N464AW

Service difficulty reports · 216

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 = 'N464AW' 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 A6WA201140914Seat Track · corrodedCARGO FLOOR TRACK RBL 9 AFT OF FS 559+80 HAS CORROSION. R & R SEAT (RAIL) TRACK AT RBL 9 AFT OF FS 559+80.Sep 15, 2011 · N464AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201140932Plate · chafedPAX DOOR FWD & AFT STRIKER PLATES CHAFED. BLENDED OUT CHAFE.Sep 15, 2011 · N464AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140913Seat Track · corrodedCARGO FLOOR TRACK, LBL 9 AFT OF FS 589+80 HAS CORROSION. R & R SEAT (RAIL) TRACK AT LBL 9 AFT OF FS 589+80.Sep 15, 2011 · N464AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201140933Structure · crackedPAX DOOR AFT EDGE MEMBER CRACKED. REPAIRED PAX DOOR AFT EDGE MEMBER IAW REO 601R5211279.Sep 15, 2011 · N464AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140908Skin · dentedON RT SIDE OTBD OF AFT EQUIPMENT BAY OTBD OF DOOR ACFT HAS A DENT WITH A SCRATCH EXTENDING THRU DENT CUTOUT DAMAGED AREA ON RT OF OTBD OF AFT EQUIPMENT BAY OTBD OF DOOR REPAIRED ARE IAW REO 601R-53-00-023 BY INSTALLING PATCH/DOUBLER OVER DAMAGED AREA.Sep 14, 2011 · N464AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA201140915Angle · crackedRIGHT OBLIQUE ANGLE CRACKED AT 621 PN 601-35012-52. R & R RT OBLIQUE ANGLE IAW REO 601R-53-61-422, REV NC.Sep 13, 2011 · N464AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201140918Retainer · crackedPYLON PANEL 422AT HAS A CRACK IN THE SEAL RETAINER. REPLACED SEAL RETAINER.Sep 13, 2011 · N464AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA201140922Seal · chafedLT SIDE OF FUSELAGE IS CHAFED BY THE LT INBD SEAL OF THE WING AND THE LT STUB FAIRING COMPLIED WITH REO 601R-53-41-341.Sep 13, 2011 · N464AW · Cndair CL6002B19 · Aerodynamic FairingsSDR A6WA201140916Angle · crackedLT OBLIQUE ANGLE CRACKED AT 621, PN 601-35012-51. R & R LT OBLIQUE ANGLE IAW REO 601R-53-61-422, REV NC.Sep 13, 2011 · N464AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201140919Doubler · crackedRIGHT JET PIPE LOWER NUTPLATE DOUBLER IS CRACKED. REMOVED DAMAGED DOUBLER AND REPLACED WITH NEW.Sep 12, 2011 · N464AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR A6WA201140917Retainer · crackedPYLON PANEL 422BT HAS A CRACK IN THE SEAL RETAINER. R & R SEAL RETAINER.Sep 12, 2011 · N464AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201140926Skin · chafedRT INBD FLAP VANE IS CHAFED IN 3 PLACES. BLENDED 3 PLACES ON LT INBD FLAP VANE REMOVED OF MAT REMAINING MAT IS WITHIN SERVICEABLE LIMITS IAW SRM 51-12-00.Sep 9, 2011 · N464AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201140925Shroud · chafedINBD FIXED LOWER SHROUD ON RT AILERON IS CHAFED. BLENDED RT AILERON LOWER SHROUD IAW SRM 51-12-00 MAT LOSS .006, REMAINING MAT IS WITHIN SERVICEABLE LIMITS IAW REO 601R-57-60-020.Sep 9, 2011 · N464AW · Cndair CL6002B19 · AileronsSDR A6WA201140921Skin · chafedLEFT INBD FLAP VANE IS CHAFED. BLENDED LT INBD FLAP VANE, REMOVED .004 MAT, REMAINING MAT IS WITHIN SERVICEABLE LIMITS IAW SRM 51-12-00.Sep 9, 2011 · N464AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201140920Shroud · chafedINBD FIXED LOWER SHROUD ON LT AILERON IS CHAFED. BLENDED INBD LOWER SHROUD ON LT AILERON IAW SRM 