N433AW

Service difficulty reports · 259

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 = 'N433AW' 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 A6WA202607028897Acm · faultedRT PACK TRIPPED OFF LINE 2 TIMES AT 80 PSI, PACK RESET EACH TIME, PACK HI TEMP CAUTION AT 30 DEG C PACK RESET PER QRH. NO PRESSURIZATION ISSUES. AIRCRAFT REMOVED FROM SERVICE, EMER DEPRESS SWITCH/ LIGHT PUSHED IN. DEACTIVATED BOTH A/C PACKS. DEACTIVATED Jul 2, 2026 · N433AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA202604068882Control Lever · faultedFLAPS FAIL AT 20* ON APPROACH C/W QRH AND LANDED NORMALLY. MAX BRAKE TEMP 04 ALL WHEELS. PREFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-18I BOX 11. FLAPS RESET. PLACARDED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE IAW W/O 347359. FLAP FAIL INTEROGATIONMar 28, 2026 · N433AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA202602228879Priority Valve · faultedGEAR DISAGREE WARNING MSG AFTER T/O. NOSE GEAR INDICATED UNSAFE AND NOT UP AND LOCKED. C/W QRH. GEAR INDICATED DOWN AND LOCKED AFTER USING EMERGENCY EXTENSION HANDLE. ALL MSG'S EXTINGUISHED AFTER QRH. GEAR DISAGREE MESSAGE ORIGINALLY APPEARED 6-10 SECONDS AFTEFeb 22, 2026 · N433AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA202601318875Selector Valve · faultedGEAR DISAGREE WARNING WITH TRIPLE CHIME AFTER TAKE OFF. C/W QRH, DECLARED EMERGENCY, AND RETURNED TO MSP. WARNING OCCURRED 28 SECONDS AFTER TAKE OFF, NO OTHER MSGS, NOSE GEAR RED, MANUAL RELEASE USED, HYD PUMPS AUTO, 160KTS, SMOOTH LANDING. REMOVED FLAGS FROM Jan 31, 2026 · N433AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA202211228386Ballast · smokeDISCREPANCY: CREW WITNESSED SMOKE COMING FROM ABOVE BIN OVER ROW 10AB AS WELL AS BURN MARKS ON THE CEILING. ****AIRCRAFT REMOVED FROM SERVICE***** REMOVED AND REPLACED SIDEWALL BALLAST LOCATED AT 10AB. OPS CHECK GOOD. IAW AMM 33-21-10. REF 339930-2 FORNov 22, 2022 · N433AW · Cndair CL6002B19 · Passenger Compartment LightingSDR A6WA202201318148None · corrodedL/H CABIN FLOOR SUPPORT BEAM P/N: 601R35031-3 HAS CORROSION AT FS 589 TO FS 621 AND LBL 27. *********AIRCRAFT REMOVED FROM SERVICE*************************** BLENDED AREA OF CORROSION ON FLOOR SUPPORT BEAM P/N: 601R35031-3 AT FS 589-621 WITH ORIGINAL MATEJan 31, 2022 · N433AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202201318147None · crackedL/H CABIN FLOOR SUPPORT ANGLE P/N: 601R 53-61-004-1 HAS A CRACK .900"L ON FORWARD INBOARD END. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED PREVIOUS REPAIR SPLICE ON L/H CABIN FLOOR SUPPORT ANGLE P/N: 601R-53-61-004-Jan 31, 2022 · N433AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202201318142None · corrodedR/H FLOOR SEAT TRACK FROM FS 364TO FS 394 AND RBL 9 HAVE SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H SIDEWALL SEAT TRACKS AT FS 364 TO FS 394 AT RBL 9 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-21-49 REV 38. *********AIRCJan 31, 2022 · N433AW · Cndair CL2151A10 · Fuselage Structure (General)SDR A6WA202201318145None · corrodedR/H FLOOR SEAT TRACK FROM FS 364TO FS 394 AND RBL 9 HAVE SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H SIDEWALL SEAT TRACKS AT FS 364 TO FS 394 AT RBL 9 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-21-49 REV 38. *********AIRCJan 31, 2022 · N433AW · Cndair CL2151A10 · Fuselage Floor PanelSDR A6WA202201318146None · corrodedL/H CABIN FLOOR LANDING PLATE P/N: 601R35011-63 HAS AREA OF SURFACE CORROSION AT FS 574 TO FS 621 AT LBL 42 TO LBL 46. *********AIRCRAFT REMOVED FROM SERVICE*************************** BLENDED AREA ON L/H CABIN