N435AW

Service difficulty reports · 249

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 = 'N435AW' 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 A6WA202112078009Skin · dentedAIRCRAFT R/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 559+80 AND S7R+3. DENT DIMENSIONS ARE: (P1) .600L X .350W X .005D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE***********Oct 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202112068004Skin · dentedAIRCRAFT L/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 310.00+7 AND S22L+2. DENT DIMENSIONS ARE: (P1) .900L X .900W X .003D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE********Oct 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Internal StairsSDR A6WA202112078011None · dentedMAINTENANCE FOUND DENT COMMON TO FWD SIDE OF AFT PRESSURE BULKHEAD AT FS621 AND RBL 41. DAMAGE MEASURES .600"L X .500"W X .012"D. DAMAGE IS NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-61-19 REV 38. ***********AIRCRAFT REMOVED FROM SERVICE*******************Oct 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202112078012Skin · dentedAIRCRAFT SKIN EXTERIOR HAS 1 EACH DENT AT FS 319.70+3 AND S27. DENT DIMENSIONS ARE: (P1) .500L X .468W X .006D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE***************Oct 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Internal StairsSDR A6WA202112078010Skin · dentedAIRCRAFT L/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 319.70+11 AND S24L+3. DENT DIMENSIONS ARE: (P1) .600L X .600W X .013D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*******Oct 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Internal StairsSDR A6WA202112068006None · gougedMAINTENANCE FOUND SETMARK DAMAGE AROUND RIVET ON AFT PRESSURE BULKHEAD AT FS621 AND RBL 38. DAMAGE MEASURES 1.00"L X .750"W X .040"D. DAMAGE IS NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-61-19 REV 38. ***********AIRCRAFT REMOVED FROM SERVICE***************Oct 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202112068007Skin · gougedMAINTENANCE FOUND 1 EACH GOUGE AT FS 640+2 AND S19L ON L/H SKIN EXTERIOR. DIMENSIONS ARE: (P1) 1.6"L X 1.2"W X .014"D. GOUGE WAS FOUND NOT TO BE WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV 38. ***************AIRCRAFT REMOVED FROM SERVICE************Oct 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202112068003Skin · gougedMAINTENANCE FOUND 3 EACH PREVIOUS BLENDS AT FS 409+48 TO FS 409+48+6 AND S27L ON L/H SKIN EXTERIOR. DIMENSIONS ARE: (P1) FS 409+48 AT S27L .600"L X .500"W X .003"D (P2) FS 409+48+1.6 AT S27L .500"L X .400"W X .002"D (P3) FS 409+48+6 AT S27L .500"L X .450"W X .Oct 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202112068001Skin · dentedAIRCRAFT L/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 700.00+13 AND S21L+4. DENT DIMENSIONS ARE: (P1) .600L X .600W X .008D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*******Oct 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202112068002Skin · gougedMAINTENANCE FOUND A PREVIOUS BLEND (P1) AT FS 409.00+80 AT S26R+1 MEASURING .500"L X 007"D AND A SCRATCH (P2) AT FS 409.00+72 AT S26R MEASURING .450"L X .005"D. BOTH AREAS FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31. ***************AIRCRAFT Oct 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202112068005Skin · gougedDURING INSPECTION, MAINTENANCE FOUND 8 EACH AREAS OF DAMAGE TO THE FUSELAGE SKIN BETWEEN FS 255.00 AND FS 267.00 AND S25R - S27R. DIMENSIONS ARE: (P1) = 0.800"L X 0.700"W X 0.007"D (P2) = 0.650"L X 0.600"W X 0.008"D (P3) = 0.650"L X 0.600"W X 0.007"D (P4) = 0.Oct 23, 2021 · N435AW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR A6WA202108237860Brake Assy · faultedTIRE #1 BLOWN. BTMS READS 14. PILOT REPORTED SMOKE FROM TIRE, CALLED FIRE DEPARTMENT THEY CHECKED TEMP IT READ 200. DEPLANED PAX ON TAXIWAY. PERFORMED INSPECTION IAW AMM 05-51-27, VERIFIED NO DAMAGE TO MLG AND NLG. PERFORMED VISUAL INSPECTION OF TIRES, NO DEAug 23, 2021 · N435AW · Cndair CL6002B19 · Landing Gear Brake SystemSDR A6WA202104067736Skin · damagedL/H ACCESS PANEL 131AL HAS A LOOSE FREEZE PLUG AT FS226.75 AND STR 19L-1.05. ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED FUSELAGE SKIN AT STATION 226.75 AND STR19L-1.05 REF ASAP EA# AWAC CRJ253-01593 REV IR DATED 3/31/2021.Mar 29, 2021 · N435AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202103307732Skin · damagedLIGHTNING STRIKE DAMAGE TOP OF FUSELAGE AT FS 381.00 L/H AND R/H OF STRINGER 0 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED DAMAGE AT FS 381.00 L/H AND R/H OF STRINGER 0. PERFORMED UT THICKNESS CHECK. REMAINING MATERIAL, 0.050". PERFORMED HFEC WITH NO DEFECTSMar 18, 2021 · N435AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202103267729Skin · damagedLIGHTNING STRIKE DAMAGE TOP OF FUSELAGE AT FS389.25 JUST RIGHT OF STR0 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED DAMAGE AT FS389.25 JUST RIGHT OF STR0, PERFORMED UT THICKNESS CHECK, REMAINING MATERIAL 0.052", PERFORMED HFEC NO DEFECTS NOTED, AREA IS WITHINMar 18, 2021 · N435AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202103267728Skin · damagedLIGHTNING STRIKE DAMAGE TOP OF FUSELAGE AT FS391.75 JUST RIGHT OF STR0 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED DAMAGE AT FS391.75 JUST RIGHT OF STR0, PERFORMED UT THICKNESS CHECK, REMAINING MATERIAL 0.051", PERFORMED HFEC NO DEFECTS NOTED, AREA IS WITHINMar 18, 2021 · N435AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202103267727Skin · damagedLIGHTNING STRIKE DAMAGE TO OF FUSELAGE AT FS383 LEFT OF STRINGER 0 TO EDGE OF ANTENNA ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED DAMAGE AT FS383 LEFT OF STR0, PERFORMED UT THICKNESS CHECK, REMAINING MATERIAL 0.052", PERFORMED HFEC NO DEFECTS NOTED, AREA IMar 18, 2021 · N435AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202101157544Control Panel · malfunctionedAFTER TAKE-OFF, CWA, LANDING GEAR WOULD NOT RETRACT, STAYED THREE GREEN. RECEIVED INBOARD A/SKID CAUTION AND PARKING BRAKE SOV CAUTION MESSAGES. PUT GEAR HANDLE DOWN, MESSAGES CLEARED. AIRCRAFT REMOVED FROM SERVICE. CODE ON PROX SYSTEM BOX. DI-11-DOWN. OJan 14, 2021 · N435AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA202010027301Bypass Valve · damagedRECEIVED LAV SMOKE DET CAUTION AT 600 FT, CW QRH NO SMOKE OR HAZE EVIDENT. HOWEVER, THERE WAS AN ODER OF "ROTTEN EGGS" RETURN TO LNK LANDING WEIGHT 42870, NORMAL LANDING. NO INDICATIONS OF FAILURE IN PACKS. AIRCRAFT REMOVED FROM SERVICE. FOUND LT CONDITIONOct 1, 2020 · N435AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA2020041747259Relay · failedAFTER TAKEOFF WE RECEIVED A GEAR DISAGREE WITH NOSE GEAR DOWN AND MAINS UP. RAN QRH LANDED WITHOUT INCIDENT. A/C WAS CARRYING 5 PASSENGERS, NO JUMPSEATER, WITH CA FLYING. FA AND PAX WERE NOTIFIED AND NO ADVERSE REACTIONS NOTED. FIRE/EMS RESPONDED DUE TO EMERGEApr 15, 2020 · N435AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA2020040347253Skin Panel · dentedDENT ON AFT FUSE AT FS 662.70 BET S22L & S23L. "AIRCRAFT REMOVED FROM SERVICE" CUT OUT DAMAGED AREA AND HFEC WITH NO INDICATIONS NOTED AT THIS TIME. FABRICATED REPAIR DOUBLER FROM 2024-T3 .063" 9.5"L X 7.5"W AND INSTALLED REF CRJ-200 SRM 53 00-31.Mar 30, 2020 · N435AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA2020040647255Skin · dentedDENT ON FUSELAGE SKIN AT FS 630.00 BETWEEN S23R & S24R. "AIRCRAFT REMOVED FROM SERVICE" CUTOUT THE DAMAGE AREA DIMENSION IS 3.1" X 2.3" WITH 