# N451AT: Aerospatiale ATR 72-212, registration cancelled 2013-09-26 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 26, 2013 - Status when cancelled: Valid registration - Airframe: [Aerospatiale ATR 72-212](https://openairdocs.org/model/aerospatiale-atr-72-212) (registry code 8680945) - Engine: [Pratt & Whitney 127](https://openairdocs.org/engine/pratt-whitney-127) (registry code 52132) - Data sheets: [TCDS A53EU](https://openairdocs.org/tcds/A53EU) (OpenAirDocs) - Serial number: 451 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: May 19, 1995 - Certificate issued: December 12, 2008 - Last registry action: January 30, 2013 - Mode S code: A575E5 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.8659° N, 112.0391° W: Placed by OpenAirDocs at the center of ZIP code 84116, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N451AT - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=451AT - Page: https://openairdocs.org/deregistered/N451AT-2013-09-26 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 Aerospatiale ATR 72-212: https://openairdocs.org/model/aerospatiale-atr-72-212.md ## Service difficulty reports (64, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR TRBA20121129001](https://openairdocs.org/sdr/TRBA20121129001), Nov 29, 2012: POWER SUPPLY. INOPERATIVE. DURING MX INSPECTION FOUND THE EMERGENCY FLOOR LIGHT, FORWARD SECTION INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R THE EMERGENCY LIGHT POWER SUPPLY IAW MM 33-5 - [SDR TRBA20121018001](https://openairdocs.org/sdr/TRBA20121018001), Oct 18, 2012: CHANNEL. CORRODED. DURING B INSPECTION, FOUND THE TAIL CONE INTERNAL LT HORIZONTAL GANG CHANNEL HAS EXFOLIATING CORROSION ABOUT 20" FROM TAIL CONE LENS ASSY. THE ACFT WAS REMOVED - [SDR TRBA20120924001](https://openairdocs.org/sdr/TRBA20120924001), Sep 24, 2012: BATTERY. DISCHARGED. DURING MX INSPECTION, FOUND THE AFT WALL FLASHLIGHT LOW BATTERY INDICATION ON LED RED LIGHT. ACFT REMOVED FROM SERVICE. R & R FLASHLIGHT BATTERY IAW MM 25-65-21 - [SDR TRBA20120919001](https://openairdocs.org/sdr/TRBA20120919001), Sep 19, 2012: COVER. LOOSE. CREW REPORTED THE EMERGENCY FLOOR LIGHTING IN GALLEY AREA WAS LOOSE & NEEDS A COVER. THE ACFT WAS REMOVED FROM SERVICE. REINSTALLED COVER AND RESECURED GALLEY A - [SDR TRBA20120825001](https://openairdocs.org/sdr/TRBA20120825001), Aug 25, 2012: POWER SUPPLY. INOPERATIVE. DURING MX INSPECTION, FOUND SEVERAL EMERGENCY LIGHTS IN THE CABIN FLOOR STRIP WILL NOT COME ON. THE ACFT WAS REMOVED FROM SERVICE. R & R THE RESPECTIVE EMERGENC - [SDR TRBA20120728001](https://openairdocs.org/sdr/TRBA20120728001), Jul 28, 2012: CAP. MISSING. DURING B INSPECTION, FOUND THE GALLEY AFT FLOOR EMERGENCY LIGHT MISSING END CAPS. THE ACFT WAS REMOVED FROM SERVICE. INSTALLED END CAPS IAW CMM 33-52-10. THE AC - [SDR