N429AW

Service difficulty reports · 190

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 = 'N429AW' 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 A6WA201040220Angle · corrodedCORROSION FOUND AT FS 333.00, STRINGER 26L-26R FLANGE. ALSO CORROSION FOUND AT FS 349.00, STRINGER 26L-27L. REPAIRED DAMAGE TO FS 333.00, STRINGER 26L-26R IAW REO 601R-53-21-1092. REPAIRED DAMAGE TO FS 349.00, STRINGER 26L-27L IAW REO 601R-53-21-1091.Feb 5, 2010 · N429AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040218Vane · crackedRT ENGINE THRUST REVERSER TOP CASCADE HAS 1 (EA) VANE GOUGED AND 1 (EA) VANE CRACKED. REPAIRED 1 INCH CRACK & 1 GOUGE ON RT ENGINE T/R TOP CASCADE IAW DWG AW 78-30-0711-04.Feb 5, 2010 · N429AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201040216Stiffener · crackedPAX DOOR ASSIST MOTOR LOWER MOUNT FITTING CRACKED. REMOVED CRACKED STIFFENER AND REPLACED WITH NEW SERVICEABLE STIFFENER PN 601R317745-7.Feb 5, 2010 · N429AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040215Support Angle · crackedPAX DOOR INNER HANDLE SUPPORT ANGLE CRACKED. REMOVED CRACKED ANGLE AND DUPLICATED IAW SRM.Feb 2, 2010 · N429AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040106Angle · crackedRT OBLIQUE ANGLE UNDERBEAM CRACKED. REMOVED RT OBLIQUE ANGLE AND REPLACED RT OBLIQUE ANGLE IAW SRM 51-24-16.Jan 31, 2010 · N429AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040105Angle · crackedLT OBLIQUE ANGLE UNDER ENGINE BEAM CRACKED. R & R LT OBLIQUE ANGLE PN 601-35012-51 IAW SRM 51-40-11, 51-42-21, 51-25-16.Jan 30, 2010 · N429AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840579Sensor · malfunctionedFLAP FAIL CAUTION MESSAGE. FLAPS AT ZERO. DIVERTED TO BWI. FOUND LT BPSU CODES CONTINUITY CHECK AND MEGGED LT WING WIRING PER WM AND FIM CHAP 27. NO FAULTS FOUND. CURRENT BPSU INSTALLED HAS REPEAT HISTORY OF FAULTS IN OTHER ACFT. SUSPECT BAD PART. REPLAAug 13, 2008 · N429AW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR A6WA200840560Bpsu · malfunctionedFLAPS FAIL CAUTION MESSAGE. FLAPS FAILED AT 8 DEGREES IN FLIGHT. R&R RT BPSU AND RE-RIGGED FLAPS IAW AMM 27-50.Aug 10, 2008 · N429AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840502Door · stiffPASSENGER DOOR WILL NOT OPEN WITHOUT EXCESSIVE FORCE. CLEANED AND LUBED PAX DOOR IAW AMM 12-26-52 AS REQUIRED OPS CHECKS SEVERAL TIMES NO DEFECTS NOTED AT THIS TIME. (A)Jun 9, 2008 · N429AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200840278Generator · failedDEPARTING BUFFALO, GENERATOR NR 1 DROPPED OFF LINE AT 700 FT PER QRH RESET. GENERATOR 2 DROPPED OFF LINE AT 1200 FT AND RESET PER QRH. BOTH GENERATORS OFF LINE FOR APPROXIMATELY 1 MINUTE. SERVICED GEN/IDG 1 WITH 4-5 PUMPS OF OIL. OPS CHECK GOOD. NO LEAKS Apr 2, 2008 · N429AW · Cndair CL6002B19 · Alternator-Generator DriveSDR A6WA200840255Window · crackedFIRST OFFICERS SIDE WINDOW CRACKED. REMOVED AND REPLACED WINDOW IAW AMM 56-12-01.Mar 26, 2008 · N429AW · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA200840091Structure · crackedREPAIR CRACK ON PAX DOOR AFT SIDEWALL LOWER SIDE FWD OF DOOR ASSIST MOTOR PULLEY ASSY. (K) CRACK ON PAX DOOR REPAIRED IAW REO 601-52-11-513 REV A. (M)Feb 13, 2008 · N429AW · Cndair CL6002B19 · Passenger Compartment EquipmentSDR A6WA200840094Bulkhead · crackedCRACK FOUND ON REAR PRESSURE BULKHEAD WEB FS 621.00, WL 106.17, LBL 36.00 (LINTEL ATTACHMENT FITTING). (K) REPAIRED REAR PRESSURE BULKHEAD IAW REO 601R-53-61-1230 REV D. (M)Feb 12, 2008 · N429AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200840087Support · crackedCRACK SUSPECTED IN AC GROUND