N415AW

Service difficulty reports · 215

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 = 'N415AW' 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 A6WA200540106Access Panel · corrodedLT LOWER WING PLANK FUEL TANK ACCESS PANEL CUT-OUT BETWEEN SS 0.00 AND WS 29.42 HAS MINOR FRETTING ON FAYING SURFACE LESS THAN .006 INCH DEEP. C/A PENDING (K)Mar 17, 2005 · N415AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540111Rib · crackedRIGHT MLG WHEEL WELL AT WS 48.3O FS 523.8 BATTERY RIB IS CRACKED APPROX 1 INCH. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW BOMBARDIER INC REO 601R-57-57-046 REV B. (M)Mar 16, 2005 · N415AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA200540112Rib · crackedLT MLG WHEEL WELL AT WS 48.30 FS 523.8 BATT RIB IS CRACKED APPROX 1 INCH.Mar 16, 2005 · N415AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA200540108Attach Angle · crackedFOUND FS 280, FRAME RBL 9, ATTACHMENT ANGLE TO BE CRACKED APPROX 1 INCH LENGTH.Mar 16, 2005 · N415AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540110Floor Support · crackedFLOOR SUPPORT ANGLE AT FS 621 RT SIDE IS CRACKED 1 INCH. PERFORMED REPAIR TO RT FS621, FLOOR SUPPORT ANGLE IAW REO. (K)Mar 16, 2005 · N415AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540109Floorbeam · crackedFLOORBEAM ANGLE AT FS 621 LT SIDE IS CRACKED 1 INCH. PERFORMED REPAIR TO RT FS 621 FLOORBEAM ANGLE IAW BOMBARDIER REO 601R-53-117 REV C. (M)Mar 16, 2005 · N415AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200540098Intercostal · crackedLT SIDE FS621-FS625.3 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS, APPROX .70 INCH. INSTALLED NEW LT INTERCOSTAL AT FS 621-625.3, STR 14L IAW BRAS EO 601R-53-6157. (K)Mar 15, 2005 · N415AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540097Intercostal · crackedRT SIDE FS 621-FS 625.3 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX .60 INCH. INSTALLED NEW RT INTERCOSTAL AT FS 621-625.3, STR 14R IAW BRAS EO 601R-53-6157. (K)Mar 15, 2005 · N415AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540043Apu · seizedAPU FAILED, REQUESTED INSPECTION. COMPLIED WITH APU INSPECTION FOUND APU TO BE SEIZED. APU INLET EXHAUST NO DEFECTS NOTED. ALSO SUSPECT BAD FCU. COMPLIED WITH ACTION PLACARD PLACED ON MEL. MAINTENANCE VERIFIED APU SEIZED. REMOVED AND REPLACED APU ASSEMBLYFeb 7, 2005 · N415AW · Cndair CL6002B19 · APU Core EngineSDR A6WA200540001Acm · odorSMOKE IN CABIN ASSOCIATED WITH APU BLEED AIR HAZE IN COCKPIT AND CABIN. REMOVED AND REPLACED LEFT AIR CYCLE MACHINE, COMPLIED WITH OPS CHECK IAW CRJ AMM 21-51-10, NO SMOKE SMELL NOTED. (M)Jan 2, 2005 · N415AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA200340153Fitting · damagedRIGHT WING FLAP HINGE FITTING ASSEMBLY AT WS 178, P/N 601R10088-8 LOWER SURFACE FORWARD EDGE HAS MUSHROOMED METAL AND GOUGES. BLENDED AREAS SMOOTH, PERFORMED EDDY CURRENT INSPECTION OF AREAS, PERFORMED ROTO/FLAP PEEN OF REPAIR AREAS AND RESTORED ORIGINAL FINIOct 28, 2003 · N415AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200340152Skin · gougedRIGHT WING UNDERSIDE SKIN HAD NUMEROUS SCRATCHES AND GOUGES OUTBOARD OF WS 178 BETWEEN X163-X199. BLENDED AND SMOOTHED OUT DAMAGED AREAS, PERFORMED EDDY CURRENT INSPECTION OF AREAS, ALODINED PRIMED AND TOP COATED ALL BARE METAL IAW WVAC EO 601R-57-4317. (M)Oct 28, 2003 · N415AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200340154Beam · damagedRT WING FLAP HINGE BEAM AT WS 178 FORWARD EDGE AND LOWER SURFACE HAS MUSHROOMED METAL AND GOUGES. BLENDED AREAS SMOOTH, PERFORMED EDDY CURRENT INSPECTION OF AREAS, PERFORMED ROTO/FLAP PEEN OF REPAIR AREAS AND RESTORED FINISH TO ORIGINAL CONFIGURATION IAW WVACOct 28, 2003 · N415AW · Cndair CL6002B19 · Wing Main, Frame StructureSDR A6WA200340112Motor · inoperativeSTAB TRIM CHANNEL 1 INOPERATIVE REMOVED AND REPLACED MOTOR CONTROL UNIT IAW MM 27-42-05. OPS CHECK GOOD. SHOP REPORT REMARKS, COMPLAINT VERIFIED, REMOVED AND REPLACED DEFECTIVE RESISTOR, INTEGRATED CIRCUIT, DIODE AND CRACKED INDUCTOR. INSPECTED UNIT IAW CMM Jul 15, 2003 · N415AW · Cndair CL6002B19 · Stabilizer Control SystemSDR A6WA200340057Outflow Valve · failedEXPERIENCED RAPID DECOMPRESSION AT FL310, COMMENCED EMERGENCY DESCENT, WERE UNABLE TO REGAIN CONTROL OF PRESSURIZATION IN MANUAL MODE, DROPPED ALL PASSENGER OXYGEN MASKS. DEPLETED OXYGEN SUPPLY, CABIN ALTITUDE RWP. REMOVED AND REPLACED OUTFLOW VALVE. SHOP FApr 19, 2003 · N415AW · Cndair CL6002B19 · Pressure Regulator/Outflow Valve
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