N465AW

Service difficulty reports · 170

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 = 'N465AW' 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 A6WA202605268890Proximity Sensor · malfunctionedRECEIVED GEAR DISAGREE WARNING MSG AFTER T/OFF CLIMBING THRU 5000'. MSG CLEARED AFTER A COUPLE SECONDS. GEAR WAS ALREADY UP/LOCKED WHEN MSG CAME ON. GEAR AND FLAP INDICATORS CAME ON BRIEFLY FOR APPROX 5 MINS AFTER GEAR DISAGREE MSG WARNING MSG MESSAGE. RECEIVEMay 26, 2026 · N465AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA202502118860Anti-Ice Valve · faultedINFIGHTING REC'D "R COWL A/I" CAUTION WITH SWITCH SELECTED OFF. FOUND R COWL PRV POPPED ON POST FLIGHT. AIRCRAFT REMOVED FROM SERVICE R&R RH COWL PRESSURE RELIEF VALVE REF 30-2204. OPS CHECK GOODFeb 11, 2025 · N465AW · Cndair CL6002B19 · Engine Anti-Icing SystemSDR A6WA202405258754Sensor · faultedUPON DEPARTURE AND CLIMB OUT OF KDAY FLAP FAILED WITH INDICATION OF 0. CREW HAS ELECTED TO FLY ONTO KORD. CREW HAS DECLARED AN EMERGENCY FOR FLAP FAILURE. CREW IS SCHEDULED TO ARRIVE AT KORD AT 0838 CENTRAL TIME. AIRCRAFT REMOVED FROM SERVICE. R&R L BPSU IAMay 25, 2024 · N465AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA202405248753Fcu · faultedRECEIVED FLAP FAIL MESSAGE BEFORE DESCENT. AIRCRAFT REMOVED FROM SERVICE. T/S PER FIM 27-50 FIG 108, FECU #1 MOST PROBABLE FAULT #12 PRESENT. REPLACED THE FECU PER AMM 27-51-05, OPS CHECK GOOD. REMOVED PLACARD/MEL.May 24, 2024 · N465AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA202312318686Unknown · unknownGEAR DISAGREE ON TAKE-OFF. WARNING MESSAGE APPEARED WITHIN 5 SECS OF SELECTION. NLG DID NOT MOVE. MLG RETRACTED NORMALLY. NOSE DOOR OPEN MESSAGE ALSO APPEARED. C/W QRH. RECEIVED THREE GREEN DOWN AND LOCKED. LANDING AT 46,500 LBS. BELOW LANDING WEIGHT. AIRCRDec 31, 2023 · N465AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA202301608430Stiffener · missingAFT PRESSURE BULKHEAD FS621 IS MISSING ALL REINFORCEMENT ANGLES, AIRCRAFT REMOVED FROM SERVICE. INSTALLED REINFORCEMENT ANGLES TO AFT PRESSURE BULKHEAD FS621. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMJan 6, 2023 · N465AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2023011688428Drag Angle · crackedPAX DOOR AFT PANEL DRAG ANGLE IS CRACKED AT PULLEY BRACKET AREA. AIRCRAFT REMOVED FROM SERVICE. REPAIRED DRAG ANGLE. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW REO 601R-52-11-513 REV C.Dec 28, 2022 · N465AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA202212278431Angle · corrodedCORROSION ON SERVICE DOOR LOWER SILL ANGLE P/N 601R38303-253 AT FS 310.0 AND RBL 43. AIRCRAFT REMOVED FROM SERVICE. REMOVED DAMAGE BY BLENDING SERVICE DOOR LOWER SILL ANGLE AT FS310.0 AND RBL 43. ORIGINAL MATERIAL THICKNESS 0.063. REMAINING THICKNESS 0.050 Dec 27, 2022 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202212168426Skin · corrodedRIGHT HAND WING INBOARD FLAP INBOARD SIDE LOWER SKIN PN 601R4008 HAS CORROSION AND 5 GOUGES AT INBOARD WING STATION 50.498 - 79.062. ***********AIRCRAFT REMOVED FROM SERVICE**************** BLENDED OUT CORROSION IAW CRJ200 SRM 51-12-00 REV 39 AND SRM 51-21-06 Dec 16, 2022 · N465AW · Cndair CL6002B19 · Aileron TabsSDR A6WA2023016258429Floorbeam · crackedCORROSION AND CRACK ON CABIN FLOORBEAM AT BS 621, LBL 27-43. AIRCRAFT REMOVED FROM SERVICE. BLENDED CORROSION, REMOVED AND REPLACED THE SECTION OF ANGLE. HFEC PERFORMED WITH NO INDICATIONS IAW NDT 51-20-06 REV 44 PART 1. RESTORED SURFACE FINISH. WORK WIDec 15, 2022 · N465AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA2023012638445Rib · damagedRIGHT WINGLET ATTACH STRUCTURE HAS ONE ELONGATED HOLE ON RIB AND STRAP AT WS404.08. REPAIRED THE RT WINGLET ATTACH STRUCTURE BY REPLACING STRAP, INSTALLED FREEZE PLUG AND COUNTERBORED FREEZE PLUG. