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 A6WA201140014Plate · corrodedLT PYLON T/E UPPER BONDING PLATES (2 EA) CORRODED. R & R LT PYLON T/E UPPER BONDING PLATES PN 601-37012-33 IAW SRM.Dec 15, 2010 · N457AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201040956Hinge Fitting · nickedUPPER CTR RUDDER HINGE PITTING ARM ON VERTICAL STAB HAS MINOR NICK ON AFT EDGE. REPAIRED IAW REO 601R-55-31-204.Dec 15, 2010 · N457AW · Cndair CL6002B19 · Rudder StructureSDR A6WA201140021Riser · crackedPAX DOOR SECOND STEP RISER AFT SIDE HAS CRACK NEAR RADIUS. REPAIRED STEP AFT SIDE IAW REO 601R-52-11-702.Dec 13, 2010 · N457AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140013Seat Track · corrodedRT SIDEWALL SEAT TRACK HAS MINOR CORROSION BETWEEN FS364 AND FS394. REMOVED UNSERVICEABLE SEAT TRACK FROM RT SIDEWALL BETWEEN FS364 AND FS394. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11.Dec 13, 2010 · N457AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201040957Skin · gougedSERVICE DOOR EXTERIOR HANDLE CUT OUT HAS 5 SMALL AREAS WITH MINOR DAMAGE. REPAIRED SERVICE DOOR SKIN AND DOUBLER AROUND EXTERIOR HANDLE CUT OUT IAW REO 601R-52-41-159, DATED 2010-12-12.Dec 13, 2010 · N457AW · Cndair CL6002B19 · Galley DoorsSDR A6WA201040933Angle · crackedFS 625 RT, LT OBLIQUE ANGLES ARE CRACKED, W/L 97.50, STRINGER 13 LWR B/L47, L/R CRACK IN ANGLE .7500 INCH LON EACH ONE. REMOVED DAMAGED OBLIQUE LT AND RT ANGLE FS625 IAW REO 601R-53-61-985 AND SRM 51-40-11, MATCHED DRILL 3 EA NEW ANGLES PN 601-35012-51, 601-3Dec 12, 2010 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040931Structure · nickedAVIONIC BAY DOOR HANDLE C/O HAS AN AREA WITH SMALL NICK. REPAIR IAW REO 601R-52-42-019.Dec 12, 2010 · N457AW · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR A6WA201040930Skin · dentedRT INBD GROUND SPOILER INBD LOWER SKIN HAS MULTIPLE SMALL DENTS. REPAIR IAW REO 601R-57-71-241.Dec 12, 2010 · N457AW · Cndair CL6002B19 · SpoilersSDR A6WA201040928Panel · chafedLT AILERON L/E PANEL 599BB HAS CHAFE DAMAGE. BLENDED DAMAGED AREA IAW REO 601R-57-60-020, REV NV AND WAS TO BE WITHIN ALLOWABLE LIMITS.Dec 10, 2010 · N457AW · Cndair CL6002B19 · AileronsSDR A6WA201140020Hinge · chafedSERVICE DOOR HINGE ASSY IS CHAFED. REMOVED CHAFED SERVICE DOOR HINGE PANEL AND INSTALLED NEW PANEL IAW SRM 51-24-36.Dec 9, 2010 · N457AW · Cndair CL6002B19 · Fuselage, Door HingeSDR A6WA201040927Track · nickedCARGO BAY AFT OTBD DOOR GUIDE TRACK HAS NICK IN TRACK ASSY. BLENDED DAMAGED AREA IAW REO 601R-53-62-024.Dec 9, 2010 · N457AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201140011Seat Track · corrodedLT SIDE SEAT RAIL HAS CORROSION FROM APPROX FS559+48 TO FS559+64. REMOVED UNSERVICEABLE LT SEAT RAIL OBTAINED SEAT TRACK FROM BULK STOCK N126-2075 INSTALLED LT SEAT RAIL PN N126-2075.Dec 8, 2010 · N457AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201140012Angle · damagedPAX DOOR RAIN GUTTER IS BENT AND DEFORMED. R & R PAX DOOR RAIN GUTTER IAW SRM 51-42-06.Dec 7, 2010 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040932Structure · nickedCARGO BAY DOOR HANDLE C/O HAS 2 AREAS WITH MINOR NICKS. REPAIRED CARGO DOOR HANDLE C/O IAW REO 601R-52-31-086.Dec 