TRBA20120709001](https://openairdocs.org/sdr/TRBA20120709001), Jul 9, 2012: PCU. UNSERVICEABLE. THE CREW REPORTED A LOUD CRACKING FROM CIRCUIT BRAKER PANEL BEHIND. FIRST OFFICER`S DC GENERATOR NR 1 FAULT LIGHT CLICKING ON AND OFF. CREATED MULTIPLE ELECTRIC - [SDR TRBA20120701001](https://openairdocs.org/sdr/TRBA20120701001), Jul 1, 2012: LIGHT. UNSECURE. DURING B INSPECTION, FOUND AFT EMERGENCY FLOOR LIGHT LOOSE AND MISSING END CAP IN GALLEY AREA. ACFT REMOVED FROM SERVICE. SECURED AFT EMERGENCY FLOOR LIGHT AND - [SDR TRBA20120616002](https://openairdocs.org/sdr/TRBA20120616002), Jun 16, 2012: CAP. MISSING. DURING B INSPECTION, FOUND THE FLOOR EMERGENCY LIGHT END CAP MISSING AT GALLEY AND SEAT 6/B. THE AIRCRAFT WAS REMOVED FROM SERVICE. C/A: INSTALLED FLOOR EMERGEN - [SDR TRBA20120616001](https://openairdocs.org/sdr/TRBA20120616001), Jun 16, 2012: LIGHT. LOOSE. DURING B INSPECTION, FOUND THE FLOOR EMERGENCY LIGHT STRIP LOOSE AT GALLEY. THE ACFT WAS REMOVED FROM SERVICE. SECURED EMERGENCY LIGHT STRIP AT GALLEY IAW JIC 2 - [SDR TRBA20120526001](https://openairdocs.org/sdr/TRBA20120526001), May 26, 2012: WIRE. BROKEN. THE CREW REPORTED THE EMERGENCY EXIT LIGHT IN THE PASSENGER ENTRY DOOR IS INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. REPAIRED BROKEN WIRE AT DOOR & OPS CHEC - [SDR TRBA20120428001](https://openairdocs.org/sdr/TRBA20120428001), Apr 28, 2012: CONNECTOR. DAMAGED. DURING B INSPECTION, FOUND THE GALLEY EMERGENCY LIGHTS INOPERATIVE. ACFT REMOVED FROM SERVICE. REPINNED CONNECTOR 163WL AND TESTED SYS IAW SPM20-44-11 & JIC 33- - [SDR TRBA20120317002](https://openairdocs.org/sdr/TRBA20120317002), Mar 17, 2012: POWER SUPPLY. FAILED. THE F/A REPORTED THE EMERGENCY LIGHTS STAYED ON DURING BATTERY SELECTION THROUGH ENTIRE FLIGHT ROW 14-17. THE ACFT WAS REMOVED FROM SERVICE. R & R THE POWER SUP - [SDR TRBA20120317001](https://openairdocs.org/sdr/TRBA20120317001), Mar 17, 2012: LIGHT. INOPERATIVE. DURING B-INSPECTION, FOUND THE GALLEY AREA EMERGENCY LIGHTS INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE GALLEY EMERGENCY LIGHTS IAW 33-50-00. OPS - [SDR TRBA201203137401](https://openairdocs.org/sdr/TRBA201203137401), Mar 13, 2012: POWER SUPPLY. INOPERATIVE. THE CREW REPORTED THAT SEVERAL EMERGENCY LIGHTS WERE OUT STARTING FROM MID CABIN TO AFT. THE ACFT WAS REMOVED FROM SERVICE. R & R 68WL POWER PACK IAW JIC 33-51- - [SDR TRBA2012054001](https://openairdocs.org/sdr/TRBA2012054001), Feb 22, 2012: LIGHT. LOOSE. DURING B-INSPECTION, FOUND THE FORWARD EMERGENCY LIGHT STRIP LOOSE AT GALLEY. THE ACFT WAS REMOVED FROM SERVICE. RESECURED THE FORWARD EMERGENCY LIGHT STRIP AT - [SDR TRBA2012020234001](https://openairdocs.org/sdr/TRBA2012020234001), Feb 2, 2012: BATTERY. INOPERATIVE. DURING MX BASE VISIT FOUND A DEAD EMERGENCY BATTERY. THE ACFT WAS REMOVED FROM SERVICE. R & R EMERGENCY BATTERY IAW