N437AW

Service difficulty reports · 234

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 = 'N437AW' 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 A6WA200840375Sill · corrodedLOWER SILL ON PAX DOOR FS 315 AND 343 LBL 40 IS CORRODED. CORROSION REMOVED ON LOWER SILL OF PAX DOOR FS 315 ANDF FS 343 LBL 40 IAW SRM 51-21-06.Apr 30, 2008 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840373Intercostal · crackedINTERCOSTAL FS 484 CRACK AT LBL 27 AND LBL 36. INTERCOSTAL FS 484 AT LBL 27 AND 36 ANGLE INSTALLED IAW REO 601R-53-41-059 REV A.Apr 30, 2008 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840372Longeron · corrodedCORROSION EXISTS ON LOWER SILL LONGERON OF PAX DOOR FS 319 TO 345. CORROSION REMOVED ON LOWER SILL LONGERON OF PAX DOOR FS 319 TO 345 IAW SRM 51-21-06.Apr 30, 2008 · N437AW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR A6WA200840371Intercostal · crackedINTERCOSTAL FS 484 CRACK AT RBL 29 AND RBL 36. INTERCOSTAL FS 484 AT RBL 27 AND RBL 36 ANGLE INSTALLED IAW REO 601R-53-41-059 REV A.Apr 30, 2008 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840395Sill · crackedCRACK EXISTS ON LOWER SILL OF CARGO DOOR FS 574 LBL 45 UNDER BRACKET. REPAIRED IAW REO 601R-53-61-1741. (A)Apr 29, 2008 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840393Frame · crackedCRACK EXISTS ON PILOT BULKHEAD FRAME FS 280 LBL 9. REPAIRED IAW REO 601R-53-11-171 REV D. (A)Apr 29, 2008 · N437AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA200840390Support Bracket · crackedHYD SUPPORT BRACKET CRACK IN LT MLG BAY AT FS 531 AND BTWN LBL 18 - 27. REPLACED IAW SRM 51-42-06. (A)Apr 29, 2008 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840389Support Bracket · crackedHYD SUPPORT BRACKET CRACK IN RT MLG BAY AT FS 523 AND BTWN RBL 18 TO RBL 27. REPLACED IAW SRM 51-42-06. (A)Apr 29, 2008 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840388Bulkhead · crackedCRACK EXISTS ON FS 202 AT LBL 23 PRESSURE BULKHEAD AROUND PARKING BRAKE CABLE. REPAIR PERFORMED ON FS 202.75 LBL 23.72 PRESSURE BULKHEAD AROUND PARKING BRAKE IAW REO 601R-53-11-563. (A)Apr 29, 2008 · N437AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200840385Stiffener · crackedSTIFFENER CRACK INSIDE PAX DOOR ON FIXED STAIR AFT PANEL. STIFFENER INSIDE PAX DOOR ON FIXED STAIR AFT PANEL REPLACED IAW SRM 51-42-06. (A)Apr 29, 2008 · N437AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200840374Support Bracket · crackedHYD SUPPORT BRACKET CRACK IN RT MLG BAY AT FS 529 AND BTWN RBL 18 TO RBL 27. REPLACED HYD SUPPORT BRACKET IN RT MLG BAY AT FS 529 RBL 18 TO RBL 27 REPLACED IAW SRM 51-42-06 AND 51-23-00.Apr 29, 2008 · N437AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200840394Bulkhead · crackedREAR PRESSURE BULKHEAD CRACK AT LINTEL ATTACHMENT POINT. AFT PRESSURE BULKHEAD IN LINTEL FITTING AREA REPAIRED IAW REO 601R-53-61-1230 REV D. (A)Apr 28, 2008 · N437AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200740621Drain Line · chafedHYD 2 LOW PRESSURE CAUTION MESSAGE WITH ZERO QUANTITY AND ZERO PRESSURE. COMPLIED WITH QRH. DECLARED EMERGENCY, NORMAL LANDING. SHUT DOWN ENGINE NR 2 AFTER LANDING. TOTAL TIME AT ZERO QUANTITY 23 MINUTES. APU BAY LEAKING FLUID. FOUND NR 2 HYDRAULIC CASE Nov 14, 2007 · N437AW · Cndair CL6002B19 · Hydraulic System, MainSDR A6WA200740614Coalescer