6, 2010 · N457AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA201140019Skin · chafedLT MLG DOOR L/E HAS CHAFING DAMAGE 2 PLACES BLENDED UPPER DAMAGED AREA AND WAS FOUND TO BE WITHIN ALLOWABLE LIMITS MATERIAL LOSS .025 AND .030 IS ALLOWABLE IAW REO 601R-52-82-033 REV A LOWER DAMAGED AREA. R & R 1 PREVIOUSLY INSTALLED ON REO 601R-52-82-034, REDec 3, 2010 · N457AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201140018Rib · crackedLT BATT RIB IS CRACKED IN LT WHEEL WELL. REPAIRED LT BATT RIB IAW REO 601R-57-51-046, REPAIR NR 2.Dec 3, 2010 · N457AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA201140008Seat Track · corrodedSEAT TRACK SECTION BETWEEN FS559+96 THRU 559+112, RBL 9 IS CORRODED. REMOVED UNSERVICEABLE SEAT TRACK REPLACED FOR NEW SERVICEABLE SEAT TRACK PN 601R38779-13 ON SECTION BETWEEN FS559+96 THRU 559+112, RBL9.Dec 3, 2010 · N457AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201140009Connector · corrodedCONNECTOR HAS CORROSION. NOTED AT CONNECTION OF GROUNDS N3597, N3598, N3599. REPAIRED IAW REO 601R-53-21-1214.Dec 3, 2010 · N457AW · Cndair CL6002B19 · Electrical Power System WiringSDR A6WA201040926Rib · crackedRT BATT RIB IS CRACKED. REPAIR RT BATT AT WS 53.60 IAW REO 601R-57-51-046, REV B, REPAIR NR 2.Dec 3, 2010 · N457AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA201040900Seat Track · corrodedFLOOR SEAT TRACKS CORRODED RBL9 AND LBL9 FS574 IN CARGO. R & R SERVICEABLE SEAT TRACK PN N126-2075 AT FS 574 IN CARGO RBL9 & LBL9 IAW AMM 53-01-11.Dec 3, 2010 · N457AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201040882Bulkhead · chafedFS280 BULKHEAD CHAFED AT RBL 11 BETWEEN BULKHEAD STR 13A AND 14A. REPAIR IAW REO 601R-53-11-1729.Dec 3, 2010 · N457AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201040881Attach Angle · crackedFS 484 INTERCOSTAL CLIPS CRACKED AT RBL 27 AND 36. REPAIR IAW REO 601R-53-41-059 AND SRM 51-24-21.Dec 3, 2010 · N457AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201040885Skin · chafedRT MLG DOOR HAS CHAFING DAMAGE IN 2 PLACES. REPAIRED RT MLG DOOR CHAFE SPOTS 2EA, 1ST SPOT ON FWD LOWER CORNER REMOVED, FABRICATED AND INSTALLED NEW REPAIR FILLER IAW REO 601R-52-82-016, REV NC 2ND SPOT, FWD EDGE 11 INCHES FROM BOTTOM EDGE, BLENDED THE SPOT BDec 3, 2010 · N457AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201140015Fitting · chafedLT OTBD FLAP, FLAP ROLLER GUIDE FITTING CHAFED. BLENDED CHAFED AREA AT LT OTBD FLAP GUIDE FITTING, REMOVING .022 OF MATERIAL WITHIN LIMITS IAW REO 601R-57-51-143.Dec 2, 2010 · N457AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201140017Cam · deformedRT OTBD FLAP VANE CAM FOLLOWER BEHIND CTR HINGE HAS DISPLACED METAL. REPAIRED TR OTBD FLAP VANE CAM FOLLOWER BY FEATHERING THE MUSHROOMED EDGE OF CAM FOLLOWER IAW SRM 51-12-00 AND REO 601R-57-53-19, REV D.Dec 2, 2010 · N457AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201140010Pressure Blkhd · gougedCARGO PRESSURE BULKHEAD HAS GOUGE ON FS 621.00 LT FWD SIDE MARKED C/W REO 601R/53-61-2155, REV.Dec 2, 2010 · N457AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201040961Fitting · chafedOTBD FLAP ROLLER GUIDE FITTING (RT SIDE) HAS CHAFING DAMAGE, BLENDED CHAFED