0.35" RADIUS ON CORNERS. HFEC PERFUMED WITH NO CRACK INDICATIONS NOTED. FABRICATED REPAIR DOUBLER FROM 2024-T3 .063"Mar 25, 2020 · N435AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA2020040347252Skin Panel · dentedDENT AT FS 692.5 & S24L-3". "AIRCRAFT REMOVED FROM SERVICE" COLD FORMED DENT TO ORIGINAL CONTOUR WITH HFEC PERFORMED WITH A.5" INDICATION. CUT OUT DAMAGE AND HFEC WITH NO INDICATIONS NOTED AT THIS TIME. FABRICATED DOUBLER FROM 2024 T-3 .063" 7" X 6.5" ANDMar 7, 2020 · N435AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA2020040247250Cable · damagedR/H O/B AILERON FUSELAGE CABLE IS FRAYED AT QUADRANT IN WHEEL WELL. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED R/H O/B AILERON FUSELAGE CABLE P/N 601R-90020-133 CRJ-200 AMM 27-00 & 27-11-00 REV 60.Mar 7, 2020 · N435AW · Cndair CL6002B19 · Aileron Control SystemSDR A6WA2020040347254Skin · dented2 FUSELAGE DENTS AT FS 703.875 & S21L AND FS 705 BETWEEN S19L & S20L. DENT @ FS 703.875 &S21L MEASURES .550"L X .4"W X .006"D DENT @ FS 705 BETWEEN S 19L & S20L MEASURES 1.0"L X 1.0"W X .022"D "AIRCRAFT REMOVED FROM SERVICE" BOTH DENTS HAVE BEEN HFEC WITHMar 4, 2020 · N435AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA2020033047249Structure · crackedMULTIPLE CRACKS ON BACK OF APU ENCLOSURE. "AIRCRAFT REMOVED FROM SERVICE" CRACK #1 IS 1.62" IN LENGTH AND LOCATED 9" AFT OF FWD EDGE AND 8" I/B OF LWR O/B EDGE. CRACK #2 IS 1.60" IN LENGTH AND LOCATED 9" AFT OF LWR FWD EDGE AND 5" O/B OF LWR I/B EDGE. BOTH Mar 4, 2020 · N435AW · Cndair CL6002B19 · APU Cowling/ContainmentSDR A6WA2020031747232Skin · dentedDENT @ FS 656 & S20L+1.5" THAT MEASURES .650"L X .3" X .0140"D WITH A W/D 21.43 DENT IS NOT WITHIN ALLOWABLE SRM LIMITS REF CRJ 200 53-00-31 FIG 103 SHEET 104 W/D <25. "AIRCRAFT REMOVED FROM SERVICE" ASAP ENGINEERING EA AWAC-CRJ253-01467 REV IR DTD 3/9/2020Mar 4, 2020 · N435AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA2020040247251Bulkhead · crackedCRACK INDICATION L/H AFT PRESSURE BULKHEAD APPROX LBL 27.5 BELOW WL 138.8. "AIRCRAFT REMOVED FROM SERVICE" MAPPED AFT PRESSURE BULKHEAD WITH A TOTAL OF 10 INDICATIONS FOUND MEASURING AT THE FOLLOWING LOCATIONS: 1. WL 109.5-110.5 & RBL 27.5 L=1.0" 2. WL 106-Mar 3, 2020 · N435AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2020032747247Control Cable · frayedL/H VERTICAL STABILIZER AUTO PILOT HAS RUST AND & FRAYED CABLE. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED FRAYED CABLES P/N 601R90020-131 & 601R90020-79, ELEVATOR SERVO MOTOR P/N 622-5027-101, AND CLUTCH ASSY 822-0260-001. OPS CHECKS OK AT THIS TMar 3, 2020 · N435AW · Cndair CL6002B19 · Elevator Control SystemSDR A6WA2020033047248Door · delaminatedR/H NLG DOOR LWR FWD CORNER HAS DELAMINATION THAT MEASURES .669"L X .299"W X .210"D. "AIRCRAFT REMOVED FROM SERVICE" TRIMMED OUT DELAMINATED AREA AND PERFORMED PERMANENT REPAIR REF ASAP EA # AWAC-CRJ252-01466 REV. A DTD 3/3/2020 AND AIR WISCONSIN SUPPLEMENTMar 2, 2020 · N435AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA2020021847184A/C Pack · malfunctionedEN ROUTE FROM ATW TO DEN OVER NEBRASKA WITH THE LH PACK ON MEL RECEIVED RH PACK OVERPRESSURE MULTIPLE TIMES. FLIGHT DECLARED AN EMERGENCY, DESCENDED TO 10,000 FT AND CONTINUED TO DEN. AIRCRAFT REMOVED FROM SERVICE CW OPS CHECK OF RH PACK IAW AMM 21-51-00. OPFeb 15, 2020 · N435AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA2019121047043Contactor · damagedAC SERVICE BUSS CAUTION. RELAY K4XA WAS FOUND OVERHEATED AND ELECTRICALLY CHARRED. RELAY IS LOCATED UNDER THE COCKPIT FLOOR ON THE RH RELAY TRAY. THIS WAS REPORTED TO ME BY AVIONICS TECH DURING MAINTENANCE. AIRCRAFT REMOVED FROM SERVICE FOUND RING TERMINALSDec 5, 2019 · N435AW · Cndair CL6002B19 · AC Power Distribution