N419AW

Service difficulty reports · 178

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 = 'N419AW' 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 A6WA202110297944None · noneWHILE ENROUTE TO KORD THE FLIGHT CREW RECEIVED A NOSE WHEEL STEERING INOP CAUTION MESSAGE. THE CREW FOLLOWED THE QRH AND THE MESSAGE REMAINED. CREW COORDINATED WITH DISPATCH AND ALSO DECLARED AN EMERGENCY WITH ATC. THE CREW CONTINUED TO KORD, LANDED, CONFEROct 29, 2021 · N419AW · Cndair CL6002B19 · Steering UnitSDR A6WA202106087800Seat Track · corrodedSEAT TRACK AT LBL9 FS 349-409+96 CORRODED, R & R SEAT TRACK IAW CRJ-200 AMM 53-01-11 ***AIRCRAFT REMOVED FROM SERVICE*** R & R SEAT TRACK IAW CRJ-200 AMM 53-01-11Jun 6, 2021 · N419AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA202106087799Seat Track · corrodedSEAT TRACK RBL9 FS 349-409+96 CORRODED, REQUIRES REPLACEMENT, R & R SEAT TRACK IAW CRJ -200 AMM 53-01-11 ***AIRCRAFT REMOVED FROM SERVICE*** R & R SEAT TRACK IAW CRJ -200 AMM 53-01-11Jun 6, 2021 · N419AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA202102127629Modulating Valve · malfunctionedWHILE CLIMBING FROM SDF TO INITIAL 10000 FT ALTITUDE RECEIVED WING OVERHEAT WARNING. LFT SIDE. PER QRH TURN WING SWITCH OFF AFTER 40 SEC MESSAGE REMAINED. (MESSAGE IN NORMAL AND STBY. STBY MODE WORKED NORMAL AFTER SECOND ATTEMPT) ***AIRCRAFT REMOVED FROM SERFeb 11, 2021 · N419AW · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR A6WA202011167414Detector · malfunctionedLT 10TH DUCT WARNING MESSAGE ILLUMINATED IN FLIGHT. C/W QRH, MESSAGE PERSISTS. DUCT (10TH) SHOWS RED BETWEEN LT 10TH SOV, PACK NR 1, 10TH ISOL VALVE, AND APU LCV ON ECS SYNOPTIC PAGE. AIRCRAFT REMOVED FROM SERVICE. R & R 10TH STAGE DUCTING LOOP B BLEED AIRNov 12, 2020 · N419AW · Cndair CL6002B19 · Fire Protection SystemSDR A6WA202021247160Controller · malfunctionedSHORTLY AFTER TAKE OFF, THE AIRCRAFT'S AIR DRIVEN GENERATOR DEPLOYED WITHOUT INPUT FROM THE CREW. THE FLIGHT AIR RETURNED TO RIC AS A RESULT. AIRCRAFT REMOVED FROM SERVICE C/W ALT INSP AFTER ADG DEPLOYMENT DURING UNSCHEDULE MX CHECK IAW AWAC SUP 16-172. Feb 9, 2020 · N419AW · Cndair CL6002B19 · AC Generation SystemSDR A6WA2020011447105Pdu · malfunctionedRECEIVED FLAP FAIL CAUTION MESSAGE AT 0 DEGREES WHEN SELECTING 0 TO 8 DEGREES. FOLLOWING LANDING THE FLAPS WERE RESET AND THE SYSTEM WAS PLACED ON MEL FOR 10 DAYS AS REQUIRED BY SUPPLEMENT 98-018G AIRCRAFT REMOVED FROM SERVICE. R/R FLAP PDU IAW AMM 27-52-01 OJan 12, 2020 · N419AW · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR A6WA2019080946786Bulkhead Web · crackedAFT PRESSURE BULKHEAD HAS CRACK AT LBL9.5 , WL75 AT THE BOTTOM OF THE LINER SUPPORT. REPAIRED AFT PRESSURE BULKHEAD IAW REO 601R-53-61-7076 REV--.Aug 9, 2019 · N419AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201908146788Beam · damagedBEAM 601R35050-64 HAS MARKS FROM DOOR CABLE ASSIST. REPLACEDAug 8, 2019 · N419AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA2019080946785Bracket · crackedRIGHT WING I/B LEADING EDGE ATTACH BRACKET IS CRACKED. REPLACED BRACKET IAW SRM 51-41-02.Aug 6, 2019 · N419AW · Cndair CL6002B19 · Wing, Attach FittingsSDR A6WA2019080546781Skin · crackedLEFT TRU SKIN LANDING CRACKED NEAR LATCH. REPAIRED SKIN IAW SUPP. 19-016B.Aug 3, 2019 · N419AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA2019080546778Angle · crackedAFB ANGLE CLIP AT RBL 36.20 CRACKED. REPLACED.Aug 3, 2019 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019080546782Angle · crackedAFT PRESSURE BULKHEAD HAS A CRACKED ANGLE CLIP ST