POWER BOX. (K) A/C CONNECTOR SUPPORT MEMBER REPLACED IAW SRM 51-42-06. (M)Feb 12, 2008 · N429AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840093Bracket · crackedCRACK EXIST ON BRACKET FS 280, LBL 9, ABD RBL 9 CRACK LENGTH .200. (K) REPAIR PERFORMED IAW REO 601R-53-11-171, FABRICATED NEW ANGLE. (M)Feb 5, 2008 · N429AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840092Structure · crackedCRACK EXIST ON FLOOR STRUCTURE FS 280, RBL 9 CRACK LENGTH .150. (K) CUT OUT DAMAGE IAW REO 601R-53-11-171. REPAIR PERFORMED IAW REO 601R-53-11-171. (M)Feb 5, 2008 · N429AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840086Intercostal · crackedCRACK EXIST ON INTERCOSTAL FS 484, RBL 36 CRACK LENGTH .200. (K) REPAIRED INTERCOSTAL IAW REO 601R-53-41-059. (M)Feb 5, 2008 · N429AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840085Intercostal · crackedCRACK EXIST ON INTERCOSTAL FS 481, LBL 36 AND LBL 27 CRACK LENGTH .200. (K) REPAIRED IAW REO 601R-53-41-059. (M)Feb 5, 2008 · N429AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840090Angle · crackedANGLE CRACK AT FS 621.0 AND MEMBER BEAM OF CARGO DOOR. (K) ANGLE REPLACED IAW SRM 51-2-16 AND 51-42-20. (M)Feb 4, 2008 · N429AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA200840089Radome · crackedLIGHT GLAZING ON RADOME FOUND CRACK. (K) REPLACED IAW SRM 51-42-20. (M)Feb 4, 2008 · N429AW · Cndair CL6002B19 · Aerodynamic FairingsSDR A6WA200840088Scuff Plate · corrodedSCUFF PLATE OF SERVICE DOOR FOUND CORRODED. (K) SCUFF PLATE REPLACED IAW SRM 51-42-06 AND 51-41-02. (M)Feb 4, 2008 · N429AW · Cndair CL6002B19 · Service DoorsSDR A6WA200840101Sill · crackedCRACK FOUND ON LOWER SILL FS 572, LBL 40, UNDER BRACKET SCUFF PLATE RETAINER. LOWER SILL PLATE REPLACED IAW REO 601R53-61-690 REV D. (M)Feb 4, 2008 · N429AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840084Bulkhead · crackedLT LWR NOSE COMPARTMENT CRACK FOUND ON PRESSURE BULKHEAD AROUND BRAKE FS 202. (K) JOB PERFORMED IAW REO 601R-53-11-563. (M)Feb 2, 2008 · N429AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200740219Wheel · vibrationHIGH SPEED ABORTED TAKE-OFF DUE TO NOSEWHEEL VIBRATION. SPEED WAS 135 KNOTS, BRAKE TEMPS WERE 7-7-7-7. COMPLIED WITH REJECTED TAKEOFF INSPECTION IAW AMM 05-51-27-210-801. NO DAMAGE NOTED. (K)Apr 25, 2007 · N429AW · Cndair CL6002B19 · Nose/Tail Landing GearSDR A6WA200640086Intercostal · crackedLT SIDE FS 621.0 TO FS 625.3 INTERCOSTAL AT STRINGER 14L ISS CRACKED NEAR RADIUS APPROX .80 INCH LONG. MAINTENANCE LT INTERCOSTAL REMOVED AND INSTALLED NEW ANGLE INTERCOSTAL IAW SRM. (K)Feb 15, 2006 · N429AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640087Intercostal · crackedRT SIDE FS 621.0 TO FS 625.3 INTERCOSTALS AT STRINGER 14R IS CRACKED NEAR RADIUS APPROX .75 INCH LONG. MAINTENANCE REMOVED RT INTERCOSTAL AND INSTALLED NEW INTERCOSTAL IAW SRM. (K)Feb 15, 2006 · N429AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540354Apu · odorSTRONG SMELL OF JET FUEL AFTER APU START IN FLIGHT APU SHUTDOWN. PERFORMED OPS TEST AND LEAK CHECK OF APU. OPS TEST GOOD AT THIS TIME, IAW AMM. NO LEAKS NOTED. NO FAULT CODES NOTED AFTER INTEROGATION OF ECU, OPS CHECK ACM SYSTEM. NO FUEL SMELL NOTED AT THDec 11, 2005 · N429AW · Cndair CL6002B19 · APU Cowling/ContainmentSDR A6WA200540353Apu · smokeREQUEST INSPECTION OF APU COMPARTMENT DUE TO EXTREME AMOUNT OF SMOKE AFTER AUTO SHUTDOWN. INSPECTED APU AW CRJ AMM. NO DEFECTS NOTED. (K)Dec 6, 2005 · N429AW · Cndair CL6002B19 · APU Core EngineSDR A6WA200540278Connector · unsecureSHORTLY AFTER TAKEOFF, STRONG SMELL OF SMOKE IN COCKPIT AND