N824AY

Service difficulty reports · 34

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 = 'N824AY' AND registry_match = 'registration'
  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 REXA2013061701191Pbe · inoperativeCAPTAIN`S PBE BLUE DOT NOT BLUE ANYMORE. R & R CREW MEMBER PBE IN COCKPIT IAW AMM 35-30-00.Jun 17, 2013 · N824AY · Cndair CL6002B19 · Emergency EquipmentSDR REXA2013032600410Skin · gougedLEFT WING PLANK ACCESS HOLE FOR PANEL 510AB GOUGED 0.008" DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.Mar 25, 2013 · N824AY · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2013032600409Skin · gougedLEFT WING PLANK ACCESS HOLE FOR PANEL 540BB GOUGED 0.003" DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.Mar 25, 2013 · N824AY · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2013032600408Skin · damagedLEFT WING PLANK ACCESS HOLE FOR PANEL 550HB CHAFED AND GOUGED 0.002" DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.Mar 25, 2013 · N824AY · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2013032500404Skin · chafedRIGHT INBOARD FLAP TRAILING EDGE SKIN CHAFED NEAR CENTER. REPAIRED IAW SRM 57-52-00.Mar 24, 2013 · N824AY · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA2013032500403Rib · crackedRIGHT MLG BATT RIB CRACKED. REPAIRED IAW BOMBARDIER REO 601R-57-51-046.Mar 22, 2013 · N824AY · Cndair CL6002B19 · Wing, Rib/BulkheadSDR REXA2013032200397Bulkhead · unknownFS 280 BULKHEAD WEB FOUND RIGHT OF RBL 9 AND LBL 9 AND UPPER AFT FLOOR ANGLE AT LBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-136/601R-53-11-171.Mar 20, 2013 · N824AY · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA2013032200396Seat Track · gougedGOUGES ON BOTTOM OF SEAT TRACKS AT LBL 9 BETWEEN FS 508 AND FS 519 AND FS 542 - FS 554. REPAIRED IAW SRM 53-41-49.Mar 20, 2013 · N824AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2013032000394Bulkhead · damagedMULTIPLE SCREW MARKS ON FS 621 BULKHEAD. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.Mar 19, 2013 · N824AY · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA2013032200398Skin · chafedLEFT ELEVATOR HAS CHAFING ON INBOARD END OF UPPER SKIN CAUSED BY CONTACT WITH SEAL. BLENDED WITHIN LIMITS IAW SRM 55-00-31.Mar 18, 2013 · N824AY · Cndair CL6002B19 · Elevator, Plate/SkinSDR REXA2012110101444Switch · out of adjustGEAR DISAGREE ON RETRACTION. GEAR EXTENSION-RETRACTION SYSTEM PLACED ON DEFERRAL. FOUND NLG OLEO STRUT EXTENSION S23 OUT OF LIMITS. RE-ADJUSTED PER AMM 32-61-05. PERFORMED GEAR SWING IN ACCORDANCE WITH AMM 32-30-00. OPS CHECK GOOD. THIS CLEARS DM# 74086 Nov 1, 2012 · N824AY · Cndair CL6002B19 · Landing Gear Position and WarningSDR REXA2012092801370Light · inoperativeLEFT FWD EMERGENCY EXTERIOR LIGHT INOP. REMOVED AND REPLACED LEFT FWD EMERGENCY EXTERIOR LIGHT IAW CRJ 200 AMM 33-51-21.Sep 28, 2012 · N824AY · Cndair CL6002B19 · Emergency LightingSDR REXA2012082001280Relay · failedRIGHT THRUST REVERSER WILL NOT DEPLOY PAST IDLE, FEELS LIKE LEVER GETS STUCK. REMOVED AND REPLACED RELAY 2K5KE IN JB 3 IAW