N462AW

Service difficulty reports · 197

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 = 'N462AW' 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 A6WA201140495Attach Bracket · chafedRT OTBD FLAP ROLLER GUIDE ATTACH CRACKED AND GUIDE FITTING HAVE CHAFE AND GOUGE DAMAGE. BLENDED RT OTBD GUIDE ATTACHED BRACKET AND RT OTBD FLAP GUIDE FITTING IWA 601R-57-51-143.Jun 12, 2011 · N462AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201140494Track · gougedCARGO DOOR AFT TRACK GOUGED. BLENDED GOUGED AREA OF THE CARGO DOOR AFT TRACK. REMOVING .055" LEAVING .215" MATERIAL IAW REO 601R-53-62-024 WITHIN LIMITS.Jun 12, 2011 · N462AW · Cndair CL600* · Fuselage Main, StructureSDR A6WA201140498Skin · chafedRT INBD FLAP VANE L/E CHAFED AT INBD CTR AND OTBD SECTIONS BLENDED CHAFE AREAS ON THE RT INBD FLAP VANE L/E AT INBD, CTR AND OTBD SECTIONS ALL 3 AREAS WITHIN LIMITS IAW REO 601R-57-52-004.Jun 12, 2011 · N462AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201140492Vane · chafedLT INBD FLAP VANE CHAFED FROM STOPS AT CTR AND OTBD LOCATIONS. BLENDED MINOR CHAFE MARKS AT LT INBD FLAP VANE CTR AND OTBD LOCATIONS. CTR AND OTBD CHAFES WITHIN ALLOWABLE LIMITS IAW 601R-57-52-004.Jun 10, 2011 · N462AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201140486Bracket · crackedSUPPORT FOR PAX DOOR BRACKET (832CT) CRACKED IN RADIUS, PAX DOOR FWD STAIR SIDE PANEL 2ND STEP WHEN OPEN. REPAIRED DAMAGE TO SUPPORT FOR 832CT (FWD SIDE) IAW REO 601R-52-11-702.Jun 9, 2011 · N462AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140485Support · crackedSUPPORT FOR 832 CT CRACKED. PAX DOOR AFT STAIR SIDE PANEL AT 2ND STEP WHEN OPEN. REPAIRED DAMAGE TO SUPPORT FOR 832CT (AFT SIDE) IAW REO 601R-52-11-702.Jun 9, 2011 · N462AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140487Hinge Fitting · gougedPAX DOOR HINGE LUG NR 3, 4 AND 25 (DOOR SIDE) HAS MINOR GOUGES BLENDED OUT MINOR GOUGES IAW SRM 51-12-00. FOUND TO BE WITHIN LIMITS IAW REO 601R-52-11-1347, TYPE 1 DISPOSITION.Jun 8, 2011 · N462AW · Cndair CL6002B19 · Fuselage, Door HingeSDR A6WA201040975Valve · malfunctionedAPU WOULD NOT START ON 1ST ATTEMPT, STRONG ODOR OF JET FUEL, BLEEDS REMAINED ON ENGINE BLEEDS. RAN APU SEVERAL TIMES, NO PROBLEMS STARTING, APU, NO LEAKS NOTED, R & R BOTH PACK COALESCER BAGS IAW AMM 21, R & R APU FUEL COMBUSTOR DRAIN VALVE IAW AMM 49, RAN APDec 28, 2010 · N462AW · Cndair CL6002B19 · APU Engine Fuel and ControlSDR A6WA201040819Unknown · odorAPU WOULD NOT START IN FLIGHT. AFTER LANDING APU STARTED & FUEL ODOR NOTED IN CABIN RT AFTER START, THEN DISSAPATED SHORTLY AFTERWARDS. INSPECTED APU, FOUND NO FUEL LEAKS. RAN APU FOR 20 MINUTES, NO ODOR NOTED. OK FOR SERVICE.Nov 15, 2010 · N462AW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA201040813Coalescer Bag · dirtySTRONG FUEL ODOR IN CABIN ON APPROACH. BEFORE APU START AND BEFORE FLAPS AND GEAR. INSPECTED FUEL SHROUD DRAINS, APU BOX AND AFT EQUIPMENT BAY NO LEAKS FOUND. R & R LT AND RT COALESCERS IAW AMM 21-51-13. OPS CHECK GOOD AT THIS TIME. NO FUEL LEAKS NOTED ONNov 9, 2010 · N462AW · Cndair CL6002B19 · Humidity Control SystemSDR A6WA200940512Overheat Loop · damagedAT CRUISE ALTITUDE, RECEIVED MLG BAY OVERHEAT FAIL CAUTION MESSAGE INTERMITTENTLY. FOLLOWED BY MLG BAY OVERHEAT WARNING MESSAGE