EX-243185-RAI-10020-002. OPS CHECKED GOOD. T - [SDR TRBA2012031002](https://openairdocs.org/sdr/TRBA2012031002), Jan 30, 2012: LIGHT. UNSERVICEABLE. DURING MX INSP FOUND THE FWD FLOOR EMERGENCY LIGHT STRIP BROKEN AT GALLEY. THE ACFT WAS REMOVED FROM SERVICE. R & R FORWARD EMERGENCY LIGHT STRIP AT GALLEY IAW - [SDR TRBA2012023002](https://openairdocs.org/sdr/TRBA2012023002), Jan 20, 2012: CAP. MISSING. DURING MX BASE VISIT, FOUND THE END CAP MISSING IN GALLEY AREA FOR THE EMERGENCY LIGHT. ACFT REMOVED FROM SERVICE. INSTALLED END CAP IAW CMM 33-50-01. ACFT RETU - [SDR TRBA2011353006](https://openairdocs.org/sdr/TRBA2011353006), Dec 18, 2011: CAP. MISSING. DURING INSPECTION, FOUND THE EMERGENCY FLOOR LIGHT STRIP MISSING END CAP AT GALLEY AREA, AT SEAT 3B AND 6B. THE ACFT WAS REMOVED FROM SERVICE. INSTALLED EMERGEN - [SDR TRBA201129903](https://openairdocs.org/sdr/TRBA201129903), Oct 7, 2011: BRAKE. WEAK. F/O LT BRAKE VERY SOFT. LT BRAKE BLED IAW JIC 32-42-00, BLD 10010, OPS CHECK GOOD. - [SDR TRBA2011F00000](https://openairdocs.org/sdr/TRBA2011F00000), Oct 7, 2011: BRAKE. WEAK. ON FLIGHT 9830, ON TAXI, THE CREW REPORTED THE F/O LT BRAKE WAS VERY SOFT. THE ACFT WAS REMOVED FROM SERVICE. LT BRAKE BLED IAW JIC 32-42-00, BLD 10010. THE OPS - [SDR TRBA201126902](https://openairdocs.org/sdr/TRBA201126902), Sep 23, 2011: BATTERY. DISCHARGED. EMERGENCY BATTERY FULLY DISCHARGED. RAI EMERGENCY BATTERY IAW W/C EX-243185-RAI-10020-002. - [SDR TRBA201126601](https://openairdocs.org/sdr/TRBA201126601), Sep 22, 2011: LAMP. INOPERATIVE. EMERGENCY EVACUATION PATH LIGHT STRIP AT 4B IS INOP. RELAMPED EMERGENCY EVACUATION PATH LIGHT STRIP AT 4B IAW JIC 33-20-00. - [SDR TRBA201124501](https://openairdocs.org/sdr/TRBA201124501), Sep 1, 2011: BULB. BURNED OUT. F/A ADVISES EVACUATION PATH EMERGENCY LIGHTING HAS BURNED OUT BULB AT ROW 4. RELAMPED FLOOR EMERGENCY LIGHT. OPS CHECKED GOOD IAW JIC 33-50-00-OPT-10000. - [SDR TRBA2011086](https://openairdocs.org/sdr/TRBA2011086), Jun 28, 2011: MASTER CYLINDER. INOPERATIVE. THE F/O REPORTED THE LT BRAKE FELT SPONGY DURING LANDING. THE ACFT WAS REMOVED FROM SERVICE. R & R THE F/O MASTER CYLINDER IAW JIC 32-42-13. THE ACFT WAS RETURN - [SDR TRBA2011072](https://openairdocs.org/sdr/TRBA2011072), Jun 12, 2011: LIGHT. INOPERATIVE. DURING THE PREFLIGHT INSP, FOUND THE FLOOR LIGHTING IS OUT AT ROW 4. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED OPS CHECK ON THE EMERGENCY LIGHT STRIP IAW EX- - [SDR TRBA2011067](https://openairdocs.org/sdr/TRBA2011067), Jun 4, 2011: BRAKE SYS. INOPERATIVE. ON FLIGHT 4901, THE CREW REPORTED THE F/O LT BRAKE WAS INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED BRAKE LOW PRESSURE BLEEDING IAW JIC 32-42-00. TH - [SDR TRBA2011038](https://openairdocs.org/sdr/TRBA2011038), Apr 10, 2011: SOCKET. BURNED. BETWEEN ROWS 9 & 12 RT SIDE SMELLS LIKE SOMETHING IS BURNING. REPLACED SOCKET FIN NR 311LGB ON PASSENGER CEILING FLOURESCENT LIGHT IAW SPM 20-43-12. - [SDR TRBA2011033](https://openairdocs.org/sdr/TRBA2011033), Apr 2, 2011: SMOKE DETECTOR. FAILED. 