ESPM 20-22-00. OPS CHECKED GOOD OF RIGHT THRUST REVERSER IAW AMM 78-30-00.Aug 20, 2012 · N824AY · Cndair CL6002B19 · Engine Thrust ReverserSDR REXA2012071901171Relay · failedRIGHT THRUST REVERSER WILL NOT RELEASE FROM IDLE AFTER DEPLOYMENT. REMOVED AND REPLACED RELAY IN JB3 DESIGNATOR 2K6KE IAW AMM/CMM 24-01-03 AND WDM 91-32-03. OPS CHECKS AT LEAST 20 TIMES AND NO DEFECTS WERE NOTED.Jul 19, 2012 · N824AY · Cndair CL6002B19 · Engine Thrust ReverserSDR REXA2012071601165Computer · malfunctionedSTALL FAIL. PUSHER DOESN'T PUSH TO EITHER SIDE. REMOVED AND REPLACED STALL PROTECT COMPUTER AND OPS CHECKS GOOD IAW AMM 27-35-01. AIRCRAFT OK FOR SERVICE.Jul 16, 2012 · N824AY · Cndair CL6002B19 · Stall Warning SystemSDR REXA2012062401019Cable · out of rigTHRUST REVERSER WILL NOT DEPLOY. RIGGED THROTTLE GEAR BOX IAW AMM 76-11-17. OP`S CHECKED GOOD AT THIS TIME RIGGED ATR CABLE IAW AMM 78-35-01. OP`S CHECK GOOD.Jun 24, 2012 · N824AY · Cndair CL6002B19 · Power LeverSDR REXA2012060500818Throttle · failedRT THRUST REVERSER HANDLE WILL NOT COME OUT OF IDLE DETENT. REMOVED AND REPLACED THROTTLE QUADRANT IAW AMM 76-11-01. RT THRUST REVERSER OPS CHECKED GOOD.Jun 5, 2012 · N824AY · Cndair CL6002B19 · Power LeverSDR REXA2012052900793Unknown · unknownRIGHT THRUST REVERSER WILL NOT DEPLOY. PERFORMED OP`S CHECK OF RIGHT THRUST REVERSER IAW AMM 78-30-00. NO DEFECTS NOTED. OK FOR SERVICE.May 29, 2012 · N824AY · Cndair CL6002B19 · Engine Thrust ReverserSDR REXA2012051400731Switch · failedRIGHT THRUST REVERSER NOT DEPLOYING, DEFER OUTBOARD IAW MEL 78-30-01 AUT NR 63568. REMOVED AND REPLACED DEPLOY SWITCH IAW AMM 78-37-01. OPS CHECK GOOD, CLEAR DM X63568 PLACARD REMOVED.May 14, 2012 · N824AY · Cndair CL6002B19 · Engine Thrust ReverserSDR REXA201100913Line · looseRIGHT OIL PRESS MASTER WARNING IN CRUISE FLT. CRUISE FLT 330 THE MSG WAS INTERMITTENT AND O2 PRESSURE INDICATION WAS ERRATIC. THE OIL PRESSURE CLIMBED AS WE DESCENDED BUT WASN’T STEADY OR IN A NORMAL RANGE UNTIL ABOUT 22000 FT. RE-SECURED LOOSE LINE ON SCAVDec 7, 2011 · N824AY · Cndair CL6002B19 · Engine Oil Distribution (Airframe Furnished)SDR REXA201100245Bulkhead · chafedFS 621.00 PRESSURE BULKHEAD HAS SCREW MARKS ON FWD SKIN ABOVE FLOOR AT WL 105.00, LBL 18, LBL 27, RBL 18, RBL 27, AND RBL 36. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.Apr 25, 2011 · N824AY · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201100243Skin · dentedAC SKIN DENTED AFT OF FS 280 BETWEEN S-24L AND 25L (LT SIDE AFT AND LEFT OF FWD JACK PAD). REPAIRED IAW BOMBARDIER REO 601R-53-21-1275.Apr 25, 2011 · N824AY · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REXA201100242Bulkhead · crackedFS 202.75 PRESSURE BULKHEAD IS CRACKED AROUND THE PARKING BRAKE CONTROL CABLE HOLE ON INBOARD SIDE. REPAIRED IAW BOMBARDIER GREO 601R-53-11-563 AND BOMBARDIER SERVICE CORPORATION EO 601R-53-0101A.Apr 25, 2011 · N824AY · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201100247Skin · scratchedFUSELAGE SKIN SCRATCHED AND DENTED AT FS 672 BETWEEN S-23R AND S-24R. REPAIRED IAW BOMBARDIER