# Service difficulty reports: N812AY, cancelled May 8, 2024 A list on [N812AY, cancelled May 8, 2024](https://openairdocs.org/deregistered/N812AY-2024-05-08.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR REXA2015072000121](https://openairdocs.org/sdr/REXA2015072000121.md): Skin · damaged · Jul 20, 2015 · N812AY · Cndair CL6002B19 · Fuselage Main, Plate/Skin > 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” DEEP. REPAIRED IAW CRJ253-03382. - [SDR REXA2013090101722](https://openairdocs.org/sdr/REXA2013090101722.md): Flashlight · inoperative · Sep 1, 2013 · N812AY · Cndair CL6002B19 · Emergency Equipment > F/A FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT ASSY IAW AMM 25-61-02. - [SDR REXA2013070401331](https://openairdocs.org/sdr/REXA2013070401331.md): Stall Warning · false activation · Jul 4, 2013 · N812AY · Cndair CL6002B19 · Stall Warning System > STALL FAIL ENROUTE. QRH COMPLETED. PERSISTED WHOLE FLIGHT. FOUND OXYGEN SERVICING PANEL DOOR WAS LEFT OPEN. INSPECTED & SECURED OXYGEN SERVICE PANEL DOOR CLOSED IAW AMM 52-45-26. PERFORMED OPS CHECK OF STALL PROTECTION SYS IAW AMM 27-35-01. OPS CHECKED G - [SDR REXA2013060801073](https://openairdocs.org/sdr/REXA2013060801073.md): Warning Message · false activation · Jun 8, 2013 · N812AY · Cndair CL6002B19 · Drag Control System > SPOILERONS FAULT/OTBD GROUND SPOILER FAULT STATUS MESAGES APPEARED ON APPROACH. INFORMATION ONLY: FOLLOWED THE FAULT RESET PROCEDURES IAW CHAPTER 6 FOR SPOILER FAULTS MESSAGE CLEARED & SYS OPERATES NORMAL. - [SDR REXA2013053000683](https://openairdocs.org/sdr/REXA2013053000683.md): Angle · cracked · May 30, 2013 · N812AY · Cndair CL6002B19 · Fuselage Main, Bulkhead > 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.md): Bulkhead · cracked · Nov 30, 2012 · N812AY · Cndair CL6002B19 · Fuselage Main, Bulkhead > 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 EXFOLIATED FROM LBL 9 TO BL 0, REPAIRED IAW BOMBARDIER REO 601R-53-11-2415. - [SDR REXA2012120201539](https://openairdocs.org/sdr/REXA2012120201539.md): Bulkhead · cracked · Nov 30, 2012 · N812AY · Cndair CL6002B19 · Fuselage Main, Bulkhead > 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.md): Skin · corroded · Nov 20, 2012 · N812AY · Cndair CL6002B19 · Wing, Plate/Skin > 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 REV J. - [SDR REXA2012112501522](https://openairdocs.org/sdr/REXA2012112501522.md): Skin · corroded · Nov 20, 2012 · N812AY · Cndair CL6002B19 · Wing, Plate/Skin > 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.md): Glowstrip · inoperative · Oct 27, 2012 · N812AY · Cndair CL6002B19 · Emergency Equipment > 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.md): Light · inoperative · Mar 12, 2012 · N812AY · Cndair CL6002B19 · Emergency Lighting > 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.md): Frame · damaged · Jan 17, 2011 · N812AY · Cndair CL6002B19 · Fuselage Main, Frame > 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 672.00 FRAME AT STRINGER 25R ON FWD AND AFT FLANGES IAW BSC EO 601R-53-20296. - [SDR REXA201100054](https://openairdocs.org/sdr/REXA201100054.md): Bulkhead · cracked · Jan 17, 2011 · N812AY · Cndair CL6002B19 · Fuselage Main, Bulkhead > 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 REPAIR OF FS 202.75 BULKHEAD AT PARKING BRAKE CABLE PASS THROUGH HOLE IAW BOMBARDIER REO 601R-53-11 - [SDR REXA201100053](https://openairdocs.org/sdr/REXA201100053.md): Seat Track · corroded · Jan 17, 2011 · N812AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > 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 449 AND 473 IAW CRJ 200 AMM 53-01-11-000-802 AND AMM 53-01-11-400-802. - [SDR REXA201000325](https://openairdocs.org/sdr/REXA201000325.md): Skin · dented · Dec 23, 2010 · N812AY · Cndair CL6002B19 · Spoilers > 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 OF 0.009 INCH AND IS LOCATED 1.25 INCHES AFT OF THE LEADING EDGE AND 9.25 INCHES FROM THE OUTBOARD - [SDR REXA201000089](https://openairdocs.org/sdr/REXA201000089.md): Light · contaminated · Jun 1, 2010 · N812AY · Cndair CL6002B19 · Flight Compartment Lighting > 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 WITHOUT INCIDENT. MAINTENANCE FOUND FLOODLIGHT ON F/O'S SIDE (P3LA) TO BE CONTAMINATED WITH WATER CAUS - [SDR REXA201000012](https://openairdocs.org/sdr/REXA201000012.md): Unknown · malfunctioned · Jan 25, 2010 · N812AY · Cndair CL6002B19 · Landing Gear Retraction/Extension System > GEAR DISAGREE ON TAKEOFF (NOSE GEAR WOULD NOT RETRACT). DEFERRED PER MEL 32-30-01. - [SDR REXA200500126](https://openairdocs.org/sdr/REXA200500126.md): Flap System · failed · Sep 28, 2005 · N812AY · Cndair CL6002B19 · Trailing Edge Flap Control System > FLAPS FAILED AT 20 DEGREES ON APPROACH. SYSTEM RESET AND PLACED UNDER 72 HOUR WATCH PER AD 98-20-01. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N812AY' AND deregistration_id = 'N812AY-2024-05-08' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N812AY-2024-05-08/reports --- 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.