WITH TRIPLE CHIME. C/W QRH, BTMS 1-1-1-1. REMOVED AND REPLACED RT WHEEL WELL LOOP IAW AMM 26-14-00. OPS CHECK GOOD. (K)Aug 25, 2009 · N462AW · Cndair CL6002B19 · Overheat DetectionSDR A6WA200940360Fitting · crackedCRACK FOUND ON REAR PRESSURE BULKHEAD AT LINTEL FITTING LOCATION. REAR PRESSURE BULKHEAD REPAIRED AT LINTEL FITTING LOCATION IAW REO 601R-53-61-1230 REV D. (K)Jun 26, 2009 · N462AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200940354Bulkhead · crackedFWD PRESSURE BULKHEAD FS 202.75, LBL 23.71 CRACKED. FWD PRESSURE BULKHEAD FS 202.75, LBL 23.71, REPAIRED IAW REO 601R-53-11-1681. (K)Jun 25, 2009 · N462AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940357Bulkhead · damaged2 RIVET DAMAGE AND SCRATCH FOUND ON FWD COMPARTMENT PRESSURE BULKHEAD FS 280.00, RBL 9.0, WL 94.50. FWD COMPARTMENT PRESSURE BULKHEAD FS 280, RBL 9 WL 94.50. REPAIRED IAW REO 601R-53-11-1677, REV A . (K)Jun 25, 2009 · N462AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940407Structure · crackedRT ENG NOSE INLET COWL BRIDGING PIECE FOUND CRACKED. RT ENG NOSE COWL BRIDGING PIECE REPLACED IAW CMM 20-41-04. (K)Jun 23, 2009 · N462AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA200940364Skin · crackedDURING MODIFICATION OF THE ENGINE SUPPORT BEAM, REWORK LT AND RT SKIN AND SKIN DOUBLER IN ORDER TO ELIMINATE EXISTING CRACK IN INTERNAL DOUBLER. REWORK LT AND RT SKIN AND SKIN DOUBLER C/O IAW MODSUM NR TC 601R17262.Jun 23, 2009 · N462AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200940365Skin · damagedDURING MODIFICATION OF THE ENGINE BEAM REWORK LT AND RT SKIN AND SKIN DOUBLER IN ORDER TO ELIMINATE ATTACHMENT AT DISCREPANT FASTENER LOCATION DUE TO FALLING CONDITION ON ANGLE PN 601R350073-3 AND -4. REWORK ON LT AND RT SKIN AND SKIN DOUBLER PERFORMED IAW MOJun 23, 2009 · N462AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200940361Throttle Cable · obstructedDURING MODIFICATION OF THE ENGINE SUPPORT BEAM REWORK ON RT AND LT UPPER AND LOWER PYLON TO FUSELAGE FITTING TO ELIMINATE HOW EDGE DISTANCE AND FOULING CONDITION WITH THE TROTTLE CABLE. REWORK ON RT LAND LT UPPER AND LOWER PYLON TO FUSELAGE FITTING C/O MODSUMJun 23, 2009 · N462AW · Cndair CL6002B19 · Power LeverSDR A6WA200940406Attach Fitting · crackedINTERCOSTAL CLIP CRACKED AT FS 484, LBL 27. INTERCOSTAL CLIP REPLACED AT FS 484, LBL 27 SRM 51-42-06 AND ARM 51-42-20. (K)Jun 22, 2009 · N462AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200940355Intercostal · crackedRT INTERCOSTAL CLIP FS 621-625 ADJACENT TO STR 14 CRACKED. RT INTERCOSTAL CLIP FS 621-625 ADJACENT TO STR 14 REPLACED IAW SRM 51-42-06 AND 51-42-21. (K)Jun 22, 2009 · N462AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940358Angle · crackedFS 280 UPPER ANGLE CRACKED AT LBL 9. FL 280 UPPER ANGLE REPAIR IAW REO 601R-53-11-138 REV NC. (K)Jun 22, 2009 · N462AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940359Floorbeam · crackedCRACK ON FLOORBEAM CLIP FS 280, LBL 9, INBD AND OTBD. FLOORBEAM CLIP REPLACED ON FS 280, LBL 9 INBD AND OTBD. (K)Jun 22, 2009 · N462AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200940356Intercostal · crackedLT INTERCOSTAL FS 621-625 ADJACENT TO STR 14 CRACKED. LT INTERCOSTAL FS 621-625 ADJACENT TO STR 14 REPLACED IAW SRM 51-42-06 AND 51-42-21. (K)Jun 