N812AY, cancelled May 8, 2024

Service difficulty reports · 18

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR REXA2015072000121Skin · damagedDURING 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.Jul 20, 2015 · N812AY · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REXA2013090101722Flashlight · inoperativeF/A FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT ASSY IAW AMM 25-61-02.Sep 1, 2013 · N812AY · Cndair CL6002B19 · Emergency EquipmentSDR REXA2013070401331Stall Warning · false activationSTALL 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 GJul 4, 2013 · N812AY · Cndair CL6002B19 · Stall Warning SystemSDR REXA2013060801073Warning Message · false activationSPOILERONS 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.Jun 8, 2013 · N812AY · Cndair CL6002B19 · Drag Control SystemSDR REXA2013053000683Angle · crackedCRACK 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.May 30, 2013 · N812AY · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA2012120301540Bulkhead · crackedCRACKS 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.Nov 30, 2012 · N812AY · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA2012120201539Bulkhead · crackedFS 621 BULKHEAD FORWARD FACE NEXT TO LINTEL FITTING LOWER INBOARD CORNER AREA CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230.Nov 30, 2012 · N812AY · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA2012112501523Skin · corrodedRIGHT 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.Nov 20, 2012 · N812AY · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2012112501522Skin · corrodedLEFT 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.Nov 20, 2012 · N812AY · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2012102701428Glowstrip · inoperativeEMERGENCY FLOOR TRACK LIGHTING APPEARS TO BE INOPERABLE. PHOTO LUMINESCENT LIGHTING STRIPS INSTALLED OPS NORMAL IAW AMM 33-51-00. OK FOR SERVICE.Oct 27, 2012 · N812AY · Cndair CL6002B19 · Emergency EquipmentSDR REXA2012031200053Light · inoperativeINTERIOR OVERHEAD EMERGENCY LIGHT NR 4 INOP. REMOVED AND REPLACED BULB IN NR 4 INTERIOR OVERHEAD EMERGENCY LT IAW AMM 33 50. OPS CHECK GOOD.Mar 12, 2012 · N812AY · Cndair CL6002B19 · Emergency LightingSDR REXA201100055Frame · damagedIN 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.Jan 17, 2011 · N812AY · Cndair CL6002B19 · Fuselage Main, FrameSDR REXA201100054Bulkhead · crackedFS 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-53-11Jan 17, 2011 · N812AY · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201100053Seat Track · corrodedLT 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.Jan 17, 2011 · N812AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR REXA201000325Skin · dentedSINGLE 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 Dec 23, 2010 · N812AY · Cndair CL6002B19 · SpoilersSDR REXA201000089Light · contaminatedTHE 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 CAUSJun 1, 2010 · N812AY · Cndair CL6002B19 · Flight Compartment LightingSDR REXA201000012Unknown · malfunctionedGEAR DISAGREE ON TAKEOFF (NOSE GEAR WOULD NOT RETRACT). DEFERRED PER MEL 32-30-01.Jan 25, 2010 · N812AY · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR REXA200500126Flap System · failedFLAPS FAILED AT 20 DEGREES ON APPROACH. SYSTEM RESET AND PLACED UNDER 72 HOUR WATCH PER AD 98-20-01.Sep 28, 2005 · N812AY · Cndair CL6002B19 · Trailing Edge Flap Control System
Back to N812AY, cancelled May 8, 2024