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFACE FINISH.Nov 30, 2022 · N465AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA2023012638448Strap · corrodedCORROSION ON FLOOR STRUCTURE RH STRAP, BS 559, RBL 27 - 42. REMOVED AND INSTALLED FLOOR STRUCTURE RT STRAP WITH FABRICATED STRAP . RESTORED SURFACE FINISH. PERFORMED IAW SRM 53-00-00, REV 39, SRM 53-41-43 REV 39, SRM 51-40-11 REV 39, SRM 51-42-06 REV 39,Nov 30, 2022 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2023012638444Floorbeam · corrodedCORROSION ON CABIN FLOOR STRUCTURE SUPPORT P/N 601R38672-1 AT FS349.0 AND RBL19.0 TO RBL21. REMOVED CORROSION BY BLENDING CABIN FLOOR STRUCTURE SUPPORT. PERFORMED HFEC WITH NO INDICATIONS. RESTORED SURFACE PROTECTIVE FINISH. ALL WORK WITHIN LIMITS PERFORMED INov 30, 2022 · N465AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA2023012638446Rib · damagedLH WINGLET ATTACH STRUCTURE HAS ONE ELONGATED HOLE ON RIB AT WS404.08. REPAIRED LH WINGLET ATTACH STRUCTURE BY REPLACING RIB P AT WS404.08 AND WGLT3.25. INSTALLED FREEZE PLUG AND COUNTERBORED FREEZE PLUG. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFACE Nov 30, 2022 · N465AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA2023012638443Floorbeam · corrodedCORROSION ON CABIN FLOOR STRUCTURE CROSSBEAM AT FS349.0 AND RBL19.0 TO RBL24. REMOVED CORROSION BY BLENDING CABIN FLOOR STRUCTURE CROSSBEAM P/N 601R32005-149 AT FS349.0 AND RBL19.0 TO RBL24. FABRICATED STRAP FROM 0.050Ï¿½ ALUM. SHEET MATERIAL HEAT TREATED TONov 30, 2022 · N465AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA2023012308440Seat Track · corrodedCORROSION ON RT SEAT TRACK FROM BS 559 - 559+84, RBL 9. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION, PERFORMED HFEC WITH NO INDICATIONS IAW NDTM 51-20-06 PART 1, REV 44. RESTORED PROTECTIVE FINISH. WORK WITHIN LIMITS IAW AMM 53-01-11 REV 66, REPLACED THNov 30, 2022 · N465AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2023012308441Floorbeam · corrodedCORROSION ON CABIN FLOOR STRUCTURE SUPPORT ANGLE AT SERVICE DOOR FS349 AND RBL28 TO RBL42. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ANGLE SUPPORT ANGLE AT SERVICE DOOR FS349 AND RBL28 TO RBL42. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITSNov 30, 2022 · N465AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA2023012308442Skin · corrodedCORROSION ON LEFT WING INBOARD FLAP LOWER SKIN FROM WS50.498- WS100.009. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED DAMAGED SECTION ON LEFT WING INBOARD FLAP LOWER SKIN FROM WS50.498 WS100.009. CUTOUT DIMENSIONS L= 29.700X W= 21.250. RESTORED SURFNov 30, 2022 · N465AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA202301208436Fitting · corrodedCORROSION ON PAX DOOR FWD ANCHOR FITTING AT BS 310, WL 75. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ON PAX DOOR FWD ANCHOR FITTING. RESTORED PROTECTIVE FINISH. WORK WITHIN LIMITS, PERFORMED IAW AMM 52-11-17-400-804, REV 66, ADJUSTMENT IAW ANov 30, 2022 · N465AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA202301208437Anchor Fitting · corrodedCORROSION ON PAX DOOR AFT ANCHOR FITTING, PLATE AND COVER AT BS 349, WL 75. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED PAX DOOR AFT ANCHOR FITTING, PLATE, AND COVER. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW AMM 52-11-1Nov 30, 2022 · N465AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA202106227805Housing · leakingAT 3,000-3,500 FEET RH ENGINE OIL (PSI) FLUXUATION FROM 15 PSI TO 51 PSI, EVEN AT CRUISING POWER, C/W QRH, AIR RETURN. AIRCRAFT REMOVED FROM SERVICE. UPON FURTHER INSPECTION FOUND OIL TO BE LEAKING FROM SCAVENGER OIL FILTER HOUSING. FOUND OIL FILTER HOUSJun 19, 2021 · N465AW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA202105287789Angle · crackedTWO CRACKED ANGLES ON PASSENGER DOOR AFT SIDE WALL PANEL AT 2ND STEP. FS340. PAX DOOR P/N 601R31701-1 S/N 7896 ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED PASSENGER DOOR FORWARD SIDE PANEL ANGLES P/N 601R-52-11-702-7 AND 601R-52-11-702-9 WITH FABRICATED AMay 22, 2021 · N465AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA202105287788Angle · crackedCRACKED ANGLE ON PASSENGER DOOR FORWARD SIDE WALL PANEL AT 2ND STEP. FS318 PAX DOOR P/N 601R31701-1 S/N 7896 ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED PASSENGER DOOR FORWARD SIDE PANEL ANGLE P/N 601R-52-11-702-10 WITH FABRICATED ANGLE, FS318. RESTORED SMay 22, 2021 · N465AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA202106017792Strap · gougedLH WINGLET HAS 3 GOUGES AT INBOARD AND OUTBOARD LOWER FORWARD STRAPS, WS389. P/N 600-15108-7 AND P/N 600-15108-18. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED 2 GOUGES AT LH LOWER FORWARD WINGLET OUTBOARD STRAP P/N 600-15108-7. DIMENSIONS 3.200Ï¿½L X 2.00Ï¿½May 21, 2021 · N465AW · Cndair CL6002B19 · Wing Main, Frame StructureSDR A6WA202105287790Angle · crackedCRACKED ANGLE ON PASSENGER DOOR FORWARD LOWER SIDE WALL PANEL AT LOWER STEP. FS318 PAX DOOR P/N 601R31701-1 S/N 7896 ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED PASSENGER DOOR FORWARD LOWER SIDE WALL PANEL AT LOWER STEP, ANGLE P/N 601R-52-11-702-44, SHIM May 20, 2021 · N465AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA202106077797Skin · dentedAFT FUSELAGE SKIN DENT FS 640.00 - 1Ï¿½ LH STR 26 + 2Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED SKIN DENT AT AFT FUSELAGE FS640.00 - 1Ï¿½ LH STR 26 +2Ï¿½. DAMAGE MEASURES 1.200Ï¿½L X 0.600Ï¿½W X 0.023Ï¿½D. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PMay 19, 2021 · N465AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202106077795Skin · gougedAFT FUSELAGE SKIN GOUGE FS 589.00 + 1Ï¿½ RH STR 25 + 2Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED SKIN GOUGE FS 589.00 + 1 RH STR 25 + 2Ï¿½. DAMAGE MEASURES 1.10Ï¿½ L X 0.007Ï¿½ W X 0.006Ï¿½ D. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FIMay 19, 2021 · N465AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202106077796Skin · dentedAFT FUSELAGE SKIN DENT FS 640.00 - 2Ï¿½ LH STR 26 + 2Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED SKIN DENT AT AFT FUSELAGE FS640.00 - 2Ï¿½ LH STR 26 +2Ï¿½.DAMAGE MEASURES 0.550Ï¿½L X 0.500Ï¿½W X 0.008Ï¿½D. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PRMay 19, 2021 · N465AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202105277787Skin · dentedAFT FUSELAGE SKIN DENT FS682.0 + 9Ï¿½ RIGHT HAND STRINGER 24 + 2Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** HAND FORMED DENT AT FS682.0 + 9Ï¿½ RIGHT HAND STRINGER 24 + 2Ï¿½, DIMENSION0.700Ï¿½L X 0.500Ï¿½W X 0.050Ï¿½W. DENT FOUND TO BE OUT OF LIMITS REF CRJ200May 19, 2021 · N465AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202106117801Bulkhead · crackedCRACK INDICATIONS (7 TOTAL) AT FS621.00 AFT PRESSURE WEB. CRACKS AT THE FOLLOWING LOCATIONS, WL 128.5 - 131.2, LBL 18.0, CRACK LENGTH 2.7"L, WL 113.5 - 114.2, LBL 9.50, CRACK LENGTH 0.7"L, 109.5 - 112.0, BL 0.0, CRACK LENGTH 2.5"L, WL 110.5 - 111.2, RBL 9.50, Apr 21, 2021 · N465AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2020072097275Rvdt · failedRECIEVED A STEERING INOPERATIVE CAUTION MESSAGE AFTER RETRACTING GEAR, COMPLIED WITH QRH, MESSAGE REMAINED, RETURNED TO DEPARTURE, LANDED NORMAL USING DIFFERENTIAL BREAKING. NO HYD SYST 3 MESSAGE, NO OTHER EICAS MESSAGES, NO STEERING ON TAXI AFTER LANDING. Jul 19, 2020 · N465AW · Cndair CL6002B19 · Landing Gear Steering SystemSDR A6WA2019091846876Unknown · malfunctionedNOSE