# N812AY: 2005 Bombardier CL-600-2B19, registration cancelled 2024-05-08 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 8, 2024 - Status when cancelled: Valid registration - Airframe: [Bombardier CL-600-2B19](https://openairdocs.org/model/bombardier-cl-600-2b19) (registry code 1390008) - Engine: [GE CF34-3B1](https://openairdocs.org/engine/ge-cf34-3b1) (registry code 30070) - Data sheets: [TCDS A21EA-1](https://openairdocs.org/tcds/A21EA-1), [TCDS E15NE](https://openairdocs.org/tcds/E15NE) (OpenAirDocs) - Serial number: 8012 - Year built: 2005 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: January 31, 2005 - Certificate issued: October 29, 2023 - Last registry action: October 29, 2023 - Mode S code: AB10E1 - Owner when cancelled: [Beautech Power Systems LLC](https://openairdocs.org/faa-owner/BEAUTECH%20POWER%20SYSTEMS%20LLC) - Location: [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas) - Owner type: LLC - Owner's area on the map: 32.7883° N, 96.7996° W: Placed by OpenAirDocs at the center of ZIP code 75201, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N812AY - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=812AY - Page: https://openairdocs.org/deregistered/N812AY-2024-05-08 From the FAA registry file of November 4, 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 Bombardier CL-600-2B19: https://openairdocs.org/model/bombardier-cl-600-2b19.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 REXA2015072000121](https://openairdocs.org/sdr/REXA2015072000121), Jul 20, 2015: SKIN. DAMAGED. DURING INSPECTION, FOUND DAMAGE TO THE LT FUSELAGE SKIN BETWEEN FS 625.00 & 654.00, STRINGER 22L & 23L. THE DAMAGE MEASURES A MAXIMUM OF 30.0” X 4.5” X .375” DE - [SDR REXA2013090101722](https://openairdocs.org/sdr/REXA2013090101722), Sep 1, 2013: FLASHLIGHT. INOPERATIVE. F/A FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT ASSY IAW AMM 25-61-02. - [SDR REXA2013070401331](https://openairdocs.org/sdr/REXA2013070401331), Jul 4, 2013: STALL WARNING. FALSE ACTIVATION. STALL FAIL ENROUTE. QRH COMPLETED. PERSISTED WHOLE FLIGHT. FOUND OXYGEN SERVICING PANEL DOOR WAS LEFT OPEN. INSPECTED & SECURED OXYGEN SERVICE PANEL DOOR CLOSED - [SDR REXA2013060801073](https://openairdocs.org/sdr/REXA2013060801073), Jun 8, 2013: WARNING MESSAGE. FALSE ACTIVATION. SPOILERONS FAULT/OTBD GROUND SPOILER FAULT STATUS MESAGES APPEARED ON APPROACH. INFORMATION ONLY: FOLLOWED THE FAULT RESET PROCEDURES IAW CHAPTER 6 FOR SPOILER - [SDR REXA2013053000683](https://openairdocs.org/sdr/REXA2013053000683), May 30, 2013: ANGLE. CRACKED. CRACK FOUND IN FS559 SEMI-PRESSURE BULKHEAD CAP ANGLE AT RBL18 AND LBL18. REPAIRED IAW PA 53-025 AND REO 601R-53-41-260/601R-53-41-609. - [SDR REXA2012120301540](https://openairdocs.org/sdr/REXA2012120301540), Nov 30, 2012: BULKHEAD. CRACKED. CRACKS FOUND ON FS 280 BULKHEAD AND UPPER FLOOR ANGLE AT LBL 9 AND RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-136/601R-53-11-171. BULKHEAD WEB SKIN EXFOLIATE - [SDR REXA2012120201539](https://openairdocs.org/sdr/REXA2012120201539), Nov 30, 2012: BULKHEAD. CRACKED. FS 621 BULKHEAD FORWARD FACE NEXT TO LINTEL FITTING LOWER INBOARD CORNER AREA CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230. - [SDR REXA2012112501523](https://openairdocs.org/sdr/REXA2012112501523), Nov 20, 2012: SKIN. CORRODED. RIGHT WING LOWER PLANK ACCESS HOLES FOR PANELS 640BB, 640FB, 650GB, AND 650EB CORRODED IN THE NON-CRITICAL REGIONS. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 R - [SDR REXA2012112501522](https://openairdocs.org/sdr/REXA2012112501522), Nov 20, 2012: SKIN. CORRODED. LEFT WING LOWER PLANK ACCESS HOLES FOR PANELS 510AB AND 540DB CORRODED IN THE NON-CRITICAL REGIONS. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV J. - [SDR REXA2012102701428](https://openairdocs.org/sdr/REXA2012102701428), Oct 27, 2012: GLOWSTRIP. INOPERATIVE. EMERGENCY FLOOR TRACK LIGHTING APPEARS TO BE INOPERABLE. PHOTO LUMINESCENT LIGHTING STRIPS INSTALLED OPS NORMAL IAW AMM 33-51-00. OK FOR SERVICE. - [SDR REXA2012031200053](https://openairdocs.org/sdr/REXA2012031200053), Mar 12, 2012: LIGHT. INOPERATIVE. INTERIOR OVERHEAD EMERGENCY LIGHT NR 4 INOP. REMOVED AND REPLACED BULB IN NR 4 INTERIOR OVERHEAD EMERGENCY LT IAW AMM 33 50. OPS CHECK GOOD. - [SDR REXA201100055](https://openairdocs.org/sdr/REXA201100055), Jan 17, 2011: FRAME. DAMAGED. IN AFT EQUIPMENT COMPARTMENT AT FS 672.00, STRINGER 25R. THE FRAME FLANGE ON FWD AND AFT EDGES ARE DENTED AND CRACKED. COMPLIED WITH PERMANENT REPAIR TO FS 672. - [SDR REXA201100054](https://openairdocs.org/sdr/REXA201100054), Jan 17, 2011: BULKHEAD. CRACKED. FS 202.75 BULKHEAD AT PARKING BRAKE CABLE PASS THROUGH HOLE FAILS NDTM WITH AN INDICATION NOTED APPROX .500" IN LENGTH, 90 PERCENT FSH. COMPLIED WITH PERMANENT - [SDR REXA201100053](https://openairdocs.org/sdr/REXA201100053), Jan 17, 2011: SEAT TRACK. CORRODED. LT AND RT SIDE SEAT TRACK CORRODED BETWEEN FS 461 AND 473 UNDER OVERWING EMERGENCY EXIT DOOR CUTOUTS. REMOVED AND REPLACED LT AND RT SIDE SEAT TRACK BETWEEN FS - [SDR REXA201000325](https://openairdocs.org/sdr/REXA201000325), Dec 23, 2010: SKIN. DENTED. SINGLE INDENTATION WAS FOUND ON THE LEFT WING INBOARD GROUND SPOILER UPPER SURFACE AT WS 89.0. THE DAMAGE IS RECORDED AS 1.00 INCH DIAMETER AND A MAXIMUM DEPTH - [SDR REXA201000089](https://openairdocs.org/sdr/REXA201000089), Jun 1, 2010: LIGHT. CONTAMINATED. THE CREW REPORTED A FUME SMELL IN THE COCKPIT PRIOR TO APPROACH. THE FUMES SMELLED ELECTRICAL. THE APU WAS OFF AT THE TIME. DECLARED EMERGENCY AND LANDED WITHOU - [SDR REXA201000012](https://openairdocs.org/sdr/REXA201000012), Jan 25, 2010: UNKNOWN. MALFUNCTIONED. GEAR DISAGREE ON TAKEOFF (NOSE GEAR WOULD NOT RETRACT). DEFERRED PER MEL 32-30-01. - [SDR REXA200500126](https://openairdocs.org/sdr/REXA200500126), Sep 28, 2005: FLAP SYSTEM. FAILED. FLAPS FAILED AT 20 DEGREES ON APPROACH. SYSTEM RESET AND PLACED UNDER 72 HOUR WATCH PER AD 98-20-01. --- 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.