N431AW

Service difficulty reports · 254

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 = 'N431AW' 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 A6WA201240230Door · crackedAPU ENCLOSURE BOX HAS MULTIPLE CRACKS AND APU ENCLOSURE BOX DOOR HAS CRACKED. REPAIRED IAW REO 601R-49-11-070, REV A.Jan 16, 2012 · N431AW · Cndair CL6002B19 · Auxiliary Power Unit (APU) DoorsSDR A6WA201240226Attach Bracket · crackedCARGO TRACK FWD LOWER ATTACH BRACKET CRACKED. R & R ATTACH BRACKET IAW SRM 57-42-06, 51-40-11.Jan 14, 2012 · N431AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201240239Rib · crackedLEFT AND RIGHT RIBS ARE CRACKED. REPAIRED LT AND RT BATT RIBS IAW REO 601R-57-51-016.Jan 14, 2012 · N431AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA201240224Seat Track · corrodedRT NR 3 SEAT TRACK CORRODED AT FS 409.00+112-FS 559.00+16. BLENDED CORRODED AREA ON RT NR 3 SEAT TRACK DAMAGE FOUND TO BE OUT OF LIMITS, IAW SRM 51-21-49. REMOVED UNSERVICEABLE SEAT TRACK IAW SRM 51-41-00. FABRICATED SERVICEABLE SEAT TRACK.Jan 13, 2012 · N431AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201240233Angle · crackedLEFT WING AT WS 143.189, INBD ANGLE IS CRACKED UNDER PANEL 520ML. R & R IAW SRM 51-41-02.Jan 12, 2012 · N431AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR A6WA201240240Mount · brokenRT STUB FAIRING FWD MOUNT LOOP BROKEN. R & R IAW SRM 51-42-21.Jan 12, 2012 · N431AW · Cndair CL6002B19 · Horizontal Stabilizer StructureSDR A6WA201240059Vane · chafedLT INBD FLAP VANE HAS 3 CHAFES. BLENDED DAMAGED AREAS IAW REO 601R-57-52-004.Jan 12, 2012 · N431AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201240058Vane · chafedRT INBD FLAP VANE IS CHAFED IN 3 PLACES. BLENDED RT INBD FLAP VANE IN 3 AREAS IAW REO 601R-57-52-004.Jan 12, 2012 · N431AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201240062Cleat · corrodedPAX DOOR CLEAT (AFT) CORRODED BEYOND SERVICEABLE LIMITS IAW SRM 53-00-00. INSTALLED SERVICEABLE PAX DOOR CLEAT IAW SRM 51-42-06 & 52-42-21.Jan 12, 2012 · N431AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201240063Fairing · chafedRT STUB FAIRING CHAFED & GOUGED FROM FLAP. BLENDE CHAFED AREA ON RT STUB FAIRING IAW REO 601R-53-82-003 & SRM 51-12-00 TO WITHIN ALLOWABLE LIMITS.Jan 12, 2012 · N431AW · Cndair CL6002B19 · Horizontal Stabilizer StructureSDR A6WA201240061Support · gougedRT FRAME SUPPORT AT FS 700 AT AEB DOOR OPENING IS GOUGED INSIDE AEB COMPARTMENT. BLENDED DAMAGED AREA TO A SMOOTH PROFILE.Jan 12, 2012 · N431AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240242Housing · gougedCARGO DOOR OUTER HANDLE HOUSING GUGED IN MULTIPLE. REPAIRED IAW REO 601R-52-31-086.Jan 11, 2012 · N431AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA201240065Panel · chafedRT WING AILERON PANEL 699BB IS CHAFING. REPAIRED RT WING AILERON PANEL 699BB IAW SRM 51-12-00 AND SRM 57-60-00.Jan 11, 2012 · N431AW · Cndair CL6002B19 · AileronsSDR A6WA201240068Hinge · gougedPAX DOOR HINGE (DOOR SIDE) HAS GOUGED LUGS NR6 & NR13. BLENDED DOOR HINGE ON NR 6 AND NR 13 LUGS IAW REO 601R-52-11-1347, ORIG MAT .110". REMOVED .002" WITH .108 MAT REMAINING ON NR6 LUG, NR13 LUG, ORIG MAT .113". REMOVED .002 MAT WITH .111 MAT REMAINING, BJan 11, 2012 · N431AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201240066Skin · chafedRT WING AILERON PANEL 699CB IS CHAFING. REPAIRED RT WING AILERON PANEL 699CB IAW SRM 51-12-00 AND SRM 57-60-00.Jan 11, 2012 · N431AW · Cndair CL6002B19 · AileronsSDR A6WA201240067Drag Angle · crackedAFT DRAG ANGLE ON PAX DOOR CRACKED ABOVE DOOR ASSIST PULLEY BRACKET. REPAIRED AFT DRAG ANGLE ON PAX DOOR IAW REO 601R-52-11-513.Jan 11, 2012 · N431AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040962Wire · sparksWHILE GETTING DE-ICED, PILOTS HEARD STRANGE SOUND IN COCKPIT, GOT