N509AE

Service difficulty reports · 217

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 = 'N509AE' 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 VNAA2020040899910Seat Track · corrodedRH SIDE SEAT TRACK FROM APPROX FS 708 TO FS 761 HAS MULTIPLE AREAS OF CORROSION.Apr 8, 2020 · N509AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202004089999Seat Track · corrodedRH SIDE SEAT TRACK FROM APPROX FS 661 - FS 708 HAS MULTIPLE AREAS OF CORROSION. REPLACED SEAT TRACKApr 8, 2020 · N509AE · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202004089998Seat Track · corrodedRH SIDE SEAT TRACK FROM APPROX FS 565 - FS 661 HAS MULTIPLE AREAS OF CORROSION.Apr 8, 2020 · N509AE · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202004089997Frame · corrodedFRAME 409 IS CORRODED AT STR 27.Apr 8, 2020 · N509AE · Bombdr CL6002D15 · Fuselage Main, FrameSDR VNAA202004089996Frame · corrodedFRAME 333 IS CORRODED BETWEEN STR25R AND STR24R. REPLACED FRAME 333.Apr 8, 2020 · N509AE · Bombdr CL6002D15 · Fuselage Main, FrameSDR VNAA202004089995Stringer · corrodedSTR24L IS CORRODED BETWEEN FS347 AND FS379.Apr 8, 2020 · N509AE · Bombdr CL6002D15 · Fuselage Main, Longeron/StringerSDR VNAA202004089994Frame · corrodedFRAME 295 IS CORRODED BETWEEN STR23R AND STR26L. REPLACED FRAME295.Apr 8, 2020 · N509AE · Bombdr CL6002D15 · Fuselage Main, FrameSDR VNAA202004089993Stringer · corrodedSTR26R IS CORRODED BETWEEN FS295 AND FS310. REPLACED STRINGER 26R.Apr 8, 2020 · N509AE · Bombdr CL6002D15 · Fuselage Main, Longeron/StringerSDR VNAA202004089992Stringer · corrodedSTR 26L IS CORRODED BETWEEN FRAMES 421 AND437. REPLACED STRINGER 26L.Apr 8, 2020 · N509AE · Bombdr CL6002D15 · Fuselage Main, Longeron/StringerSDR VNAA202004089991Support Angle · corrodedFS 280 AVIONICS FLOOR BOARD SUPPORT ANGLE IS CORRODED. REPLACED SUPPORT ANGLE.Apr 8, 2020 · N509AE · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA2019112861101Battery Pack · dischargedEMERGENCY BATTERIES LEFT ON ALL NIGHT. REMOVED AND REPLACED EPSU BATTERY PACK IAW CRJ 700 AMM. OPS CHECK GOOD AT THIS TIME / #1 POWER SUPPLY BATTERY P/N AD2013-1A S/N 231815, #2 BATTERY P/N 2013-1A S/N 104602, #3 BATTERY P/N AD2013-1A S/N 68782, #4 BATTERY 2Nov 26, 2019 · N509AE · Cndair CL6002C10 · Emergency LightingSDR VNAA2019090511101Warning System · false activationDURING CLIMB OUT OF HPN THE CREW RECEIVED A NOSE WHEEL STEERING INOP CAUTION MESSAGE. UPON ARRIVE INTO CLT THE CREW DECLARED AN EMERGENCY AND TRUCK ROLLED. THE AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE. B1 CODE 007464. PERFORMED SYSTEM RESET. PROBLEM DISep 5, 2019 · N509AE · Cndair CL6002C10 · Landing Gear Steering SystemSDR VNAA2019080111102Warning Message · false activationCREW RECEIVED A NOSE WHEEL STEERING INOPERATIVE CAUTION MESSAGE. CREW CYCLED SYSTEM CIRCUIT BREAKERS. MSG CLEARED.Jul 31, 2019 · N509AE · Cndair CL6002C10 · Landing Gear Steering SystemSDR VNAA2019071511102Warning System · false activationCREW REPORTED RECEIVING A STEERING INOP CAUTION MSG JUST AFTER TAKEOFF. RAN THEIR QRH AND COULD NOT GET THE MESSAGE TO CLEAR. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO PHL FOR THE LONG RUNWAY. ON ARRIVAL THE CREW HAD THE CABIN PREPARED FOR AN EMERGENCYJul 15, 2019 · N509AE · Cndair CL6002B19 · Landing Gear Steering SystemSDR VNAA20190310111Drain · contaminatedON TAKEOFF ROLL, STALL FAIL CAUTION AND RUD LIMIT FAULT STATUS MSG PERFORMED INSP AND DRAIN MOISTURE ON STANDBY PITOT/STATIC DRAIN ASSY "P3" IAW AMM 34-11-00-220-801. OPS CHECK GOOD. NO FURTHER DEFECT NOTED AT THIS TIME.Mar 10, 2019 · N509AE · Cndair CL6002C10 · Pitot/Static SystemSDR VNAA2019021111101Unknown · odorOIL SMELL IN COCKPIT AND CABIN ON TAKE-OFF AND DECENT WITH APU OFF. INSPECTED AFT EQUIPMENT BAY AND DUCTING, NO DEFECTS FOUND. RAN BOTH ENGINES, NO SMELLS DETECTED. AIRCRAFT RETURNED TO SERVICE.Feb 11, 2019 · N509AE · Cndair CL6002C10 · Air Distribution SystemSDR VNAA2019010111102Loop · out of positionTHE AIRCRAFT REPORTED A RIGHT BLEED DUCT WARNING FOLLOWED BY A BLEED DUCT CAUTION. THE AIR CONDITIONING PACKS AUTO SHUTDOWN THEN THE CREW RECEIVED A CABIN ALT CAUTION MESSAGE. THE OXYGEN MASKS DEPLOYED WITH PASSENGER USE. MAINTENANCE INSPECTED THE LOOPS AND INDec 28, 2018 · N509AE · Cndair CL6002C10 · Pneumatic Indicating SystemSDR VNAA2018010399911Floor Support · crackedLEFT AND RIGHT COCKPIT FLOOR SUPPORT ANGLES CRACKED. REMOVED AND INSTALLED THE FLOOR SUPPORT ANGLES.Jan 3, 2018 · N509AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2018010399910Floorbeam · crackedBS 280 LBL AND RBL 9 FLOORBEAM CRACKED. REPLACED THE FLOORBEAM ANGLE.Jan 3, 2018 · N509AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2018010399909Floorbeam · corrodedRIGHT FLOORBEAML AT BS 280 HAS CORROSION. REPLACED THE FLOORBEAM ANGLE.Jan 3, 2018 · N509AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2018010399908Frame · corrodedFUSELAGE FRAME BS 349 IS CORRODED BETWEEN STRINGERS 26L AND 26R. REPLACED THE FRAME SECTION.Jan 3, 2018 · N509AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2018010399907Seat Track · corrodedRH SIDE SEAT TRACK DAMAGED AT BS 436 - 872. REPLACED THE SEAT TRACK.Jan 3, 2018 · N509AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018010399906Seat Track · corrodedLEFT SEAT TRACK HAS DAMAGE AT BS 403 - 936. REPLACED THE SEAT TRACKJan 3, 2018 · N509AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018010399905Floorbeam · corrodedFLOORBEAM CAP CORRODED IN AFT BAGGAGE BAY AT BS 1031, LBL 27. REPLACED THE FLOORBEAM.Jan 3, 2018 · N509AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2018010399904Floorbeam · crackedBS 280 FLOORBEAM IS CRACKED AT RBL 13. PERFORMED SB670BA-53-041, REV C.Jan 3, 2018 · N509AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2018010399903Angle · corrodedJ-ANGLE IS CORRODED AT BS 280 BETWEEN LBL 12 AND RBL 12. PERFORMED SB670BA-53-041 REV C.Jan 3, 2018 · N509AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2018010399902Bulkhead Web · corrodedBS 280 RT BULKHEAD WEB IS CORRODED ON AFT FACE AT WL 73.5, RBL 14. REPAIRED THE BULKHEAD WEB IAW SRM 63-11-10-201-004-A01.Jan 3, 2018 · N509AE · Cndair CL6002C10 · Fuselage Main, BulkheadSDR VNAA2018010399901Floorbeam · corrodedBS 280 FLOORBEAM IS CORRODED ALONG TOP AT MULTIPLE AREAS. PERFORMED