N440AW

Service difficulty reports · 176

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 = 'N440AW' 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 A6WA200740164Smoke Detector · malfunctionedSMOKE TOILET CASS MESSAGE AFTER TAKEOFF WITH LAV SMOKE ALARM ACTIVATED RAN QRH, MESSAGE EXTINGUISHED ALARM OFF F/A REPPORTED NO INDICATION OF SMOKE OR FIRE ON INSPECTION. RAN ENGINE WITH APU AIR SWITCH OVER TO BLEED AIR AND NO SMOKE CAUTION MESSAGE WITH EITHEMar 16, 2007 · N440AW · Cndair CL6002B19 · Smoke DetectionSDR A6WA200640405Flap System · malfunctionedFLAPS FAILED TO EXTEND WHEN SELECTED ON APPROACH. COMPLIED WITH SUPPLEMENT 98-018A, FLAP RESET AND OPERATE NORMALLY. (K)Dec 7, 2006 · N440AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200640389Coalescer Bag · dirtyDURING POST DE-ICING RUN UP, RECEIVED LAV SMOKE MESSAGE. COMP;IED WITH QRH AND MESSAGE CLEARED. PERFOMED LAV SMOKE DE4TECTOR TEST IAW AMM. OPPS CHECKED GOOD. REMOVED AND REPLACED COALESCER BAGS IAW AMM, OPS CHECK GOOD. NO MESSAGE OR SMOKE SMELL FOUND. (KNov 21, 2006 · N440AW · Cndair CL6002B19 · Humidity Control SystemSDR A6WA200640401Wire · looseENROUTE, SPARKS OBSERVED COMING FROM F/O`S YOKE MAP LIGHT. CB2U6 POPPED. LOOSE CONNECTION ON F/O`S MAP LIGHT FOUND. RESECURED LOOSE CONNECTION. OPS CHECK GOOD IAW 33-13-13. (K)Nov 7, 2006 · N440AW · Cndair CL6002B19 · Flight Compartment LightingSDR A6WA200640136Doubler · crackedFOUND RIGHT SIDE FS 640 FRAME DOUBLER IS CRACKED AT STRINGER 10R APPROX 1 INCH LONG. MAINTENANCE REPAIRED BY PERFORMING JOB CARD 4EOMFG08415 AWAC EO E02/087/453 REV A INSPECTION AND MODIFICATION OF AFT FUSELAGE FRAME AT FS 640 BL 45 BETWEEN STRINGERS 9 AND 12Apr 3, 2006 · N440AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA200640110Skin · dentedDENT FWD AND LT OF NOSE JACK POINT .8 INCH X 14 INCH AND .2500 INCH DEEP. CORRECTIVE ACTION IN PROGRESS. (K) MAINTENANCE REPAIRED FUSELAGE SKIN AT FS 272 STRINGER.Apr 3, 2006 · N440AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200640135Angle · crackedFS 484 ANGLE CRACKED AT LBL 36 APPROX .5 INCH LONG. (K) MAINTENANCE REPAIRED FLANGE AT FS 484, LBL 36 IAW BOMBARDIER REO 601R-53-41-059 REV A AND BOMBARDIER REO 601R-53-41-059 REV A AND BOMBARDIER STANDARD REPAIR 601R-53-0030A. (M)Mar 31, 2006 · N440AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640134Angle · crackedFS 484 ANGLE CRACKED AT LBL 27 APPROX .5 INCH LONG. (K) MAINTENANCE REMOVED AND REPLACED CLIP IAW BSC STANDARD REPAIR 601R-53-0029A AND SRM 51-42-06, 51-42-21. (M)Mar 31, 2006 · N440AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200640133Clip · crackedFS 280, RBL 9 IB CLIP IS CRACKED. (K) MAINTENANCE REMOVED CRACKED CLIP AND INSTALLED NEW SERVICEABLE CLIP IAW CRJ 200 SRM 51-42-06, 51-42-21. (M)Mar 29, 2006 · N440AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200640132Clip · crackedFS 280, LBL 9 OB CLIP IS CRACKED. (K) MAINTENANCE CRACKED CLIP AND INSTALLED NEW SERVICEABLE CLIP IAW CRJ200 SRM 51-42-06, 51-42-21. (M)Mar 29, 2006 · N440AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200640130Clip · crackedFS 280, LBL 9, IB CLIP IS CRACKED. (K) MAINTENANCE REMOVED CRACKED CLIP AND INSTALLED NEW SERVICEABLE CLIP IAW CRJ 200 SRM 51-42-06 AND 51-42-21. (M)Mar 29, 2006 · N440AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200640129Clip · crackedFS 280, RBL 9 OB CLIP IS CRACKED. CA IN PROGRESS. (K) MAINTENANCE REMOVED CRACKED CLIP AND INSTALLED NEW SERVICEABLE CLIP IAW CRJ 200 SRM 51-42-06, 51-42-21, 51-42-13, AND BOMBARDIER STANDARD REPAIR 601R-53-0057A. (M)Mar 29, 2006 · N440AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200640118Skin · corrodedLT LWR WING PLANK HOLE NR 2, WS 12.245, HAS CORROSION AT IB SIDE 3.5 INCH L X .002 INCH-.003 INCH DEEP. (K) MAINTENANCE REPAIRED LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT PANEL 510AB, WS 12.245, HOLE NR 2 BY REMOVING CORROSION ON INBOARD EDGE TOMar 25, 2006 · N440AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200640117Skin · corrodedLT LWR WING PLANK, HOLE NR 16, WS 303.861, HAS CORROSION AROUND ENTIRE CIRCUMFERENCE, .002 INCH- .003 INCH DEEP. (K) MAINTENANCE LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUT OUT AT PANEL 550HB, WS 303.861, HOLE NR 16 BY REMOVING CORROSION TO A MAX DEPTH OMar 25, 2006 · N440AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200640121Skin · corrodedRT LWR WING PLANK HOLE NR 16, WS 303.861 HAS CORROSION AROUND ENTIRE CIRCUMFERENCE .002 INCH-.003 INCH DEEP. (K) MAINTENANCE REPAIRED RIGHT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT BY REMOVING CORROSION AND TREATING AREA AT PANEL 650HB, WS 303.861, HOLMar 25, 2006 · N440AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200640120Skin · corrodedLT WING, LWR WING PLANK, HOLE NR 1, WS 54.897, HAS CORROSION AT IB SIDE 12 INCH L X .002 INCH-.003 INCH DEEP AND OB FWD SIDE 1 INCH L X .001 INCH - .002 INCH DEEP AND AT OB FWD SIDE 1 INCH L X .001 INCH- .002 INCH DEEP. (K) MAINTENANCE REPAIRED LEFT WING LOWMar 25, 2006 · N440AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200640119Skin · corrodedLT LWR WING PLANK, HOLE NR 11, WS 209.040, HAS CORROSION ON AFT OB SIDE 8.5 INCH L X .002 INCH, .003 INCH DEEP. (K) MAINTENANCE REPAIRED LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT PANEL 550CB, WS 209.040, HOLE NR 11 OUTBOARD EDGE BY REMOVING CORROMar 25, 2006 · N440AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200640116Web · crackedENGINE SUPPORT BEAM LOWER WEB CRACKED LT SIDE FROM ACCESS PANEL NUTPLATE, APPROX FS 628, LBL 39, WL 111.09. (K) MAINTENANCE REPAIRED LOWER WEB BY INCORPORATION AWAC E02/081/453 MODIFICATION OF THE ENGINE SUPPORT BEAM (BOMBARDIER SERVICE BULLETIN A601R-53-059 Mar 22, 2006 · N440AW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR A6WA200640113Doubler · crackedRT SIDE FS 640 FRAME DOUBLER IS CRACKED AT STRINGER 10R APPROX 1.0 INCH LONG. CORRECTIVE ACTION IN PROGRESS. (K)Mar 22, 2006 · N440AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA200640112Intercostal · crackedRT SIDE FS 621.0 TO FS 625.3 INTERCOSTAL AT STRINGER 14R IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. CORRECTIVE ACTION IN PROGRESS. (K)Mar 22, 2006 · N440AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640111Intercostal · crackedLT SIDE FS 621.0 TO FS 625.3 INTERCOSTAL AT STRINGER 14L IS CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. (K) MAINTENANCE REMOVED AND REPLACED FS 621 TO 625.3 INTERCOSTAL AT STRINGER 14L IAW CRJ SRM 51-42-06. (M)Mar 22, 2006 · N440AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640109Stringer · damagedSTRINGER 26L, 10 INCHES FWD OF FS 280 IS DAMAGED. (K) MAINTENANCE REMOVED DAMAGED SECTION OF STRINGER 26L FROM FS 257 TO FS 272. FABRICATED SECTION OF REPAIR STRINGER AND SPLICES FROM P/N 600-33011-161. INSTALLED REPAIRED STRINGER AND SPLICES IAW BSC EO 60Mar 21, 2006 · N440AW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR A6WA200440182Skin · dentedRT IB FLAP BOTTOM SKIN IS DENTED APPROX .7500 INCH LONG X .6250 INCH WIDE AND .040 DEEP WITH GOUGES IN CENTER OF DENT. DENT IS 1.7500 INCH FORWARD OF AFT EDGE AND 8 INCH OB FROM IB ENGINE. PERFORMED A MAJOR REPAIR BY CUTTING OUT DAMAGED SKIN AND INSTALLING DNov 8, 2004 · N440AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200440177Bushing · migratedLT MAIN LANDING GEAR AFT TRUNNION BUSHING MIGRATED 0.005 INCH. REMOVED LT AFT MLG TRUNNION BUSHING IAW AMM 20-26-00-910-803. INSTALLED A NEW OVERSIZE (2ND) BUSHING PN 601R5721003-23. IAW REO 601R57-21-003B. REAMED INSIDE DIA TO 2.4384 IAW DWG 601R85007RWC.Nov 7, 2004 · N440AW · Cndair CL6002B19 · Main Landing GearSDR A6WA200340128Engine · failedUPON TAKEOFF NOTED NR 1 ENGINE ITT AT 900. DURING CLIMB NOTED ITT AT 858-874. AT FL280 HEARD THUMP AND NR 1 ENGINE SPOOLED DOWN. SECURED PER QRH AND COMPLIED WITH SINGLE ENGINE OPERATIONS. REMOVED AND REPLACED NR 1 ENGINE. SHOP REPORT REMARKS, REPLACED NR Aug 29, 2003 · N440AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA200340076Line · failedOXYGEN MASK SUPPLY LINE FAILED. COCKPIT 02 SUPPLY DEPLETED. INSTALLED NEW SUPPLY HOSE FROM OBSERVERS OXYGEN STORAGE BOX AND RECHARGED OXYGEN SYTEM TO 1520 PSI. NO FURTHER LEAKS NOTED. (M)May 25, 2003 · N440AW · Cndair CL6002B19 · Crew Oxygen System
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