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 A6WA200740182Angle · cracked625 OBLIQUE ANGLE CRACKED IN RADIUS APPROX 1.0 INCH LONG, RT SIDE. (K) [SUP 5-1-07] MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE P/N 601-35012-52, IAW CRJ SRM 51-42-06. (M)Apr 3, 2007 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740181Angle · cracked625 OBLIQUE ANGLE CRACKED IN RADIUS APPROX 1.0 INCH LONG, LT SIDE. (K) [SUP 05-09-07] MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE, P/N 601-35012-51, IAW CRJ SRM 51-42-06. (M)Apr 3, 2007 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA207740179Support Fitting · crackedPAX - DOOR ASSIST MOTOR SUPPORT FITTING (PN 601R317745-7) CRACKED APPROX .2 INCH LONG. MAINTENANCE TRIMMED OUT CRACKED IAW BSC EO 601R-52-11427. (M)Apr 1, 2007 · N457AW · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR A6WA200740180Drag Angle · crackedPASSENGER DOOR AFT DRAG ANGLE CRACKED APPROX 1.5 INCH LONG. (K) [SUP 05-09-07] MAINTENANCE CUTOUT DAMAGED SECTION AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R-53-11-513 REV A. (M)Apr 1, 2007 · N457AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740179Attach Fitting · crackedPAX DOOR ASSIST MOTOR SUPPORT FITTING (PN 601R317745-7) CRACKED APPROX .2 INCHES LONG. (K)Apr 1, 2007 · N457AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740178Intercostal · crackedRT FS 484.0 INTERCOSTAL CRACKED AT RBL 36.0 APPROX .1 INCH LONG AT FLOOR SUPPORT BEAM. (K) [SUP 5-9-07] MAINTENANCE CUT OUT DAMAGED FLANGE AND INSTALLED REPAIR FLANGE IAW BOMBARDIER REO 601R-53-41-059 REV A AND BSC SR 601R-53-0030A. (M)Mar 31, 2007 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740177Intercostal · crackedLT FS 484.0 INTERCOSTAL CRACKED AT LBL 36.0 APPROX .1 INCH LONG AT FLOOR SUPPORT BEAM. (K) [SUP 05-09-07] MAINTENANCE CUT OUT DAMAGED FLANGE AND INSTALLED REPAIR FLANGE IAW BOMBARDIER REO 601R-53-41-059 REV A AND BSC SR 601R-53-0030A. (M)Mar 31, 2007 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740176Angle · crackedLT FS 484.0 ANGLE AT LBL 27.0 CRACKED APPROX .1 INCH LONG AT FLOOR SUPPORT BEAM. (K) [SUP 05-09-07] MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R-54-41-059 REV A AND BSC SR 601R-53-0029B. (M)Mar 31, 2007 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740175Floor Support · crackedLT FS 621.0 FLOOR SUPPORT ANGLE CRACKED APPROX .3 INCH LONG. (K) [SUP 05-01-07] MAINTENANCE CUT AWAY CRACKED ANGLE AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R-53-61-117 REV C. (M)Mar 31, 2007 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740174Floor Support · crackedRT FS 621.0 FLOOR SUPPORT ANGLE CRACKED APPROX.3 INCH LONG. (K) [SUP 05-01-07] MAINTENANCE CUT AWAY CRACKED ANGLE AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R-53-61-117 REV C. (M)Mar 31, 2007 · N457AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740173Skin · corrodedWING PLANK AT WS 54.897 HAS SEVERAL PITS ON AFT EDGE THE DEEPEST IS .005 INCH. (K) [SUP 05-01-07] MAINTENANCE REMOVED CORROSION AND REPAIRED AREA IAW REO 601R-57-21-030. (M)Mar 30, 2007 · N457AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200640004Windshield · failedLT WINDSHIELD CENTER PANE SHATTERED AT FL320 UNDER NORMAL FLIGHT CONDITIONS. REMOVED AND REPLACED LT WINDSHIELD. OPS CHECK GOOD. (K)Jan 9, 2006 · N457AW · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA200540360Windshield · crackedFO`S A WINDSHIELD CRACKED AT FLT LEVEL 350. REMOVED AND REPLACED WINDSHIELD IAW AMM, PRESSURE CHECK GOOD. WINDSHIELD HEAT CHECK GOOD. (K)Dec 26, 2005 · N457AW · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA200540241Engine · odorINFLIGHT DETECTED OILY ODOR AFTER BLEED AIR CHANGE OVER FROM APU TO ENGINE AIR IN COCKPIT. FERRIED FOR ENGINE NR 1 CHANGE. (K) REMOVED AND REPLACED COALESCER SOCKS IN LEFT AND RIGHT WATER SEPARATORS, NO FURTHER ODOR NOTED. (M)Jul 13, 2005 · N457AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA200540171Skin Panel · dentedREPAIR DENT IN FUSELAGE SKIN AT FS 202.75 STRINGER 13R. REMOVED SKIN PANEL 601R33010-26 ON RT SIDE OF AIRCRAFT FS 202.75, STRINGER 13R, AND INSTALLED NEW SKIN PANEL 601R33010-26 IAW CRJ200FRM 51-42-06, 51-42-13, 51-42-21 AND CRJ 200 AMM 51-23-00 AND DRAWING 6Apr 17, 2005 · N457AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200440046Line · leakingAT FL310, STRONG ODOR OF JET FUEL FUMES, FLIGHT ATTENDANT ALSO HAD SAME SMELL FROM ROW 2 FORWARD TO GALLEY. NO ODOR AT REAR OF CABIN, DESCENDED TO FL280, SAME ODOR, DESCENDED TO FL240 ODOR WENT AWAY. IN DESCENT CENTER TANK QTY FLUCTUATING BETWEEN 0-20 LBS. Apr 17, 2004 · N457AW · Cndair CL6002B19 · APU Engine Fuel and ControlSDR A6WA200340155Odor · detectedAIRCRAFT HAS PETROLEUM ODOR. ACCOMPLISHED PACK BURN. COULD NOT DETECT ANY ODORS AT THIS TIME. (M)Oct 30, 2003 · N457AW · Cndair CL6002B19 · Air Distribution System
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