N464AW

Service difficulty reports · 216

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 = 'N464AW' 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 A6WA20074055Support Beam · crackedFOUND CARGO DOOR TRACK SUPPORT BEAM ANGLE AT FS 621 IS CRACKED AT BOTTOM ANGLE. (M)Aug 12, 2007 · N464AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA200740458Skin · corrodedTHE RT WING LOWER PLANK ACCESS HOLE FOR PANEL 640BB HAS PITTING APPROX .005 INCH DEEP AT THE INBOARD AND OUTBOARD RADIUS. 10-04-07 MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV F. (M)Aug 12, 2007 · N464AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740453Attach Fitting · crackedFOUND FS 280 LBL 9 INBOARD AND OUTBOARD FLOOR SUPPORT CLIPS ARE CRACKED. 10-04-07 MAINTENANCE REPLACED CLIPS IAW BSC STANDARD REPAIR 601R-53-0057A AND CRJ 200 SRM 51-42-13 AND 51-42-21. (M)Aug 12, 2007 · N464AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740451Floorbeam · crackedANGLE CRACKED IN FLOOR SUPPORT STRUCTURE AT FS 484 RBL 27, WL 73.50. 10-04-07 MAINTENANCE REPLACED ANGLE IAW BOMBARDIER REO 601R-53-41-059 AND BSC STANDARD REPAIR 601R-53-0029B. (M)Aug 11, 2007 · N464AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740449Floorbeam · crackedFOUND LEFT FS 621 FLOOR SUPPORT ANGLE CRACKED APPROX .3 INCH LONG. 10-04-07 MAINTENANCE REPLACED ANGLE IAW BOMBARDIER REO 601R-53-61-117. (M)Aug 11, 2007 · N464AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740452Floorbeam · crackedANGLE CRACKED IN FLOOR SUPPORT STRUCTURE AT FS 484 LBL 27, WL 73.50. 10-04-07 MAINTENANCE REPLACED ANGLE IAW BOMBARDIER REO 601R-53-41-059 AND BSC STANDARD REPAIR 601R-53-0029B. (M)Aug 11, 2007 · N464AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740448Intercostal · crackedLT FS 621-625 INTERCOSTAL ANGLE, P/N 601-35012-51, CRACKED APPROX .2 INCH LONG. 07-04-07 MAINTENANCE REPLACED ANGLE IAW BOMBARDIER REO 601R-53-61-422 AND CRJ 200 SRM 51-42-06 AND 51-42-21. (M)Aug 11, 2007 · N464AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740447Intercostal · crackedFOUND RIGHT FS 621-625 INTERCOSTAL ANGLE, P/N 601-35012-52 CRACKED APPROX .2 INCH LONG. 10-04-07 MAINTENANCE REPLACED ANGLE IAW BOMBARDIER REO 601R-53-61-422 AND CRJ 200 SRM 51-42-06 AND 51-42-21. (M)Aug 11, 2007 · N464AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740450Floorbeam · crackedFOUND RIGHT FS 621 FLOOR SUPPORT ANGLE CRACKED APPROX .3 INCH LONG. 10-04-07 MAINTENANCE REPLACED ANGLE IAW BOMBARDIER REO 601R-53-61-117. (M)Aug 11, 2007 · N464AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740137Connector · unknownDURING FLIGHT , IDG NR 2 MESSAGE CAME ON AFT 28,000 FT, COMPLIED WITH QRH. AIR DIVERSION TO MDT, PERFORMED EMERGENCY LANDING. REMOVED AND REPLACED IDG NR 2, NO FIX. REMOVED AND REPLACED IDG NR 2 TEMP BULB, NO FIX. REMOVED AND REPLACED IDG HEAT EXCHANGER, NMar 19, 2007 · N464AW · Cndair CL6002B19 · Air Conditioning System WiringSDR A6WA200740117Flap · malfunctionedFLAPS FAIL CAUTION WHILE IN FLIGHT, FAILED AT 30. COMPLIED WITH AWAC SUPPLEMENT 98-018A, NO FLAP TWISTING, SKEWING OR DEFORMATION NOTED. RESENT CIRCUIT BREAKERS ONCE, MESSAGE CLEARED. FLAPS OPERATE NORMALLY. PLACED ON 72 HOUR WATCH. (K)Mar 9, 2007 · N464AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200640359Connector · looseFLAP FAIL MESSAGE DURING FLAP RETRACTION FROM 8 DEGREES TO 0 DEGREES, FLAP INDICATOR INDICATES 20 DEGREES. CHECKED FECU WHICH LED TO NR 1 OR LEFT BPSU. FOUND CONNECTOR TO BPSU LOOSE WITH MOISTURE INSIDE. CLEANED CONTRACTS AND RECONNECTED. REF 27-51-00, OPSOct 6, 2006 · N464AW · Cndair CL6002B19 · Flight Control System WiringSDR A6WA200640291Water Separator · malfunctionedWATER POOLING ON FLOOR BY 13C AND 13A, WATER APPEARS TO BE COMING FROM BEHIND CARPETED SIDEWALL PANEL. REPLACED RIGHT SIDE WATER SEPARATOR IAW AMM 21-51-13, OPS CHECK GOOD. (M)Jul 26, 2006 · N464AW · Cndair CL6002B19 · Humidity Control SystemSDR A6WA200540352Flap System · failedFLAPS FAILED AT 20 DEGREES ON APPROACH. NO DEFECTS NOTED. (K)Dec 10, 2005 · N464AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200540285Structure · damagedWHILE RETRACTING RIGHT MLG DAMAGE OCCURRED TO THE UPLOCK APRON ASSEMBLY BY PUNCHING A HOLE APPROX 1.5 INCH BY 1 INCH. REPAIRED RIGHT MLG WHEEL WELL CHANNEL BY CUTTING OUT DAMAGE FABRICATING AND INSTALLING REPAIR IAW BRAS EO 601R-53-7036. (M)Aug 11, 2005 · N464AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA200540002Skin · crackedAIRCRAFT HAS EXTERNAL SKIN DAMAGE AROUND A/C POWER RECEPTACLE. (M)Dec 29, 2004 · N464AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
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