N426AW

Service difficulty reports · 233

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 = 'N426AW' 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 A6WA202412138845Control Handle · malfunctionedAFTER TAKEOFF RECEIVED ANTISKID IB AND PAKING BRAKE SOV CAUTION MESSAGES AFTER GEAR SELECTED TO UP POSITION. GEAR INDICATED DOWN 3 GREEN WITH GEAR LEVER IN UP POSITION DID NOT RECEIVE GEAR DISAGREE WARNING. DID NOT EXCEED SPEED LIMITATIONS REMAINED UNDER 250 KDec 13, 2024 · N426AW · Cndair CL6002B19 · Landing Gear SelectorSDR A6WA202403048720Landing · cracked50057 334424 601R-57-21-3821 HRS 24.45 CRACK FOUND ON LOWER WING SKIN LANDING UNDER ACCESS PANEL 601R10213-4. AIRCRAFT REMOVED FROM SERVICE. (RH MLG) REPAIR WAS PERFORMED TO THE RH WING LOWER AFT PLANK BY MHI MRT. REF. MHI RJ REO 601R-57-21-3821 REV. A DAMar 4, 2024 · N426AW · Cndair CL6002B19 · Wing Main, Frame StructureSDR A6WA202402218717Doubler · corrodedCORROSION ON STRUCTURE AT FS605 BETWEEN STR 25R AND 26R. AIRCRAFT REMOVED FROM SERVICE. EVALUATED AND REMOVED CORROSION FROM FUSELAGE SKIN AT FS605 TO 621 STR 25R AND 26R REF CRJ200 SRM 53-00-00, AND 53-00-31 REV39, AND REMOVED AND REPLACED INTERNAL DOUBLEFeb 21, 2024 · N426AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA202401248711Bracket · crackedCRACKED BRACKET ON PREVIOUS REPAIR ON AFT PRESSURE BULKHEAD NEAR LINTEL AT FS 629.00 AND LBL36. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CHANNEL AT FS 629.00 AND LBL36 WITH FABRICATED NEW CHANNEL. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITJan 24, 2024 · N426AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA202303148500Unknown · unknownRECEIVED GEAR DISAGREE AND NOSE DOOR WARNING MSGS ON TAKEOFF CW QRH MSGS CLEARED. MSGS POSTED ABOUT 6 SECONDS AFTER RETRACTION WAS SELECTED. NO HYD SYSTEM ABNORMALITIES WERE NOTED LANDING WEIGHT WAS 46800 AND LANDING WAS SMOOTH. NO GEAR LIT UP RED ON EICAS. Mar 13, 2023 · N426AW · Cndair CL6002B19 · Landing Gear Door ActuatorSDR A6WA2023012768447Ecu · faultedSTEERING INOP CAUTION CLIMBING THROUGH FL140. C/W QRH MESSAGE PERSISTS. AFTER LANDING WITH NWS ARMED, MESSAGE RETURNED. *****AIRCRAFT REMOVED FROM SERVICE****** R&R NWS ECU IAW AMM 32-51-10. PERFORMED OPS CHECK, OPS CHECK GOOD.PN: 16900-107 S/N OFF: 02-744Jan 26, 2023 · N426AW · Cndair CL6002B19 · Landing Gear Steering SystemSDR A6WA202301208433Rib · damagedTEMPORARY REPAIR TO THE R/H HORIZONTAL STABILIZER CLOSING RIB ******AIRCRAFT REMOVED FROM SERVICE****** REPAIRED CLOSING RIB REF REO 601R-55-11-739 REV A DATED 2023-01-19Jan 20, 2023 · N426AW · Cndair CL6002B19 · Horizontal Stabilizer, Spar/RibSDR A6WA202112318175None · corrodedR/H SIDEWALL SEAT TRACKS (3 EA) FROM FS 409+111.98 TO FS 549.06 HAVE SEVERAL AREAS SURFACE CORROSION. EVALUATED CORROSION ON R/H SIDEWALL SEAT TRACKS AT FS 409+111.98 TO FS 549.06 FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-49 REV 38. *********AIDec 31, 2021 · N426AW · Cndair CL6002B19 · Fuselage, Door HingeSDR A6WA202112288174Skin · dentedDENT ON FORWARD FUSELAGE LOWER SKIN AT FS283 AND STR23R - STR24R. ****AIRCRAFT REMOVED FROM SERVICE **** HAND DRESSED DENT ON AFT FUSELAGE SKIN AT FS283 AND STR23R - STR24R. PN 601R31022-3. DENT DIMENSIONS P1- L = 1.20Ï¿½ X W = 1.00Ï¿½ X D = 0.023Ï¿½. ORIGINALDec 28, 2021 · N426AW · Cndair CL6002B19 · Fuselage Internal StairsSDR A6WA202112288172Skin · dentedDENT ON AFT FUSELAGE SKIN AT FS605.00 Ï¿½ FS621.00 AND S25L - S26L. ***AIRCRAFT REMOVED FROM SERVICE **** VERIFIED NO LOOSE OR PULLED FASTENERS AROUND DENT ON AFT FUSELAGE SKIN AT FS605.00 Ï¿½ FS621.00 AND S25L - S26L. PN 601R35005-143. DENT DIMENSIONS P1- L Dec 28, 2021 · N426AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202112288170Seat Track · corrodedRH SIDEWALL SEAT TRACK FROM FS364 TO FS409.00 + 16 HAS SURFACE CORROSION. ****AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED RH SIDEWALL SEAT TRACK PN 20276-144-0-0 FROM FS364 TO FS409.00 + 16. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS Dec 28, 2021 · N426AW · Cndair CL6002B19 · Fuselage Fixed PartitionsSDR A6WA202112288171Skin · dentedDENT ON AFT FUSELAGE SKIN AT FS654.50 Ï¿½ FS672.20 AND S25L - S26L. ****AIRCRAFT REMOVED FROM SERVICE ***** HAND DRESSED DENT ON AFT FUSELAGE SKIN AT FS654.50 Ï¿½ FS672.20 AND S25L - S26L. PN 601R35005. DENT DIMENSIONS P1- L = 0.500Ï¿½ X W = 0.500Ï¿½ X D = 0.Dec 28, 2021 · N426AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202112288169Seat Track · corrodedRH SIDEWALL SEAT TRACK FROM FS409.00 + 16 TO FS409.00 + 112 HAS SURFACE CORROSION. ***AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED RH SIDEWALL SEAT TRACK PN 20276-144-0-0 FROM FS409.00 + 16 TO FS409.00 + 112. RESTORED PROTECTIVE FINISH. ALL WORK WDec 28, 2021 · N426AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202112288173Fitting · gougedCHAFE DAMAGE TO THE LEFT WING INBOARD FLAP AFT HINGE FITTING. ****AIRCRAFT REMOVED FROM SERVICE ****** BLENDED CHAFE DAMAGE TO THE LEFT WING INBOARD FLAP AFT HINGE FITTING PN601R10315. CHAFE DIMENSIONS L = 0.500Ï¿½ X W = 1.750Ï¿½ X D = 0.020Ï¿½. PERFORMED HFECDec 28, 2021 · N426AW · Cndair CL6002B19 · Leading Edge DevicesSDR A6WA202111187973None · corrodedPAX DOOR FWD ANCHO FITTING PLATE P/N600-38061-11 WAS FOUND CORRODED. THE EXPANSION CAUSED THE PAX DOOR FWD ANCHOR FITTING TO CRACK. ***AIRCRAFT REMOVED FROM SERVICE*** R&R PAX DOOR FWD ANCHOR PLATE AND ALL ATTACHING HARDWARE, FWD PAX DOOR SWIVEL CABLE END, Nov 13, 2021 · N426AW · Cndair CL6002B19 · Horizontal Stabilizer, Tab StructureSDR A6WA2020031047220Wire Harness · defectiveON FINAL NLG DID NOT SHOW DOWN & GREEN. DID NOT RECEIVE GEAR DISAGREE MESSAGE. NLG INDICATED RED. RAN GEAR DISAGREE QRH. NLG BOX TURNED GREEN