N710CA, cancelled Jul 16, 2013

Service difficulty reports · 94

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 = 'N710CA' AND deregistration_id = 'N710CA-2013-07-16'
  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 COMA2010061550129Pseu · failedEN ROUTE FROM MEM TO PIT RECEIVED GROUND PROX SYS CAUTION MSG. EMERGENCY DECLARED, A/C DIVERTED TO CVG LANDED SAFELY. REMOVED AND REPLACED PSEU. OPS CHECK GOOD.Jun 14, 2010 · N710CA · Cndair CL6002B19 · Landing Gear Position and WarningSDR COMA2009081050177Warning System · activatedON CLIMBOUT FROM LEX RECEIVED RT REV UNLOCK CAUTION MSG, REV DID NOT DEPLOY AND ATR DID NOT ENGAGE. EMERGENCY DECLARED, A/C RETURNED TO LEX LANDED SAFELY. TRANSFERRED TO DEFERRED LIST PER MEL 78-30-01.Aug 6, 2009 · N710CA · Cndair CL6002B19 · Engine Thrust ReverserSDR COMA2009052750143Sill · corrodedSEVERE CORROSION WAS FOUND ON LEFT FLOOR SILL AFT OF PAX DOOR BETWEEN FS 349.00 AND FS 364.00. REMOVED AND SPLICED IN SERVICEABLE SECTION OF FLOOR SILL IAW EA 10-5320-02609 AND SR 99-5140-0001.May 22, 2009 · N710CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA2009052750142Skin · corrodedLT WING FUEL ACCESS PANEL CUTOUT AT 540AB HAS FRETTING CORROSION AROUND EDGES. REMOVED CORROSION IN THE CRITICAL AREA AT FUEL ACCESS PANEL 540AB CUTOUT AND FOUND THAT MATERIAL REMOVED WAS WITHIN LIMITS PER REO 601R-57-21-030 REV G.May 22, 2009 · N710CA · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA2009052750141Skin · corrodedLT WING FUEL ACCESS PANEL CUTOUT AT 540EB HAS FRETTING CORROSION AROUND EDGES. REMOVED CORROSION IN THE CRITAL AREA AT FUEL ACCESS PANEL 540EB CUTOUT AND FOUND THAT MATERIAL REMOVED WAS WITHIN LIMITS PER REO 601R-57-21-030 REV G.May 22, 2009 · N710CA · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA2009052750140Skin · corrodedLT WING FUEL ACCESS PANEL CUTOUT AT 540FB HAS FRETTING CORROSION AROUND EDGES. REMOVED CORROSION IN THE CRITAL AREA AT FUEL ACCESS PANEL 540FB CUTOUT AND FOUND THAT MATERIAL REMOVED WAS WITHIN LIMITS PER REO 601R-57-21-030 REV G.May 22, 2009 · N710CA · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA2009052750139Skin · corrodedLT WING FUEL ACCESS PANEL CUTOUT AT 550BB HAS FRETTING CORROSION AROUND EDGES. REMOVED CORROSION IN THE CRITICAL AREA AT FUEL ACCESS PANEL 550BB CUTOUT AND FOUND THAT MATERIAL REMOVED WAS WITHIN LIMITS PER REO 601R-57-21-030 REV G.May 22, 2009 · N710CA · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA2009022450085Wire Harness · faultyEN ROUTE FROM YYZ TO JFK RECEIVED PAX DOOR WARNING, CARGO DOOR AND SERVICE DOOR CAUTION MSG'S, WITH NO LOSS OF CABIN PRESSURE. A/C DIVERTED TO SYR LANDED SAFELY. FOUND PAX DOOR WIRE HARNESS TO BE FAULTY. REPLACED PAX DOOR WIRE HARNESS.Feb 23, 2009 · N710CA · Cndair CL6002B19 · Door System WiringSDR COMA086359Line · chafedEN ROUTE FROM JAX TO LGA RECEIVED HYD SYS NR 1 LOW PRESS CAUTION MSG. FOLLOWED QRH, HYD QTY SHOWED, PRESS DROPPED TO 0 PSI. ACFT DIVERTED TO RIC AND LANDED SAFELY. FOUND LT ENG EDP SUPPLY LINE CHAFED. REPAIRED EDP SUPPLY LINE IAW CRJ AMM TASK 