N405AW

Service difficulty reports · 198

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 = 'N405AW' 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 A6WA201308244114Rib · crackedLEFT WHEEL WELL BATTERY RIB DRAG ANGLE IS CRACKED. REMOVED UNSERVICEABLE DRAG ANGLE AND INSTALLED SERVICEABLE DRAG ANGLE ON LT WHEEL WELL BATTERY RIB.Aug 24, 2013 · N405AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA201308224106Floor Support · corrodedRT FLOOR SUPPORT CORRODED FS 621 - 559+96. BLENDED IAW REO 601R-53-00-526, FOUND OUT OF LIMITS. R & R FLOOR SUPPORT.Aug 22, 2013 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201308224101Bracket · crackedRT WINDSHIELD SIDE POST SUPPORT BRACKET IS CRACKED. REPLACE PART.Aug 22, 2013 · N405AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA201308214108Threshold · corrodedSERVICE DOOR THRESHOLD & SHIM ARE CORRODED & UNSERVICEABLE. R & R THRESHOLD PLATE AND SHIM.Aug 21, 2013 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201308214M107Angle · crackedINTERCOSTAL ANGLE CRACKED AT FS 484, RBL 27. REMOVED & REPLACED INTERCOSTAL ANGLE.Aug 21, 2013 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201308204105Seat Track · corrodedCORRODED SEAT TRACK AT RBL 9, FS 559+80. REMOVED AND REPLACED NEW SEAT TRACK.Aug 20, 2013 · N405AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201307264025Bpsu · failedFLAPS FAIL CAUTION MESSAGE, RESET IAW SUPP 98-018F, FLAPS FAILED DURING 4TH CYCLE OF FLAPS . R & R RT BPSU IAW AMM 27-51-10. OPS CHECKED GOOD.Jul 25, 2013 · N405AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA201211184000Engine · malfunctionedAT 12,000 FEET IN CRUISE AIRCRAFT STARTED TO VIBRATE WITH INCREASING FREQUENCY AND INTENSITY OVER A PERIOD OF APPROXIMATELY 5-10 SECONDS, FOLLOWED BY UNCOMMANDED ENGINE SHUTDOWN. NO INDICATION OF A FIRE OR OVERTEMP. DIVERTED TO CAE. SINGLE ENGINE LANDING WANov 18, 2012 · N405AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA20121011508Ballast · malfunctionedLAV BURNING SMELL NOTICED. REMOVED AND REPLACED BALLAST ASSY AND ALL LAMPS. ALSO REPAIRED GROUND TERM. SYS TEST OK PER AMM 33-25-07. NO SMELL AFTER TEST.Oct 11, 2012 · N405AW · Cndair CL6002B19 · Passenger Compartment LightingSDR A6WA20121011507Power Unit · faultySTRONG BURNING SMELL EMITTING IN REAR OF A/C STRONGEST NEAR LAV. FOUND LAV LIGHT POWER UNIT BURNT. REMOVED AND REPLACED POWER UNIT REF CRJ AMM 33-25-07. OPS CHECKS GOOD AT THIS TIME. STRONG SMELL DISSIPATED.Oct 9, 2012 · N405AW · Cndair CL6002B19 · Passenger Compartment LightingSDR A6WA201140813Skin · chafedLT INBD FLAP VANE L/E IS CHAFED IN 3 PLACES. REPAIRED IAW REO 601R-57-52-004.Aug 24, 2011 · N405AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201140815Skin · chafedRT INBD FLAP VANE L/E ARE CHAFED IN 3 PLACES. REPAIRED IAW REO 601R-57-52-004.Aug 24, 2011 · N405AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201140804Bracket · chafedBRACKET APPROX FS 559+112 RT SIDE, JUST AFT OF SIDE SEAT RAIL HAS A HOLE CHAFED THROUGH. R & R BRACKET FS 559.0+112 RT SIDE, AFT OF SIDE SEAT RAIL IAW SRM 51-11-20.Aug 17, 2011 · N405AW · Cndair CL6002B19 · Fuselage, Equipment Attach FittingsSDR A6WA201140809Attach Fitting · brokenATTACH