SystemSDR A6WA2019091046857Warning System · activatedON DEPARTURE THE FLIGHT CREW EXPERIENCED A LT PACK HIGH PRESSURE CAUTION MESSAGE WITH RT PACK ALREADY ON MEL. THEY ACCOMPLISHED THE QRH, COMMUNICATED WITH DISPATCH, ADVISED ATC OF THE PROBLEM, REQUESTED DELAY VECTORS TO BURN OFF FUEL AND DECLARED AN EMERGENCY.Sep 8, 2019 · N435AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA2018041145767Door Sill · corrodedFWD SERVICE DOOR AFT LOWER SILL CORRODED AT FS 349.00, RBL36. REPAIRED FLOOR SILL AT FS 349.00, RBL36 AFT OF SERVICE DOOR LOWER SILL IAW AWAC EA# AWAC-CRJ253-00925 REV-IR.Apr 10, 2018 · N435AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018041045764Skin · crackedRIGHT WING DRAIN HOLE AT WS 85.50 CRACKED.Apr 9, 2018 · N435AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA2018041045765Skin · crackedLEFT LOWER NOSE HYDRAULIC COMPARTMENT SKIN PANEL CRACKED AT AFT LATCH CUT-OUT.Apr 9, 2018 · N435AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA201845763Frame · crackedFRAME BS 605 IS CRACKED IN 2 SPOTS ON THE FWD SIDE JUST ABOVE AND BELOW STRINGER 9L. REPAIRED THE FRAME.Apr 8, 2018 · N435AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA2018040945761Skin · chafedRIGHT WING AILERON IS CHAFING ON LEADING EDGE LOWER SKIN BETWEEN INBD HINGE AND INBD PCU LINK.Apr 7, 2018 · N435AW · Cndair CL6002B19 · AileronsSDR A6WA2018040945753Bracket · crackedRIGHT MLG PRESSURE TRANSDUCER BRACKET IS CRACKED. REPLACED THE BRACKET IAW SRM 51-42-06, 51-40-11, AND 51-25-16.Apr 4, 2018 · N435AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2018040945758Fitting · crackedBATHTUB FITTING CRACKED AT BS 461.00 OTBD SIDE OF LBL 9. REPLACED THE FITTING IAW SRM 51-40-11, 51-42-06, AND 51-42-21.Apr 2, 2018 · N435AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2018040345749Angle · crackedREAR PRESSURE BULKHEAD, STRINGER 15L OBLIQUE ANGLE IS CRACKED. REPLACED THE OBLIQUE ANGLE IAW SRM 51-42-21, AND 51-42-06.Apr 1, 2018 · N435AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018040345748Angle · corrodedLOWER SERVICE DOOR SILL ANGLE AT BS 319 FOUND CORRODED. REPLACED THE DOOR SILL ANGLE.Apr 1, 2018 · N435AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018040345750Angle · crackedREAR PRESSURE BULKHEAD, STRINGER 14L OBLIQUE ANGLE IS CRACKED. REPLACED THE ANGLE IAW SRM 51-42-21, AND REO 601R-53-61-422.Apr 1, 2018 · N435AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2018040945760Floorbeam · damagedDURING REPAIR OF FS 280 FLOORBEAM, A DAMAGED LIGHTING HOLE BELOW FLOOR WAS FOUND. REPAIRED IAW ROE 601R-53-11-3243 REV --.Mar 31, 2018 · N435AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA2018040345746Angle · crackedPANEL 412BT DIVERTER ANGLES CRACKED. REPLACED THE DIVERTER ANGLES IAW SRM 51-42-06.Mar 31, 2018 · N435AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA2018040345745Channel · crackedCARGO DOOR FWD TRACK LOWER CHANNEL CRACKED. REPLACED THE CHANNEL IAW SRM 51-42-06.Mar 31, 2018 · N435AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2018040345747Angle · crackedPANEL 442BT DIVERTER ANGLES CRACKED. REPLACED THE DIVERTER ANGLES IAW SRM 51-42-06.Mar 31, 2018 · N435AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA2018040345742Retainer · crackedPANEL 422DB SEAL RETAINER CRACKED.Mar 30, 2018 · N435AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA2018040345743Retainer · crackedPANEL 412BT SEAL RETAINER IS CRACKED.Mar 30, 2018 · N435AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA2018040645754Floorbeam · crackedFLOORBEAM ANGLE CRACKED OTBD OF LBL 9 BS 280. REPLACED THE ANGLE IAW REO 601R-53-11-136, REV A.Mar 29, 2018 · N435AW · Cndair CL6002B19 · Fuselage Floor Panel
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