N457AW

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 = 'N457AW' 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 A6WA2020041347258Oil System · lowTURBULENCE AP DISENGAGED AND RECIEVED RT OR LF ENGINE OIL LOW PRESS WARNING. CREW UNABLE TO DETERMINE LT OR RT ENGINE. NO EXCENDENCES FOUND IN MAIN DATA COMPUTER "AIRCRAFT REMOVED FROM SERVICE" INTERROGATED MDC NO EXCEEDANCE'S FOUND. RAN BOTH ENGINES WITH CRApr 12, 2020 · N457AW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA2019031846485Mount Bracket · crackedDURING OPS CHECK OF PAX DOOR ASSIST MOTOR FOUND CRACKED AND DISPLACED PULLEY MOUNTING BRACKET.Mar 16, 2019 · N457AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA2019013146348Flap System · malfunctionedON FINAL APPROACH TO LAND, FLAP FAIL CAUTION MESSAGE WHEN FLAPS SELECTED TO 30 DEGREES. FLAPS FAILED IN 20 DEGREE POSITION. COMPLIED WITH QRH.Jan 29, 2019 · N457AW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR A6WA2018121446229Access Panel · corrodedLEFT WING FUEL TANK ACCESS PANEL 540BB HOLE CUT-OUT HAS FRETTING CORROSION AT INBD END MEASURING APPROX. 7" LONG X .10" LONG.Dec 10, 2018 · N457AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA2018120946225Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT BL 0.0, WL 113, 5 INCHES LONG 60% FSH, FAILED NDT INSPECTION. REPAIRED REAR PRESSURE BULKHEAD WEB AT BL 0.0, WL 113.5, IAW REO 601R-53-61-1285.Dec 9, 2018 · N457AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2018120946226Angle · crackedFOUND REAR PRESSURE BULKHEAD Z-MEMBER HAS INDICATION NOTED BL 0.0, WL 113, 1 INCH LONG, 100% FSH, FAILED NDT INSPECTION. REPAIRED REAR PRESSURE BULKHEAD Z-MEMBER AT BL 0.0, WL 113 IAW 601R-53-61-1285, REV E, DATED 2016-10-31.Dec 9, 2018 · N457AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2018120946222Bulkhead · crackedREAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT RBL 18.00 WL75, 4 INCHES LONG 90% FSH, FAILED NDT INSPECTION. REPAIRED DAMAGE TO REAR PRESSURE BULKHEAD WEB AT RBL 18.00, WL 75 IAW REO 601R-53-61-1240 REV D, DATED 2016-10-31 AND REO 601R-53-61-128Dec 8, 2018 · N457AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2018120946224Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 27.50, WL 86, 2 INCHES LONG, 50% FSH, FAILED NDT INSPECTION. REPAIRED REAR PRESSURE BULKHEAD WEB AT LBL 27.50, WL 86, IAW REO 601R-53-61-6793, REV -, DATED 2018-12-07.Dec 8, 2018 · N457AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2018120946223Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT RBL 9.50, WL 75, 5 INCHES LONG, 90% FSH, FAILED NDT. REPAIRED REAR PRESSURE BULKHEAD WEB AT RBL 9.50, WL 75 IAW REO 601R-53-1240, REV D, DATED 2016-10-31 AND REO 601R-53-61-6793, REV E, DATED Dec 8, 2018 · N457AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2018120946213Post · crackedFOUND INDICATION FS 409+128 LBL18 POST AFT FLANGE RADIUS APPROX .250" LONG 65% FSH FAILS NDT.Dec 3, 2018 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018120346213Post · crackedFOUND INDICATION FS 409+128 LBL18 POST AFT FLANGE RADIUS APPROX .250" LONG 65% FSH. FAILS NDT.Dec 3, 2018 · N457AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2018120346206Angle · crackedAFT EQUIPMENT BAY RT FS 621.00 TO 625.00 OBLIQUE ANGLE CRACKED.Dec 2, 2018 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018120346204Fitting · crackedRT FS 484.00 INTERCOSTAL CLIP IS CRACKED.Dec 2, 2018 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018120346203Fitting · crackedFS 484.00 INTERCOSTAL CLIP AT LBL 27.0 IS CRACKED.Dec 2, 2018 