REO 601R-53-52-4048.Apr 23, 2011 · N824AY · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REXA201100244Skin · dentedLEFT INBD FLAP UPPER SKIN SURFACE IS DENTED AT WS 63.49. REPAIRED IAW BOMBARDIER REO 601R-57-52-1544 AND BOMBARDIER SERVICE CORPORATION EO 601R-57-21207.Apr 23, 2011 · N824AY · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA201100241Rivet · damagedFS 621 PRESSURE BULKHEAD HAS DAMAGED RIVETS AT WL 90, LBL 9, LBL 18, LBL 27, LBL 36, RBL 9, RBL 18, AND RBL 27. REPLACED DAMAGED RIVETS IAW SRM 51-42-06.Apr 19, 2011 · N824AY · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201000297Skin · damagedWHILE BEING REPAINTED IN GLH A DENT WITH A SCRATCH IN THE FUSELAGE SKIN WAS DISCOVERED. THE DENT IS 3.75" X 1.0" X .078" DEEP, THE SCRATCH IS .004 DEEP. THE DAMAGE IS AT FS 654 - FS 672 BETWEEN STR 23R - STR 24R. FERRY FLIGHT FROM GLH TO MEM IAW BOMBARDIERDec 11, 2010 · N824AY · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REXA201000175Support Bracket · crackedTWO CRACKS WERE FOUND IN THE LOWER AFT CORNER OF THE NR 2 HYDRAULIC RETURN SYSTEM SUPPORT BRACKET AT FUSELAGE STATION 718. THE FIRST CRACK IS 0.5 INCH LONG BEFORE IT TURNED AND PROCEEDED FOR AN ADDITION 0.25 INCH (TOTAL LINEAR LENGTH OF 0.75 INCH). A SECOND COct 2, 2010 · N824AY · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201000156Strip · damagedRADOME LIGHTNING DIVERTER STRIP UPPER RT WITH 13.5 INCH REMAINING STRIP FROM LIE GOING BACK TO THE TIE: 6" THEN 3" THEN 4.5" FOR A TOTAL OF 13.5". FLY ON PER BOMBARDIER REO 601R-53-81-221 FOR 100 FH WITHIN WHICH TIME DAMAGE MUST BE REPAIRED OR RADOME MUST BE Sep 22, 2010 · N824AY · Cndair CL6002B19 · Aerodynamic FairingsSDR REXA200700045Unknown · odorON TAKEOFF GOT SMOKE AND SWEET BURNING ODOR. QRH FOLLOWED RETURNED TO AIRPORT. FOUND TO BE RESIDUAL DE-ICE FLUID IN ECS SYSTEM. ENGINE RUNS PERFORMED OPERATIONAL CHECKED GOODMar 4, 2007 · N824AY · Cndair CL6002B19 · Cabin Compressor SystemSDR REXA200600119Acm · smokeON APPROACH, HAD SMOKE/FUMES IN COCKPIT/CABIN WITH SMOKE MESSAGE. LEFT ACM PACK SHUTDOWN. MAINTENANCE DEFERRED LEFT PACK IAW MEL 21-51-11.Dec 19, 2006 · N824AY · Cndair CL6002B19 · Cabin Cooling SystemSDR REXA200600078Bracket · crackedBRACKET FOUND CRACKED AT (JUST AFT OF) FWD MOST LUG. REMOVED AND REPLACED BRACKET IAW EO (REO) 601R-53-41-432.Jul 31, 2006 · N824AY · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR REXA200600008Trim Switch · dirtySTAB TRIM DISENGAGED AND WOULD NOT RESET. FOUND TRIM SWITCH STUCK. CLEANED AND LUBRICATED TRIM SWITCH, OPERATIONALLY CHECKS GOOD.Feb 3, 2006 · N824AY · Cndair CL6002B19 · Stabilizer Control SystemSDR REXA200500157Fuel Control · defectiveON DESCENT, THE FLIGHT CREW DISCOVERED THAT THE RT ENGINE WAS UNRESPONSIVE TO THRUST LEVER INPUTS. THE FLIGHT CREW PERFORMED THE QRH AND DECLARED AN EMERGENCY. AN OTHERWISE UNEVENTFUL SINGLE ENGINE APPROACH AND LANDING WAS MADE. MAINTENANCE DISCOVERED THE MAIDec 14, 2005 · N824AY · Cndair CL6002B19 · Fuel Control/Turbine Engines
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