N423AW

Service difficulty reports · 165

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 = 'N423AW' 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 A6WA200740392Angle · crackedRT FS 484 INTERCOSTAL ANGLE CRACKED AT RBL 27 APPROX .1 INCH LONG UNDER CABIN FLOOR PANEL 262DRF. (K) MAINTENANCE REMOVED CRACKED ANGLE, FABRICATED NEW ANGLE AND INSTALLED IAW BSC STANDARD REPAIR 601R-53-0029B AND 601R-53-41-059. (M)Jul 15, 2007 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740040Selector Valve · unknownNOSE GEAR DISAGREE ILLUMINATED ON GEAR RETRACTION. FOLLOWED QRH, PUT GEAR DOWN, MESSAGE CLEARED. REMOVED AND REPLACED NOSE LANDING GEAR SELECTOR VALVE PER AMM 32-22-02, OPS CHECK GOOD. (M)Jan 31, 2007 · N423AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA200740005Pcu · unknownFLIGHT SPOILER CONFIG WARNING AND AURAL WHEN APPLICATION OF POWER UNTIL THRUST LEVERS MOVED BACK TO IDLE, THE RT FLIGHT SPOILER TURNED WHITE ON SYSTEM PAGE. REMOVED AND REPLACED RT INBOARD FLIGHT SPOILER PCU PER AMM. OPS CHECK GOOD. (M)Dec 30, 2006 · N423AW · Cndair CL6002B19 · Drag Control SystemSDR A6WA200540219Angle · crackedLT FS 621.00 ANGLE IS CRACKED .5 INCH LONG ON OB RADIUS. REPAIRED BY REMOVING DAMAGED SECTION OF ANGLE, FABRICATING REPAIR ANGLES AND STRAP, INSTALLING REPAIR PARTS IAW MFG REO. (K)Jun 22, 2005 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540217Threshold · crackedCARGO DOOR THRESHOLD PLATE HAS A .2500 INCH CRACK AT FS 589.00, LBL 41.5. REPAIRED BY REMOVING DAMAGED SECTION OF FLOOR LANDING PERFORMING EDDY CURRENT INSP, PAINTING REPAIR AREA AND FILLED REDUNDANT HOLE IAW MFG REO. (K)Jun 22, 2005 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540218Angle · crackedRT FS 621.00 ANGLE IS CRACKED .5 INCH LONG ON OB RADIUS. REPAIRED BY REMOVING DAMAGED SECTION OF ANGLE, FABRICATING ANGLES AND STRAP, INSTALLING REPAIR PART IAW MFG REO. (K)Jun 22, 2005 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540216Angle · crackedRT FS 460.00 ANGLE AT RBL 9 HAS A .5 INCH CRACK. REMOVED CRACK ANGLE AND INSTALL NEW ANGLE AT RBL 9. (K)Jun 21, 2005 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540215Intercostal · crackedRT FS 484.00 INTRCOSTAL AT LBL 36.0 HAS A .5 INCH LONG CRACK. FABRICATED ANGLE IAW EO. REMOVED FLANGE AND INSTALLED ANGLE IAW MFG REO. (K)Jun 21, 2005 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440227Landing Gear · malfunctionedNOSE GEAR WOULD NOT EXTEND. MANUAL EXTENSION OK. COMPLIED WITH GEAR SWING 8 TIMES. (5 TIMES REGULAR/ 3 TIMES ON EMERGENCY) OPS CHECK GOOD. (K)Dec 19, 2004 · N423AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA200440149Indicator · contaminatedON TAKEOFF ROLL THROUGH 80 KNOTS, STANDBY AIRSPEED INDICATION REMAINED AT 0 KNOTS. INSPECTED STANDBY SYSTEM AND FOUND WATER TO BE IN SYSTEM. PURGED WATER FROM SYSTEM AND PERFORMED LEAK CHECK IAW MM 34-11-00. OPS CHECK GOOD.Oct 13, 2004 · N423AW · Cndair CL6002B19 · Airspeed/Mach IndicatorSDR A6WA200440097Unknown · fumesFUMES ENTERING COCKPIT AND CABIN WHEN ADJUSTING THE TEMP. PERFORMED OPS CHECK OF NR 1 AND NR 2 PACK NO FUMES NOTED. OK FOR SERVICE. (M)Jul 4, 2004 · N423AW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA200440075Idg · lowGEN NR 2 CAS MESSAGE AFTER TAKEOFF. RETURNED TO CID. SERVICED NR 2 IDG IAW MM. OPS CHECK NORMAL.Jun 9, 2004 · N423AW · Cndair CL6002B19 · Alternator-Generator DriveSDR A6WA200340185Bushing · looseFOUND LT MLG AFT WING SPAR BUSHING MIGRATED .052 INCH. REMOVED MIGRATED BUSHING ON LEFT MLG, AND INSTALLED FIRST OVERSIZE BUSHING, P/N 601R-57-21-003-21 IAW REO 601R-57-21-003 REV B. (M)Dec 1, 2003 · N423AW · Cndair CL6002B19 · Wing Main, Frame StructureSDR A6WA200340184Skin · chafedFOUND LEFT OUTBOARD FLAP HAS DEEP CHAFF IN FIXED VANE AT FAR OUTBOARD END LEADING EDGE .050 TO .075 DEPTH. PERFORMED A MAJOR REPAIR TO THE LEFT OUTBOARD FLAP LEADING EDGE FIXED VANE BY REMOVING AND REPLACING LEADING EDGE CAP, P/N 601R-14574-7 IAW CRJ SRM 57-3Nov 29, 2003 · N423AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200240023Smoke Detector · inoperativeSMOKE CARGO FIRE WARNING DURING CLIMB C/W QRH FOR SMOKE CARGO, DISCHARGED BOTH CARGO FIRE BOTTLES. MAINTENANCE REMOVED AND REPLACED CARGO SMOKE DETECTOR, OPS CHECKED GOOD.Jul 16, 2002 · N423AW · Cndair CL6002B19 · Extinguishing System
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