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018120346205Fitting · crackedFS 484.00 INTERCOSTAL CLIP AT RBL 27 IS CRACKED.Dec 2, 2018 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018120346201Mount · corrodedLT SIDE WARDROBE FLOOR MOUNT AT FS 310.00 IS CORRODED.Dec 2, 2018 · N457AW · Cndair CL6002B19 · Fuselage, Equipment Attach FittingsSDR A6WA2018120346202Fitting · crackedRT EXHAUST NOZZLE FAIRING (446AL) HAS A CRACKED VENT FITTING.Dec 2, 2018 · N457AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR A6WA2018120346197Fitting · crackedFS 484 INTERCOSTAL CLIP AT LBL 27 IS CRACKED.Nov 30, 2018 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018111246147Rvdt · defectiveIN FLIGHT RECEIVED NWS INOP CAUTION MSG. C/W QRH. MSG PERSISTED SUCCESSFUL LANDING. NWS WORKED UPON LANDING AND TAXIED TO THE GATE. PERFORMED GVI OF NWS HARNESS, NO DEFECTS NOTED. PERFORMED OPS TEST OF NWS WITH TORQUE LINKS DISCONNECTED IAW AMM 32-51-00, OPS TNov 10, 2018 · N457AW · Cndair CL6002B19 · Landing Gear Steering SystemSDR A6WA2018032245713Selector Valve · faultyGEAR DISAGREE WARNING FOR NOSE GEAR DURING RETRACTION. C/W QRH FOR NORMAL LANDING. CHANGED LANDING GEAR SELECTOR VALVE.Mar 20, 2018 · N457AW · Cndair CL6002B19 · Landing Gear SelectorSDR A6WA2018020245603Rvdt · failedNOSE WHEEL STEERING INOPERATIVE CAUTION CAS MESSAGE INFLIGHT. COMPLIED WITH QRH MESSAGE PERSISTED, NO ADDITIONAL RELATED EICAS MESSAGE. COMPLIED WITH FIM RESET MESSAGE PERSISTED. REMOVED AND REPLACED THE LT RVDT IAW 15-177A AND STEERING HARNESS IAW 12-Jan 30, 2018 · N457AW · Cndair CL6002B19 · Steering UnitSDR A6WA2017010944732Flap System · malfunctionedFLAP FAIL CAUTION AT ZERO DEGREES IN LANDING CONFIGURATION, UNEVENTFUL FLAP FAIL LANDING, COMPLIED WITH FLAP RESET PROCEDURE IAW SUPP 98-186 BOX 12 FLAPS RESET.Jan 7, 2017 · N457AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA2016121644666Bpsu · malfunctionedDURING APPROACH, FLAPS FAILED AT 0 DEGREES. PERFORMED QRH AND DIVERTED. NO IMPROPER HANDLE MOVEMENT AND NO ICE ACCUMULATION. REPLACED THE BPSU.Dec 15, 2016 · N457AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA2016121244655Stringer · crackedSTRINGER 3L AT BS 379 IS CRACKED. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06, AND 51-42-21.Dec 9, 2016 · N457AW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR A6WA201644652Stringer · corrodedSTRINGER 24R HAS CORROSION AT BS 303.Dec 8, 2016 · N457AW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR A6WA2016121244653Frame · corrodedBS 310 FRAME FWD FACE HAS CORROSION BETWEEN STRINGERS 23 - 25R.Dec 8, 2016 · N457AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA2016120744641Support Bracket · crackedRIGHT OVERWING PANEL SUPPORT BRACKET IS CRACKED AT BS 449.85.Dec 6, 2016 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2016120744649Attach Angle · crackedRIGHT WING LE TRANSITION PANEL UPPER ATTACH ANGLE CRACKED.Dec 6, 2016 · N457AW · Cndair CL6002B19 · Wing, Attach FittingsSDR A6WA2016120744642Support Bracket · crackedLEFT OVERWING PANEL SUPPORT BRACKET AT BS 477 IS CRACKED.Dec 6, 2016 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2016120744648Fitting · corrodedFLOORBEAM FITTING AT LBL 27, BS 615 CORRODED AT OTBD FLANGE.Dec 6, 2016 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2016120744644Support Bracket · crackedRIGHT OVERWING PANEL SUPPORT BRACKET IS CRACKET AT BS 469.Dec 6, 2016 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2016120744643Support Bracket · crackedLEFT OVERWING PANEL SUPPORT BRACKET IS CRACKED AT BS 449.Dec 6, 2016 