51-12-00 MAT LOSS .008, REMAINING MAT IS WITHIN SERVICEABLE LIMITS IAW REO 601R-57-60-020.Sep 9, 2011 · N464AW · Cndair CL6002B19 · AileronsSDR A6WA201140924Shroud · chafedRT AILERON SHROUD PANEL 699BB IS CHAFED. BLENDED RT AILERON SHROUD PANEL 699BB IAW SRM 51-12-00 MAT LOSS, .009 REMAINING MAT IS WITHIN SERVICEABLE LIMITS IAW REO 601R-57-60-020.Sep 9, 2011 · N464AW · Cndair CL6002B19 · AileronsSDR A6WA201140923Shroud · chafedRT AILERON SHROUD PANEL 699AB IS CHAFED. BLENDED RT AILERON SHROUD PANEL 699AB IAW SRM 51-12-00 MAT LOSS, .007 REMAINING MAT IS WITHIN SERVICEABLE LIMITS IAW REO 601R5-57-60-020.Sep 9, 2011 · N464AW · Cndair CL6002B19 · AileronsSDR A6WA201140672Acm · failedSTRONG SULFUR/PLASTIC ODOR FROM PACK, AND LOUD WHINNING NOISE FROM REAR OF PLANE AT SAME TIME. CONFIRMED LT PACK ACM SEIZED, SEE 230117/4 FOR LT PACK MEL. R & R RT PACK PRSOV IAW AMM 21-51-43, RT PACK OPS CHECKED GOOD.Aug 1, 2011 · N464AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA201140170Engine · flamed outAFTER 10,000 FT AND INCREASING TO CLIMB POWER, LEFT ENG ITT 854C, 62 DEGREE HIGHER THAN RT ENG ACARS`D MX, THEY REQUESTED CHECK WITH SPEED SWITCHES OFF, COMPLIED, NO DIFFERENCE NOTED REDUCED POWER, TURNED RT SPEED ON, NO DIFFERENCE. TURNED LT SPEED ON, ENGINEMar 7, 2011 · N464AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA201040540Ignition Unit · inoperativeAPU WILL NOT START, START SEQUENCE NORMAL TO 25 PERCENT RPM, THEN RPM HANGS AND STRONG ODOR OF JET FUEL PRESENT. RAMP AGENTS REPORT SMOKE FROM APU EXHAUST. REPLACED APU IGNITION UNIT IAW AMM 49-41-01. OPS CK OF APU GOOD AT THIS TIME.Jul 21, 2010 · N464AW · Cndair CL6002B19 · APU Start/Ignition SystemSDR A6WA201040227Apu · odorAFTER TRANSFERRING BLEEDS OT APU, SMOKE ENGULFED THE COCKPIT AND CABIN AREA, REQUEST INSP. FOUND ODOR TO BE PRESERVATIVE OIL USED IN APU. PERFORMED OPS CK OF LT/RT ACM`S. RAN ACM`S TO BURN RESIDUAL PRESERVATIVE OIL. NO ODOR NOTED AT THIS TIME.Mar 17, 2010 · N464AW · Cndair CL6002B19 · APU Core EngineSDR A6WA200940545Seal · failedUPON CLIMBOUT, CABIN RATE CLIMB ABNORMALLY. ACFT NEVER PRESSURIZED CABIN ALT WAS 6700 FT AT 8000FT. C/W QRH SELECTED TO MANUAL PRESSURIZATION. ACFT DID NOT PRESSURIZE. REMOVED AND REPLACED SERV DOOR SEAL IAW 52-41-07. ALL WORK DONE ON W/O 140531. (K)Sep 6, 2009 · N464AW · Cndair CL6002B19 · Service DoorsSDR A6WA200940555Lug · damagedLT MLG DOOR LUG DAMAGED DUE TO WRONG HARDWARE INSTALLED ON ROD DOOR, LT MLG DOOR LUG REPAIRED IAW REO 601R-52-82-247 NC. (K)Aug 25, 2009 · N464AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA200940556Lug · gougedRT MLG DOOR LUG HAS GOUGES DUE TO END ROD. RT MLG DOOR LUG REPAIRED IAW REO 601R-52-82-247. (K)Aug 25, 2009 · N464AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA200940548Floorbeam · corrodedFWD ANGLE FLOORBEAM AT FS 280.00 CORRODED. FWD ANGLE FLOORBEAM AT FS 280.00 CORROSION REMOVED IAW SRM 51-21-06.Aug 25, 2009 · N464AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200940559Sill · crackedLT STGR 17 ON FLOOR SILL, QTY (X3) CRACK FOUND AROUND FASTENER HOLE OF RETAINING CLIP, DIMENSIONS ARE 0.100 TO .250 INCHES LONG. REPAIR AT FS 575.5 LT STGR 17 ON SILL FLOOR IAW REO 601R-53-61-1741. (K)Aug 25, 2009 · N464AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940554Frame · crackedLT TOP