SB 670BA-53-041, REV C.Jan 3, 2018 · N509AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2017111211102Gcu · failedFLIGHT CREW REPORTED AC ESSENTIAL BUSS CAUTION MESSAGE AND A GENERATOR 1 FAULT IN FLIGHT. CREW RAN QRH AND ATTEMPTED TO START APU WHICH TOOK THREE ATTEMPTS. FLT DIVERTED AND DECLARED EMERGENCY. LANDED SAFELY. REPLACED APU GCU AND K117. OPS CHECKED GOOD.Nov 12, 2017 · N509AE · Cndair CL6002C10 · AC Generator-AlternatorSDR VNAA2017012100028Retainer · damagedPASSENGER DOOR SEAL RETAINER DAMAGED. REMOVED AND REPLACED SEAL RETAINER.Jan 21, 2017 · N509AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2016091700021Warning Message · illuminatedINBOARD FLIGHT SPOILER, INBOARD SPOILERON CAUTION MESSAGES. MAINTENANCE COMPLIED WITH SYSTEM RESET. MESSAGE SHOULD NOT APPEAR AGAIN. AIRCRAFT RELEASED FOR SERVICE.Sep 17, 2016 · N509AE · Cndair CL6002C10 · Drag Control SystemSDR VNAA2016091100008Retaining Ring · not seatedLT ENGINE VIBE OF 4.7 AND AN INTENTIONAL ENGINE SHUTDOWN AFTER TAKEOFF. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FORWARD BLIND CAP, RETAINING RING, AFT SPINNER AND FORWARD SPINNER, AND PSep 11, 2016 · N509AE · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR VNAA2016081700017Control Quadrant · bindingAUTO PILOT, RT WING DOWN CAUTION MESSAGE IN FLIGHT. THE CREW CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. THE ACFT WAS FERRIED TO A REPAIR FACILITY. MAINTENANCE TROUBLESHOT, R & R THE RT FEEL UNIT QUADRANT AND PERFORMED CHECKS IAW THE AMM. THE ACFTAug 17, 2016 · N509AE · Cndair CL6002C10 · Flight Control SystemSDR VNAA2016050400003Frame · corrodedFRAME IS CORRODED FS 549 BELOW WL 72.5 WHERE THE FLOORBEAM ATTACHES AT THE LT SIDE. MAINTENANCE REPARED FRAME SECTOR AT FS 549 IAW REO 670-53-31-364 REV DATED 2016-04-14.May 4, 2016 · N509AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2016050400002Frame · corrodedFRAME IS CORRODED AT FS 565 BELOW WL 72.5 WHERE THE FLOORBEAM ATTACHES AT THE LT SIDE. MAINTENANCE REPAIRED FRAME SECTOR AT FS 565 IAW REO 670-53-31-364, REV.May 4, 2016 · N509AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2016050400001Mount · corrodedPASSENGER DOOR LOWER SILL ANGLE MOUNT STRUCTURE IS CORRODED WITH FILAFORM CORROSION. MAINTENANCE R & R PASSENGER DOOR LOWER SILL ANGLE MOUNT STRUCTURE AND CAP ANGLES IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-77-00-001-001May 4, 2016 · N509AE · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR VNAA2016020700012Filter · warning messageCREW REPORTED RECEIVING A DISPLAY COOL FAIL MESSAGE WHEN CLIMBING TO FL190. THE CREW INITIATED EMERGENCY PROCEDURES AND DIVERTED TO NEAREST FIELD. THE CREW LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REPLACED FLIGHT COMPARTMENT FILTER AND PERFORMED CHFeb 7, 2016 · N509AE · Cndair CL6002C10 · Cabin Cooling SystemSDR VNAA2016020700011Flow Sensor · malfunctionedCREW REPORTED RECEIVING A DISPLAY COOL FAIL MESSAGE WHEN CLIMBING TO FL190. THE CREW INITIATED EMERGENCY PROCEDURES AND DIVERTED TO NEAREST FIELD. THE CREW LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REPLACED THE LOW FLOW SENSOR AND PERFORMED CHECKS IAFeb 