AND MESSAGE CLEARED. NO ABNORMAL HYD INDICATIONS. NO OTHER EICAS MESSAGES NOTED. AIRCRAFT REMOVED FROM Mar 8, 2020 · N426AW · Cndair CL6002B19 · Landing Gear System WiringSDR A6WA2020010647091Skin · damagedPER CUSTOMER REQUEST, APPLY GENERIC REO 601R-53-11-0048 ON LEFT SIDE SKIN RADIUS AT FS 235. AIRCRAFT REMOVED FROM SERVICE REPAIRED NLG CUTOUT, LH SIDE, AT FS235 I/A/W BOMBARDIER REO 601R-53-11-0048 REV. D.Jan 4, 2020 · N426AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA2020010647094Skin · crackedFUSELAGE SKIN AT AFT RIGHT CORNER NEXT TO SPADE DOOR IS CRACKED. AIRCRAFT REMOVED FROM SERVICE REPAIRED FUSELAGE SKIN IAW REO 601R-53-11-3525 REV-- DATED 01-02-2020.Jan 4, 2020 · N426AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA2020010647092Stiffener · crackedRIGHT HAND VERTICAL STIFFENER ON OUTBOARD SIDE OF NOSE LANDING GEAR WHEEL WELL STRUCTURE IS CRACKED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED RH SIDE VERTICAL STIFFENER ON OUTBOARD SIDE OF NLG WHEEL WELL IAW CRJ200 SRM 51-42-06 AND 51-42-21.Jan 4, 2020 · N426AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2020010647090Retainer · chafedCARGO DOOR SEAL RETAINER CHAFFED IN MULTIPLE SPOTS. AIRCRAFT REMOVED FROM SERVICE REPLACED CARGO DOOR SEAL RETAINER I/A/W CRJ200 SRM 51-42-06 & 51-42-21. CARGO DOOR LEAK CHECK GOOD I/A/W CRJ200 AMM 52-31-07-710-801Jan 4, 2020 · N426AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA2020010647088Strut · crackedBOTTOM SIDE OF APU ENCLOSURE WELD REPAIR IS CRACKED AIRCRAFT REMOVED FROM SERVICE REPAIRED APU ENCLOSURE IAW AWAC SUP 19-341CJan 2, 2020 · N426AW · Cndair CL6002B19 · APU Cowling/ContainmentSDR A6WA2019123047081Rib · crackedPANEL 446AL HAS PREVIOUS REPAIR DOUBLER CRACKED ON 2ND RIB AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED 2ND RIB ON PANEL 446AL IAW BOMB. CMM 20-42-06Dec 22, 2019 · N426AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019122347078Floor Support · corrodedRIGHT FLOOR SILL CORRODED AT NUT PLATE, FS 295.00-319.70, STR17R. AIRCRAFT REMOVED FROM SERVICE REPLACED SILL IAW CRJ200 SRM 51-42-13.Dec 20, 2019 · N426AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019122047070Fitting · crackedRIGHT LOWER WING TO FUSELAGE FAIRING FITTING CRACKED. AIRCRAFT REMOVED FROM SERVICE REPLACED FITTING IAW CRJ 200 SRM 51-42-21.Dec 18, 2019 · N426AW · Cndair CL6002B19 · Aerodynamic FairingsSDR A6WA20192047072Bracket · crackedLEFT WING TO FUSELAGE FAIRING ATTACH BRACKET CRACKED. AIRCRAFT REMOVED FROM SERVICE REPLACED BRACKET IAW CRJ 200 SRM 51-42-06.Dec 17, 2019 · N426AW · Cndair CL6002B19 · Aerodynamic FairingsSDR A6WA20195047074Bracket · crackedLEFT WING TO FUSELAGE FAIRING ATTACH BRACKET CRACKED. AT FS461.00,LBL45. AIRCRAFT REMOVED FROM SERVICE REPLACED BRACKET IAW CRJ200 SRM 51-42-06.Dec 17, 2019 · N426AW · Cndair CL6002B19 · Aerodynamic FairingsSDR