CABIN. NO VISUAL SMOKE, PACK TEMP NORMAL. (AIR RETURN) DURING TAXI PACK NR 2 HI TEMP INDICATION. INSPECTED AFT EQUIPMENT BAY AREA AND FOUND RT PACK ACM TEMP SWITCH HANGING FROM CONNECTOR PLUG. NO Aug 4, 2005 · N429AW · Cndair CL6002B19 · Air Conditioning System WiringSDR A6WA200540227Control Unit · malfunctioned(CONFIG SPOILER) CAS MESSAGE ILLUMINATED ON TAKEOFF, ABORTED TAKEOFF. PERFORMED BELOW 20 KNOTS. REMOVED AND REPLACED SECU NR 1 IAW AMM. OPS CHECK GOOD. (K)Jul 9, 2005 · N429AW · Cndair CL6002B19 · Drag Control SystemSDR A6WA200540083Smoke · detectedEXCESSIVE SMOKE OUT OF RT ENGINE ON SHUTDOWN ALL INDICATIONS WERE NORMAL. PERFORMED ENGINE RUN OF ENGINE NR 2 IAW CRJ AMM TASK 71-00-00-848-806. NO DEFECTS NOTED. AIRCRAFT SAFE FOR SERVICE. (M)Mar 2, 2005 · N429AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA200440138Bracket · bentSELECTING GEAR UP RECEIVED NOSE DOOR OPEN AND GEAR DISAGREE MSG. PERFORMED QRH AND RETURNED TO FIELD. PERFORMED QRH AND RETURNED TO FIELD. FOUND BRACKET FOR NOSE LANDING GEAR CENTERED SENSOR BENT. REMOVED AND REPLACED BRACKET AND ADJUSTED SENSOR PS14GA IAWSep 29, 2004 · N429AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA200440104Bushing · migratedAT LEFT MLG MOUNTING TRUNNION BUSHING IS MIGRATED .004 WS 66. PERFORMED A MAJOR REPAIR BY REMOVING MIGRATED LEFT MLG AFT TRUNNION BUSHING AND INSTALLED FIRST OVERSIZE BUSHING P/N 601R5720113-21, IAW BOMBARDIER REO 601R-57-21-003 REV B. (M)Jul 18, 2004 · N429AW · Cndair CL6002B19 · Wing Main, Frame StructureSDR A6WA200440105Bushing · migratedAFT RIGHT MLG MOUNTING TRUNNION BUSHING IS MIGRATED .015, WS 66. PERFORMED A MAJOR REPAIR BY REMOVING MIGRATED RIGHT MLG AFT TRUNNION BUSHING AND INSTALLING FIRST OVERSIZE BUSHING. (M)Jul 18, 2004 · N429AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA200440112Striker · damagedPASSENGER DOOR SEAL STRIKER HAS DAMAGE AT FS 349 APPROXIMATELY MID POINT OF DOOR OPENING. REPAIRED PASSENGER DOOR SEAL STRIKER AT FS 349 IAW BOMBARDIER REO 601R-53-22-033 REPAIR 4. (M)Jul 17, 2004 · N429AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200440111Striker · damagedPASSENGER DOOR SEAL STRIKER HAS DAMAGE AT FS 310 APPROXIMATELY MID POINT OF DOOR OPENING. REPAIRED PASSENGER DOOR SEAL STRIKER AT FS 310 IAW BOMBARDIER REO 601R-53-22-033. (M)Jul 17, 2004 · N429AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200440102Floor Support · crackedFOUND FLOOR SILL SUPPORT ANGLE AT FS 621 RBL 45 IS CRACKED. PERFORMED A MAJOR REPAIR BY TRIMMING OUT CRACKED AREA OF SUPPORT AGNLE AND INSTALLING REPAIR ANGLE P/N 601R53-61-117-4 IAW BOMBARDIER REO 601R-53-61-117 REV B. (M)Jul 17, 2004 · N429AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440106Vane · chafedRIGHT INBOARD FLAP VANE AT FLAP STATION 60.005 IS CHAFED .012 INCH DEEP. PERFORMED A MAJOR REPAIR TO RIGHT INBOARD FLAP VANE BY REMOVING INBOARD END LEADING EDGE SKIN AND INSTALLING NEW LEADING EDGE SKIN, P/N 601R14303-54 IAW CRJ SRM 51-42-13. (M)Jul 17, 2004 · N429AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200440015Flap · stuckON TAKEOFF, FLAPS STUCK AT 20 DEGREES. FECU INTERROGEAED NIL FAULTS FOUND. AIRCRAFT HANGARED 4.5 HOURS. FECU SYSTEM TESTED AS PER 27-51-05-946-009 JOB TASK. FLAPS CYCLED ALL POSITIONS, CHECKED SERVICEABLE. (M)Jan 30, 2004 · N429AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200340115Idg · lack of lubeGENERATOR 2 FAILED UPON APPLICATION OF TAKEOFF POWER. SERVICED IDG OIL AS REQUIRED, OPS CHECK GOOD.Jul 30, 2003 · N429AW · Cndair CL6002B19 · AC Generation System
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