. MALFUNCTIONED. FLT 600 - MEX-ALT - AIRCRAFT RETURNED TO PLATFORM, DURING ENGINES STARTING, MESSAGE EICAS STATUS MAIN BATTERY CHARGE. RESET PROCEDURE WAS PERFORMED AND MESSAGES - [SDR MEX2002346](https://openairdocs.org/sdr/MEX2002346), Nov 21, 2002: INDICATOR. MALFUNCTIONED. FLT 171 - JIJ- DURING TAKEOFF EPR INDICATIONS WAS BLANK RIGHT ENGINE AND N1 WITH FLUCTUATIONS AT REDUCE POWER ON RIGHT ENGINE AFTER 5 MINUTES INDICATIONS WAS NO - [SDR MEX2002297](https://openairdocs.org/sdr/MEX2002297), Sep 13, 2002: HYDRAULIC LINE. LEAKING. FLT 405 - JFK - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF AN HYDRAULIC LEAKAGE IN THE RIGHT SYSTEM. TECHNICIAN REVIEWED SUCH SYSTEM AND FOUND LEAKAGE IN A - [SDR MEX2002145](https://openairdocs.org/sdr/MEX2002145), Sep 5, 2002: WARNING SYSTEM. ACTIVATED. FLT 902 - MEX-MTY - AIRCRAFT RETURN TO GATE DUE TO CENTRAL AND LEFT HYDRAULIC SYSTEM RSVR LIGHT CAME ON. SUPPLY LINES AND DEPRESSURIZATION VALVES WERE CHECKED N - [SDR MEX2002187](https://openairdocs.org/sdr/MEX2002187), Jun 12, 2002: SLIDE. OUT OF ADJUST. FLT 170 - MEX-TIJ - CAPTAIN REPORTED THAT THE DOOR NR 1 SLIDE WAS NOT ARMED. DURING CHECK WAS DETECTED THAT THE ARMED LIGHT WAS INOPERATIVE AND THE ACTIVATION M ## Other aircraft with N805AM - [Registered now](https://openairdocs.org/aircraft/N805AM): Piper PA-28-181, S/N 28020036, built 2021 --- 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.