A6WA20192047076Bracket · crackedRIGHT WING TO FUSELAGE FAIRING ATTACH BRACKET CRACKED AT FS 449.85, RBL45. AIRCRAFT REMOVED FROM SERVICE REPLACED BRACKET IAW CRJ200 SRM 51-42-06.Dec 17, 2019 · N426AW · Cndair CL6002B19 · Aerodynamic FairingsSDR A6WA20192047075Bracket · crackedLEFT WING TO BODY FAIRING ATTACH BRACKET CRACKED AT FS 449.85, LBL 45. AIRCRAFT REMOVED FROM SERVICE REPLACED BRACKET IAW CRJ 200 SRM 51-42-06.Dec 17, 2019 · N426AW · Cndair CL6002B19 · Aerodynamic FairingsSDR A6WA20192047071Bracket · crackedLEFT FUSELAGE TO WING FAIRING BRACKET CRACKED. AIRCRAFT REMOVED FROM SERVICE REPLACED BRACKET IAW CRJ 200 SRM 51-42-06.Dec 17, 2019 · N426AW · Cndair CL6002B19 · Aerodynamic FairingsSDR A6WA2019121947068Attach Bracket · crackedFAIRING ATTACH BRACKET ON FUSELAGE LONGERON AT RBL 45 AND FS 469.63 IS CRACKED AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED BRACKET IAW CRJ-200 SRM 51-42-06Dec 17, 2019 · N426AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2019121847066Fitting · crackedLEFT LOWER SIDE WINDOW JOINT TO FUSELAGE ATTACH FITTING IS CRACKED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED ATTACH FITTING IAW CRJ 200 SRM 51-42-21Dec 16, 2019 · N426AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2019123047082Support · crackedFS621 APB SUPPORT CRACKED AT LBL45 WL80 AN AFT SIDE OF BULKHEAD AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED STIFFNER IAW CRJ 200 SRM 51-42-06Dec 15, 2019 · N426AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2019121847063Floorbeam · crackedL/H FLOOR SUPPORT SILL PLATE CRACKED AT FS 605.0 ADJACENT TO FASTENER COMMON TO SILL AND FLOOR SUPPORT BEAM AIRCRAFT REMOVED FROM SERVICE REPAIRED L/H FLOOR SILL PLATE AT FS 605.0 IAW REO 601R-53-61-433Dec 14, 2019 · N426AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA2019121847060Skin · crackedLEFT HAND DOOR 211AL AFT LATCH CUT-OUT IS CRACKED REPAIRED SKIN IAW AWAC SUP. 19-016BDec 13, 2019 · N426AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA2019121847058Bulkhead Web · crackedPERFORM MODIFICATION OF THE REAR PRESSURE BULKHEAD WEB FS 621.0 AIRCRAFT REMOVED FROM SERVICE COMPLETED MODIFICATION OF THE REAR PRESSURE BULKHEAD AT FS 621.0 IAW REO 601R-53-61-1240 REV DDec 13, 2019 · N426AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2019121847062Attach Angle · crackedATTACH ANGLE COMMON TO FS621.0 RPB AND CARGO NET AFT TIE DOWN FITTING SUPPORT STRUCTURE IS CRACKED AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED ANGLE IAW CRJ -200 SRM 51-42-21Dec 13, 2019 · N426AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2019121847059Skin · chafedR/H AILERON OUTBOARD LOWER SKIN LEADING EDG IS CHAFFED AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED LEADING EDGE IAW CRJ-200 SRM 51-42-21 AND 51-42-06Dec 13, 2019 · N426AW · Cndair CL6002B19 · AileronsSDR