UP FROM SEAT, SAW WIRES FROM CB PANEL 2 GLOWING AND SPARKING. HAD F/O TURN NR 2 GEN OFF, SELECTED AUTO TRANSFER SWITCH OFF, GRABBED COCKPIT FIRE EXTINGUISHER, PUT GLOWING AND SPARKED WIRES (REFDec 16, 2010 · N431AW · Cndair CL6002B19 · Electrical Power System WiringSDR A6WA201040811Sensor · shorted"ANTI-ICE DUCT" WARNING MESSAGE INFLIGHT. SYNOPTIC PAGE SHOWED RT WING RED. C/W QRH AND MESSAGE CLEARED. FOUND SHORT TO GROUND ON RT WING OTBD L/E SENSOR S28WK. REPLACED TEMP SENSOR IAW AMM 36-21-03. OPS TEST GOOD AT THIS TIME.Nov 4, 2010 · N431AW · Cndair CL6002B19 · Pneumatic Indicating SystemSDR A6WA201040816Sensor · malfunctionedANTI-ICE DUCT WARNING MESSAGE INFLIGHT. SYNOPTIC PAGE SHOWED RT WING RED. COMPLIED WITH QRH AND MESSAGE CLEARED. FOUND SHORT TO GROUND ON RT WING OTBD L/E SENSOR S28WK. REPLACED TEMP SENSOR IAW AMM 36-21-03. OPS TEST GOOD AT THIS TIME.Nov 4, 2010 · N431AW · Cndair CL6002B19 · Pneumatic Indicating SystemSDR A6WA201040528Fitting · misalignedRT ELEVATOR INDICATES HALF SCALE PITCH DOWN. INSTALLED NEW LOCK FASTENER IN LOWER POSITION ON AFT ACTUATOR FITTING ASSY, ON ELEVATOR RT SIDE IAW DWG NR 601R-24-05-6.Jul 11, 2010 · N431AW · Cndair CL6002B19 · Elevator StructureSDR A6WA201040398Structure · damagedACFT RT WING TIP STRUCK WING OF PARKED ACFT DURING TAXI. R & R RT WINGLET AFT/FWD SPAR CHANNEL REF DWG NR 600-15108, SRM 51-42-2, 51-42-26, 51-40-11 AND DWG NR 600-15102.May 31, 2010 · N431AW · Cndair CL6002B19 · Wing Main, Frame StructureSDR A6WA201040163Seat Track · damagedDOUBLE DRILLED HOLE ON PILOT SEAT TRACK INBD TRACK COMPLIED WITH REPAIR OF DOUBLE DRILLED HOLE ON PILOT INBD SEAT TRACK IAW DWG CAS-CRJ-534702.Feb 17, 2010 · N431AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201040134Angle · corrodedSERVICE DOOR THRESHOLD ANGLE CORRODED. R & R THRESHOLD ANGLE IAW SRM 51-24-16, 51-42-21, 51-42-13.Feb 17, 2010 · N431AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040119Bulkhead · crackedFS 202.75 PRESSURE BULKHEAD CRACKED AT BRAKE CABLE PASS THROUGH. REPAIRED FS 202.75 PRESSURE BULKHEAD IAW REO 601R53-11-563.Feb 15, 2010 · N431AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201040135Bulkhead · damagedFS559 PRESSURE BULKHEAD REG`S REO 601R-53-41-260. REPAIRED FS559.00 IAW REO 601R-53-41-260.Feb 14, 2010 · N431AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201040122Floorbeam · cracked280 AFT FLOOR SUPPORT ANGLE CRACKED LBL 9 REPAIRED IAW REO 601R-53-11-138.Feb 12, 2010 · N431AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201040118Seal · damagedLT JET PIPE UPPER AND LOWER SEALS REQUIRE REPLACEMENT. R & R UNSERVICEABLE SEALS ON LT JET PIPE UPPER AND LOWER IAW CMM 78-11-00.Feb 12, 2010 · N431AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR A6WA201040117Rib · corrodedCORROSION ON RT WING OTBD L/E WHERE PICCOLO TUBE ATTACHES. R & R UNSERVICEABLE RIB PN 601R12063.Feb 12, 2010 · N431AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA201040222Floorbeam · crackedMWC 51552-2000-0130 FS 280 FLOOR SUPPORT CRACKED AT RBL 9. COMPLIED WITH REO 601R-53-11-1842.Feb 11, 2010 · N431AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201040121Attach Fitting · crackedFS 280, RBL 9 OTBD ATTACH CLIP CRACKED. REMOVED DAMAGED CLIP. DUPLICATED PART, AND INSTALLED NEW SERVICEABLE CLIP.Feb 11, 2010 · N431AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201040120Floorbeam · crackedFS280, RBL 9 INBD CLIP CRACKED. REMOVED DAMAGED CLIP, DUPLICATED PART AND INSTALLED NEW SERVICEABLE CLIP.Feb 11, 2010 · N431AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201040104Stiffener · damagedVERTICAL STIFFENER AT RBL 18 HAS DRILL START DAMAGED DUMMY 621 MOD REPAIRED IAW REO NR 601R53-61-3529, REV A.Feb 10, 2010 · N431AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040103Panel · crackedREPAIR CRACK ON PAX DOOR TOP PANEL UNDER TOP STEP AFT SIDE AND REQUIRED. REMOVED DAMAGED PAX DOOR EDGE MEMBER UNDER TOP STEP AND INSTALL SERVICEABLE EDGE MEMBER IAW SRM 51-42-06.Feb 10, 2010 · N431AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040102Angle · corrodedPAX DOOR FWD INNER AND OUTER CORNER ANGLES AND DATUM 8 CORRODED. R & R FWD INNER AND OUTER CORNER ANGLES IAW SRM 51-42-06 AND 51-42-21.Feb 9, 2010 · N431AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040101Angle · corrodedPAX DOOR AFT INNER AND OUTER CORNER ANGLES AT DATUM 8 CORRODED. R & R AFT INNER AND OUTER CORNER ANGLES IAW SRM 51-42-06 AND 51-42-21.Feb 9, 2010 · N431AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040100Floorbeam · crackedFITTING AT RBL 10, FS 461.0, ON FLOOR SUPPORT BEAM CRACKED (BATH TUB) PN 600-31068-19. R & R FITTING IAW SRM.Feb 7, 2010 · N431AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201040098Floorbeam · crackedFS 280 FLOOR SUPPORT CRACKED AT LBL 9 AT ALT RELEASE CABLE MOUNT BRACKET. PERMANENT REPAIR INCORPORATED IAW GENERIC REO 601R-53-11-171, REV D.Feb 5, 2010 · N431AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201040097Floorbeam · crackedFLOORBOARD SUPPORT (OTBD) ANGLE CRACKED ATTACHED TO FS 280 FRAME AT LBL 9. FABRICATED NEW CLIP AND INSTALLED IAW REO 601R-53-11-171, REV D.Feb 5, 2010 · N431AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201040096Attach Fitting · crackedFS 280, LBL 9, INBD CLIP CRACKED. FABRICATED NEW CLIP AND INSTALLED IAW REO 601R-53-11-171 REV D.Feb 5, 2010 · N431AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201040095Bulkhead · damagedWHILE REMOVING BRACKET IN LT WW FOR 559 REPAIR, FOUND PREVIOUS DOUBLE DRILLED HOLES UNDER BRACKET. 2 EA DOUBLE DRILLED HOLES LT WHEEL WELL AT FS 559, BL 18.00. REPAIRED BY PO NR 961789.Feb 5, 2010 · N431AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201040226Angle · corrodedPAX DOOR FS 320.163 AT DATUM 8 INBD & OTBD ANGLES ARE CORRODED. R & R INBD AND OTBD ANGLES IAW SRM 51-42-06, 51-42-13, 51-42-21.Feb 4, 2010 · N431AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040225Angle · corrodedPAX DOOR FS 329.503 AT DATUM 8 ANGLE IS CORRODED. R & R ANGLE IAW SRM 51-42-06, 51-42-13 & 51-42-21.Feb 4, 2010 · N431AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040224Angle · corrodedPAX DOOR FS 338.968 AT DATUM 8 INBD AND OTBD ANGLES ARE CORRODED. R & R INBD & OTBD ANGLES IAW SRM 51-42-06, 51-42-13, 51-42-21.Feb 4, 2010 · N431AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040099Attach Fitting · crackedRT INBD FS 484, RBL 27 CLIP CRACKED. REPAIRED IAW REO 601R-53-41-059 REV A.Feb 3, 2010 · N431AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201040221Floorbeam · crackedFLOOR SUPPORT AT FS 621 LT END CRACKED AT PREVIOUS REPAIR. (LBL 36) REPLACED FILLER IAW REO 601R-53-61-117.Feb 2, 2010 · N431AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201040223Skin · gougedLT WING OTBD L/E INNER SKIN AT INBD END GOUGED. TRIMMED EDGE IAW SRM 57-00-31.Feb 2, 2010 · N431AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA201040094Skin · crackedINNER SKIN OF RT OTBD WING L/E CRACKED. REPLACED WEB IAW SRM 51-42-10.Feb 2, 2010 · N431AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA201040093Attach Angle · crackedCENTER L/E ON RT WING INBD ATTACH FLANGE CRACKED. R & R ANGLE IAW SRM.Feb 2, 2010 · N431AW · Cndair CL6002B19 · Wing, Attach FittingsSDR A6WA201040092Frame · crackedPAX DOOR UPPER FRAME CRACKED AT FS 338.90. REPAIR IAW REO 601R-52-11-402.Feb 2, 2010 · N431AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040091Attach Fitting · crackedINTERCOSTAL CLIP CRACKED AT FS 484, RBL 36 REPAIRED IAW REO 601R-53-41-059.Feb 2, 2010 · N431AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
Back to N431AW