GEAR WOULD NOT RETRACT AFTER T/O. EICASE SHOWED NOSE GEAR DOWN AND NOSE GEAR OPEN INDICATIONS. RAN QRH. SELECTED GEAR DOWN. GEAR EXTENDED AND NORMAL LANDING.Sep 17, 2019 · N465AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA2019053046642Stiffener · crackedFOUND INDICATION AT FS 409.00+128 OTBD RBL 18 POST AFT FLANGE RADIUS APPROX .250" LONG FSH FAILS NDT.May 30, 2019 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019053046641Bracket · crackedAC GROUND POWER RECEPTACLE STRUCTURE CRACKED @ MOUNT FASTENERS.May 30, 2019 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019052046621Seat Track · corrodedRT WALL SEAT TRACK IS CORRODED AT FS 409+128.May 18, 2019 · N465AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2019052046620Bulkhead · crackedINDICATION NOTED AT FS621 REAR PRESSURE BULKHEAD FWD FACE AT BL0.00, WL 131 APROX 7.5" LONG AND 53% FULL SCREEN HEIGHT FAILING NDT.May 18, 2019 · N465AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2019061446610Intercostal · corrodedINTERCOSTAL CORRODED BETWEEN F.S.349.00 AND F.S.364.00, STRG 26L AND 27.May 17, 2019 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019052046613Seat Track · corrodedLT WALL SEAT TRACK IS CORRODED AT VF.S.409+128.May 17, 2019 · N465AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2019052046609Fitting · crackedRT F.S.484 CLIP IS CRACKED AT RBL27.May 17, 2019 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019052046611Seat Track · corrodedRT WALL SEAT TRACK IS CORRODED AT F.S.513.May 17, 2019 · N465AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2019052046612Seat Track · corrodedRT WALL SEAT TRACK IS CORRODED AT F.S.513.May 17, 2019 · N465AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2019052046608Vane · chafedLT WING OUTBOARD FLAP FIXED VANE IS CHAFED AT W.S.274.May 17, 2019 · N465AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA2019051746607Seat Track · corrodedLT SIDEWALL SEAT TRACK IS CORRODED AT FS 529.00.May 17, 2019 · N465AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2019051646606Post · crackedFOUND INDICATIONS AT FS409+128 BL 0 LT AND RT POSTS AFT FLANGE RADIUS APPROX. .500" LONG 100% FSH BOTH FAILS NDT.May 16, 2019 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019051646605Angle · crackedFOUND INDICATIONS AT FS 409+128 B.L.0.00 LT AND RT POSTS AFT FLANGE RADIUS APPROX. .500" LONG 100% FSH BOTH FAIL NDT.May 16, 2019 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018053145855Flap System · malfunctionedDURING TAKEOFF, THE FLAPS FAILED AT 3 DEGREES WHEN SELECTING FLAPS FROM 0 TO 8. RAN QRH, RETURNED TO DEPARTURE, EMERGENCY WAS DECLARED. AFTER LANDING FLAPS SYSTEM WAS SUCCESSFULLY RESET IAW 98-018G.May 30, 2018 · N465AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA2018040645751Stiffener · crackedPAX DOOR MOTOR FOUND CRACKED IN THE LOWER VERTICAL STIFFENER. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-42-06, AND 51-42-13.Apr 5, 2018 · N465AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201745473Pin · pulled4182 EMERGENCY PATH LIGHTING FROM ROW 5 TO 8 INOP. FOUND PIN PULLED OUT OF ENVIRONMENTAL SPLICE AT ROW 7. R&R'D PIN IAW ESPM 20-17, FUNCTION CHECK GOOD.Dec 11, 2017 · N465AW · Cndair CL6002B19 · Light System WiringSDR A6WA2017120745456Light · inoperative4231 EMERGENCY LIGHTS ROW 5 INOP ON FLOOR. PLACARDED & PLACED ON MEL. REMOVED & REPLACED EMERGENCY LIGHT STRIP ROW 5 IAW 33-51 & AWAC SUPP 16-371A. OPS CHECK GOOD.Dec 6, 2017 · N465AW · Cndair CL6002B19 · Emergency LightingSDR A6WA2017061445057Frame · corrodedFRAME BS 409+16 HAS CORROSION ON THE FWD AND AFT SIDE BETWEEN STRINGERS 26R AND 26LJun 13, 2017 · N465AW · Cndair CL6002B19 · Fuselage Main, Frame
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