N826AY

Service difficulty reports · 26

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 = 'N826AY' 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 REXA2013030900386Skin · chafedREMOVED CHAFE ON RIGHT WING FUEL CUTOUT PANEL LANDING 640BB, HOLE NR 1, IN THE NON-CRITICAL AREA WITHIN LIMITS IAW BOMBARDIER REO 601R-57-21-030 REV J.Mar 7, 2013 · N826AY · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2013030900385Angle · crackedRIGHT FS 280 BEAM LOWER ANGLE IS CRACKED AT VERTICAL POSTS JUST OUTBOARD OF RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-171.Mar 7, 2013 · N826AY · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2013030900384Angle · crackedRIGHT FLOOR SILL PLATE ANGLE OVERWING BOX CORRODED. REPAIRED IAW BOMBARDIER REO 601R-53-41-666.Mar 7, 2013 · N826AY · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2013030900383Angle · crackedLEFT FLOOR SILL PLATE ANGLE OVERWING BOX CORRODED. REPAIRED IAW BOMBARDIER REO 601R-53-41-666.Mar 7, 2013 · N826AY · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2013030900382Angle · crackedLEFT FS 280 BEAM LOWER ANGLE CRACKED JUST BELOW THE PULLEY BRACKET AND OUTBOARD OF LBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-171.Mar 7, 2013 · N826AY · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2013030900381Angle · crackedLEFT FS 280 BEAM UPPER ANGLE IS CRACKED JUST OUTBOARD OF LBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-138.Mar 7, 2013 · N826AY · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2013030900380Bulkhead · corrodedAFT CARGO COMPARTMENT FLOORBOARD LANDING CORRODED ON FWD FACE OF THE FS 621 BULKHEAD AT LBL 39. REPAIRED IAW BOMBARDIER REO 601R-53-61-117.Mar 7, 2013 · N826AY · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA2013012300177Fuel Control · out of rigDURING START TO TAKE AIRCRAFT TO THE GATE RECEIVED HOT ICON, NO FUEL APPLIED, FLAMES COMING OUT OF ENGINE AND ENGINE FIRE BOTTLES WERE DISCHARGED. REMOVED AND REPLACED NR 2 FIRE BOTTLE IAW AMM 26-21-10. RIGGED RIGHT FUEL CONTROL IAW AMM 76-10-00. OK FOR SERJan 23, 2013 · N826AY · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR REXA2013012100171Actuator · failedON FLIGHT 3867 (BUF TO DTW) RECEIVED FLAPS FAIL AT 20 DEGREES ON APPROACH INTO DTW. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 44 IAW AD2009-06-12 PARAGRAPH (H)(6)(I), AMOC DATED DECEMBER 07, 2012 AND PA AD27-052J (DOCUMENT WORK PERFORMED) INSPECTED FLAJan 21, 2013 · N826AY · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR REXA2013011500145Light · inoperativeCEILING EMERGENCY FLOOD LIGHT, LIGHT NR 1. RE-LAMP CEILING LEVEL EMERGENCY FLOOD LIGHT IAW 33-51-16.Jan 14, 2013 · N826AY · Cndair CL6002D24 · Emergency LightingSDR REXA2013123000051Priority Valve · malfunctionedON FLIGHT 4145 (PVD TO DTW) CREW RECEIVED NOSE GEAR DISAGREE MESSAGE AND THE CREW DECLARED AN EMERGENCY. HYDRAULIC PRESSURE SHOWED NORMAL (2900), NOSE GEAR STAYED DOWN (DID NOT RETRACT). MAIN GEAR RETRACTED NORMALLY. QRH COMPLETE. THE FLIGHT PERFORMED AN ADec 30, 2012 · N826AY · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR REXA2012050300606Bracket · damagedAFTER T/O NOSE GEAR DID NOT RETRACT RECEIVED NOSE DOOR OPEN AND GEAR DISAGREE MASTER WARNING. COMPLIED SCENARIO 1 OF PA -05-018F AND FOUND CENTERING /OLEO EXTENSION PROX SENSOR BRACKET DAMAGED. SEE AML 2167904 DISC NR 2 FOR CORRECTIVE ACTION.May 3, 2012 · N826AY · Cndair CL6002B19 · Landing Gear Position and WarningSDR REXA2012031300354Arm · unsecureAIR RETURN FOR THE FOLLOWING: AFTER LIFT OFF, HEARD CLUNCKING IN RT NOSE AREA. FOUND RADOME SECURE ARMS UNSECURED AND FREE MOVING RESECURED ARMS IAW AMM 53-81-01.Mar 13, 2012 · N826AY · Cndair CL6002B19 · Fuselage, Equipment Attach FittingsSDR REXA201100884Wire · damagedIDG 2 CAUTION MSG. EMERGENCY DECLARED. IDG 2 INTERMITTENT