A6WA2019111847014Connector · looseGEN #1 CAUTION MESSAGE IN CRUISE C/W QRH DID NOT RESET. AIRCRAFT REMOVED FROM SERVICE. #1 IDG TEMP BULB CANNON PLUG FOUND LOOSE RE-SECURED CANNON PLUG REF AMM 24-12 OPS CHECK GOOD.Nov 15, 2019 · N426AW · Cndair CL6002B19 · Electrical Power System WiringSDR A6WA2018111246144Unknown · malfunctionedAT CRUISE FL250 NOTICED RT PACK OFF STATUS MESSAGE AND RT PACK OFF SWITCH LIGHT ILLUMINATED. CYCLED RT PACK SWITCH TWICE. PACK REMAINED OFF. SELECTED ECS PAGE ON EICAS. RT 10TH STAGE BLEED CLOSED. CYCLED R 10TH SWITCH CLOSED THEN OPEN. PRESSURIZATION RESUMED. Nov 9, 2018 · N426AW · Cndair CL6002B19 · Pneumatic Distribution SystemSDR A6WA2018100846101Acm · malfunctionedDURING SINGLE PACK OPERATION ON ENGINE BLEED AIR IN CLIMB AT APPROX 92% N1 RECEIVED RIGHT PACK OFF LIGHT AND RIGHT PACK OVERPRESS MESSAGE C/W QRH AND IAC RIGHT PACK OPERATION NORMAL ON APU BLEED R/R ACM IAW 21-51-10. OPS CK GOOD.Oct 5, 2018 · N426AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA2017122145495Skin · dentedRIGHT INBD FLAP LOWER SKIN IS DENTED 22 INCHES FROM INBD EDGE AND 16 INCHES FROM T/E.Dec 20, 2017 · N426AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA2017122145491Frame · crackedFRAME BS 333 BETWEEN STRINGER 2 AND 3 LEFT IS CRACKED.Dec 20, 2017 · N426AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA2017122145496Bulkhead Web · damagedAFT PRESSURE BULKHEAD ABOVE FLOOR HAS SCRATCHES AND BARE METAL. REPAIRED THE BULKHEAD.Dec 20, 2017 · N426AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2017122145492Skin · corrodedLEFT INBD FLAP LOWER SKIN PANEL PITTED WITH BARE METAL AT WS 56.30 TO WS 75.27.Dec 20, 2017 · N426AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA2017122145493Frame · crackedFRAME AT BS 605 ATTACHMENT FLANGES CRACKED ABOVE AND BELOW STRINGER 9L. REPAIRED THE FRAMEDec 20, 2017 · N426AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA2017122145494Vane · chafedLEFT INBD FLAP VANE CHAFED ON THE LE IN MULTIPLE AREAS. REPLACED THE FLAP VANE.Dec 20, 2017 · N426AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA2017121945486Floorbeam · crackedFLOORBEAM BS 280 IS CRACKED AT THE LOWER ANGLE JUST OB OF THE MLG ALT CABLE PULLEY BRACKET. REPAIRED THE ANGLE.Dec 15, 2017 · N426AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA2017121945485Floorbeam · crackedBS 280, LBL 10 FLOORBEAM ANGLE CRACKED. REPLACED THE ANGLEDec 14, 2017 · N426AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA2017121945484Floorbeam · crackedBS 280 RBL 10 FLOORBEAM ANGLE CRACKED. REPLACED THE ANGLEDec 14, 2017 · N426AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201745480Angle · cracked1015090-3000-0014 - L/H UPPER OBLIQUE ANGLE CRACKED AFT PRESSURE BULKHEADDec 13, 2017 · N426AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
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