FITTING BROKEN FOR 10TH STAGE BLEED LINE ON ENG BEAM RT SIDE TOP. R & R FITTING IAW SRM 51-42-11.Aug 17, 2011 · N405AW · Cndair CL6002B19 · Fuselage, Equipment Attach FittingsSDR A6WA201140819Angle · wornDIVIDER GUIDE ON PANEL 422BT WORN. R & R DIVIDER GUIDE ANGLE WITH SERVICEABLE PN 601-37003-184 IAW SRM 51-42-06.Aug 16, 2011 · N405AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA201140803Intercostal · dentedCARGO BEAM INTERCOSTAL AT LBL 27 BETWEEN BS 589-605, DENTED. R & R INTERCOSTAL IAW SRM.Aug 16, 2011 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201140806Bulkhead · chafedBULKHEAD BS 280 AFT SIDE IS CHAFED, RT SIDE BEHIND GALLEY. REPAIRED CHAFE DAMAGE ON 280 IAW 601R-53-11-1727.Aug 16, 2011 · N405AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201140805Cargo Track · corrodedCARGO TRACK CORRODED TO CONTAIN EXFOLIATION CORROSION AROUND COUNTERSUNK SCREWS. R & R WITH SERVICEABLE CARGO TRACK.Aug 15, 2011 · N405AW · Cndair CL6002B19 · Fuselage, Equipment Attach FittingsSDR A6WA201140802Seat Track · corrodedRT NR 4 FLOOR SEAT TRACK CORRODED. R & R SEAT TRACK.Aug 12, 2011 · N405AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201140817Intercostal · crackedCRACKED INTERCOSTAL IN PAX DOOR PANEL 832BR AREA. REMOVED CRACKED PAX DOOR INTERCOSTAL AT 832 BR PANEL THEN INSTALLED NEW INTERCOSTAL AT 832 PANEL IAW SRM 51-40-11, 51-42-06.Aug 10, 2011 · N405AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140811Structure · chafedRT ENGINE LOWER NOSE COWL AFT EDGE IS KNIFE EDGED. R & R AFT EDGE STRIP IAW CMM 71-14-01, REPAIR.Aug 10, 2011 · N405AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201140808Seat Track · corrodedLT NR1 SEAT TRACK HAS CORROSION AT FWD EDGE. R & R WITH A SERVICEABLE SEAT TRACK PIECE. LOCATED AND INSTALLED.Aug 10, 2011 · N405AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201140807Seat Track · corrodedRT SEAT TRACK HAS EXFOLIATION CORROSION AT FWD EDGE. REMOVED UNSERVICEABLE RT SEAT TRACK, FABRICATED, LOCATED AND INSTALLED REPLACEMENT SEAT TRACK, STOCK PN N126-2075.Aug 10, 2011 · N405AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201140810Angle · crackedLEFT BS 621 OBLIQUE ANGLE CRACKED, R & R.Aug 9, 2011 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201140801Hinge · gougedPAX DOOR HINGE HALF MOUNTED FUSELAGE HAS SEVERAL GOUGES. BLENDED GOUGES ON PAX DOOR HINGE HALF OF FUSELAGE IAW SRM 51-12-00 FOUND TO BE WITHIN LIMITS IAW REO 601R-53-21-814.Aug 8, 2011 · N405AW · Cndair CL6002B19 · Fuselage, Door HingeSDR A6WA201140816Skin · chafedRT AILERON LWR FIXED L/E INBD END IS CHAFED. REPAIRED IAW REO 601R-57-60-020.Aug 8, 2011 · N405AW · Cndair CL6002B19 · AileronsSDR A6WA201140743Bulkhead · crackedFS 202, BULKHEAD CRACKED AT PARKING BRAKE CABLE HOLE. REPAIRED FS 202 BULKHEAD CRACK AT PARKING BRAKE CABLE HOLE BY FULLY INCORPORATING REO 601R-53-11-563, REV A.Aug 8, 2011 · N405AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201140814Skin · chafedLT AILERON UPPER AND LOWER L/E SKIN IS CHAFED BY THE RUB SEALS. BLENDED OUT MINOR CHAFTING TO UPPER AND LOWER AILERON L/E IAW REO 601R-52-60-013 AND SRM 51-12-00. RESTORED FINISH BY ALODINE IAW SRM 51-21-11, FR PRIME IAW SRM 