Bag · dirtyMEDIUM TO STRONG ODOR OF FUEL NOTICED FLIGHT DECK AND FORWARD CABIN AREA. REMOVED AND REPLACED COALESCER BAGS IAW CRJ AMM 21-51-13, RAN PACKS USING BOTH APU AND ENGINE AIR. NO DEFECTS NOTED. VISUAL INSPECTION FOR LEAKS, NO LEAKS NOTED. (M)Nov 10, 2007 · N437AW · Cndair CL6002B19 · Humidity Control SystemSDR A6WA200740151Apu · failedAPU FAULT MESSAGE AND FAINT ODOR OF SOMETHING BURNING AT GATE, APU EGT NOTED IN RED. APU WAS SUPPLYING BLEEDS AND ELECTRICS. REMOVED AND REPLACED APU ASSEMBLY. (M)Mar 21, 2007 · N437AW · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) SystemSDR A6WA200640304Brake Assy · brokenDURING NR 2 MAIN LANDING GEAR TIRE ASSEMBLY CHANGE, NR 2 BRAKE ASSEMBLY, OUTBOARD ROTOR ASSEMBLY WAS BROKEN IN HALF AT THE TRUNNION CONTACT AREA. BRAKE ASSEMBLY WAS REMOVED AND REPLACED IAW AMM.Aug 2, 2006 · N437AW · Cndair CL6002B19 · Landing Gear Brake SystemSDR A6WA200640206Skin · dented1 DENT TO LEFT FUSELAGE 7.375 INCH AFT OF FS 755 JUST FORWARD OF MID SPAR DATUM VS 43.75. MAINTENANCE REPAIRED PER BOMBARDIER ENGINEERING ORDER 601R-53-9230B. COMPLIANCE WITH FAR 25.571, REQUIRED WITHIN 12 MONTHS. (M)May 19, 2006 · N437AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200640201Drag Angle · crackedFOUND DOOR AFT DRAG ANGLE CRACKED APPROX 1.4 INCH LONG IN AREA OF PULLEY BRACKET. MAINTENANCE REPAIRED PAX DOOR AFT DRAG ANGLE IAW BOMBARDIER REO 601R-52-11-513 REV A. (M)May 15, 2006 · N437AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200640197Floorbeam · crackedOUTBOARD CLIP AT FS 280, RBL 9, FLOORBEAM IS CRACKED IN RADIUS APPROX .5 INCHES. MAINTENANCE REMOVED & REPLACED FS 280 RBL 9 OUTBOARD CLIP IAW CRJ 20 SRM 51-42-21, 51-42-13, AND BSC STANDARD REPAIR 601R-53-0057A. (M)May 15, 2006 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200640196Floorbeam · damagedINBOARD CLIP AT FS 280, RBL 9, FLOORBEAM IS CRACKED IN RADIUS APPROX .5 INCH. MAINTENANCE REMOVED AND REPLACED FS 280 RBL 9 INBOARD CLIP IAW CRJ 200 SRM 51-42-21, 51-42-13 AND BSC STANDARD REPAIR 601R-53-0057A. (M)May 15, 2006 · N437AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200640200Intercostal · crackedRIGHT SIDE FS 621 TO FS 625.3 INTERCOSTAL AT STRINGER 14R IS CRACKED NEAR RADIUS APPROX .8 INCH LONG. MAINTENANCE REMOVED AND REPLACED INTERCOSTAL IAW CRJ200 SRM 52-42-06. (M)May 14, 2006 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640199Frame · crackedLEFT SIDE FS 640 FRAME DOUBLER IS CRACKED IN RADIUS APPROX .6 INCH LONG AT WL 119, STRINGER 10L. MAINTENANCE REMOVED CRACKED DOUBLER AREA WAS MODIFIED AND REPAIRED WHILE INCORPORATING SB 601R-53-059 REV F.May 14, 2006 · N437AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA200640198Frame · crackedRIGHT SIDE FS 640 FRAME DOUBLER IS CRACKED IN RADIUS APPROX .8 INCHES LONG AT WL 119, STRINGER 10R. MAINTENANCE REMOVED CRACKED DOUBLER AREA WAS MODIFIED AND REPAIRED WHILE INCORPORATING SB 601R-53-059 REV F. (M)May 14, 2006 · N437AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA200640158Odor · detectedAT THE GATE, APU FAULT MESSAGE APPEARED, APU AUTO SHUTDOWN OCCURRED. ALSO, BEFORE SHUTSDOWN OCCURRED, COULD DETECT ELECTRICAL BURNING ODOR THROUGHOUT CABIN WITH PACKS ON APU AIR. INSPECTED APU, NO NOTICEABLE BURNS NOTED. REMOVED AND REPLACED APU, S/N P-626,Apr 24, 2006 · N437AW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA200640101Skin · damagedFUSELAGE SKIN AROUND THE GROUND AIR SUPPLY CONNECTION DOOR IS DAMAGED. MAINTENANCE REMOVED DAMAGED SKIN SECTION, FABRICATED FILLERS FROM 2024-T3 .050 INCH, FABRICATED FILLER AND 2 EXTERNAL DOUBLERS FROM 2024-T3 .063 INCH, INSTALLED FILLERS AND NON-FLUSH EXTEMar 13, 2006 · N437AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200640100Stringer · crackedSTRINGER 17L IS CRACKED AND BENT JUST ABOVE THE GROUND AIR SUPPLY DOOR. MAINTENANCE REMOVED STRINGER 17L FROM FS 626 TO FS 660, FABRICATED STRINGER AND SPLICE FROM (PN 601R35004-51 AND INSTALLED REPAIR PARTS IAW SRM. (K)Mar 13, 2006 · N437AW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR A6WA200540134Tire · damagedREQUEST INSPECTION LT MLG TIRE FOR WEAR. AC PASSENGERS AND CARGO WERE UNLOADED, AIRCRAFT DEFUELED. AIRCRAFT WAS TOWED ONT RAMP AREA. WITHOUT INJURY OR DAMAGE TO AIRCRAFT, GEAR SWING AND MLG BAY ACCOMPLISHED AND REMOVAL/REPLACEMENT LT MLG TIRES AS A PRECAUTIApr 2, 2005 · N437AW · Cndair CL6002B19 · TireSDR A6WA200440168Computer · unreliablePITCH AND ROLL ANNUNCIATOR ILLUMINATED ON CAPTS EFIS IN FLIGHT. PITCH UNRELIABLE, MORE THAN 6 DEGREES THAN F/O EFIS ATTITUDE. PITCH ILLUMINATED ON GROUND DEPOWERED AND REPOWERED. TAXI TEST OK. PROBLEM REOCCURRED IN FLIGHT. REMOVED AND REPLACED NR 1 AHRS COct 25, 2004 · N437AW · Cndair CL6002B19 · Attitude and Direction Data SystemSDR A6WA200440167Ahrs · inoperativeAFTER SWITCHING ATT/HDG FROM NORM TO (2) AT 31000, BOTH CAPT AND F/O AHRS WENT BLANK. A/P KICKED OFF AND YAW NR 2 DISENGAGED SWITCHED TO NORM AND CAPT AHRS CAME BACK. THEN 5 SECS LATER F/O AHRS CAME BACK. REENGAGED A/P AND YAW DAMP, TO FURTHER PROBLEM. REMOct 25, 2004 · N437AW · Cndair CL6002B19 · Attitude and Direction Data SystemSDR A6WA200440157Bushing · migratedRT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .041. REMOVED ORIGINAL BUSHING IAW MM 20-26-00-910-802, REAMED WING TRUNNION IAW REO 601R-57-21-003B, INSTALLED NEW 1ST OVERSIZED BUSHING IAW REO 601R-57-21-003B AND REAMED INNER DIAMETER IAW DRG 601R85007Oct 18, 2004 · N437AW · Cndair CL6002B19 · Main Landing GearSDR A6WA20044151Intercostal · crackedFS 621-FS 625.3 INTERCOSTAL, RT SIDE STR 14R, IS CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL PN 601R35012-52, IAW SRM 51-42-06.Oct 17, 2004 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440151Intercostal · crackedFS 621- FS 625-3 INTERCOSTAL, RT SIDE STR 14R, IS CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL (PN601R35012-52), IAW SRM 51-42-06.Oct 17, 2004 · N437AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440152Intercostal · crackedFS 621-FS 625.3 INTERCOSTAL, LT SIDE, AT STR 14R IS CRACKED NEAR RADIUS, APPROX .75 INCH LONG. REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL, PN 601-35012-51, IAW SRM 51-42-06.Oct 17, 2004 · N437AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200440031Warning System · activatedABORTED TAKEOFF DUE TO AILERON MISCONFIGURATION WARNING MESSAGE ABOVE 80 KNOTS. BTMS READINGS 03, 03, 04, 06 REPORTED WEIGHT 52,000 LBS. COMPLIED WITH SPECIAL INSPECTION PROCEDURE IAW 5-51-27, ABORTED TAKEOFF. REMOVED AND REPLACED NR 3 AND NR 4 MLG TIRES. Mar 13, 2004 · N437AW · Cndair CL6002B19 · Aileron Control System
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