N467AW

Service difficulty reports · 166

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 = 'N467AW' 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 A6WA201310044336Fitting · crackedAT STRINGER 3L, FS 283 LINTEL FITTING CRACKED. REPLACED FITTING.Oct 4, 2013 · N467AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201310034251Floor Support · corrodedFLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT AND FABRICATED & INSTALLED SERVICEABLE FLOOR SUPPORT IAW SRM 51-42-21, 51-24-16.Oct 3, 2013 · N467AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201310024340Structure · crackedPAX DOOR LOWER EDGE MEMBER CRACKED AT AFT RADIUS. REMOVED EDGE MEMBER CRACK INSTALLED FILLER DOUBLER REPAIR.Oct 2, 2013 · N467AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA20121226056Unknown · malfunctionedFLT 3755: AFTER HOLDING AT LOW ALTITUDES FOR OVER AN HOUR, IN CONSTANT LITE RAIN/SNOW - RECIEVED EFIS COMP MON CAUTION AND IAS YELLOW FLAGS ON BOTH PFD'S AIRSPEED 8-10 KNTS WITHIN 10-15 MINUTES, 20 KNOTS OFF. DETERMINED THAT CAPT'S AIRSPEED WAS MOST ACCURATE.Dec 26, 2012 · N467AW · Cndair CL6002B19 · Integrated Flight SystemSDR A6WA201240586Proximity Sensor · malfunctionedDURING CLIMBOUT, WITH GEAR RETRACTED, REC A GEAR DISAGREE WARNING WITH RED DASHES INDICATED FOR THE NOSE GEAR, MSG CLEARED AFTER RUNNING QRH. C/ FIM 32-60-07, FOUND STORED PSEU CODE S21 NEAR (NOSE GEAR DL1). ADJUSTED GAP AT DOWNLOCK PROXIMITY SENSOR TO 0.064Jun 8, 2012 · N467AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA201140973Acm · odorWHEN PULLING INTO GATE, F/A NOTIFIED CREW OF SMOKE IN CABIN, PERFORMED IAC FOR EVACUATION, DID NOT DISCHARGE LT OR RT ENGINE FIRE BOTTLE OR APU FIRE BOTTLE, LSU SMOKE DETECTOR WENT OFF BOTH PACKS WERE RUNNING ON APU BLEED AIR FOR APPROX 3 MINUTES. RAN BOTH PANov 15, 2011 · N467AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA201141083Skin · chafedLOWER CORE COWL INNER SKIN CHAFED AND GOUGED IN 5 AREAS CUT OUT DAMAGE AND INSTALL REPAIR DOUBLER IAW CMM 71-12-01, AREAS 3, 4, 5 FOUND TO BE LIMITED TO PAINT ONLY.Oct 16, 2011 · N467AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201141089Panel · chafedPANEL 699AB IS CHAFED. BLENDED DAMAGE ON PANEL 699AB IAW SRM 51-12-00, MAX DAMAGE LOSS .015 MAT REMAINING .046 WITHIN SERVICEABLE LIMITS IAW REO 601R-57-60-020.Oct 13, 2011 · N467AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA2011741088Panel · chafedPANEL 699BB CHAFED, BLENDED DAMAGED ON PANEL 699BB IAW 51-12-00, MAX DAMAGE LOSS .010 MAX REMAINING .045 WITHIN LIMITS IAW REO 601R-57-60-020.Oct 13, 2011 · N467AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA201141092Skin · chafedCARGO DOOR EXTERNAL SKIN IS CHAFED NEXT TO HANDLE. BLENDED DAMAGED AREA IAW REO 601R-53-31-086 .100 MAT THICKNESS .025 MAT LOSS .075 MAT REMAINING MAX IS WITHIN SERVICEABLE LIITS IAW REO 601R-53-31-086.Oct 13, 2011 · N467AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA201141085Fitting · looseRT THRUST REVERSER HAS 2 LOOSE INTERLOCK FITTINGS. REMOVED UNSERVICEABLE FASTENERS AND INSTALLED SERVICEABLE FASTENERS IN RT T/R INTERLOCK FITTINGS (2 EA).Oct 13, 2011 · N467AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201141086Skin · chafedLT INBD FLAP VANE SKIN HAS CHAFING DAMAGE IN 3 EA FROM STOPS EVALUATED DAMAGE ON LT INBD FLAP VANE IAW SRM 51-12-00 BLENDED IAW SRM 51-12-00 MAT LOSS .019 AT FLAP STATION 60.005.015 AT FLAP STATION 98.505.005 AT FLAP STATION 137.012 WITHIN SERVICEABLE