FLANGE OF AFT ANGLE AT FS 280.00 CRACKED LT TOP FLANGE OF AFT ANGLE AT FS 280.00 CRACKED REPAIRED IAW REO 601R-53-11-138. (K)Aug 21, 2009 · N464AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA200940561Frame · crackedBOTTOM FLANGE OF FS 280.00 CRACKED AT LBL 9.0 BOTTOM FLANGE OF FS 280.00. REPAIRED IAW REO 601R-53-11-171 REV D. (K)Aug 21, 2009 · N464AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA200940560Attach Bracket · crackedRT HYDRAULIC MANIFOLD BRACKET AT FS 718.00 AFT AREA CRACKED. (.200") LONG. REO 601R-53-62-031, REV A. CARRIED OUT ON RT HYD MANIFOLD BRACKET AT FS 718.00. (K)Aug 21, 2009 · N464AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200940551Structure · crackedINBD AND OTBD OF LBL 9.0, CLIPS FS 280.00 CRACKED. INBD AND OTBD OF LBL 9.0, CLIPS FS 280.00, CRACKED REPLACED IAW SRM 51-42-06 AND 51-42-20. (K)Aug 21, 2009 · N464AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940553Frame · crackedRT BOTTOM FLANGE FS 280.00 AT RBL 9.0 CRACKED. BOTTOM FLANGE AT FS 280.00, RBL 9.0 CRACK REPAIRED IAW REO 601R-53-11-171, REV D. (K)Aug 21, 2009 · N464AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA200940552Structure · crackedINBD AND OTBD OF RBL 9.0, CLIPS FS 280 CRACKED. INBD AND OTBD OF RBL 9.0, CLIPS FS 280.00, CRACKED REPLACED IAW SRM 51-42-06 AND 51-42-20. (K)Aug 21, 2009 · N464AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940557Intercostal · crackedINTERCOSTAL AT FS 484.00, RBL 36 FOUND CRACKED (.25 LONG) INTERCOSTAL AT FS 484.00, FBL 36.00. REPAIRED IAW REO 601R-53-41-059, REV A. (K)Aug 20, 2009 · N464AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940565Longeron · corrodedCORROSION ON PAX DOOR LOWER SILL LONGERON. CORROSION ON PAX DOOR LOWER SILL LONGERON OTBD FACE REMOVED IAW SRM 51-21-06. (K)Aug 20, 2009 · N464AW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR A6WA200940558Intercostal · crackedINTERCOSTAL AT FS 484.00, LBL 36.00 FOUND CRACKED. INTERCOSTAL AT FS 484.00, LBL 36.00. REPAIRED IAW REO 601R-53-41-059, REV "A".Aug 20, 2009 · N464AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940564Seat Track · corrodedFLOOR SEAT TRACK BTWN FS 364.00 AND FS 390.00, LBL 9.00 CORRODED. FLOOR SEAT TRACK CORROSION BTWN FS 364..00 AND FS 390.00, LBL 9.00. REMOVED IAW SRM 51-21-06 AND FOUND WITHIN LIMITS IAW SRM 53-21-49. (K)Aug 19, 2009 · N464AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA200940563Seat Track · corrodedFLOOR SEAT TRACK BTW FS 364.00 AND FS 390.00, RBL 9.00 CORRODED. CORROSION ON FLOOR SEAT TRACK. (K)Aug 19, 2009 · N464AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA200940562Bulkhead · crackedAFT PRESSURE BULKHEAD AT FS 621.00, LBL 27.50, WL 130.00 ABOVE CARGO DOOR TRACK FOUND CRACKED (.500 LENGTH). AFT PRESSURE BULKHEAD REPAIRED AT FS 621.00, LBL 27.50, WL 130 ABOVE CARGO DOOR TRACK CARRIED OUT IAW REO 601R-53-61-1541 REV "B".Aug 13, 2009 · N464AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940326Door · lack of lubeF/A REPORTS SERVICE DOOR DIFFICULT TO OPERATE. CLEANED AND LUBED SERV DOOR OPS CK NORMALLY IAW AMM 52-40-00. (K)Jun 16, 2009 · N464AW · Cndair CL6002B19 · Service DoorsSDR A6WA200940021Unknown · unknownIDG NR2 CAUTION MESSAGE ON TAKEOFF AT 50 KNOTS. ABORTED TAKEOFF. BRAKE TEMP DIDN`T EXCEED 4. COMPLIED WITH IDG CAUTION QRH. DISCONNECTED