N829AY

Service difficulty reports · 33

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 = 'N829AY' 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 REXA2013030600547Battery Pack · inoperativeFORWARD OVERHEAD CEILING EMERGENCY FLOOD LIGHT IS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-04.Mar 6, 2013 · N829AY · Cndair CL6002B19 · Emergency LightingSDR REXA2013022700371Vane · chafedRIGHT INBOARD FLAP VANE LEADING EDGE HAS CHAFE DAMAGE IN 3 AREAS, FLAP STA137.012 AND 108.135 WERE WITHIN LIMTS OF BOMBARDIER REO 601R-57-52-004. DAMAGE AT FLAP STA 60.005 OUT OF LIMITS AND REPLACED.Feb 26, 2013 · N829AY · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA2013022700374Bulkhead · gougedAFT PRESSURE BULKHEAD AT FS 621 FOUND TO BE GOUGED IN 10 AREAS FROM WL 88.43 TO WL 102.43, BETWEEN LBL 18 AND RBL 36.2 UP TO 0.005" DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-4818.Feb 25, 2013 · N829AY · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA2013022700373Structure · corrodedWING PANEL ACCESS HOLE FOR PANEL 540BB AT WS 54.897 (HOLE 1) WAS FOUND CORRODED 0.003" DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-21-030J.Feb 25, 2013 · N829AY · Cndair CL6002B19 · Wing Miscellaneous StructureSDR REXA2013022700372Structure · corrodedWING PANEL ACCESS HOLE FOR PANEL 650FB AT WS 274.319 (HOLE 14) WAS FOUND CORRODED 0.002" DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-21-030J.Feb 25, 2013 · N829AY · Cndair CL6002B19 · Wing Miscellaneous StructureSDR REXA2013022700370Flap · dentedLEFT INBOARD FLAP INADVERTANTLY DROPPED DURING MAINTENANCE OPERATIONS AND DENTED IN SEVERL LOCATIONS. REPAIRED IAW SRM 57-52-00 REPAIR 3.Feb 25, 2013 · N829AY · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA2013022700369Intercostal · crackedINTERCOSTAL AT FS 484 IS CRACKED AT RBL 27 AND RBL 36. REPAIRED IAW BOMBARDIER REO 601R-53-41-059B.Feb 25, 2013 · N829AY · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2013022500342Fitting · crackedFS 280 CLIP CRACKED AT RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-136/601R-53-11-171.Feb 25, 2013 · N829AY · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2013022500341Fitting · crackedFS 280 CLIP CRACKED AT LBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-136/601R-53-11-171.Feb 25, 2013 · N829AY · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2013022500340Angle · crackedFOUND UPPER AFT FLOOR ANGLE 2 EACH CRACKED AND FOUND LOWER FLOOR WEB 2 EACH CRACKS AT FS 280 LBL 9 AND RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-136/601R-53-11-171.Feb 24, 2013 · N829AY · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2013022500339Frame · corrodedFRAME AT FS 605 HAS CORROSION BETWEEN S-26L AND S-27. REPLACED IAW SRM 51-42-06 AND 51-42-21.Feb 24, 2013 · N829AY · Cndair CL6002B19 · Fuselage Main, FrameSDR REXA2013022500338Intercostal · crackedINTERCOSTAL AT FS 484 IS CRACKED AT RBL 27 AND RBL 36. REPAIRED IAW BOMBARDIER REO 601R-53-41-059.Feb 24, 2013 · N829AY · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2013022200236Intercostal · crackedINTERCOSTAL AT FS 484 IS CRACKED AT LBL 27 AND LBL 36. REPAIRED IAW BOMBARDIER REO 601R-53-41-059B.Feb 19, 2013 · N829AY · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2013010600112Life Vest · unserviceableINFANT LIFE VEST BAG TORN. REMOVED AND REPAIRED INFANT LIFE VEST IAW AMM 25-61-03.Jan 6, 2013 · N829AY · Cndair CL6002B19 · Life JacketSDR REXA2012121001757Unknown · malfunctionedON LEFT BRAKE ONE BTMS SAYS 00 THE OTHER FOR THE LEFT BRAKE SAYS 05 DISCONNECTED AND RE-ATTACHED LEFT O/B BRAKE LINE QUICK DISCONNECT IAW AMM 32-43-26. LEFT O/B BRAKE CHECKS NORMAL. OK FOR SERVICE.Dec 10, 2012 · N829AY · Cndair CL6002B19 · Landing Gear Brake SystemSDR REXA2012120701752Cover · unknownF/A NO SMOKING/FASTEN SEAT BELT SIGN IN GALLY NEEDS COVER REPLACED. 