LIMITS IOct 13, 2011 · N467AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201240027Stiffener · chafedVERTICAL STIFFENER ON AFT SIDE OF 621 BULKHEAD AT BL0 TOWARDS TOP IS CHAFED. BLENDED DAMAGE ON VERTICAL STIFFENER AFT SIDE OF 621 BULKHEAD AT BL0 DAMAGE FOUND TO BE WITHIN LIMITS: MAX DEPTH OF DAMAGE 0.009 IN/ MAX LENGTH OF DAMAGE 0.025 IN IAW REO 601R-53-61Oct 12, 2011 · N467AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201141081Stiffener · chafedVERTICAL STIFFENER ON AFT SIDE OF BS 621 BULKHEAD AT BL 0 TOWARDS TOP IS CHAFED. BLENDED DAMAGE ON VERTICAL STIFFENER AND FOUND TO BE WITHIN LIMITS. MAX DEPTH O DAMAGE 0.009" MAX LENGTH OF DAMAGE 0.025 IN IAW REO 601R-53-61-1523.Oct 12, 2011 · N467AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201141076Stop Fitting · chafedFWD RT STOP FITTING ON THE AVIONIC DOOR IS CHAFED. BLENDED CHAFED AREA AT FWD RT STOP FITTING ON AVIONICS DOOR IAW REO 601R-53-21-2194.Oct 12, 2011 · N467AW · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR A6WA201140903Floorbeam · crackedCLIPS ON FS 280 FLOORBEAM AT LBL9 AND RBL9 ARE CRACKED. REMOVED UNSERVICEABLE CLIPS ON FS 280 FLOORBEAM AT LBL9 AND RBL9. INSTALLED SERVICEABLE CLIPS ON FS280 FLOORBEAM AT LBL9 AND RBL9 IAW SRM 51-42-21, SRM 53-21-43, SRM 51-24-16, SRM 51-40-11.Oct 12, 2011 · N467AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201140904Seat Track · corrodedLBL9 AND RBL9 CARGO BAY SEAT TRACKS, FS 574 CORRODED. REMOVED UNSERVICEABLE SEAT TRACKS AND REPLACED WITH SERVICEABLE SEAT TRACKS IAW SRM 51-41-02.Oct 11, 2011 · N467AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201141080Floorbeam · crackedFLOORBEAM CRACKED AT FS 484, LBL 27 & 36. REPAIRED FLOORBEAM.Oct 10, 2011 · N467AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201141079Floorbeam · crackedFLOORBEAM CRACKED AT FS RBL 27. REPAIRED FLOORBEAM .Oct 9, 2011 · N467AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201141090Roller · chafedRT WING FLAP ROLLER FITTING IS CHAFED. BLENDED CHAFED AREA AT RT WING FLAP ROLLER FITTING IAW REO 601R-57-51-143. ROTO PEENED AREA IAW REO 601R-57-51-143.Oct 8, 2011 · N467AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201141087Fairing · crackedLT OTBD CENTER HINGE ARM FLAP FAIRING GUIDE CRACKED, R & R.Oct 8, 2011 · N467AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201141091Vane · chafedRT INBD FLAP VANE CHAFED ON L/E. BLENDED AREAS ON RT INBD FLAP VANE IAW REO 601-57-52-004 AND SRM 51-12-00. TREATED AREA IAW SRM 51-21-16 AND SRM 51-25-26.Oct 7, 2011 · N467AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201141082Angle · crackedLT SIDE OBLIQUE ANGLE ON FS 621 AFT FACE CRACKED. R & R LT OBLIQUE ANGLE IAW SRM 51-40-11 & REO 601R-53-61-422.Oct 6, 2011 · N467AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201141084Spar · chafedLT ENGINE FWD MOUNT SPAR IN PYLON CHAFE FROM ANTI-ICE DUCT. BLENDED CHAFED AREA ON LT ENG FWD MOUNT SPAR IAW REO 601R-54-50-006 & SRM 51-12-00.Oct 6, 2011 · N467AW · Cndair CL6002B19 · Nacelle/Pylon, Frame/Spar/RibSDR A6WA201140864Angle · crackedRT SIDE OBLIQUE ANGLE ON FS621 AFT SIDE CRACKED. REPLACED RT OBLIQUE ANGLE ON FS 621 IAW SRM 51-42-21.Oct 5, 2011 · N467AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201140440A/C Pack · odorRIGHT PACK OVERTEMP AT GATE WITH ACRID ODOR, P/P ON MEL. R & R RT ACM AND RAM AIR CHECK VALVE AND COALESCER SOCK IAW 21-51-10 AND 21-52-07 AS REQUIRED, OPS CK LEAK GOOD. REMOVED PLACARD AND MEL.Jun 