BUT MOSTLY ON AFTER FL170. REPAIRED WIRE TO RT IDG OVERTEMP SWITCH IAW ESPM 20-17-10. RECONNECTED RT IDG IAW AMM 24-11-01. OPC GOOD.Nov 28, 2011 · N826AY · Cndair CL6002B19 · Electrical Power System WiringSDR REXA201100440Uplock · malfunctionedGEAR UP DISAGREE WARNING MSG IN FLIGHT, AFTER QRH MSG CLEARED REMOVED AND REPLACED RT MLG UPLOCK IAW AMM 32-32-05. VERIFIED PART EFFECTIVITY & COMPLIED WITH PA 05-018B GEAR DISAGREE EVENT PROCEDURES.Jul 4, 2011 · N826AY · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR REXA201100347Bpsu · malfunctionedFLAPS FAILED AT ZERO AFTER TAKEOFF CONTINUED ON, LANDED WITHOUT INCIDENT. /R RT BPSU IAW AMM 27-51-10 OP CHECK GOOD.Jun 6, 2011 · N826AY · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA201100246Skin · dentedEXISTING FUSELAGE REPAIR DOUBLER JUST FORWARD OF FS 640 BETWEEN STRINGERS S-21R AND 23R FOUND DENTED. REPAIRED IAW BOMBARDIER SERVICE CORPORATION 601R-53-21208A AND ASSOCIATED 8110-3 DATED 4/21/11.Apr 23, 2011 · N826AY · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REXA201100122Fastener · missingONE OF THE STUD NUT FASTENERS (P/N CA2023-5) FOR THE RT WING LANDING RECOGNITION LIGHT WAS FOUND MISSING. TEMPORARY REPAIR IAW STS ENGINEERING EA 09-2011-040. REPEAT INSPECT EVERY 150 FH. WITHIN 500 FLIGHT HOURS, ACCOMPLISH A PERMANENT REPAIR TO THE DAMAGEDFeb 14, 2011 · N826AY · Cndair CL6002B19 · Exterior LightingSDR REXA201100089Door Seal · leakingFLT 3837 YOW-DTW DIVERTED TO YYZ HAD LOUD DOOR SQUEAL FOLLOWED BY LOSS OF PRESSURIZATION APPROX 45 MIN INTO THE FIGHT. EMERGENCY DESCENT TO 1000 FT. EMERGENCY DECLARED AND DIVERTED TO YYZ. A/C LANDED SAFELY IN YYZ. INSPECTED AND CLEANED DOOR SEAL AND DOOR Feb 7, 2011 · N826AY · Cndair CL6002B19 · Passenger/Crew DoorsSDR REXA201000328Unknown · unknownEN ROUTE AT FL290 FROM KBHM TO KDTW THE FLIGHT CREW DETECTED THE SOUND OF A HIGH PITCHED RUSHING AIR SOUND. CABIN ALTITUDE INDICATED A 1000-1300 FPM CLIMB. THE FLIGHT CREW DONNED O2 MASKS, DECLARED AN EMERGENCY AND BEGAN AN EMERGENCY DESCENT. ON DESCENT ARODec 25, 2010 · N826AY · Cndair CL6002B19 · Cabin Pressure Control SystemSDR REXA201000149Doubler · dentedDENT 2"L X 1.9"W X .075" DEEP, ON DOUBLER INSTALLED BETWEEN FS 640-625 AND STR 21R-23R PER PREVIOUS REO 601R-53-61-3563. FLY-ON FOR 1650 FH PER REO 601R-53-61-3823 TO NEXT C CHECK WHEN A PERMANENT REPAIR WILL BE PERFORMED.Sep 17, 2010 · N826AY · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA200900077Acm · failedON TAXI, ODOR OF SMOKE NOTICED IN CABIN, RETURNED TO BLOCK. AIRCRAFT INSPECTED AND DETERMINED TO BE A FAILED RIGHT AIR CYCLE MACHINE (ACM). DEFERRED PER MEL RETURNED TO SERVICE.Jul 13, 2009 · N826AY · Cndair CL6002B19 · Cabin Cooling SystemSDR REX2009F00016Smoke Detector · false indicationAFTER TAKE OFF RECEIVED LAVATORY SMOKE MSG WITH NO ACTUAL VISUAL SMOKE OR FUMES. TROUBLESHOT LAVATORY SMOKE DETECTION SYSTEM AND DETERMINED TO BE A FALSE SMOKE INDICATION. SYSTEM DEFERRED UNDER MEL 26-16-01.Jan 18, 2009 · N826AY · Cndair CL6002B19 · Smoke DetectionSDR REXA200500131Actuator · failedFLAPS FAIL ON APPROACH WHEN SELECTED TO 30. FOLLOWED QRH, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATORS POSITION 1 AND 2 P/N 852D100-19.Oct 7, 2005 · N826AY · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR REX2005F00042Fcu · failed(REF NR: 05-061) FLAPS FAIL AT ZERO ON CLIMB-OUT. QRH FOLLOWED, EMERGENCY DECLARED RETURNED TO DEPARTURE WITH UNEVENTFUL LANDING. REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT. (FECU) (K)May 6, 2005 · N826AY · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REX2005F00043Bpsu · failed(REF NR: 05-060) FLAP FAIL MESSAGE UPON POWER UP. REMOVED AND REPLACED RT BRAKE POSITION SENSING UNIT (BPSU). (K)May 5, 2005 · N826AY · Cndair CL6002B19 · Trailing Edge Flap Control System
Back to N826AY