N468AW

Service difficulty reports · 177

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 = 'N468AW' 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 A6WA200940667Panel · damagedRT INBD FLAP, PANEL 684AB L/E SCREW HOLES DAMAGED. RT INBD FLAP, PANEL 684AB L/E, RETAINING PLATE REPLACED IAW SRM 51-42-06. (K)Sep 29, 2009 · N468AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200940663Access Panel · wornSEPARATOR WORN ON RT PYLON ACCESS PANEL 422DB. SEPARATOR ON RT PYLON ACCESS PANEL 422DB REPLACED IAW SRM 51-42-06 AND 51-42-13. (K)Sep 29, 2009 · N468AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA200940648Plate · crackedLT SILL (FLOOR LANDING PLATE PN 601R35011-53) CRACKED AT FS 589.00 AND FS 605.00, BOTH CRACKS LENGTH .500" LT SILL (FLOOR LANDING PLATE) REPAIRED IAW REO 601R-53-61-433. (K)Sep 29, 2009 · N468AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940664Drag Angle · crackedPASSENGER DOOR AFT DRAG ANGLE FOUND CRACK AT FS 349.00, 1" LONG. PASSENGER DOOR AFT DRAG ANGLE REPAIRED. JOB COMPLETED IAW REO 601R-52-11-513, REV A. (K)Sep 29, 2009 · N468AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200940675Bulkhead · crackedAFT PRESSURE BULKHEAD AT FS 621.00 FOUND CRACKED AT LINTEL FITTING LOCATION (.250 LONG). AFT PRESSURE BULKHEAD FS 621.00 AT LINTEL LOCATION REPAIR PERFORMED IAW REO 601R-53-61-1230. (K)Sep 29, 2009 · N468AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200840302Door · stuckUNABLE TO OPEN SERVICE DOOR USING OUTSIDE HANDLE. (M)Apr 9, 2008 · N468AW · Cndair CL6002B19 · Service DoorsSDR A6WA200840108Unknown · smokeSMOKE TOILET CAUTION MESSAGE ON SHORT FINAL. FLIGHT ATTENDANT REPORTS PHYSICAL SMOKE COMING FROM AREA OF LAV CEILING. REMOVED SMOKE DETECTOR AND LAV SPEAKER AND INSPECTED AREA BEHIND BOTH. REINSTALLED AND PERFORMED OPS TEST OF DETECTOR PER AMM 26-16-01. NOFeb 22, 2008 · N468AW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA200840053Smoke Warning · malfunctionedINFLIGHT DURING BLEED TRANSFER (SMOKE TOILET) CAS MESSAGE APPEARED. COMPLIED WITH QRH. MESSAGE WENT AWAY. FLIGHT ATTENDANT REPORTED ACRID SMELL IN CABIN. (K)Jan 26, 2008 · N468AW · Cndair CL6002B19 · Smoke DetectionSDR A6WA200840002Terminal · burnedGENERATOR NR 1 CAUTION RECEIVED AT CRUISE, COMPLIED WITH QRH. FOUND AC GENEATOR BURNED UP AT TERMINALS. REMOVED AND REPLACED GENERATOR NR 1 ASSY IAW AMM 24. (K)Dec 2, 2007 · N468AW · Cndair CL6002B19 · Electrical Power System WiringSDR A6WA200740576Skin · corrodedRIGHT LOWER WING PLANK FOR FUEL PANEL 650AB CUT OUT HOLE NR 9 HAS MINOR CORROSION IN NON-CRITICAL AREA APPROX .003 INCH DEEP. MAINTENANCE REPAIRED RT LOWER WING PLANK FOR FUEL PANEL 650AB CUT OUT HOLE NR 9 IAW AIR WISCONSIN E06/021/457 AND BOMBARDIER REO 601RSep 25, 2007 · N468AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740575Skin · corrodedLT LOWER WING PLANK FUEL PANEL CUTOUT FOR PANEL 510AB HOLE NR 2 HAS MINOR CORROSION IN NON-CRITICAL AREA APPROX .003 INCH DEEP. MAINTENANCE REPAIRED LT LOWER WING PLANK FUEL PANEL CUT OUT FOR PANEL 510AB HOLE NR 2 IAW AIR WISCONSIN E06/021/457 AND BOMBARDIER Sep 25, 2007 · N468AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740577Skin · corrodedRIGHT LOWER WING PLANK FUEL PANEL CUT OUT FOR PANEL 640BB HOLE NR 1 HAS MINOR CORROSION IN NON-CRITICAL AREA APPROX .003 INCH DEEP. MX REPAIRED RIGHT LOWER WING PLANK FUEL PANEL CUT OUT FOR PANEL 640BB HOLE NR 1 IAW AIR WISCONSIN E06/021/457 AND BOMBARDIER RESep 25, 2007 · N468AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740522Angle · crackedFOUND LEFT 484 ANGLE IS CRACKED AT LBL 27 APPROX .25 INCH LONG. 10-15-07 MAINTENANCE REMOVED CRACKED ANGLE AT FS 484 LBL 27. FABRICATED REPAIR ANGLE FROM PREFORMED ANGLE LOCATED DRILLED AND INSTALLED IAW BSC STANDARD REPAIR 601R-53-0029B. (M)Sep 20, 2007 · N468AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740521Angle · crackedFOUND LEFT 484 ANGLE IS CRACKED AT LBL 36 APPROX .25 INCH LONG. 10-25-07 MAINTENANCE