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2016120744645Support Bracket · crackedRIGHT OVERWING PANEL SUPPORT BRACKET IS CRACKET AT BS 461.Dec 6, 2016 · N457AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2016120744646Bracket · crackedLEFT OVERWING PANEL SUPPORT BRACKET AT BS 469.0 IS CRACKEDDec 6, 2016 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201644647Stringer Clip · crackedUPPER FUSELAGE STRINGER CLIP 3L IS CRACKED AT BS 280Dec 6, 2016 · N457AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2016120744635Angle · crackedAFT PRESSURE BULKHEAD INTERCOSTAL ANGLE STRINGER 14L, BS 625, LBL 48 IS CRACKED.Dec 5, 2016 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2016120744638Angle · crackedBS 409+128 BL 0 VERTICAL POST LEFT AFT ANGLE IS CRACKED.Dec 5, 2016 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2016120744639Angle · crackedBS 409+128 BL 0 VERTICAL POST RIGHT AFT ANGLE IS CRACKED.Dec 5, 2016 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2016120744633Angle · crackedAFT PRESSURE BULKHEAD INTERCOSTAL ANGLE AT STRINGER 14, BS 625 LBL 52 CRACKED ON OTBD LEG.Dec 5, 2016 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2016120744636Attach Bracket · crackedRIGHT WING LE TRANSITION AREA INBD LE PANEL OTBD ATTACH BRACKET CRACKED.Dec 5, 2016 · N457AW · Cndair CL6002B19 · Wing, Attach FittingsSDR A6WA201644637Attach Bracket · crackedRIGHT WING LE TRANSITION AREA, MID LE PANEL INBD ATTACH BRACKET CRACKEDDec 5, 2016 · N457AW · Cndair CL6002B19 · Wing, Attach FittingsSDR A6WA201644634Structure · crackedAFT PRESSURE BULKHEAD INTERCOSTAL AT STRINGER 13, BS 625 LBL 52 IS CRACKED.Dec 5, 2016 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2016120544629Fitting · crackedWINDSHIELD AFT CENTER POST LOWER RT FITTING AS BL 0 CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-42-21.Dec 4, 2016 · N457AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA2016120544630Cargo Track · corrodedCARGO TRACK SECTION IN CARGO AREA AT LBL 9, BS 559+110 TO 559+122 HAS CORROSION. AFTER BLENDING , THE CARGO TRACK WAS OUT OF LIMITS. REPLACED THE CARGO TRACK IAW AMM 53-00-49.Dec 4, 2016 · N457AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201644628Fitting · crackedWINDSHIELD AFT CENTER POST LOWER LT FITTING AT BL 0 CRACKED IN THE RADIUS. REMOVED AND REPLACED THE FITTING IAW SRM 51-42-21.Dec 4, 2016 · N457AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA201644631Cargo Track · corrodedCARGO TRACK CORRODED, BS 559+110 TO 559+122, RBL9. THE CARGO TRACK WAS BLENDED OUT OF LIMITS IAW SRM 51-21-06, 53-61-49. REPLACED THE CARGO TRACK IAW AMM 53-00-49.Dec 4, 2016 · N457AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2016121244657Angle · corrodedPAX DOOR LOWER SILL ANGLE HAS CORROSION UNDER NUTPLATE LOCATIONS.Dec 3, 2016 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2016120544624Angle · crackedLEFT WINDSHIELD SIDE POST IS CRACKED ON LOWER OB ANGLE. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-21.Dec 3, 2016 · N457AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA2016120544627Cargo Track · corrodedTHE CARGO TRACK SECTION IN CARGO AREA AT LBL 9 AND BS 559+86 TO 559+95 WAS FOUND CORRODED. REMOVED AND REPLACED CARGO TRACK SECTION IAW SRM 51-21-06, 53-61-49, AMM 53-00-49 , AND REO 601R-53-00-485 REV-B.Dec 3, 2016 · N457AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201644623Angle · crackedRIGHT WINDSHIELD SIDE POST LOWER OB ANGLE IS CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-21.Dec 3, 2016 · N457AW · Cndair CL6002B19 · Fuselage Main, Structure
Back to N457AW