51-25-06 AND TOP COAT IAW SRM 51-Aug 6, 2011 · N405AW · Cndair CL6002B19 · AileronsSDR A6WA201140818Intercostal · crackedCRACKED INTERCOSTAL IN UPPER PAX DOOR NEAR HINGE IN AREA OF PANEL 832GL. GL THEN LOCATED AND INSTALLED NEW SERVICEABLE INTERCOSTAL. REMOVED CRACKED INTERCOSTAL IN UPPER FWD AREA AT PANEL 832.Aug 6, 2011 · N405AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140812Stiffener · crackedRT JET PIPE FAIRING HAS CRACKED STIFFENER. REMOVED UNSERVICEABLE STIFFENER ON RT JET PIPE FAIRING IAW CMM 20-421-06. LOCATED AND DRILLED SERVICEABLE STIFFENER IAW CMM 20-40-11 INSTALLED SERVICEABLE STIFFENER ON RT JET PIPE IAW CMM 20-42-06.Aug 5, 2011 · N405AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR A6WA201140039Warning Message · illuminatedRT STATIC HEAT MSG RECEIVED IN FLIGHT, C/W`D QRH AND MESSAGE REMAINED. PERFORMED RESET PROCEDURE IAW FIM 30-30-00. OPS CK GOOD.Jan 7, 2011 · N405AW · Cndair CL6002B19 · Pitot/Static Anti-Ice SystemSDR A6WA201040935Control Column · bindingAILERONS BINDING AND AUDIBLE SNAP SOUND DURING FLIGHT CONTROL CHECK. BOTH CONTROL COLUMNS AND BOTH DIRECTIONS. LT COLUMN BINDING AT LT DEFLECTION, RT COLUMN BINDING MID AND 1/2 DEFLECTION. C/W PARA 4 OF GREO 601R-27-11-031 "DISPOSITION FOR ACFT DISPATCH. RDec 8, 2010 · N405AW · Cndair CL6002B19 · Control Column SectionSDR A6WA201040580Warning Message · activatedAFTER LANDING, AC BUSS 1 FAILED FOLLOWED BY AC AUTO TRANSFER FAIL FOLLOWED BY ALL ASSOCIATED NR 1 AC BUSS SYSTEM FAILUE MESSAGES. CHECKED ALL CONTACTORS-NO LOOSE WIRES. C/W OPS CKS OF A/C GENERATORS SYS IAW AMM 24-20-00, OPS CK GOOD.Aug 4, 2010 · N405AW · Cndair CL6002B19 · AC Generation SystemSDR A6WA201040541None · noneFLIGHT CONTROLS FELT VERY "MUSHY" WITH A LOT OF SLACK BETWEEN YOKE INPUTS AND PLANE REACTION. UNRESPONSIVENESS OCCURRED IN BOTH PITCH AND ROLL INPUTS FROM BOTH CAPTAINS AND F/O YOKES. INSPECTED FLT CONTROL SYS IAW 27-31-00. NO FAULTS FOUND ALL WORK DONE ON Jul 25, 2010 · N405AW · Cndair CL6002B19 · Flight Control SystemSDR A6WA2010410387Display · failedWALKED ONTO ACFT, BATTERY SWITCH WAS ON. COCKPIT SMELLED OF ELECTRONICS OVERHEATING AND RED DISPLAY MESSAGE SAYING " DISPLAY TEMP" ON ED1 AND ED2 ILLUMINATED. IMMEDIATELY SHUT BATTERY OFF. R & R EFD3 AND EFD4 IAW AMM 31-61-01. OPS CK GOOD.May 27, 2010 · N405AW · Cndair CL6002B19 · Central ComputersSDR A6WA201040387Battery · activatedWALKED ONTO ACFT, BATTERY SWITCH WAS ON. COCKPIT SMELLED OF ELECTRONICS OVERHEATING AND RED DISPLAY MESSAGE SAYING "DISPLAY TEMP" ON ED1 AND ED2 ILLUMINATED. IMMEDIATELY SHUT BATTERY OFF. OPENMay 27, 2010 · N405AW · Cndair CL6002B19 · Battery/Charger SystemSDR A6WA201040343O-Ring · leakingAT CRUISE, LOW OIL PRESS MASTER WARNING MSG C/W QRH. LT ENG AT IDLE, OIL PRESS APPROX 30 PSI. REPLACED OUTER O-RING ON LT IDG CARBON SEAL AND CARBON SEAL IAW SUP 05-018C & AMM 24-11-01 REF W/C NR 2 FOR LEAK CHECK.May 7, 2010 · N405AW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA201040279Wire Harness · defectiveRT MAIN GEAR DISAGREE WARNING AFT TAKEOFF. RT MLG DID NOT RETRACT, COMPLIED WITH QRH. WO NR 153271, CARDS 1-6 AND 13-18. R & R RT INBD MLG HARNESS IAW SUPP 09 062B ALSO FOUND RT MLG UPLOCK TAT LOOSE RESECURED 