IDG NR2. APU OIL LEVEL CHECKS GOOD IAW AMM 12-13-49, REF 187080/ 1 AND 2 FOR THE DIL AND MEL. LOG 187080/2 RECONNECTEJan 19, 2009 · N464AW · Cndair CL6002B19 · Electrical Power SystemSDR A6WA200940005Unknown · unknownFLIGHT CONTROLS TAKE 2 TO 3 TIMES THE NORMAL AMOUNT OF PRESSURE TO MOVE SURFACE TO LIMITS WITH ALL HYD PUMPS ON. ONLY AILERONS AND ELEVATORS, RUDDER IS NORMAL, IN FLIGHT OR ON THE GROUND WITH AUTOPILOT OFF FROM BOTH CAPTS AND FO`S SIDE. C/W AWAC AMM SUP 2006Jan 6, 2009 · N464AW · Cndair CL6002B19 · Flight Control SystemSDR A6WA200840346Connector · looseGROUND LIFT DUMP AUTO DEPLOY ON ENGINE START. TIGHTENED RADIO ALTIMETER ANTENNA COAX CONNECTOR AND PERFORMED BONDING TEST PER AMM 51-80-00. SPOILER CONTROL SYSTEM OPS CHECK GOOD IAW AMM 27-65-00. RADIO ALTIMETER OPS CHECK GOOD IAW 34-44-01.Apr 17, 2008 · N464AW · Cndair CL6002B19 · Ground Proximity SystemSDR A6WA200840095Coffeemaker · malfunctionedIN FLIGHT WHEN FLIGHT ATTENDANT TURNED ON COFFEE MAKER IT STARTED TO SMOKE. STOPPED SMOKING WHEN IT WAS TURNED OFF. REMOVED AND REPLACED COFFEE MAKER. (K)Feb 13, 2008 · N464AW · Cndair CL6002B19 · Buffet/GalleysSDR A6WA200740704Unknown · unknownON TAKEOFF ROLL, AC VEERED RT, TOOK ALMOST FULL LT RUDDER TO STAY CENTERED ON RUNWAY. N1 SPEEDS WERE MATCHED. REDUCED POWER TO ABORT T/O AT 60 KNOTS. AIRCRAFT THEN TRAVELED STRAIGHT. BRAKE TEMPS WERE A 7 ON LT MAIN GEAR AND 3 AND 4 ON RT. WINDS 180 AT 5 KDec 18, 2007 · N464AW · Cndair CL6002B19 · Standard Practices/StructuresSDR A6WA200740702Warning Light · illuminatedFLAPS FAIL MESSAGE ON APPROACH, FAILED AT 20 DEGREES WHEN SELECTING 30 DEGREES. RESET IAW SUPPLEMENT 98-018B. OPS CHECK NORMAL. (K)Dec 18, 2007 · N464AW · Cndair CL6002B19 · Central WarningSDR A6WA200740500Warning Light · false activationON TAKEOFF ROLL, AIRCRAFT PULLED HARD LEFT, AT 10 KNOTS ABORTED. BRAKE TEMPS NORMAL 3, 3, 3, 3. AFTER REDUCING POWER TO IDLE RECEIVED CONFIG SPOILER MESSAGE. ENGINE POWER SETTINGS EQUAL. INSPECTED NLG TIRES AND MLG BRAKES 1 AND 2 PER AMM 32-40-00, NO FAULTAug 31, 2007 · N464AW · Cndair CL6002B19 · Central WarningSDR A6WA200740455Support Beam · crackedFOUND CARGO DOOR TRACK SUPPORT BEAM ANGLE AT FS 621 IS CRACKED AT BOTTOM ANGLE. MAINTENANCE REPLACED ANGLE IAW CRJ 200 SRM 51-42-21. (M)Aug 12, 2007 · N464AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA200740457Skin · corrodedTHE LEFT WING LOWER PLANK ACCESS HOLE FOR PANEL 510AB AT WS 12.245 HAS PITTING APPROX .007 INCH DEEP. 10-04-07 MAINTENANCE C/W REPAIR OF LT WING LOWER PLANK ACCESS HOLE PANEL 510AB IAW REO 601R-57-20-030 REV F. (M)Aug 12, 2007 · N464AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740456Skin · corrodedTHE LEFT WING LOWER PLANK ACCESS HOLE FOR PANEL 540BB AT WS 54.897 HAS PITTING APPROX .005 INCH DEEP AT THE INBOUND AND OUTBOARD RADIUS. 10-04-07 MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV F. (M)Aug 12, 2007 · N464AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740454Nut Clip · crackedFOUND FS 280 RBL 9 INBOARD AND OUTBOARD FLOOR SUPPORT CLIPS ARE CRACKED. 10-04-07 MAINTENANCE REPLACED CLIPS IAW BSC STANDARD REPAIR 601R-53-0057A AND CRJ 200 SRM 51-42-13 AND 51-42-21. (M)Aug 12, 2007 · N464AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
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