FLOOR LANDING PLATE P/N: 601R35011-63 ATJan 31, 2022 · N433AW · Cndair CL2151A10 · Fuselage Structure (General)SDR A6WA202201318136Fitting · corrodedCORROSION ON PASSENGER DOOR FITTING P/N: 601R31527-217 AT FS 341 TO FS 345 AND LBL 42 TO LBL 44 AND WL 73.50. ************AIRCRAFT REMOVED FROM SERVICE**************************** UPON FURTHER INSPECTION, FOUND SEVERE CORROSION ON PASSENGER DOOR BRACKET P/NJan 31, 2022 · N433AW · Cndair CL6002B19 · Fuselage Floor PanelSDR A6WA202201318135None · corrodedR/H O/B FLOOR SILL AT FS 559+80 TO FS 559+115 AND LATERAL FLOOR BEAM AT 559+80 I/B AFT CORNER ARE CORRODED. CLEANED I/B LATERAL FLOOR BEAM AT FS 559+80 IAW CRJ200 51-26-00 REV 38. UPON FURTHER INVESTIGATION OF I/B LATERAL FLOOR BEAM AT FS 559+80 FOUND NO CORJan 31, 2022 · N433AW · Cndair CL2151A10 · Fuselage Structure (General)SDR A6WA202201318132None · dentedAIRCRAFT L/H SKIN EXTERIOR HAS 2 EACH DENTS AT FS 625 TO FS 640 AND S19L TO S20L. DENT DIMENSIONS ARE: (P1) 1.0"L X .900"W X .015"D; (P2) .800"L X .800"W X .012"D. EVALUATED BOTH DENTS AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. *Jan 31, 2022 · N433AW · Cndair CL2151A10 · Fuselage Structure (General)SDR A6WA202201318131None · gougedCARGO DOOR FWD ROLLER TRACK AT FS 574.00 AND STR 12L TO STR 13L HAS WEAR DAMAGE MEASURING .200"L X .200"W X .020"D (P1) ON UPPER SIDE AND .300"L X .200"W X .040"D (P2) ON LOWER SIDE. THE TRACK IS MACHINED FROM 7075-T7451 PLATE WITH A LOCAL FLANGE THICKNESS OF Jan 31, 2022 · N433AW · Cndair CL2151A10 · Fuselage Structure (General)SDR A6WA202201318122None · corrodedR/H SIDEWALL SEAT TRACKS FROM FS 409+111.98 TO FS 559+79 HAVE SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H SIDEWALL SEAT TRACKS AT FS409+111.98 TO FS 559.00+79 AT RBL 42 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-49 REV 38.Jan 31, 2022 · N433AW · Cndair CL2151A10 · Fuselage, Door HingeSDR A6WA202201318123None · corrodedR/H SIDEWALL SEAT TRACKS FROM FS 349.00 TO FS 409+128 HAVE SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H SIDEWALL SEAT TRACKS AT FS349 TO FS 409+16 AT RBL 42 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-49 REV 38. R/H SEAT TRJan 31, 2022 · N433AW · Cndair CL2151A10 · Fuselage, Door HingeSDR A6WA202201318121None · corrodedL/H SIDEWALL SEAT TRACKS FROM FS 409+111.98 TO FS 559+79 HAVE SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON L/H SIDEWALL SEAT TRACKS AT FS409+111.98 TO FS 559.00+79 AT RBL 42 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-49 REV 38.Jan 31, 2022 · N433AW · Cndair CL2151A10 · Fuselage Structure (General)SDR A6WA202201318124None · corrodedAFT LAVATORY SERVICE DOOR LOWER HINGE HAS CORROSION. REMOVED CORROSION AT AFT LAVATORY SERVICE DOOR LOWER HINGE BRACKET IAW CRJ200 SRM 51-12-00 REV 38. EVALUATED CORROSION REMOVAL ON AFT LAVATORY SERVICE DOOR HINGE BRACKET AND FOUND NOT WITHIN ALLOWABLE LIMJan 31, 2022 · N433AW · Cndair CL2151A10 · Fuselage Structure (General)SDR A6WA202111107957Control Unit · failedCLIMBING THRU FLIGHT LEVEL 180 RECEIVED FLAP FAIL MSG CW QRH LANDED AT FLAP ZERO DEG. SMOOTH LANDING MAX BTMS 4. PERFORMED FLAP RESET PROCEEDURE IAW AWAC SUP 98-018I BOX 12 FLAPS RESET. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLAP ELECTRONIC CONNov 10, 2021 · N433AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA202109107875Water Separator · odorHAZE/SMOKE IN CABIN ON INSPECTION RT PACK 120C. UNABLE TO COOL IN MANUAL OR AUTO MODE. LT PACK IS OPERATING NORMALLY. BOTH PACKS WERE RUNNING OFF OF APU AIR. ***AIRCRAFT REMOVED FROM SERVICE*** REF WO 310433 WC 3,4,5 FOR R&R OF LH ACM IN COMPLIANCE OF AWSep 9, 2021 · N433AW · Cndair CL6002B19 · Humidity Control SystemSDR A6WA202011307429Bpsu · malfunctionedFLAPS FAILED AT ZERO IN CRUISE. ALT 14K FT PERFORMED QRH UNEVENTFUL LANDING. PERFORMED FLAP RESET PROCEEDURE, IAW AWAC SUP 98-18I BOX 12 FLAPS RESET. PLACRDED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT FLAP BPSU, PER AMM 2Nov 24, 2020 · N433AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA2020021347173Control Cable · damagedOUTBOARD FUSELAGE AILERON CIRCUIT CABLE FOUND DAMAGED AT QUADRANT. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED LEFT HAND OUTBOARD FUSELAGE CABLE REF. CRJ-200 AMM 27-00-00 AND 27-11-00 REV. 60Jan 30, 2020 · N433AW · Cndair CL6002B19 · Aileron Control SystemSDR A6WA2020021247163Skin · damagedL/H WING LWR AFT PLANK I/B OF FWD FITTING @ WS 178.00 HAS A SCRATCH INTO METAL. AIRCRAFT REMOVED FROM SERVICE BLENDED SCRATCH ON L/H WING LWR AFT PLANK I/B OF FWD FITTING @ WS 178.00 BLEND MEASUREMENTS ARE 1.0"L X .040"W X .006"D, NO CRACKS NOTED AT THIS TIMJan 28, 2020 · N433AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA202047171Control Cable · damagedRIGHT HAND OUTBOARD AILERON FUSELAGE CABLE FRAYED AT RIGHT HAND QUADRANT. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED RIGHT HAND OUTBOARD AILERON FUSELAGE CABLE REF. CRJ-200 AMM 27-11-00 REV. 60Jan 27, 2020 · N433AW · Cndair CL6002B19 · Aileron Control SystemSDR A6WA2020021247165Fitting · gougedL/H WING AFT WING TO FUSELAGE FITTINGS (UPPER & LOWER) HAVE TOOLING MARKS. AIRCRAFT REMOVED FROM SERVICE BLENDED DAMAGE TO SMOOTH CONTOUR ON THE L/H WINGBOX TO FUSELAGE MACHINED FRAME AT FS 473.15 BLEND DIMENSIONS FOUND TO BE .500"L X .200"W X .043"D, NDTJan 26, 2020 · N433AW · Cndair CL6002B19 · Wing, Fuselage Attach FittingsSDR A6WA202021247164Hinge · gougedENTRY DOOR HINGE ON DOOR SIDE HAS MULTIPLE LUGS WITH WEAR. AIRCRAFT REMOVED FROM SERVICE LUG #26 BLENDED BELOW .100" LIMIT REFERENCE REO REF REO 601R-52-11-1347 REV C DTD 2017-08-02. DOOR HINGE LUG BLENDED TO .094" PERFORMED A SMOOTH CONTOUR OF 5:1 PERFORMEJan 25, 2020 · N433AW · Cndair CL6002B19 · Fuselage, Door HingeSDR A6WA2019112147026Pressure Switch · malfunctioned3158 - L WING ANTI ICE CAUTION MESSAGE IN FLIGHT. C/W QRH MESSAGE CLEARED AND LEFT ICING CONDITIONS MESSAGE OCCURED BETWEEN CLIMBOUT AND CRUISE WITH WING ANTI ICE SELECTED ON. L WING SHOWED YELLOW ON SYNOPTIC MESSAGE CLEARED WHEN 14TH STAGE ISOL VALVE OPENED Nov 19, 2019 · N433AW · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR A6WA2019083046822Landing Gear · malfunctionedAFTER TAKE-OFF, RECEIVED WARNING FOR GEAR DISAGREE. NOSE WHEEL WAS SHOWING YELLOW BOX, THEN UP 2 TIMES. ON EXTENSION, NOSE GEAR TOOK LONGER TO EXTEND WITH EXTRA NOISES FROM GEAR DURING EXTENSION. HYDRAULIC SYSTEMS SHOW NORMAL. CREW REPORTED VIA ACARS THAAug 28, 2019 · N433AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA201908146792Warning Message · illuminatedR TR UNLOCK (C) IN FLIGHT AT 29,000FT 290 KT AMBER REV ICON. T/R APPEARS PHYSICALLY STOWED. EMER STOW PRESSED MSG REMAINED. DURING THE CRUISE, THE FLIGHT CREW RECEIVED A THRUST REVERSER UNLOCKED CAUTION MESSAGE. AFTER COORDINATING WITH DISPATCH AND WORKING THAug 12, 2019 · N433AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA2019053046640Warning System · false activation4804 RT REV UNLCKEDE CAUTION MSG ILLUMINATED IN FLT. CW QRH MSG DID NOT CLEAR. DIVERTED TO DAY. REV ICON IN RT N1 IND. MSGS CLEARED ON ENGINE SHUTDOWN. RT TR APPEARS TO BE STOWED.May 30, 2019 · N433AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA2018032645731Pseu · faultedDURING CRUISE, RECEIVED A PROXIMITY SYS