10 MINS AFTER POWER UP, MASTER WARNING ON CAP. ELECTRICAL SMOKE. R & R AVIONIC SMOKE DETECTOR IAW JIC 26-15-21, OPS CK GOOD. - [SDR TRBA2010116](https://openairdocs.org/sdr/TRBA2010116), Oct 8, 2010: WARNING LIGHT. ILLUMINATED. UNSAFE LANDING GEAR ON THE LT MAIN GEAR ON BOTH PANEL. FOLLOW THE AOE MANUAL CHECK LIST AND RETURNED TO DEPARTURE. (DECLARED EMERGENCY) REMOVED WATER AND CLEANE - [SDR TRBA2010103](https://openairdocs.org/sdr/TRBA2010103), Aug 23, 2010: ENGINE. ODOR. AFTER PARKING THE ACFT AND SHUTTING DOWN THE NR 1 ENGINE A VERY STRONG PLASTIC BURNING ODOR ENTERED THE COCKPIT AND CABIN. INSPECTED CABIN & COCKPIT FOR PLASTIC - [SDR TRBA2009089](https://openairdocs.org/sdr/TRBA2009089), Sep 28, 2009: LIGHT. MALFUNCTIONED. FIRST 6 LIGHTS ON THE FLOOR EMERGENCY LIGHTS STAYS ON IN FLIGHT. PERFORMED OPS CHECK OF EMERGENCY LIGHTING SYS AND CANNOT DUPLICATE DISCREPANCY AT THIS TIME IAW - [SDR TRBACPCP20090006](https://openairdocs.org/sdr/TRBACPCP20090006), Mar 18, 2009: FLANGE. UNKNOWN. LAVATORY SERVICE DOOR CUT OUT AT FUSELAGE LINE 0451. REMOVED AND REPLACED DOUBLER FLANGE IAW SRM NR 51-25-01. - [SDR TRBACPCP20090008](https://openairdocs.org/sdr/TRBACPCP20090008), Mar 10, 2009: MOUNT. CORRODED. FOUND CORROSION ON LT WING AT NR 1 ENG UPPER AFT INBD ENGINE MOUNT. ACCOMPLISHED EO NR E2-57MR-308 LT WING FWD SPAR LWR SLAT EXTERNAL CORROSION REPAIR AT RIB 10 - [SDR TRBACPCP20090007](https://openairdocs.org/sdr/TRBACPCP20090007), Mar 10, 2009: SKIN. CORRODED. RT FUEL PUMP HAS CORROSION AROUND PUMP AREA. COMPLIED WITH EO NR E2-57MR-305 RT WING LWR SKIN PANEL EXTERNAL CORROSION AT FUEL PUMP CUT-OUT BETWEEN RIBS 4 - 5. - [SDR TRBA2009022](https://openairdocs.org/sdr/TRBA2009022), Feb 10, 2009: LIGHT. MALFUNCTIONED. EMERGENCY LIGHTING ILLUMINATES IN ARMED POSITION. TURNING THEM OFF THEN ARMING RESETS THE LIGHTS TEMPORARILY. PERFORMED AN OPERATIONAL TEST OF THE EMERGENCY LIG - [SDR TRBA2009021](https://openairdocs.org/sdr/TRBA2009021), Feb 9, 2009: BATTERY PACK. FAILED. FORWARD "HALF" OF THE EMERGENCY LIGHTS ARE ILLUMINATED WHILE THE SWITCH IS IN THE ARM POSITION. REMOVED AND INSTALLED ALL EMERGENCY LIGHT POWER SUPPLY BATTERIES - [SDR TRBA2009020](https://openairdocs.org/sdr/TRBA2009020), Feb 8, 2009: UNKNOWN. UNKNOWN. EMERGENCY LIGHTS STAY ON. PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTS AND FOUND ALL WORKING NORMALLY IAW JIC NR 33-50-00-OPT-10000. - [SDR TRBA2009019](https://openairdocs.org/sdr/TRBA2009019), Feb 4, 2009: LIGHT. INOPERATIVE. FORWARD LEFT UPPER EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BURNED BULB IAW MM NR 33-50-00. OPERATIONAL CHECK OK. - [SDR