22, 2009 · N462AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940367Floorbeam · corrodedFS 280.0 FLOORBEAM CRACKED AT RBL 9.0 LOWER RADIUS FS 280.0 FLOORBEAM AT RBL 9.0 REPAIR CARRIED OUT IAW REO 601R-53-11-171, REV D. SCHEME B. (K)Jun 18, 2009 · N462AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200940352Intercostal · crackedCRACK FOUND ON INTERCOSTAL FS 484, LBL 36. REPAIR PERFORMED ON INTERCOSTAL FS 484, LBL 36 IAW REO 601R 53-41-59 REV A. (K)Jun 18, 2009 · N462AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940353Intercostal · crackedCRACK FOUND ON INTERCOSTAL FS 484, RBL 36. REPAIR PERFORMED ON INTERCOSTAL FS 484, RBL 36, IAW REO 601R-53-41-059 REV A. (K)Jun 18, 2009 · N462AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940366Bracket · crackedCARGO DOOR FLOOR SILL CRACKED AT FWD STOW PLATE BRACKET (CRACK LENGTH .500) CARGO DOOR FLOOR SILL AT FWD STOW PLATE BRACKET REPAIRED IAW REO 601R-53-61-1741. (K)Jun 17, 2009 · N462AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940378Flex Drive · corrodedFLEXSHAFT ON FLAP FOUND WITH HEAVY CORROSION ON 70 PERCENT OF THE COIL SURFACE AND SEIZED IN ACTUATOR. B-NUT FOUND IMPROPERLY TORQUED AT THE SEIZED END. SUBSEQUENT DAMAGE ON TERMINAL. C/A IN PROGRESS. (K)Jun 15, 2009 · N462AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200940006Line · brokenHYDRAULICS 1 LOW PRESSURE MSG. CW QRH NR 1 HYD PRESSURE AT ZERO PSI AND NR 1 HYD QUANTITY SHOWS AMBER DASHES. DIVERTED TO CRW. FLIGHT TIME AT ZERO PSI WAS 46 MINUTES. 1B PUMP OPERATED FOR 2 MINUTES. FOUND BROKEN LINE ON NR 1 NYD SYSTEM FROM EDP TO CASE DRJan 4, 2009 · N462AW · Cndair CL6002B19 · Hydraulic System, MainSDR A6WA200840299Connector · looseINTERMITTENT MLG BAY OVERHEAT FAULT THEN MLG BAY OVER HEAT INDICATION DIVERTED TO SCE. BRAKE TEMPS INDICATED NORMAL AT ALL TIMES (01 ON ALL FOUR). SECURED LOOSE CONNECTION ON RT MLG BAY FIRELOOP. REPAIRED BROKEN CONNECTION ON LT MLG FIRELOOP. COMPLIED WITH FUApr 7, 2008 · N462AW · Cndair CL6002B19 · Fire Protection System WiringSDR A6WA200840178Landing Gear · malfunctionedAFTER TAKEOFF UPON GEAR RETRACTION NOSE GEAR SHOWED DOWN WITH GEAR DISAGREE, COMPLIED WITH QRH, PERFORMED MANUAL GEAR EXTENSION, RETURNED TO ROS. (M)Mar 10, 2008 · N462AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA200840174Structure · damagedWINDSHEAR DURING LANDING LEFT WING PUSHED UP AND RIGHT WINGSTRIP SCRAPED RUNWAY. (M)Mar 8, 2008 · N462AW · Cndair CL6002B19 · Wing Main, Frame StructureSDR A6WA200840048Pitot System · contaminatedON TAKEOFF ROLL STANDBY IAS READS -0- KNOTS, REJECTED TAKEOFF AT ABOUT 85 KNOTS, MAX BTMS = 8,7,6,6. NOTE: NO HES/RTO INSPECTION REQUIRED. FOUND WATER IN THE STANDBY PITOT/STATIC SYSTEM. PERFORMED CONTAMINATION REMOVAL OF THE STANDBY PITOT/ STATIC SYSTEM. Feb 2, 2008 · N462AW · Cndair CL6002B19 · Pitot/Static SystemSDR A6WA200740431Control Unit · failedCAUTION MESSAGE INFLIGHT, STAB TRIM, MACH TRIM, AUTOPILOT TRIM NOSE DOWN. PITCH STUCK AT 6.0. WHEN AUTOPILOT DISENGAGED AT 1000` AGL ALL MESSAGES DISAPPEARED PITCH TRIM WAS OPERATIONAL. HSTCU FAIL, REMOVED AND REPLACED HSTCU IAW 27-41-01, NO FAULTS NOTED. Jul 30, 2007 · N462AW · Cndair CL6002B19 · Elevator Control SystemSDR A6WA200740345Channel · crackedHYDRAULIC PRESSURE TRANSDUCER HAT