20-22-00-910-Aug 17, 2008 · N710CA · Cndair CL6002B19 · Hydraulic System, MainSDR COMA0860176Uplock · out of rigFLIGHT 5653 - GEAR DISAGREE MESSAGE ON APPROACH INTO MCI. AIRCRAFT LANDED SAFELY. FOUND NLG UPLOCK PIN OUT OF RIG. PERFORMED RIGGING OF NLG UPLOCK PIN, OPS CHECK GOOD.Mar 14, 2008 · N710CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA0760539Selector Valve · faultyFLIGHT 5258 - DURING LANDING GEAR EXTENSION, RECEIVED GEAR DISAGREE MESSAGE. NOSE GEAR DID NOT COME DOWN. REPLACED NOSE GEAR SELECTOR VALVE. NO FURTHER DEFECTS.Aug 21, 2007 · N710CA · Cndair CL6002B19 · Landing Gear SelectorSDR COMA0760531Priority Valve · faultyFLIGHT 5376 - NOSE GEAR WOULD NOT EXTEND. CYCLED GEAR, ON SECOND ATTEMPT GEAR EXTENDED NORMALLY. LANDED WITHOUT INCIDENT. REPLACED MAIN AND NOSE LANDEING GEAR PRIORITY VALVES. NO FURTHER DEFECTS.Aug 16, 2007 · N710CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA0760175Oxygen System · leakingFLIGHT 4941- EN ROUTE YYZ-JFK DISCOVERED A CREW OXYGEN SUPPLY LEAK, FLIGHT DIVERTED TO AVP. SERVICED THE CREW OXYGEN SYSTEM.Feb 11, 2007 · N710CA · Cndair CL6002B19 · Crew Oxygen SystemSDR COMA0660323Skin Panel · crackedLEFT WING LEADING EDGE HAS CRACK PROPAGATING FROM RIVET AT WS 199. REMOVED AND REPLACED LEFT WING CENTER LEADING EDGE IAW CRJ AMM 57-41-01-400-804. INSTALLED P/N 601R1204403 PER EA 10-5741-01196.May 2, 2006 · N710CA · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA0560831Trim System · malfunctionedFLIGHT 5442 - DURING TAKEOFF ROLL, BOTH STAB TRIM AND MACH TRIM DISENGAGED, ABORTED TAKEOFF AND RETURNED TO GATE. PERFORMED AN OPERATIONAL CHECK OF THE HSTCU AND GROUND RUNS, DISCREPANCIES COULD NOT BE DUPLICATED.Jan 27, 2006 · N710CA · Cndair CL6002B19 · Stabilizer Position IndicatingSDR COMA0560745Priority Valve · faultyFLIGHT 9644 - DURING FERRY FLIGHT 9644 CLE-MCO, RECEIVED A GEAR DISAGREE MESSAGE. FLIGHT DIVERTED TO CAK. REPLACED THE NLG PRIORITY VALVE.Dec 22, 2005 · N710CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA0560741Priority Valve · unreliableFLIGHT 5274 - GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE.Dec 20, 2005 · N710CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA0560574Trim Switch · malfunctionedFLIGHT 5116 - STAB TRIM 1 AND 2 DISCONNECT AND MACH TRIM INOPERABLE. REPLACED THE CO-PILOT TRIM DISCONNECT SWITCH.Oct 27, 2005 · N710CA · Cndair CL6002B19 · Stabilizer Position IndicatingSDR COMA0560326Frame · crackedLT 621.00 FRAME CRACKED. REPAIRED IAW REO 601R-53-61-117.Jun 1, 2005 · N710CA · Cndair CL6002B19 · Fuselage Main, FrameSDR COMA0560327Frame · crackedLT FRAME CRACKED AT STR 10. REPAIRED IAW REO 601R-53-61-487.Jun 1, 2005 · N710CA · Cndair CL6002B19 · Fuselage Main, FrameSDR COMA0560328Door Frame · crackedPAX DOOR FRAME CRACKED AT FS 320 AND 338. REPAIRED IAW REO 601R-52-11-402.Jun 1, 2005 · N710CA · Cndair CL6002B19 · Fuselage Main, StructureSDR COMA0560332Frame · crackedLT AND RT FS 718 FRAME CRACKED. REPAIRED IAW EO 53-027.Jun 1, 2005 · N710CA · Cndair CL6002B19 · Fuselage Main, FrameSDR COMA0560331Support Beam · crackedCENTER ENGINE SUPPORT BEAM (LOWER WEB) CRACKED. REPAIRED IAW REO 601R-53-61-1353.Jun 1, 2005 · N710CA · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR COMA0560330Drag Angle · crackedLT MLG DRAG ANGLE INBOARD OF BATTERY RIB CRACKED. REPAIRED IAW CRJ SRM 51-42-21.Jun 1, 2005 · N710CA · Cndair CL6002B19 · Fuselage, Landing Gear Attach FittingsSDR COMA0560329Rib · crackedRT BATT RIB CRACKED. REPAIRED IAW REO 601R-57-51-046.Jun 1, 2005 · N710CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA0560230Engine · out of toleranceFLIGHT 5267 DURING CLIMBOUT OF CVG THE RIGHT ENGINE WOULD NOT ACHIEVE CHARTED RATED THRUST. AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT ENGINE ASSEMBLY.Apr 5, 2005 · N710CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA0560148Wire Harness · faultyFLIGHT 5153 AFTER TAKEOFF FROM CVG RECEIVED A GEAR UP DISAGREE MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. REPLACED THE NLG WIRING HARNESS ASSEMBLY.Feb 28, 2005 · N710CA · Cndair CL6002B19 · Landing Gear System WiringSDR COMA0460446Sensor · malfunctionedFLIGHT 5492, RT ENGINE HIGH OIL TEMP. REPLACED THE OIL TEMP SENSOR.Aug 3, 2004 · N710CA · Cndair CL6002B19 · Engine Oil QuantitySDR COMA0460347Reservoir · malfunctionedFLIGHT 5556 LANDING GEAR DISAGREE WARNING. REPLACED THE NR 3 SYSTEM HYDRAULIC RESERVOIR.Jun 2, 2004 · N710CA · Cndair CL6002B19 · Hydraulic Reservoir, MainSDR COMA0460242Receiver · malfunctionedFLIGHT 5837 COPILOTS GLIDESLOPE FLAG ON APPROACH. REPLACED THE NR 2 NAV RECEIVER.Apr 1, 2004 · N710CA · Cndair CL6002B19 · Glide Slope SystemSDR COMA0360490Flap · malfunctionedFLIGHT 5144 FLAPS FAIL WARNING MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.Nov 8, 2003 · N710CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0360428Light · defectiveFLIGHT 5601 DURING INSPECTION FOUND THE FLOOR EMERGENCY LIGHTING INOPERATIVE AT ROWS 8 THROUGH 13. REPLACED SECTION OF THE FLOOR EMERGENCY LIGHTING STRIP.Sep 24, 2003 · N710CA · Cndair CL6002B19 · Emergency LightingSDR COMA0360257Pump · failedFLIGHT 5830 GEAR DISAGREE WARNING DURING GEAR EXTENSION AND RETRACTION. REPLACED HYDRAULIC PUMP 3B.May 30, 2003 · N710CA · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR COMA0360174Control Panel · malfunctionedFLIGHT 5843 CARGO FIRE BOTTLE "LOW" CAUTION MESSAGE. REPLACED THE FIRE PANEL.Mar 30, 2003 · N710CA · Cndair CL6002B19 · Extinguishing SystemSDR COMA0360173Fire Bottle · dischargedFLGIHT 5198 - CARGO FIRE BOTTLE "LOW" CAUTION MESSAGE. REPLACED THE CARGO FIRE BOTTLESMar 30, 2003 · N710CA · Cndair CL6002B19 · Fire Bottle, FixedSDR COMA0360172Bottle · dischargedFLIGHT 5198 CARGO FIRE BOTTLE "LOW" CAUTION MESSAGE. REPLACED THE CARGO FIRE BOTTLES.Mar 30, 2003 · N710CA · Cndair CL6002B19 · Fire Bottle, FixedSDR COMA0360047Fire BottleFLIGHT 5292 CARGO FIRE BOTTLE LOW MESSAGE.COULD NOT DUPLICATE. INPSECTED BOTTLE AND WIRING - NO DEFECTS.Jan 23, 2003 · N710CA · Cndair CL6002B19 · Extinguishing SystemSDR COMA0260681Pdu · malfunctionedFLIGHT 5238 FLAPS FAILED AT 8 DEGREES.REPLACED THE PDU.Nov 30, 2002 · N710CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0260677FlapFLIGHT 6009 FLAPS FAILED AT ZERO DEGREES.COULD NOT DUPLICATE. C/W EO 27-045 AND 27-046. NO DEFECTS FOUND.Nov 27, 2002 · N710CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0260670FlapFLIGHT 5371 FLAPS FAILED AT 0 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01.Nov 26, 2002 · N710CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0260603DoorFLIGHT 5670 LOUD SQUEAL AND VIBRATION IN FLIGHT.FOUND AIRCRAFT EXTERNAL SERVICE PANEL OPEN. INPSPECTED FOR DAMAGE AND SECURED DOOR.Oct 22, 2002 · N710CA · Cndair CL6002B19 · Service DoorsSDR COMA0260422Check Valve · wornFLIGHT 5703 R/H ENGINE OIL TEMP INDICATED 165 DEGREES C DURING CLIMBFOUND ENGINE OIL OVER SERVICED - DRAINED EXCESS OIL AND REPLACED LUBE PUMP OIL FILTER CHECK VALVE.Jul 10, 2002 · N710CA · Cndair CL6002B19 · Engine Oil Indicating SystemSDR COMA0260235Bpsu · malfunctionedFLIGHT 5297 FLAPS FAILED AT 0 DEGREES.REPLACED THE R/H BPSU.Apr 5, 2002 · N710CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0260205Control Unit · malfunctionedFLIGHT 5279 R/H 14TH STAGE BLEED AIR DUCT WARNING IFSD.REPLACED THE BLEED AIR CONTROL UNIT.Mar 20, 2002 · N710CA · Cndair CL6002B19 · Pneumatic Indicating SystemSDR COMA0260017ComputerFLIGHT 5371 T/O CONFIG OK MESSAGE WENT OUT DURING T/O.COULD NOT DUPLICATE, ALL T/O CONFIG MESSAGE NORMAL DURING TEST.Dec 27, 2001 · N710CA · Cndair CL6002B19 · Central WarningSDR COMA0160885Web · crackedTHE ENGINE SUPPORT BEAM LOWER WEB WAS CRACKED AT L/H AND R/H SIDES.REMOVED THE CRACKED PORTIONS OF THE LOWER WEB AND PERFORMED A MAJOR REPAIR I/A/W REO 601R-53-61-366 REV D.Nov 10, 2001 · N710CA · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR COMA0160882Frame · crackedDISC CRACKED FRAME FLANGE @F.S.718 R/H SIDE.CORRECTIVE ACTION; CUT OUT DAMAGED FRAME, FABRICATED AND INSTALLED REPAIR SECTION MADE FROM P/N 600-36030-24. ALL WORK PERFORMED I/A/W WVAC EO 601R-53-2828, CANADAIR CRJ REO 601R-53-61-193 AND CRJ SRM REF LOG PAGENov 9, 2001 · N710CA · Cndair CL6002B19 · Fuselage Main, FrameSDR COMA0160657DoorFLIGHT #5967. DURING TAXI OUT DISCOVERED THAT THE COCKPIT DOOR WOULD NOT LATCH, AIRCRAFT RETURNED TO THE GATE.REPLACED THE COCKPIT DOOR ASSEMBLY.Aug 29, 2001 · N710CA · Cndair CL6002B19 · Flight Compartment EquipmentSDR COMA0160463Fcu · failedAFTER T/O FROM CVG FLAP FAULT CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIELD.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "SECOND EVENT" MAINTENANCE ACTION, PARAGRAPH (B)3(D AND E)4. REPLACED THE FLAP ELECTRONIC CONTROL UNIT.Jul 11, 2001 · N710CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0160466Bpsu · failedFLAP FAIL CAUTION FLIGHT TEST OF FLAP SYSTEM, AIRCRAFT RETURNED TO CVG AND LANDED SAFETY.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "SECOND EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 3 AND (D AND E) 4. REPLACED THE RIGHT BRAKE POSITIONING SENSING UNIT.Jul 11, 2001 · N710CA · Cndair CL6002B19 · Trailing Edge Flap Control System
Back to N710CA, cancelled Jul 16, 2013