REPAIRED IAW REO 601R-53-41-059. (M)Sep 20, 2007 · N468AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740520Angle · crackedFOUND RIGHT 484 ANGLE IS CRACKED AT RBL 36 APPROX .25 INCH LONG. 10-25-07 MAINTENANCE REPAIRED IAW REO 601R-53-41-059. (M)Sep 20, 2007 · N468AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740519Angle · crackedFOUND RIGHT 484 ANGLE IS CRACKED AT RBL 27 APPROX .25 INCH LONG. 10-25-07 MAINTENANCE REMOVED CRACKED ANGLE AT FS 484 RBL 27. FABRICATED REPAIR ANGLE FROM PERFORMED ANGLE LOCATED, DRILLED AND INSTALLED IAW BSC STANDARD REPAIR 601R-53-0029B. (M)Sep 20, 2007 · N468AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740518Angle · crackedFOUND LEFT 621 ANGLE IS CRACKED APPROX 1.5 INCH LONG. 10-25-07 MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R5361117. (M)Sep 20, 2007 · N468AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740517Angle · crackedFOUND RIGHT 621 ANGLE IS CRACKED APPROX 1.5 INCH LONG. 10-25-07 MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R-53-61-117. (M)Sep 20, 2007 · N468AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740516Attach Fitting · damagedRIGHT ELEVATOR NR 3 HYD SYSTEM PCU ATTACHMENT FITTING ASSY ON ELEVATOR, P/N 601R24056-41, HAS SHEARED LOCK FASTENER AT BOTTOM OF LINK. 10-25-07 MAINTENANCE REPLACED LOCK FASTENER IAW SRM 51-42-21. (M)Sep 19, 2007 · N468AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA200740515Attach Fitting · damagedLT ELEVATOR NR 2 HYD SYSTEM PCU ATTACHMENT FITTING ASSY ON ELEVATOR, P/N 601R24056-443, HAS SHEARED LOCK FASTENER AFT BOTTOM OF LINK. IAW SRM 51-42-21. (M)Sep 19, 2007 · N468AW · Cndair CL6002B19 · Wing, Attach FittingsSDR A6WA200740514Attach Fitting · damagedLT ELEVATOR NR 1 HYD SYSTEM PCU ATTACHMENT FITTING ASSY ON ELEVATOR, P/N 601R24056-45, HAS SHEARED LOCK FASTENER AT BOTTOM OF LINE. 10-25-07 MAINTENANCE REPLACED LOCK FASTENER IAW SRM 51-42-21. (M)Sep 19, 2007 · N468AW · Cndair CL6002B19 · Wing, Attach FittingsSDR A6WA200740513Intercostal · crackedFOUND LEFT FS 621 TO 625.30 INTERCOSTAL AT STRINGER 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. 10-25-07 MAINTENANCE REMOVED AND REPLACED LT SIDE INTERCOSTAL LOCATED AT FS 621 TO 625.30 STRINGER 14 P/N 601-35012-51 IAW CRJ200 SRM 51-42-06. (M)Sep 17, 2007 · N468AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740512Intercostal · crackedFOUND RIGHT FS 621 TO FS 625.30 INTERCOSTAL AT STRINGER 14R IS CRACKED NEAR RADIUS APPROX 1 INCH LONG. 10-25-07 MAINTENANCE REPLACED RT INTERCOSTAL AT FS 621 TO 625.30 AT STRINGER 14R IAW CRJ 200 SRM 51-42-06. (M)Sep 17, 2007 · N468AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740183Unknown · unknownUPON LANDING THRUST REVERSERS WOULD NOT DEPLOY UNTIL AFTER 3,000 FT ROLLOUT, NEITHER REVERSER WOULD UNLOCK UNTIL BRAKES TOOK EFFECT. PERFORMED BRAKES OPS TEST IAW 32-43-00, PERFORMED ANTI-SKID COMPUTER BITE TEST IAW 32-44-06. INTERROGATED MDC, NO FAULTS FOUNApr 2, 2007 · N468AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA200640357Adg · unwanted deployAIR DRIVEN GENERATOR AUTO DEPLOYED IN FLIGHT. NO ADVERSE ELECTRICAL MESSAGES. NOTED ADG HANDLE STOWED. FLIGHT LEVEL 370. RESTOWED AIR DRIVEN GENERATOR IAW CRJ AMM 24-23-01 AS REQUIRED. UPLOCK FUNCTIONS NORMALLY. (M)Oct 3, 2006 · N468AW · Cndair CL6002B19 · AC Generation SystemSDR A6WA200540350Door · missingON CLIMB OUT, FELT LURCH. UPON INSPECTION, DISCOVERED LT ENGINE DOOR MISSING. REMOVED AND REPLACED LT LOWER COWL DOOR. (PN 228-50081-141). (K)Dec 7, 2005 · N468AW · Cndair CL6002B19 · Engine Cowling SystemSDR A6WA200440077Wheel · damagedUPON LANDING, NOSEWHEEL MADE STRANGE NOISE, STOP ON TAXI WAY AND LEFT NOSEWHEEL MISSING BEARING AND ABOUT TO FALL OFF. REMOVED AND REPLACED NLG SLIDING MEMBER, PER AIRCRAFT AMM 32-21-30. ALL OPS CHECK NORMAL. REMOVED AND REPLACED BOTH NLG WHEEL ASSEMBLIES. Jun 10, 2004 · N468AW · Cndair CL6002B19 · Wheel/Ski/Float
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