CHANNEL (PN 601R75262-159) CRACKED APPROX .2 INCH LONG IN LT MLG WHEEL WELL CEILING. MAINTENANCE REMOVED AND REPLACED CHANNEL PN 601R75262-159 IAW SRM 51-42-06. (K)Jun 25, 2007 · N462AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740343Bracket · crackedHYDRAULIC LINE Z-BRACKET (PN 601R75262-153) CRACKED APPROX .1 INCH LONG IN RT MLG WHEEL WELL. MAINTENANCE REMOVED AND REPLACED BRACKET (PN 601R75262-153) IAW SRM 51-42-06. (K)Jun 25, 2007 · N462AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740342Transducer · crackedHYDRAULIC PRESSURE TRANSDUCER (PN 610R75262-157) CRACKED APPROX .2 INCH LONG INRT MLG WHEEL WELL CEILING. MAINTENANCE REMOVED CRACKED HAT CHANNEL AND INSTALLED SERVICEABLE HAT CHANNEL PN 601R75262-157 IAW SRM 51-42-06. (K)Jun 25, 2007 · N462AW · Cndair CL6002B19 · Hydraulic Indicating SystemSDR A6WA200740335Floorbeam · crackedLT FS 621 FLOOR SUPPORT ANGLE CRACKED APPROX .2 INCH LONG. MAINTENANCE CUT OUT DAMAGED AREA AND INSTALLED REPAIR ANGLE IAW REO 601R-53-61-117. (K)Jun 25, 2007 · N462AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740334Floor Support · crackedRT FS 621 FLOOR SUPPORT ANGLE APPROX .2 INCH LONG. MAINTENANCE REMOVED DAMAGED AREA AND INSTALLED REPAIR ANGLE IAW REO 601R-53-61-117. (K)Jun 25, 2007 · N462AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740344Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED JUST ABOVE ASSIST MOTOR PULLEY BRACKET. MAINTENANCE CUT OUT DAMAGED AREA AND INSTALLED REPAIR ANGLE IAW REO 601R-52-11-513. (K)Jun 24, 2007 · N462AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740340Floorbeam · crackedRT FS 484 ANGLE IS CRACKED AT RBL 27 AND 36 APPROX 1.4 INCH L. MAINTENANCE REPAIRED RT FS 484 ANGLES AT RBL 27 AND RBL 36 IAW REO 601R-53-41-059 AND BSC STANDARD REPAIR 601R-53-0030A. (K)Jun 24, 2007 · N462AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740339Floorbeam · crackedLT FS 484 ANGLE IS CRACKED AT LBL 36 AND 27 APPROX 1.4 INCH L. MAINTENANCE REPAIRED LT FS 484 IAW REO AND SRM. (K)Jun 24, 2007 · N462AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740338Channel · crackedCARGO DOOR FWD TRACK C-CHANNEL HAS A .5 INCH LONG CRACK WL. (K)Jun 24, 2007 · N462AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA200740336Intercostal · crackedLT FS 625 OBLIQUE ANGLE IS CRACKED APPROX 1 INCH L. MAINTENANCE REMOVED AND REPLACED ANGLE IAW SRM 51-42-06, 51-42-21 AND REO 601R-53-61-422. (K)Jun 23, 2007 · N462AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640390Control Unit · unknownSTAB CHANNEL 1 INOP STATUS MESSAGE IN FLIGHT, COULD NOT RESET. AIR RETURN TO DEPARTURE. REMOVED AND RETURNED HSTCU IAW AMM 27-41-01. OPS CHECK GOOD. (K)Nov 22, 2006 · N462AW · Cndair CL6002B19 · Stabilizer Control SystemSDR A6WA200640369Idg · malfunctionedIDG NR 1 CAUTION MESSAGE ON TAKEOFF ROLL. ABORTED TAKEOFF AT LESS THAN 40 KNOTS. BTMS TEMPS WERE 2-2-3-2. REMOVED AND REPLACED IDG NR 1, OPS CHECK GOOD, IAW 24-11-01. LEAK AND OPS CHECK GOOD. (M)Oct 23, 2006 · N462AW · Cndair CL6002B19 · AC Generator-AlternatorSDR A6WA200540257Channel · crackedCHANNEL OF MAIN UNDERCARRIAGE AND UPLOCK APRON BENT AND CRACKED. REPAIRED IAW EO. (K)Jul 2, 2005 · N462AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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