LBL36.20 BY THE 4TH INTERCOSTAL FROM THE FLOOR. REPLACED CLIP IAW CRJ200 SRM 51-42-21.Aug 3, 2019 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019080546779Bracket · crackedPOWER REC PLUG BOX LOWER BRACKET CRACKED. REPLACED.Aug 2, 2019 · N419AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201904156559Warning Message · illuminatedWHEN DE-SELECTING COWL A/ICE AT FL280, LH COWL A/ICE CAUTION WHEN SWITCH IN OFF POSITION. C/W QRH. DIVERTED TO BNAApr 14, 2019 · N419AW · Cndair CL6002B19 · Ice/Rain Protection SystemSDR A6WA2018121746243Unknown · odorCHEMICAL SCENT/LIGHTLY ACRID SMELL OBSERVED IN FLIGHT. ALL OTHER INDICATIONS NORMAL. ONLY OBSERVABLE IN COCKPIT. USING ENGINE AIR.Dec 16, 2018 · N419AW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA201745154Floor Support · corrodedFLOOR SUPPORT BETWEEN LBL27 AND LBL9 HAS CORROSION AT FS621.Aug 3, 2017 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2017080445156Rib · crackedRIGHT PYLON RIB FOWARD LOWER SUPPORT FLANGE CRACKED UNDER PANEL 421ALAug 3, 2017 · N419AW · Cndair CL6002B19 · Nacelle/Pylon, Frame/Spar/RibSDR A6WA201745153Frame · corrodedFRAME AT BS 605 IS CORRODED BETWEEN STRINGERS 20L AND 24L.Aug 3, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA201745155Skin · dentedSKIN DENTED BS 295 - 310, STRINGER 12R - 16RAug 3, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA201745152Door Sill · crackedBAGGAGE LT SILL IS CRACKED AT PREVIOUS CUTOUT AT FS 605.Aug 2, 2017 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2017080345149Floor Support · corrodedRBL27 FLOOR SUPPORT HAS CORROSION FROM BS 559+80 TO 564 AROUND SCREW HOLESAug 1, 2017 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201745147Floor Support · corrodedLEFT CARGO FLOOR SUPPORT FROM BS 568 TO 621 CORRODED.Jul 31, 2017 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201745148Floor Support · corrodedRBL 27 FLOOR SUPPORT BTW BS 574 TO 621 HAS CORROSION AROUND SCREW HOLES.Jul 31, 2017 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2017073145145Floor Support · corrodedRIGHT FLOOR SUPPORT CORRODED BETWEEN BS 349 AND 364.Jul 30, 2017 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2017073145146Crossbeam · corrodedCROSSBEAM BS 349 IS CORRODED AT RBL 42Jul 30, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA2017073145143Bulkhead · crackedAFT PRESSURE BULKHEAD CRACKED AT LBL 18 AND WL 131.Jul 28, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2017073145137Seat Track · corrodedLEFT SEAT TRACK CORRODED FROM BS 409+126 TO 559+4, LBL 9.Jul 21, 2017 · N419AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2017073145136Seat Track · corrodedRIGHT FLOOR SEAT TRACK CORRODED FROM BS 409+128 TO 559+16, STRINGER 17L.Jul 21, 2017 · N419AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2017072545126Attach Bracket · crackedLEFT SIDE OVERWING ACCESS PANEL ATTACH BRACKET CRACKED AT BS 449. REPLACED ATTACH BRACKET IAW SRM 51-42-06, AND 51-42-13.Jul 21, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2017072545128Attach Bracket · crackedRIGHT OVERWING ACCESS PANEL ATTACH BRACKET CRACKED AT BS 449. REPLACED THE ATTACH BRACKET IAW SRM 51-42-06, AND 51-42-13.Jul 21, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2017072545127Attach Bracket · crackedRIGHT SIDE OVERWING EXIT ACCESS PANEL ATTACH BRACKET CRACKED, BS 468. REPLACED BRACKET IAW SRM 51-41-02, 51-42-06, AND 51-42-13.Jul 21, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2017073145144Bulkhead · crackedAFT PRESSURE BULKHEAD CRACKED AT RBL18 AND WL119.Jul 20, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2017071945105Stiffener · crackedLEFT EXHAUST FAIRING CRACKED ON FWD STIFFENER. REPAIRED THE FAIRING IAW CMM 78-11-00-300-810-A01, REPAIR SRS042.Jul 15, 2017 · N419AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR A6WA2017073145138Frame Splice · corrodedCIRCUMFERENTIAL SPLICE JOINT CORRODED BETWEEN STRINGER 26L AND 26R AFT OF FRAME BS 409. REPLACED CIRCUMFERENTIAL JOINT SPLICE IAW SRM 51-40-11, AND 53-21-15.Jul 14, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA201745028Battery Pack · dischargedEMER FLOOR LIGHTING AT ROW 9 AND AFT INOP. R&R BATTERY PACK POSITION 4 IAW AMM 33-51-04. OPS CHECKED GOOD.May 17, 2017 · N419AW · Bombdr CL6002D15 · Emergency LightingSDR A6WA2017021344792Frame · corrodedFRAME BS 310 IS CORRODED BETWEEN STRINGERA 23R AND 23LFeb 10, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA201744793Angle · corrodedREINFORCEMENT ANGLE 600-32002-113 IS CORRODED AT BS 310, STRINGERS 23 AND 24RFeb 10, 2017 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201744794Frame · corrodedFRAME BS 319 CORRODED AT STRINGER 23RFeb 10, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA2017021344791Stringer · corroded1014036-2000-0004 - STRINGER 23R IS CORRODED BETWEEN FS 304 AND FS 327Feb 10, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR A6WA2017021344795Strap · corroded1014036-2000-0012 - SPLICE STRAP UNDER STGR 23R BETWEEN FS 310 AND FS 319 IS CORRODEDFeb 10, 2017 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201744796Frame · corrodedFRAME BS 310 CORRODED, STRINGER 22, AND 23RFeb 10, 2017 · N419AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA2017010944734Altimeter · reads highAT 32,000FT AND 300 KNOTS, CAPTAIN'S ALTIMETER WAS 100FT HIGH, STANDBY WAS 600FT HIGH AND FO'S READ 32,000FT. STANDBY ALTIMETER WAS NOT CLICKING.Jan 8, 2017 · N419AW · Cndair CL6002B19 · Altimeter, Barometric/EncoderSDR A6WA201744724Light · brokenIN CABIN, THE FWD EMERGENCY LIGHT NOT WORKING AND PLASTIC COVER BROKEN ORANGE STRIP LIGHT STICKING UP AND EXPOSED. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-51-01.Jan 3, 2017 · N419AW · Cndair CL6002B19 · Emergency LightingSDR A6WA201643482Unknown · malfunctionedSHORT ERRATIC UNCOMMANDED YAW MOTION, FOLLOWED BY YAW DAMPER 2 INOPERATIVE STATUS MSG. RE-ENGAGED YAW DAMPER 2 & UNCOMMANDED YAW PERSISTED. DISENGAGED BOTH YAW DAMPERS, THE RE-ENGAGED YAW DAMPER 1 ONLY. NO FURTHER UNCOMMANDED YAW.Jan 20, 2016 · N419AW · Cndair CL6002B19 · Autopilot SystemSDR A6WA201543108Handle · damagedSERVICE DOOR WILL NOT OPEN FROM OUTSIDE. REMOVED SERVICE DOOR OUTER HANDLE IAW AMM 52-41-03, FOUND DAMAGE ON HANDLE & HOUSING. REINSTALLED ORIGINAL HANDLE, PLACED ON MEL. REMOVED HANDLE ASSEMBLY & INSPECTED HOUSING IAW AMM 52-41-03 & SUPP 11-029B, NO DEFECTOct 6, 2015 · N419AW · Cndair CL6002B19 · Service DoorsSDR A6WA201542920Beam · corrodedLBL 27 AT FS 621 - 559+112 HAS CORROSION.Jul 10, 2015 · N419AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA201542917Skin · chafedLEFT OTBD FLAP VANE HAS CHAFE.Jul 10, 2015 · N419AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201542914Mount · crackedAEB NR 2 HYD SYS RETURN FILTER MOUNT PLATE HAS CRACK IN AFT LOWER CORNER.Jul 9, 2015 · N419AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201542913Attach Fitting · chafedRIGHT HORIZONTAL STAB SCREW JACK ATTACH FITTING HAS CHAFES & GOUGES ON THE OTBD UPPER FWD & LOWER EDGES.Jul 9, 2015 · N419AW · Cndair CL6002B19 · Horizontal Stabilizer Structure
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