32 32. OPS CHECK GOOD.Apr 7, 2010 · N405AW · Cndair CL6002B19 · Landing Gear System WiringSDR A6WA200940698Unknown · malfunctionedPRESSURIZATION PROBLEM. RAPID DEPRESSURIZATION, CAUSING FIRST A CABIN PRESSURE CAUTION FOLLOWED BY A CABIN PRESSURE WARNING IN RAPID SUCCESSION.Oct 25, 2009 · N405AW · Cndair CL6002B19 · Cabin Pressure Control SystemSDR A6WA200940783Angle · crackedPRESSURE BULKHEAD CAP ANGLE IS CRACKED IN THE RADIUS. FS 559, RBL 18. CRACK LENGTH IS .350" ANDWEB CRACKED AT FS 669 BTWN RBL 9 TO 18 CRACK LENGTH .520:. PRESSURE BULKHEAD STRUCTURE FS 559, RBL 9 TO RBL 18. REPAIRED IAW REO 601R-53-41-260, REV C AND REO 6Oct 20, 2009 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940595Skin · corrodedCORROSION ON INTERNAL SURFACE OF LT WING L/E 520ML. CORROSION REMOVED IAW SRM 51-21-06 ON L/E 520ML. (K)Sep 18, 2009 · N405AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA299040585Vane · dentedDENT ON LT WING, INBD FLAP VANE L/E BTWN WS 75.27 TO WS 97.70 LT WING, INBD FLAP VANE L/E REPAIRED IAW SRM 57-52-00, PAGE 201. DUE TO DENT FOUND OUT OF LIMITSIAW SRM 57-52-00, FIG 101 (PAGE 102) REPAIR NR 01. (K)Sep 16, 2009 · N405AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200940576Skin · damagedRT HORIZONTAL STAB L/E DAMAGED BY FOD AT RBL 18.91. CRACK LENGTH 0.500", SKIN DEPRESSION: 0.250" RT HORIZ STAB L/E REPAIRED IAW SRM 55-12-01, PAGE 201 TO 206. (K)Sep 15, 2009 · N405AW · Cndair CL6002B19 · Horizontal Stabilizer, Plate/SkinSDR A6WA200940583Skin · corrodedCORROSION FOUND ON SKIN AT MANY PLACES BTWN FS 280.00 AND FS 559+80 AND BTWN LT AND RT STRINGER 6. CORROSION REMOVED IAW SRM 51-21-06. (K)Sep 15, 2009 · N405AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200940593Sill · corrodedCORROSION ON LWR SILL ANGLE OF SERVICE DOOR SURROUND BTWN FS 319 TO FS 349.00 AND STR 18 SERVICE DOOR SURROUND, LWR SILL ANGLE PN 601R38303-253. REPLACED IAW SRM 51-42-06 AND SRM 51-42-21. (K)Sep 14, 2009 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940581Housing · crackedMAIN AVIONICS COMPARTMENT DOOR, HANDLE HOUSING CRACKED. HANDLE HOUSING REPLACED IAW SRM 51-42-06.Sep 14, 2009 · N405AW · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR A6WA200940594Crossbeam · corrodedCORROSION ON UPPER FLANGE OF CROSSBEAM AT FS 349 AND RBL 45. CORROSION REMOVED IAW REO 601R-53-21-1047.Sep 11, 2009 · N405AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA200940587Fitting · crackedCRACK ON REAR PRESSURE BULKHEAD WEB AT LINTEL FITTING CRACK LENGTH .500. REAR PRESSURE BULKHEAD WEB AT LINTEL FITTING REPAIRED IAW REO 601R-53-61-1230, REV D. (K)Sep 11, 2009 · N405AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200940575Intercostal · crackedINTERCOSTAL FS 484 UNDERFLOOR CRACKED AT RBL 27 AND RBL 36. (CRACK LENGTH 0.500") INTERCOSTAL FS 484 UNDER FLOOR AT RBL 27 AND RBL 36 REAPIRED IAW REO 601R-53-41-059, REV A. (K)Sep 11, 2009 · N405AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940577Rib · corrodedRT WING OTBD RIB AFT UPPER FLANGE VIA PANEL 640BT FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-2006. (K)Sep 10, 2009 · N405AW · Cndair CL6002B19 · Wing, Rib/Bulkhead
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