2LA007353-50. OPS CHECK OK. REMOVED AND REPLACED F/A GALLEY NO SMOKING LIGHT IAW CRJ200 AMM 33-24-00. THIS CLOSES OUT DM 76112.Dec 7, 2012 · N829AY · Cndair CL6002B19 · Passenger Compartment LightingSDR REXA2012112101695Life Vest · unserviceableONE INFANT LIFE VEST HAS HOLE IN BAG. REMOVED AND REPLACED INFANT LIFE VEST IAW AMM 25-61-03.Nov 21, 2012 · N829AY · Cndair CL6002B19 · Life JacketSDR REXA2012110201549Light · inoperativeMID AFT CABIN OVERHEAD EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED BULB IAW AMM 33-21-01. OP CHECKS GOOD DM 74146 CLOSED.Nov 2, 2012 · N829AY · Cndair CL6002B19 · Emergency LightingSDR REXA2012081601264Bulb · inoperativeRIGHT EMERGENCY OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY LIGHT BULB NR 3 IAW AMM 33-51-21. OPS CHECKED GOOD.Aug 16, 2012 · N829AY · Cndair CL6002B19 · Emergency LightingSDR REXA2012021000216Pseu · malfunctionedAIR RETURN FOR PROX SYS FAULT STATUS IN FLIGHT IN CLIMBOUT THRU 10000. FOUND PSEU CODE A06 - NVRAM. REMOVED AND REPLACED PSEU & OP CHECK GOOD IAW AMM 32-61-01. OK FOR SVC.Feb 10, 2012 · N829AY · Cndair CL6002B19 · Landing Gear Position and WarningSDR REXA201100429Bpsu · malfunctionedCREW DECLARED EMERGENCY DUE TO FLAPS FAILED AT ZERO EN ROUTE. REMOVED AND REPLACED LT BPSU IAW AMM 27-51-10. FLAPS OP CHECK NORMAL IAW AMM 27-54-00. OK FOR SERVICE. PART EFFECTIVELY VERIFIED.Jun 26, 2011 · N829AY · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA201100428Bpsu · malfunctionedFLAPS FAIL AT 18 DEG OUTBOUND OF ROC. A/C DID AIR RETURN AND DECLARED AN EMERGENCY. REMOVED AND REPLACED BPSU IAW AMM 27-51-10.Jun 26, 2011 · N829AY · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA201100427Flap · malfunctionedFLAPS FAIL AT 0 ON CLIMBOUT DTW CREW DECLARED AN EMERGENCY ON APPROACH TO BUF RESET AND PLACED ON DI FOR 10 CYC.Jun 25, 2011 · N829AY · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA201100404Flap · failedCREW REPORTED FLAPS FAILED AT ZERO AFTER CLIMBOUT CONTINUED ON TO DTW LANDED WITHOUT INCIDENT. PERFORMED TROUBLESHOOTING PER BOMBARDIER FCM REV 39 IAW AD 2009-06-12 PARAGRAPH (H) (6) (I), AMOC DATED MARCH 27, 2009, TR 27-012 PER AMOL DATED DECEMBER 18, 2009 AJun 20, 2011 · N829AY · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA201100386Flap · malfunctionedCREW REPORTED FLAPS FAIL CAUTION WITH FLAPS RETRACTED TO '0' AIRSPEED 200/250. DEFERRED FLAP SYSTEM IAW MEL 27-50-00 DM-45378.Jun 13, 2011 · N829AY · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA201100248Bulkhead · chafedFWD FACE OF FS 621 BULKHEAD CHAFED IN 9 EACH PLACES NO DEEPER THAN 0.003 INCHES. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155 AND 601R-53-61-4042.Apr 20, 2011 · N829AY · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201100218Yoke · scratchedRIGHT FORWARD ENGINE MOUNT YOKE HAS FOUR SCRATCHES AT TOP FORWARD LUG ON FORWARD FACE. TWO SCRATCHES MEASURE .156 INCH LONG AND UP TO 0.025 INCH DEEP. TWO SCRATCHES MEASURE 0.375 INCH LONG AND UP TO 0.007 INCH DEEP. REPAIRED IAW BOMBARDIER REO 601R-71-21-04Apr 11, 2011 · N829AY · Cndair CL6002B19 · Engine Mount SectionSDR REXA201100183Panel · openLOUD NOISE COMING FROM THE NOSE OF THE A/C FOLLOWED BY A STALL FAIL MSG DURING INITIAL CLIMBOUT. FOUND PANEL 212BR OPEN. PERFORMED OPS CHECK ON STALL PROTECTION SYSTEM IAW 27-35-00.Mar 11, 2011 · N829AY · Cndair CL6002B19 · Aircraft StructuresSDR REXA201100123Web · canningDAMAGE WAS FOUND ON THE AFT SIDE PANEL WEB OF THE MAIN PASSENGER DOOR STAIRS (P/N 601R31701-01, S/N 8029) NEAR THE TOP OF THE 2ND STEP (AT FS 349). THE DAMAGE IS OIL CANNING WITH A DENT PROTRUDING OUTWARD. ONLY THE WEB IS DAMAGED NO INTERNAL STRUCTURE IS AFFFeb 14, 2011 · N829AY · Cndair CL6002B19 · Passenger/Crew DoorsSDR REXA201100109Skin · crackedA DENT WAS FOUND ON THE UPPER SURFACE OF THE RIGHT WING OUTBOARD GROUND SPOILER (P/N 600-10502-56, S/N 3971165). THE DENT MEASURES 0.625 X 0.625 X 0.011 DEEP; IT IS 2.8 FROM THE OUTBOARD EDGE AND 2.0 FROM THE LEADING EDGE. REPAIRED IAW STS ENGINEERING EA 09-Feb 12, 2011 · N829AY · Cndair CL6002B19 · SpoilersSDR REXA201000041Warning System · malfunctionedGEN 2 OFF CAUTION SVC NR 2 IDG IAW AMM 12-13-24. OPC GOOD THIS CLEARS DM 19630. OK FOR SERVICE.Apr 5, 2010 · N829AY · Cndair CL6002B19 · Central WarningSDR REXA200600046Flap · failedFLAPS FAILED AT 30 DEGREES ON APPROACH. APPROACH ABORTED QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.Apr 7, 2006 · N829AY · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REX200500137Flap System · malfunctionedFLAPS FAIL AT GATE. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD98-20-01.Nov 15, 2005 · N829AY · Cndair CL6002B19 · Trailing Edge Flap Control System
Back to N829AY