CHANNEL CAUTION MESSAGE. COMPLIED WITH QRH. MANUAL GEAR EXTENSION, NWS SELECTED OFF, LANDED WITHOUT ISSUE, TOWED OFF RUNWAY TO THE GATE. PSEU FAULTED, REPLACE PSEUMar 25, 2018 · N433AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA201845544Frame · corrodedFRAMES 333 BETWEEN STR'S 25R AND 25L CORRODED. REPLACEDJan 5, 2018 · N433AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA2018010445536Structure · dentedSTRUCTURE DENTED BETWEEN BS 589 AND 604. REPAIRED THE STRUCTURE.Jan 2, 2018 · N433AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA2018010445538Floor Support · corrodedMAIN CABIN LEFT FLOOR SUPPORT IN PAX DOOR CORRODED. REPLACED THE FLOOR SUPPORTJan 2, 2018 · N433AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018010445537Frame · corrodedE&E BAY FRAME BS 349, STRINER 25L TO 25R CORRODED. REPLACED THE FRAME.Jan 2, 2018 · N433AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA2017010245531Vane · chafedLEFT INBD FLAP VANE IS CHAFED ON THE LE IN MULTIPLE AREAS. REPLACED THE FLAP VANEDec 30, 2017 · N433AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA2017010245530Rib · damagedON REMOVAL OF THE LT WING FLAP VANE INBD LE, FOUND DAMAGED FASTENER HOLES IN THE INBD RIB. REPLACED THE RIB.Dec 30, 2017 · N433AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA2017010245532Attach Fitting · crackedNR 1 PYLON LE ACCESS ATTACH FLANGE IS CRACKED ON THE LOWER PYLON.Dec 30, 2017 · N433AW · Cndair CL6002B19 · Nacelle/Pylon, Attach FittingsSDR A6WA2017010245525Frame · crackedFRAME AT BS 605 ATTACH FLANGES CRACKED JUST ABOVE AND BELOW STRINGER 9L. REPAIRED THE FRAME.Dec 29, 2017 · N433AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA2017010245527Floor Support · corrodedLEFT CABIN FLOOR SUPPORT BS 349 - 409, LBL 42-46 CORRODED. REPAIRED THE FLOOR SUPPORTDec 29, 2017 · N433AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2017010245526Intercostal · corrodedPAX DOOR INTERCOSTAL DD 7 CORRODED. REPLACED THE INTERCOSTAL.Dec 28, 2017 · N433AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201745514Skin · crackedCRACKED SKIN ON THE LT LOWER NOSE HYD COMPARTMENT AFT UPPER LATCH CUT OUT.Dec 28, 2017 · N433AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA201745512Skin · damagedRIGHT INBD FLAP LOWER SURFACE SKIN NICKED.Dec 27, 2017 · N433AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201745506Skin · corrodedLEFT INBD FLAP INBD LOWER SKIN PANEL PITTED.Dec 26, 2017 · N433AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA2017010245509Frame · crackedBS 718 FRAME FLANGE CRACKED. REPAIRED THE FRAME.Dec 26, 2017 · N433AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA2017010245507Structure · corrodedMAIN CABIN, BS 343, LBL 39 HINGE CUTOUR IS CORRODED. REPLACED THE STRUCTURE.Dec 26, 2017 · N433AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2017010245508Structure · corrodedMAIN CABIN, BS 316, LBL 39 HINGE CUTOUT IS CORRODED. REPLACED THE STRUCTURE.Dec 26, 2017 · N433AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA2017010245502Fastener · missingRIGHT UPPER PRESSURE FLOOR SKIN IS MISSING 7 RIVETS FROM BS 513 - 559 ON TOP OF RBL 36, IN THE CABIN.Dec 23, 2017 · N433AW · Cndair CL6002B19 · Fuselage Floor PanelSDR A6WA2017010245511Stringer Clip · crackedBS 280 STRINGER 3L CRACKED. REPLACED THE STRINGER CLIP.Dec 22, 2017 · N433AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201745499Angle · corrodedLT PRESSURE FLOOR STRUCTURE ANGLE AT LBL43 IS CORRODED FROM FS409+128 TO FS559.Dec 21, 2017 · N433AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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