7, 2016 · N509AE · Cndair CL6002C10 · Instrument PanelSDR VNAA2015081200024Unknown · smokeDURING ENGINE START, CREW REPORTED SMOKE HAZE IN CABIN WITH A BURNING ODOR. RETURNED TO GATE. MAINTENANCE RAN BOTH PACKS HOT AND COLD IN ALL BLEED CONFIGURATIONS AND PERFORMED OPS CHECKS IAW AMM. OPS CHECK GOOD. COULD NOT DUPLICATE DISCREPANCY. ACFT RELEAAug 12, 2015 · N509AE · Cndair CL6002C10 · Air Distribution SystemSDR SIMA20150604003Skin · dentedRIGHT WING INBD FLAP LOWER SURFACE HAS A DENT, ONE FOOT FROM INBD EDGE. COMPLIED WITH ERS-CR-57MR-449.Jun 4, 2015 · N509AE · Cndair CL6002C10 · Trailing Edge FlapsSDR SIMA20150525006Web · corrodedMAIN AVIONICS UNDERFLOOR DOOR SURROUND LT WEB BETWEEN FS 349.00 & 364.00 IS CORRODED ON THE INBD & OTBD SIDES. INSTALLED WEB IAW SRM 51-42-06, 51--42-13 & 51-42-21.May 25, 2015 · N509AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20150525007Web · corrodedMAIN AVIONICS UNDERFLOOR DOOR SURROUND RT WEB BETWEEN FS 349.00 & 364.00 IS CORRODED ON THE INBD & OTBD SIDES. INSTALLED WEB IAW SRM 51-42-06, 51--42-13 & 51-42-21.May 25, 2015 · N509AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20150521011Structure · crackedFORWARD EQUIP BAY FLOOR CRACKED AT THE RT AFT CORNER. REPAIRED IAW ETN-CR-53-099.May 21, 2015 · N509AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20150521012Bracket · crackedRIGHT WING ANTI-ICE TELESCOPIC DUCT CLOSING PLATE HAS LOOSE MOUNT SCREWS & IS CRACKED 1/4 INCH. R & R RT WING ANTI-ICE TELESCOPIC DUCT PLATE INTERNAL BRACKET IAW SRM 51-42-00.May 21, 2015 · N509AE · Cndair CL6002C10 · Airfoil Anti/De-ice SystemSDR SIMA20150521013Structure · crackedFORWARD EQUIP BAY FLOOR CRACKED AT THE LT CORNER UNDER THE ADG PUMP. REPAIRED FWD EQUIP BAY FLOOR IAW ETN-CR-53-099.May 21, 2015 · N509AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20150519019Light · inoperativeGALLEY G2 LOWER EMER SIGN LIGHT BULB BURNT OUT. R & R BULBS. OPERATIONS CHECKED GOOD IAW MM 33-51-00.May 19, 2015 · N509AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20150519018Intercostal · corrodedINTERCOSTAL AT FS 333 TO 349 IS CORRODED AT STRINGER 21L. INSTALLED NEW SERVICEABLE INTERCOSTAL AT FS 333.00 TO FS 349.00 AT STRINGER 21L IAW SRM 51-42-06.May 19, 2015 · N509AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20150519017Light · inoperativeEXTERIOR EMER LIGHTS INOPERATIVE ON LT SIDE SECOND ONE PAST OVERWING EMER EXIT LOOKING AFT & RT SIDE FIRST ON PAST OVERWING EMER EXIT LOOKING AFT. R & R 2 EA EXTERIOR EMER LIGHTS. LT SIDE SECOND ONE PAST OVERWING EMER EXIT LOOKING AFT & RT SIDE FIRST ONE PASMay 19, 2015 · N509AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20150519016Light · inoperativeEMERGENCY LIGHT ON GALLEY 1 LOWER CORNER HAS 2 BURNT OUT LIGHTS. R & R GALLEY 1 LOWER CORNER EMER LIGHT BULBS IAW MM 33-51-05.May 19, 2015 · N509AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20150519015Angle · crackedRIGHT ANGLE AT BL 9.04 IS CRACKED AT FS 280.00. FABRICATED NEW ANGLES & SHIM. INSTALLED IAW SRM 53-11-41.May 19, 2015 · N509AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
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