2, 2011 · N467AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA201040462Door · bindingUNABLE TO OPEN MAIN CABIN DOOR FROM INSIDE, OPENED FROM OUTSIDE, INNER HANDLE ONLY MOVED 1/2 TRAVEL. CA IN PROGRESS.Jun 24, 2010 · N467AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200940573Lug · corrodedLT WING FLAP HINGE BOX AT WS 220.00, AFT LUG CORRODED UNDER BUSHING. LT WING FLAP HINGE BOX AT WS 220.00 AFT LUG REPAIRED IAW REO 601R-57-21-1164. (K)Sep 11, 2009 · N467AW · Cndair CL6002B19 · Wing, Control Surface Attach FittingsSDR A6WA200940571Lug · corrodedLT WING FLAP HINGE BOX AT WS 80.50 AFT LUG CORRODED UNDER BUSHING INBD LT WING FLAP HINGE BOX AT WS 80.50 AFT LUG INBD REPAIRED IAW REO 601R57-21-1164. (K)Sep 11, 2009 · N467AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200940570Bulkhead · crackedAFT PRESSURE BULKHEAD WEB AT THE LINTEL LOCATION IS CRACKED. REO 601R-53-61-1230 REV D CARRIED OUT. (K)Sep 8, 2009 · N467AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA20940570Bulkhead · crackedAFT PRESSURE BULKHEAD WEB AT THE LINTEL LOCATION IS CRACKED. REO 601R-53-61-1230 REV D CARRIED OUT. (K)Sep 8, 2009 · N467AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940569Bracket · crackedLT ENGINE TAILPIPE FAIRING OTBD ATTACHMENT, NUT PLATE BRACKET ASSY IS CRACKED. REPLACED IAW SRM 51-42-06. (K)Sep 2, 2009 · N467AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR A6WA200940568Sill · crackedFS 589.00, LBL 47.00 CRACK FOUND ON CARGO ENTRANCE SILL. FS 589.00 LBL 47.00 ON CARGO ENTRANCE SILL DAMAGE REPAIRED IAW REO 601R-53-61-433, REV NC. (K)Sep 2, 2009 · N467AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940567Intercostal · crackedFS 484.00, LBL 36 INTERCOSTAL FOUND CRACKED. CRACK ON INTERCOSTAL AT FS 484.00, LBL 36, REPAIRED IAW REO 601R-53-41-059, REV A. (K)Sep 1, 2009 · N467AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940566Intercostal · crackedFS 484.00, RBL 27 CLIP OF INTERCOSTAL FOUND CRACKED (CRACK LENGTH .300 INCH). CLIP OF INTERCOSTAL AT FS 484.00, RBL 27 REMOVED AND REPLACED IAW SRM 51-42-06 AND 51-42-21. (K)Aug 31, 2009 · N467AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940302Pressure Switch · malfunctioned204552/2 - ON CLIMBOUT, LT ENG OIL PRESS CAS WARNING MULTIPLE TIMES. ACCOMPANIED BY OIL PRESS OF 22-24 PSI UP TO 44 PSI. OIL TEMP WAS 10 DEGREES HIGHER THAN RT. WARNING WENT AWAY WITH POWER REDUCTION. REMOVED AND REPLACED LT LOW OIL PRESSURE SWITCH IAW AMMJun 9, 2009 · N467AW · Cndair CL6002B19 · Engine Oil PressureSDR A6WA200840609Sensor · shortedRECEIVED LT STAGE DUCT MSG INFLIGHT. MSG STAYED ON AFTER RETARDING THRUST LEVER TO IDLE. C/W GVI OF LT 10TH STAGE DUCTING WITH ENGINE RUNNING. NO LEAKS DETECTED. LT 10TH STAGE WARN MSG OCCURRED AGAIN WITH ENGINES SHUTDOWN. CONFIRMED BAD INDICATION. REF 1Nov 15, 2008 · N467AW · Cndair CL6002B19 · Overheat DetectionSDR A6WA200840539Cable · dislodgedPASSENGER DOOR WILL ONLY PARTIALLY OPEN. FOUND POWER ASSIST MOTOR CABLE WAS OUT OF ROLLER TRACK. REMOVED AND REPLACED PAX DOOR POWER ASSIST MOTOR IAW 52-11-08. C/W ELECTRICAL 52 &51. DOOR ASSIST OPS CHECKS GOOD. (A)Jul 9, 2008 · N467AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200840068Flap · malfunctionedFLAPS FAIL CAUTION DISPLAYED ON FINAL APPROACH, COMPLIED WITH QRH BOTH FLAPS DISPLAYED 45 DEGREES. RESET FLAPS, OPS CHECK OK IAW AMM 27-50-AND AWAC SUPLEMENT 98-018B. (K)Feb 12, 2008 · N467AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200740595Computer · malfunctionedAFTER TAKEOFF RT TRANSFER SHUT OFF VALVE CAUTION MESSAGE ILLUMINATED AS WELL AS FUEL CHANNEL 1 STATUS MESSAGE. LOST RT ANF AND TOTAL FUEL IND (AMBER DASHES) CENTER TANK INDICATED 0 DURING FLIGHT AUTO CROSSFLOW INHIBIT STATUS MSG ILLUMINATED DURING FINAL APPROOct 24, 2007 · N467AW · Cndair CL6002B19 · Aircraft Fuel SystemSDR A6WA200740487Web · crackedFOUND AFT WEB CRACKED IN RADIUS .300 INCH LONG AT STEP 832CT ON PAX DOOR. 10-04-07 MAINTENANCE REPAIRED WEB IAW BOMBARDIER REO 601R-52-11-702. (M)Aug 26, 2007 · N467AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740488Web · crackedFOUND FORWARD WEB CRACKED IN RADIUS .400 INCH LONG AT STEP 832CT ON PAX DOOR. S/D - MAINTENANCE REPLACED IAW BOMBARDIER REO 601R-52-11-702. (M)Aug 26, 2007 · N467AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740530Skin · dentedLEFT INBOARD FLAP LOWER SKIN DENTED APPROX 2 INCHES DIAMETER BY .083 INCH DEEP, 1.5 INCH FROM TRAILING EDGE OF FLAP, 1 INCH FROM INBOARD EDGE OF FLAP, FLAP P/N 601R14002-1, S/N SB/RJ/937. MAINTENANCE REPAIRED FLAP LOWER SKIN USING EXTERNAL DOUBLER IAW CRJ 200Aug 24, 2007 · N467AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200740532Panel · crackedRT LOWER VISOR PANEL 326BR, P/N 600-21134-44, CRACKED APPROX 4.5 INCH LONG AT FORWARD END OF PANEL. MAINTENANCE REPLACED DAMAGED PANEL WITH A SERVICEABLE REPAIRED PANEL P/N 600-31134-44. (M)Aug 23, 2007 · N467AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740531Support Beam · crackedCARGO DOOR SUPPORT BEAM LOWER ANGLE, P/N 601R35050-109, CRACKED IN RADIUS APPROX 1.2 INCHES LONG. MAINTENANCE REMOVED AND REPLACED BRACKET (ANGLE) P/N 601R-35050-109 IAW CRJ 200 SRM 51-42-21. (M)Aug 23, 2007 · N467AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA200740476Channel · crackedLT MLG WHEEL WELL BRAKE PRESSURE TRANSDUCER HAT CHANNEL IS CRACKED AT INBOARD LEGS APPROX .20 INCH LONG. MAINTENANCE REMOVED AND REPLACED HAT CHANNEL P/N 601R75262-159 IAW CRJ SRM 51-42-06. (M)Aug 22, 2007 · N467AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740469Skin · corrodedLT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT WS 12.245 (510AB, HOLE NR 2) HAS FRETTING DAMAGE AROUND ENTIRE CIRCUMFERENCE OF HOLE, IN CRITICAL AREA, APPROX .30 INCH WIDE BY .006 INCH DEEP. MAINTENANCE REPAIRED DAMAGED AREA IAW REO 601R-57-21-030 REV FAug 20, 2007 · N467AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740473Floorbeam · crackedFOUND LT FS 621 FLOORBEAM ANGLE CRACKED. MAINTENANCE REPAIRED LT FS 621 FLOORBEAM ANGLE BY CUTTING AWAY DAMAGE AREA AND INSTALLING REPAIR PARTS IAW BOMBARDIER REO 601R-53-61-117 REV C. (M)Aug 20, 2007 · N467AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740471Skin · damagedRIGHT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT WS 54.897 9640BB, HOLE NR 1) HAS FRETTING DAMAGE AT INBOARD AND OUTBOARD ENDS OF CUTOUT IN NON-CRITICAL AREA. INBOARD AREA MEASURES APPROX 6 INCH LENGTH BY .30 INCH WIDE BY .005 INCH DEEP. OUTBOARD AREA Aug 20, 2007 · N467AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740470Skin · corrodedLEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT WS 54.897 (540BB, HOLE NR 1) HAS FRETTING DAMAGE AT INBOARD AND OUTBOARD ENDS. INBOARD END MEASURES APPROX 9.5 INCH BY .30 INCH BY .004 INCH DEEP. OUTBOARD END MEASURES APPROX 4.5 INCH BY .30 INCH BY .004Aug 20, 2007 · N467AW · Cndair CL6002B19 · Wing, Plate/Skin
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