AREA AT RT OTBD FLAP GUIDE FITTING, REMOVING .028 OF MATERIAL WITHIN LIMITS IAW REO 601R-57-51-1453.Dec 2, 2010 · N457AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040884Skin · chafedLT INBD FLAP, FLAP VANE HAS (3 EA) AREAS ON L/E WITH CHAFE DAMAGE WHERE VANE CONTACTS STOPS. REPAIRED CHAFED AREAS IAW REO 601R-57-52-004.Dec 2, 2010 · N457AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040883Heat Shield · detachedAFT APU EXHAUST HEAT SHIELD HAS (2 EA) SCREWS PULLED THRU SHIELD. REPAIRED HEAT SHIELD IAW REO 601R-49-81-051.Dec 2, 2010 · N457AW · Cndair CL6002B19 · APU Cowling/ContainmentSDR A6WA201040386Smoke Detector · malfunctionedPERSIST SMOKE TOILE CAUTION MSG INCRUISE FLIGHT, C/W QRH, UPON LANDING AIRPORT RESC FIREFIGHTING CONDUCTED THERMAL INSP FWD NO SIGNS OF FIRE. R & R LAVATORY SMOKE DETECTOR IAW AMM 26-16-01. OPS CHECK GOOD, CLEARS PLACARD AND MEL. ACCOMPLISHED LAV SECURITY IMay 26, 2010 · N457AW · Cndair CL6002B19 · Smoke DetectionSDR A6WA201040396Fairing · crackedLT UPPER STANG FAIRING CRCKED PN 228-50253-805 LT ENG R & R LT UPPER STANG FAIRING IAW SRM 51-41-02.May 11, 2010 · N457AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201040344Bulkhead · crackedCRACK FOUND AT FS 559, LBL9 INBD POST FROM BOTTOM RIVET TO EDGE OF CHANNEL. REPAIRED FS 559, IAW REO 601R-53-41-260, REV D AND REO 601R-53-41-609, REV B DEVIATION "E".May 11, 2010 · N457AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2010410342Bracket · brokenBONDING JUMPER ATTACH CLIP BROKEN ON LT INBD FLAP HINGE ARM. REMOVED BROKEN BONDING JUMPER BRACKET AND REPLACED WITH NEW BONDING JUMPER BRACKET IAW SRM 51-42-00.May 9, 2010 · N457AW · Cndair CL6002B19 · Wing, Attach FittingsSDR A6WA200940205Pump · malfunctionedAFTER SELECTING GEAR UP, RECEIVED GEAR DISAGREE RED MSG AND GEAR DISAGREE AURAL WARNING APPROX 10 SECONDS AFTER UP SELECTION, ALSO RECEIVED NOSE DOOR RED MSG ALONG WITH NOSE DOOR AURAL WARNING. NOSE GEAR DID NOT RETRACT. C/Q`D QRH, PERFORMED ALTERNATE GEAR EApr 6, 2009 · N457AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA200940072Idg · malfunctionedABORTED TAKEOFF AT 20 KNOTS FOR IDG CAUTION MESSAGE. REMOVED AND REPLACED NR 1 IDG IAW AMM 24-11-01 AND TEMP REV 24-146. OPS CHECK GOOD AT THIS TIME. REMOVED PLACARD AND REMOVED FROM MEL. (K)Feb 15, 2009 · N457AW · Cndair CL6002B19 · AC Generator-AlternatorSDR A6WA200940050Support Bracket · crackedRT ENGINE TAIL PIPE FIRE LOOP CONNECTOR SUPPORT BRACKET CRACKED. RT ENGINE TAIL PIPE FIRE LOOP BRACKET SUPPORT FABRICATED IAW CRJ 200 SRM 51-24-16 AND INSTALLED EAW CRJ 200 SRM 57-42-06.Jan 15, 2009 · N457AW · Cndair CL6002B19 · Fire DetectionSDR A6WA200940049Handle · corrodedCREW ESCAPE HATCH FAILED FUNCTIONAL TEST DUE TO OUTER HANDLE DOES NOT EJECT WHEN TRIGGER PLATE IS PUSHED. AFTER INVESTIGATION OUTER HANDLE FOUND CORRODED. OUTER HANDLE REPLACED.Jan 12, 2009 · N457AW · Cndair CL6002B19 · Emergency ExitsSDR A6WA200940032Crossbeam · crackedCROSSBEAM AT FS 280.00, BL 9.00 IS CRACKED IN THE LWR RADIUS. CRACK MEASURES 2.00 INCH LONG. CROSSBEAM AT FS 280.00, BL 9.00 REPAIRED IAW REO 601R-53-11-171, REV D. (K)Jan 12, 2009 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940031Floor Support · crackedINBD FLOOR SUPPORT ANGLE AT FS 280.00, RBL 9.00 IS CRACKED. DIMENSION OF CRACK IS .300 INCH LONG INBD FLOOR ANGLE AT FS 280.00, RBL 9.00 INSTALLED IAW SRM 51-42-06 AND SRM 51-42-71. (K)Jan 9, 2009 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940008Floorbeam · crackedINBD AND OTBD FLOOR SUPPORT ANGLE AT FS 280.00 LBL 9.00 ARE CRACKED DIMENSION OF CRACKS ARE .300 FT INBD, .200 INCH OTBD. INBD AND OTBD FLOOR SUPPORT ANGLE AT FS 280.00, LBL 9.00 INSTALLED IAW SRM 51-42-06 AND SRM 51-42-21. (K)Jan 8, 2009 · N457AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200940033Angle · cracked131193-64 CRACK FOUND ON LWR ANGLE OF CARGO DOOR BEAM FS 621. LWR ANGLE OF CARGO DOOR BEAM FS 621 REPLACED IAW SRM 51-42-20. (K)Jan 6, 2009 · N457AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA200940030Angle · crackedCRACK FOUND ON LWR ANGLE OF CARGO DOOR BEAM FS621. LWR ANGLE OF CARGO DOOR BEAM FS 621 REPLACED IAW SRM 51-42-20. (K)Jan 6, 2009 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940029Bulkhead · crackedAFT PRESSURE BULKHEAD CRACK AT LINTEL LOCATION, CRACK LENGTH .500 AFT PRESSURE BULKHEAD AT LINTEL LOCATION. REPAIR CARRIED OUT IAW REO 601R-53-61-1230 REV D. (K)Jan 6, 2009 · N457AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA20090018Bulkhead · crackedCRACK FOUND ON PRESSURE BULKHEAD, FS 202.75, LBL 23.71 AT PARKING BRAKE LOCATION. PRESSURE BULKHEAD FS 202.75, LBL 23.71 AT PARKING BREAK. REPAIRED IAW REO 601R-53-11-563. (K)Jan 6, 2009 · N457AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940028Panel · crackedPAX DOOR FWD SIDE PANEL CRACK 1 IN AT ZONE 2 IAW REO 601R-52-11-702. PAX DOOR FWD SIDE PANEL CRACK 1 IN AT ZONE 2 REPAIRED IAW REO 601R-52-11-702. (K)Jan 5, 2009 · N457AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200940027Panel · crackedPAX DOOR AFT SIDE PANEL CRACK 1 IN AT ZONE 2 IAW REO 601R-52-11-702. PAX DOOR AFT SIDE PANEL CRACK 1 ON OF ZONE 2, REPAIRED IAW REO 601R-52-11-702. (K)Jan 5, 2009 · N457AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200940007Angle · crackedCRACK FOUND ON ANGLE OF PAX DOOR FIXED STAIR RETAINING MOTOR ASSIST DOOR, UPPER ANGLE MOTOR ASSIST DOOR RETAINING UPPER ANGLE REPLACED IAW SRM 51-42-06. (K)Jan 5, 2009 · N457AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200840590Oil System · fluctuatesON REACHING CRUISE ALTITUDE, EICAS SHOWN RT ENGINE OIL LOP MASTER WARNING OIL PRESSURE FLUX BETWEEN 38-53 PSI UNTIL JUST BEFORE LANDING WHEN AGAIN RECEIVED RT ENGINE LOP. CORRECTIVE ACTION IN PROGRESS. (K)Sep 18, 2008 · N457AW · Cndair CL6002B19 · Engine Oil PressureSDR A6WA200740357Actuator · inoperativeELEVATOR STIFF DURING FLIGHT CONTROL CHECK. REMOVED AND REPLACED PITCH FEEL LINEAR ACTUATOR NR 2, DUE LOW INPUT IMPEDANCE. (K)Jun 24, 2007 · N457AW · Cndair CL6002B19 · Elevator Tab Control SystemSDR A6WA200740210Skin · dentedBIRD STRIKE ON SHORT FINAL DENT FOUND ON LOWER LEFT INBOARD FLAP SKIN. MAINTENANCE PERFORMED A MAJOR REPAIR TO LT INBOARD FLAP LOWER SKIN BY INSTALLING A 10 INCH BY 9.25 INCH EXTERNAL REPAIR DOUBLER IAW BSC EO 601R-57-11408B. (M)Apr 9, 2007 · N457AW · Cndair CL6002B19 · Trailing Edge Flaps
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