N940CA, cancelled Apr 18, 2018

Service difficulty reports · 127

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 = 'N940CA' AND deregistration_id = 'N940CA-2018-04-18'
  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 COMA2011031750028Skin · crackedDURING EDDY CURRENT OF LWR WING AREA, LT MLG TRUNNION FASTENERS HOLES FOUND ONE FASTENER HOLE CRACKED. REPAIRED LT MLG FASTENER HOLE IAW BOMBARDIER REO 601R-57-21-1388 AS REQUIRED.Mar 17, 2011 · N940CA · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA2010071250142Pump · failedON T/O FROM BTV RECEIVED GEAR DISAGREE WARNING MSG, NOSE GEAR DID NOT RETRACTED MAINS DID. FOLLOWED QRH, EMERGENCY DECLARED. A/C RETURNED TO BTV LANDED SAFELY, ALL GEAR DOWN AND GREEN FOR LANDING. REMOVED AND REPLACED HYDRAULIC PUMP 3A. NO FURTHER DEFECTS.Jul 6, 2010 · N940CA · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR COMA2010010650005Angle · crackedFS 559.00 LEFT CAP ANGLE CRACKED AT LBL 18.00. REPAIRED CRACK AT LEFT FS 559.00 IAW REO 601R-53-41-260.Jan 5, 2010 · N940CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA2010010450004Bulkhead · crackedRIGHT SIDE SEMI PRESSURE BULKHEAD CRACKED A RBL 9, FS 559. CUT OUT DAMAGED WEB AREA AND INSTALLED DOUBLERS IAW REO 601R-53-41-260 REV D, AND DEVIATION REO 601R-53-41-609 REV B.Jan 4, 2010 · N940CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA2009122250302Bulkhead · crackedBULKHEAD WEB CRACKED AROUND LINTEL ATTACH FITTING AT FS 621, LT SIDE. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1230 REV D.Dec 21, 2009 · N940CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA2008122850049Warning System · malfunctionedDURING CLIMBOUT EN ROUTE BOS-CVG RECEIVED A NOSE GEAR DOOR AND GEAR DISAGREE MESSAGE, FLIGHT RETURNED TO BOS. PERFORMED A LANDING GEAR EXTENSION/RETRACTION CHECK, NO DISCREPANCIES NOTED, NO MESSAGES RECEIVED.Dec 28, 2008 · N940CA · Cndair CL6002B19 · Landing Gear Position and WarningSDR COMA2008122250038Clamp · looseON CLIMBOUT FROM CVG RECEIVED ANTI-ICE DUCT WARNING MSG. EMERGENCY DECLARED, A/C RETURNED TO CVG LANDED SAFELY. INSPECTED ACFT, FOUND CLAMP AT LEFT I/B PICCOLO TUBE LOOSE. RETORQUED CLAMP, OPS AND LEAK CHECKS GOOD.Dec 16, 2008 · N940CA · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR COMA2008121650024Duct · crackedRECEIVED LEFT WING ANTI-ICE DUCT WARNING MSG. RETURNED TO YYZ. LANDED WITHOUT INCIDENT. FOUND LEFT WING OUTBOARD ANTI-ICE DUCT CRACKED. REPLACED DUCT WITH SERVICEABLE DUCT. NO FURTHER DEFECTS.Dec 11, 2008 · N940CA · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR COMA2008112450003Flap System · failedFLAPS FAILED AT 0 DEG ON APPROACH INTO DTW. EMERGENCY DECLARED, A/C LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I0002, FLAPS FAIL CAUTION MESSAGE FOLLOW UP MAINTENANCE ACTION.Nov 21, 2008 · N940CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0860392Priority Valve · failedFLIGHT NR 6274 ON T/O FROM CVG RECEIVED NOSE GEAR DISAGREE MSG. EMERGENCY DECLARED. A/C RETURNED BACK TO CVG AND LANDED SAFELY. R&R NLG PRIORITY VALVE.Sep 16, 2008 · N940CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA0860391Wire Harness · failedRECEIVED GEAR DISAGREE MSG ON T/O. NLG DID NOT RETRACT. PERFORMED QRH FOR GEAR DISAGREE. EMERGENCY DECLARED, A/C RETURNED BACK AND LANDED SAFELY. REMOVED AND REPLACED NLG WOW NR 2 WIRE HARNESS. (K)Sep 15, 2008 · N940CA · Cndair CL6002B19 · Landing Gear System WiringSDR COMA0860329Selector Valve · failedON CLIMBOUT FROM CVG RECEIVED NOSE GEAR DISAGREE. EMERGENCY DECLARED, A/C RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED NLG SELECTOR VALVE. (A)Jul 22, 2008 · N940CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA0860100Actuator · faultyFLIGHT 5220 - RECEIVED FLAP FAIL MESSAGE ON APPROACH. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. PERFORMED SI-2-27I0002, AND REPLACED RIGHT INBOARD FLAP ACTUATOR. NO FURTHER DEFECTS. Jan 26, 2008 · N940CA · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR COMA0760424Selector Valve · failedFLIGHT 4947 - AFTER TAKEOFF NOSE GEAR DID NOT RETRACT, AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED NLG SELECTOR VALVE.Jun 8, 2007 · N940CA · Cndair CL6002B19 · Landing Gear SelectorSDR COMA0760392Bulkhead · crackedDURING FS 559 INSPECTION FOUND CRACK AT SEMI-PRESSURE BULKHEAD, FS 559, RBL 9, WL 54.1. STOP DRILLED CRACK AND INSTALLED TEMPORARY DOUBLER PER CRJ REO 601R-53-41-353.May 22, 2007 · N940CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA0760391Stiffener · crackedDURING FS 559 INSPECTION FOUND CRACK AT LOWER END OF VERTICAL STIFFENER, FS 559, RBL 27, INBOARD SIDE. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW CRJ REO 601R-53-41-283.May 22, 2007 · N940CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0760181Flap · malfunctionedFLIGHT 5448 - DURING BGR APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C) FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES.Feb 12, 2007 · N940CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0660481Socket · faultyFLIGHT 5320 - THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT FAILED TEST. REPLACED DEFECTIVE LIGHT SOCKET.Aug 9, 2006 · N940CA · Cndair CL6002B19 · Emergency LightingSDR COMA0660138Spring · faultyFLIGHT 5245 - EN ROUTE CVG-PIT RECEIVED A CABIN DOOR LATCH CAUTION MESSAGE FOLLOWED BY A CABIN DOOR HANDLE WARNING MESSAGE. REPLACED THE CABIN DOOR INNER HANDLE TENSION SPRING.Feb 12, 2006 · N940CA · Cndair CL6002B19 · Door Warning SystemSDR COMA0660136Landing Gear · contaminatedFLIGHT 5818 - DURING GEAR RETRACTION CLIMBING OUT OF MEM RECEIVED A GEAR DISAGREE WARNING MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO MEM. FLIGHT LANDED WITHOUT INCIDENT. REMOVED ICE AND SNOW FROM WHEEL WELLS, PERFORMED SYSTEM TEST OF THE LANDING GEARFeb 11, 2006 · N940CA · Cndair CL6002B19 · Landing Gear Position and WarningSDR COMA0560457Scavenge Pump · malfunctionedFLIGHT 5630 - LEFT ENGINE OIL PRESSURE FLUCTUATING. REPLACED THE SCAVENGE LUBE PUMP.Aug 21, 2005 · N940CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR COMA0560454BOil System · overservicedFLIGHT 5786- LEFT ENGINE OIL PRESSURE WARNING. FOUND OIL SYSTEM OVERSERVICED. REMOVED EXCESS OIL AND OPERATIONAL CHECKS WERE NORMAL.Aug 19, 2005 · N940CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR COMA0560109Control Unit · malfunctionedFLIGHT 5322 FLAPS FAIL CAUTION. REPLACED THE FECU.Feb 5, 2005 · N940CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0560098Smoke · detectedFLIGHT 5128 SMOKE IN COCKPIT AFTER T/O. COULD NOT DUPLICATE. FOUND NO EVIDENCE OF SMOKE, OPERATED ALL SYSTEMS AND FOUND NO DEFECTS.Jan 29, 2005 · N940CA · Cndair CL6002B19 · Air Distribution SystemSDR COMA0460595Warning Light · illuminatedFLIGHT 5152 FLAPS FAILED CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.Nov 2, 2004 · N940CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0460585Structure · corrodedFLIGHT DURING HEAVY MAINTENANCE CHECK (NO ASSOCIATED TASK CARD APPLIED), THE PAX DOOR FORWARD AND AFT BOTTOM CORNERS WERE FOUND TO BE SEVERELY CORRODED. BOTH PARTS WERE REPLACED IN ACCORDANCE WITH BOMBARDIER REO 601R-52-11-567.Oct 27, 2004 · N940CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0460586Skin Panel · crackedDURING COMPLIANCE OF TASK 002-53-160-610 (COMAIR TASK CRJ-2-162011) 2 CRACKS WERE FOUND IN THE PRESSURE FLOOR SKIN FORWARD AND AFT TO FS 461.0, BETWEEN BL 0.0 AND RBL 9.0. THE FORWARD CRACK 2.25 INCH IN LENGTH. THE AFT CRACK WAS 1 INCH IN LENGTH. THE PRESSUOct 20, 2004 · N940CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR COMA0460579Skin Panel · crackedDURING COMPLIANCE OF TASK 002-53-160-610 (COMAIR TASK CRJ-2-162011), 1 CRACK WAS FOUND IN THE PRESSURE FLOOR SKIN NEAR FS 461.0 BETWEEN BL0.0 AND RBL 9.0. THE CRACK 2.25 INCH IN LENGTH. THE PRESSURE FLOOR SKIN WAS REPAIRED IN ACCORDANCE WITH BOMBARDIER REO 6Oct 20, 2004 · N940CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR COMA0460577Channel · corrodedFLIGHT UPON COMPLIANCE OF COMAIR TASK CRJ-2-841010, THE SERVICE DOOR CUTOUT LOWER SILL CHANNEL WAS FOUND CORRODED. THE CHANNEL WAS REMOVED AND REPLACED WITH A NEW PART USING THE CRJ SRM STANDARD PRACTICES.Oct 20, 2004 · N940CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0460477Warning Light · illuminatedFLIGHT 5495 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.Aug 20, 2004 · N940CA · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR COMA0460382Wire · dirtyFLIGHT 5141 FORWARD SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOP. CLEANED WIRE CONNECTION, SYSTEM TEST NORMAL.Jun 15, 2004 · N940CA · Cndair CL6002B19 · Light System WiringSDR COMA0460301Priority Valve · unreliableFLIGHT 5579 GEAR DISAGREE WARNING, REPLACED THE NLG PRIORITY VALVEMay 6, 2004 · N940CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA0360187Drag Brace · lack of lubeFLIGHT 5756 GEAR DISAGREE WARNING, NLG DID NOT RETRACT. LUBRICATED THE NLG DRAG BRACE, OPERATIONAL CHECK SATISFACTORY.Apr 7, 2003 · N940CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA0360183Switch · malfunctionedFLIGHT 5930 CREW REPORTED AT BEGINNING OF TAKEOFF ROLL RECEIVED A STEERING INOP CAUTION MESSAGE. TAKEOFF WAS ABORTED AT LESS THAN 50 KTS. AFTER CLEARING THE RUNWAY, CREW RESET THE STEERING ARM SWITCH, WHICH CLEARED THE MESSAGE. A SUBSEQUENT TAKEOFF WAS PERRMar 22, 2003 · N940CA · Cndair CL6002B19 · Landing Gear Steering SystemSDR COMA0360152Proximity SensorFLIGHT 5031 GEAR DISAGREE WARNING - NLG FAILED TO RETRACT.SERVICED THE NLG STRUT, SUSPECT NOT FULLY EXTENDING.Mar 17, 2003 · N940CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA0360153Proximity SensorFLIGHT 5930 GEAR DISAGREE WARNING, NLG FAILED TO RETRACT.ADJUSTED THE NLG "CENTERED" PROXIMITY SENSOR.Mar 16, 2003 · N940CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA0360128Thrust ReverserFLIGHT 5053 R/H REVERSER UNLOCKED MESSAGE DURING T/O.DEFERRED MAINT PER MEL.Feb 28, 2003 · N940CA · Cndair CL6002B19 · Engine Thrust ReverserSDR COMA0360050FlapFLIGHT 5173 FLAPS FAIL CAUTION MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.Jan 23, 2003 · N940CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0360046Bpsu · unreliableFLIGHT 5608 FLAPS FAILED DURING APPROACH.REPLACED THE L/H BPSU.Jan 23, 2003 · N940CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0260627Pdu · malfunctionedFLIGHT 9493 FLAPS FAILED WHEN SELECTED TO 8 DEGREES.REPLACED THE PDU.Nov 1, 2002 · N940CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0260625Engine · failedFLIGHT 5546 LEFT ENGINE OIL PRESSURE WARNING MESSAGE.REPLACED THE LEFT ENGINE.Oct 30, 2002 · N940CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA0260535Door Seal · leakingFLIGHT 5768 LOUD SQUEAL FROM CABIN DOOR.REPLACED THE DOOR SEAL.Sep 17, 2002 · N940CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0260418Computer · malfunctionedFLIGHT 5322 FLAPS FAIL CAUTION MESSAGE DURING LANDING.REPLACED THE FECUJul 6, 2002 · N940CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0260219FlapFLIGHT 5654 FLAPS FAILED AFTER T/O.COULD NOT DUPLICATE. INSPECTED FLAP SYSTEM, NO DEFECTS FOUND.Mar 26, 2002 · N940CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0260074Thrust ReverserFLIGHT 6013 R/H REVERSER UNLOCK MESSAGE DURING T/O.DEFERRED MAINT. PER M.E.L.Jan 29, 2002 · N940CA · Cndair CL6002B19 · Engine Exhaust SystemSDR COMA0160987Actuator · malfunctionedFLIGHT 5957 FLAPS FAILED WHEN SELECTED FOR APPROACH.COULD NOT DUPLICATE DISCREPANCY; ALL 8 FLAP ACTUATORS REPLACED.Dec 21, 2001 · N940CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0160947FlapFLIGHT #5996 FLAPS FAILED AT ZERO WHEN SELECTED DOWN.RESET THE FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.Dec 6, 2001 · N940CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0160905Beam · crackedCRACK ON ENGINE SUPPORT BEAM UPPER WEB.REPAIRED I/A/W REO 601R-53-61-345.Nov 18, 2001 · N940CA · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR COMA0160875FlapFLIGHT #5872. FLAPS FAILED WHEN SELECTED FOR APROACH.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.Nov 5, 2001 · N940CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0160799ApuFLIGHT #5790 - L/H AC PACK EMITS OILY SMELL WHEN APU BLEED SOURCE USED.COULD NOT DUPLICATE OPERATED L/H AND R/H AC PACKS ON APU AND NO SMOKE OR ODOR WAS NOTED.Oct 10, 2001 · N940CA · Cndair CL6002B19 · APU Bleed Air System
Back to N940CA, cancelled Apr 18, 2018