TRBA2008036](https://openairdocs.org/sdr/TRBA2008036), Apr 1, 2008: PSU. FAILED. SMOKE FROM PASSENGER READING LIGHT AT 5AB. FLIGHT DIVERTED TO MIA FROM FLL. REMOVED AND REPLACED PSU (PASSENGER SERVICE UNIT) AT SEAT 5AB. PERFORMED OPT CK IAW - [SDR TRBA2008015](https://openairdocs.org/sdr/TRBA2008015), Feb 3, 2008: LIGHT. INOPERATIVE. ON POST FLIGHT, FOUND EMERGENCY LIGHT AT MAIN CABIN DOOR STEP INOPERATIVE. REMOVED AND REPLACED MAIN CABIN DOOR EMERGENCY LIGHT ASSEMBLY IAW JIC NR 33-51-24. OP - [SDR SDR2005083](https://openairdocs.org/sdr/SDR2005083), Dec 6, 2005: SKIN. CORRODED. DURING INSPECTION FOUND LT WING LOWER EXTERNAL SKIN WITH CORROSION AT THE T/E (UNDERWING BOX ANGLE END). REMOVED CORROSION AND TREATED IAW SRM. DEFERRED IAW SRA - [SDR TRB2005F00006](https://openairdocs.org/sdr/TRB2005F00006), Sep 13, 2005: COMPRESSOR. FOD. ( REF NR: SDR2005065 ) DURING TAKEOFF ROLL, SPARKS WERE COMING OUT THE RT ENGINE. TAKEOFF ABORTED. FOUND FOD DAMAGE IN THE COMPRESSOR BLADES. ENGINE REPLACED. ( - [SDR 2005F00079](https://openairdocs.org/sdr/2005F00079), Apr 7, 2005: WIRE HARNESS. BROKEN. WHILE IN CLIMB, LANDING GEAR DID NOT RETRACT WHEN SELECTED TO THE UP POSITION. AIRCRAFT RETURNED. REPLACED RT MLG INTERNAL UPPER HARNESS. (M) - [SDR 2002F00914](https://openairdocs.org/sdr/2002F00914), Aug 24, 2002: CONTROL CABLE. DAMAGED. DURING ACCOMPLISHMENT OF A FLEET CAMPAIGN DIRECTIVE FCD, IT WAS FOUND THAT THE CAPTAINS RUDDER CABLE LOCATED AT FK 12 COMING APART. REMOVED AND REPLACED RUDDER - [SDR 20001127AP004](https://openairdocs.org/sdr/20001127AP004), Aug 2, 2000: SPACER. CRACKED. DURING PERFORMANCE OF FCD E2-32-004, FOUND CRACK ON FRONT FACE OF LEFT LANDING GEAR SWINGING LEVER SPACER. (M) - [SDR 2000ZZZM21](https://openairdocs.org/sdr/2000ZZZM21), Oct 8, 1999: FLOORBEAM. CORRODED. FLOORBEAM 36 IS CORRODED BETWEEN F/A SEAT TRACKS IN TWO PLACES. BLENDED OUT AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-58. REMOVED AND REPLACED IAW SRM 51-25-0 - [SDR 2000ZZZM20](https://openairdocs.org/sdr/2000ZZZM20), Oct 8, 1999: SEAT TRACK. CORRODED. LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 32 AND 33OVER 33, 34, 29 AND 30. BLENDED OUT IAW SRM 53-00-00 AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLAC - [SDR 2000ZZZM19](https://openairdocs.org/sdr/2000ZZZM19), Oct 8, 1999: SEAT TRACK. CORRODED. LEFT OUTBOARD AFT MID SEAT TRACK, CORRODED BETWEEN FRAMES 28B AND 28C. BLENDED OUT OAN FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 FIG 304SHEET 2. BETWEEN F/A SE All 64: https://openairdocs.org/deregistered/N451AT-2013-09-26/reports.md ## Other aircraft with N451AT - [Registered now](https://openairdocs.org/aircraft/N451AT): Robinson Helicopter R44, S/N 2636, built 2021 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). 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