N713CA, cancelled Aug 16, 2013

Service difficulty reports · 63

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 = 'N713CA' AND deregistration_id = 'N713CA-2013-08-16'
  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 COMA2011092650071Mechanism · out of adjustEN ROUTE FROM MSP TO CVG, RECEIVED PAX DOOR LATCH CAUTION MSG. STAYED ON ABOUT 15 MIN UNTIL WE HIT BUMPS AT 6000FT. EMERGENCY DECLARED, A/C DIVERTED TO ORD LANDED SAFELY. ADJUSTED PAX DOOR LATCH MECHANISM IAW CRJ AMM. OPS CHECK GOOD.Sep 23, 2011 · N713CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA2011091950070Bulkhead · crackedREAR PRESSURE BULKHEAD CRACKED AT TOP OF AFT CARGO TRACK. REMOVED DAMAGED AREA FABRICATED PARTS PER REO 601R-53-61-1541. INSTALLED ALL FABRICATED PARTS PER REO 601R-53-61-1541.Sep 19, 2011 · N713CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA2011091550069Bulkhead · crackedREAR PRESSURE BULKHEAD CRACKED AT LINTEL ATTACHMEMT AREA. REMOVED DAMAGE AREA OF REAR BULKHEAD AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1230 AND REO 601R -53-61-4190.Sep 15, 2011 · N713CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA2011091550068Bulkhead · dentedREAR PRESSURE BULKHEAD DENTED AND GOUGED JUST INBOARD OF CONNECTOR J257. REMOVED DAMAGE AREA OF REAR BULKHEAD JUST ABOVE LINTEL FITTING AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-4190.Sep 15, 2011 · N713CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA2011091450067Beam · crackedCRACK ON BOTTOM OF FS 280 BEAM AT RBL 9. REMOVED DAMAGE FABRICATED REPAIR PARTS AND INSTALLED IAW REO601R-53-11-171 REV D.Sep 13, 2011 · N713CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA2011091250066Floor Support · corrodedCOCKPIT FLOOR SUPPORT AT FS 280 IS HEAVILY CORRODED (CAMLOCK ANGLE). REPLACED CAMLOCK ANGLE P/N 600-34017-351S IAW SRM 51-42-06 AND 51-42-21.Sep 12, 2011 · N713CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA2011091250065Beam · crackedCRACK ON TOP ANGLE OF 280 BEAM AT RBL 9. REPAIRED 280 BEAM P/N 600-34017-595 IAW REO 601R-53-11-136 REV A DATED 11/01/07.Sep 12, 2011 · N713CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA2011031750027Control Unit · failedON CLIMBOUT FROM BOS TO RDU WITH ANTI-ICE ON RECEIVED WING OVHT WARNING MSG AT ABOUT 3000FT. EMERGENCY DECLARED, FOLLOWED QRH, MSG STAYED ON OVER 40 SEC AND EXTINGUISHED WITH RT 14TH STAGE OFF. MSG DID NOT RETURN WITH ANTI-ICE IN STBY. A/C LANDED SAFELY IN Mar 16, 2011 · N713CA · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR COMA2009092150194Fuel Control · leakingEN ROUTE FROM JFK TO BNA CREW NOTICED FUMES IN THE COCKPIT. PERFORMED QRH, EMERGENCY DECLARED. A/C DIVERTED TO CRW LANDED SAFELY. INSPECTED A/C FOUND APU FUEL CONTROL LEAKING. REMOVED AND REPLACED APU FUEL CONTROL.Sep 16, 2009 · N713CA · Cndair CL6002B19 · APU Engine Fuel and ControlSDR COMA2009081150181Frame · crackedLEFT FRAME CAP ANGLE BEND RADIUS AT FS 559.00 CRACKED AN BL 18.00. REPAIRED CRACK AT FS 559.00 IAW REO 601R-53-41-260.Aug 11, 2009 · N713CA · Cndair CL6002B19 · Fuselage Main, FrameSDR COMA2009062250154Coalescer Bag · dirtyON T/O F/A AND PASSENGERS REPORTED A BURNING SMELL. EMERGENCY DECLARED, ACFT RETURNED TO DEPARTURE, LANDED SAFELY. REMOVED AND REPLACED COALESCER BAGS. NO FURTHER DEFECTS NOTED.Jun 20, 2009 · N713CA · Cndair CL6002B19 · Humidity Control SystemSDR COMA2008122450045Controller · faultyDURING CRUISE FLIGHT RECEIVED A LEFT WING ANTI-ICE MESSAGE, FLGIHT DIVERTED TO GSO. REPLACED THE ANTI-ICE CONTROLLER.Dec 24, 2008 · N713CA · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR COMA2008121750036Shutoff Valve · faultyON CLIMBOUT FROM CVG RECEIVED WING OVERHEAT WARNING MSG WITH SYSTEM ON, AND IN STANDBY. ACFT RETURNED TO CVG LANDED SAFELY. REMOVED AND REPLACED LEFT ANTI-ICE MODULATING SHUTOFF VALVE.Dec 15, 2008 · N713CA · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR COMA0860300Fire Bottle · intermittentEN ROUTE FROM CLE TO SYR RECEIVED CARGO BOTTLE LOW CAUTION MSG AT 28500, STAYED ON FOR 3 MIN THEN WENT OUT. EMERGENCY DECLARED, ACFT RETURNED BACK TO CLE AND LANDED SAFELY. REMOVED AND REPLACED CARGO FIRE BOTTLE. (S)Jun 20, 2008 · N713CA · Cndair CL6002B19 · Fire Bottle, FixedSDR COMA0860299Fire Bottle · intermittentEN ROUTE FROM CLE TO SYR RECEIVED CARGO BOTTLE LOW CAUTION MSG AT 28500. STAYED ON FOR 3 MIN THEN WENT OUT. EMERGENCY DECLARED, ACFT RETURNED BACK TO CLE AND LANDED SAFELY. REMOVED AND REPLACED CARGO FIRE BOTTLE. (S)Jun 20, 2008 · N713CA · Cndair CL6002B19 · Fire Bottle, FixedSDR COMA0860287Priority Valve · leakingLANDING GEAR WOULD NOT EXTEND. FLUID LEVEL OF HYD SYSTEM 3 WAS 5%. DECLARED EMERGENCY, PERFORMED EMERGENCY EXTENSION, LANDED WITHOUT INCIDENT. REPLACED MLG PRIORITY VALVE, WHICH WAS LEAKING AT EXPANSION FITTING. SERVICED SYSTEM 3. NO FURTHER DEFECTS. (S)Jun 13, 2008 · N713CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA0860284Priority Valve · faultyRECEIVED NOSE GEAR DISAGREE MESSAGE ON APPROACH. FOLLOWED QRH, DECLARED EMERGENCY. LANDING GEAR LOWERED ON RECYCLE. LANDED WITHOUT INCIDENT. REPLACED MGL PRIORITY VALVE. NO FURTHER DEFECTS. (S)Jun 10, 2008 · N713CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA0860276Priority Valve · faultyON APPROACH INTO CVG DURING GEAR DOWN SELECTION RECEIVED GEAR DISAGREE MSG, EXECUTED MISAPPROACH. RAN QRH SECOND GEAR DOWN SELECTION WAS SUCCESSFUL. ACFT LANDED SAFELY IN CVG. REMOVED AND REPLACED NLG PRIORITY VALVE. (S)Jun 9, 2008 · N713CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA0760728Transducer · faultyFLIGHT 9658 - DURING CRUISE FLIGHT RECEIVED A RIGHT ENGINE OIL PRESSURE WARNING MESSAGE, CREW DECLARED AN EMERGENCY, PERFORMED AN I.F.S.D. AND DIVERTED TO MDT. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT ENGINE OIL PRESSURE TRANSDUCER.Dec 14, 2007 · N713CA · Cndair CL6002B19 · Engine Oil PressureSDR COMA0760727Pump · faultyFLIGHT 9658 - DURING CRUISE FLIGHT RECEIVED A RIGHT ENGINE OIL PRESSURE WARNING MESSAGE, CREW DECLARED AN EMERGENCY, PERFORMED AN I.F.S.D. AND DIVERTED TO MDT. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT ENGINE LUBRICATION AND SCAVENGE PUMP.Dec 14, 2007 · N713CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR COMA0760440Gearbox · overheatedFLIGHT 5589 - EN ROUTE CVG-NAS RECEIVED A RIGHT ENGINE OIL HIGH TEMPERATURE INDICATION. FLIGHT RETURNED TO CVG. SERVICED RIGHT ENGINE AGB.Jun 17, 2007 · N713CA · Cndair CL6002B19 · Turbine Engine Reduction GearSDR COMA0660689Warning Message · illuminatedFLIGHT 5099 - NOSE WHEEL STEERING CAUTION MESSAGE DURING TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. INSPECTED NWS SYSTEM, NO DEFECTS NOTED. PERFORMED OPS CHECK, NO DEFECTS NOTED IAW AMM 32-51-00.Dec 6, 2006 · N713CA · Cndair CL6002B19 · Central WarningSDR COMA0660195Warning System · malfunctionedFLIGHT 5843 - DURING TAKEOFF AT ORF RECEIVED A TRIM CONFIGURATION MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. PERFORMED AN OPERATIONAL CHECK OF FLIGHT CONTROL TRIM SYSTEMS AND INTERROGATED HSTCU, DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE.Feb 26, 2006 · N713CA · Cndair CL6002B19 · Stabilizer Position IndicatingSDR COMA0560701Actuator · unreliableFLIGHT 5653 - FLAPS FAIL CAUTION. REPLACED THE LT FLAP ACTUATOR.Dec 9, 2005 · N713CA · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR COMA0560678Warning System · activatedFLIGHT 5457 - DURING DCA APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTDec 7, 2005 · N713CA · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR COMA0560178Proximity Switch · malfunctionedFLIGHT 9452 CABIN DOOR OUTER HANDLE WARNING. REPLACED PROXIMITY SWITCH DI17.Mar 14, 2005 · N713CA · Cndair CL6002B19 · Door Warning SystemSDR COMA0560048Wire · looseFLIGHT 5509 - 3 EMERGENCY LIGHTS INOP. REPAIRED LOOSE WIRING.Jan 11, 2005 · N713CA · Cndair CL6002B19 · Light System WiringSDR COMA0460416Frame · corrodedDURING A 72/48 MO INSP, TASK CRJ-2-142005, FOUND FUSELAGE FRAME CORRODED ON TOP EDGE. PERFORMED PERMANENT REPAIR IAW COMAIR EA 10-5310-00389.Jul 14, 2004 · N713CA · Cndair CL6002B19 · Fuselage Main, FrameSDR COMA0460257Warning Light · illuminatedFLIGHT 5205 FLAP FAIL CAUTION AFTER LANDING. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.Apr 13, 2004 · N713CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0460253Latch · openFLIGHT 5219 CABIN DOOR HANDLE CAUTION MESSAGE. COULD NOT DUPLICATE. FOUND DOOR HANDLE IN OPEN POSITION. OPERATIONAL CHECK OF DOOR LATCH MECH WAS NORMAL.Apr 10, 2004 · N713CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0360572Bracket · crackedTHERE WAS A CRACKED INTERCOSTAL SUPPORT BRACKET BEHIND HYDRAULIC SYSTEM NR 1 RETURN FILTER BOWL. REMOVED THE CRACKED BRACKET. FABRICATED AND INSTALLED A NEW BRACKET IAW WVAC EO 601R-53-4486.Dec 19, 2003 · N713CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0260722Landing GearFLIGHT 5053 GEAR DISAGREE WARNING MESSAGE.COULD NOT DUPLICATE EXTENSION AND RETRACTION CHECKS ALL NORMAL. HYDRAULIC PUMPS AND RESERVOIR REPLACED FOR TROUBLESHOOTING.Dec 17, 2002 · N713CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA0260704Thermister · malfunctionedFLIGHT 5859 LT WINDOW HEAT CAUTION MESSAGE. SWAPPED CONTROLLER CONNECTIONS TO THE SPARE THERMISTORS, OPERATIONAL CHECK WAS NORMAL.Dec 10, 2002 · N713CA · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR COMA0260659Windshield Wiper · brokenFLIGHT 5080 COPILOTS WINDSHIELD WIPER CAME APART DURING T/O.REPALCED WIPER BLADE ASSY.Nov 19, 2002 · N713CA · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR COMA0260570Control Cable · lack of lubeAILERON CONTROLS SEEMED STIFFENER THEN NORMAL. LUBRICATED THE LEFT AND RIGHT AILERON CONTROL ASSEMBLY PER EO 27-069RB.Oct 5, 2002 · N713CA · Cndair CL6002B19 · Aileron Control SystemSDR COMA0260450SkinI/H WING LOWER SKIN FUEL PANEL LANDINGS @ W.S. 106.40, 127.25, 264.00 AND 294.50 HAVE CORROSION FROM 0.010" - 0.012" DEEP.REMOVED CORROSION BY BLENDING. PERFORMED EDDY CURRENT INSP TO ENSURE COMPLETE DAMAGE REMOVAL. FLAP PEENED RE-WORKED AREAS, AND REAPPLIED PJul 24, 2002 · N713CA · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA0260449Skin · crackedPAX DOOR NIB IS DAMAGED AT F.S. 310.00CUT OUT DAMAGE AND INSTALLED STRAP P/N 601R-52-11-008-1 I/A/W CRJ EO 601R-52-11-008 REV B REPAIR A.Jul 23, 2002 · N713CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0260448Angle · crackedTHE ANGLES AT BL 27 LH AND RH AND INTERCOSTAL AT RBL 36 AT FS 484 WERE FOUND CRACKED.REMVOED DISCREPANT PARTS, FABRICATED AND INSTALLED AND REPLACEMENT PARTS I/A/W WVAC EO 601R-53-3380 DATED 07/22/02.Jul 22, 2002 · N713CA · Cndair CL6002B19 · Fuselage Fixed PartitionsSDR COMA0260368AileronFLIGHT 5759 HEAVIER THAN NORMAL CONTROL FORCE REQUIRED FOR ROLL AND PITCH.INSPECTED FLIGHT CONTROLS AND CABLE TENSIONS. NO DEFECTS FOUND. FORCE CHECKS WITHIN LIMITS.Jun 12, 2002 · N713CA · Cndair CL6002B19 · Aileron Control SystemSDR COMA0260369FlapFLIGHT 5285 FLAPS FAILED MESSAGE DURING LANDING.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01Jun 11, 2002 · N713CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0260344Engine · failedFLIGHT 5376 R/H ENGINE OIL PRESSURE WARNING - FAILED BY ENGINE FAILURE.REPLACED R/H ENGINE.May 30, 2002 · N713CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA0260246PaintFLIGHT 5012 AIRCRAFT ROLLS RIGHT WHEN FLAPS EXTENDED.SANDED ROUGH PAINT ON R/H OUTBD FLAP.Apr 10, 2002 · N713CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0260238Actuator · bindingFLIGHT 5234 FLAPS FAILED MESSAGE. R/H OUTBD FLAP IS TWISTED.REPLACED R/H OUTBD FLAP ACTUATORS,Apr 6, 2002 · N713CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0260237Actuator · malfunctionedFLIGHT 5393 FLAPS FAIL MESSAGE. REPLACED THE LT INBOARD FLAP ACTUATORS.Apr 5, 2002 · N713CA · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR COMA0260143Bpsu · malfunctionedFLIGHT 5079 FLAPS FAIL MESSAGE AFTER T/O.REPLACED THE L/H BPSU.Mar 2, 2002 · N713CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0260097Landing GearFLIGHT 5557 GEAR DISAGREE WARNING, NLG DID NOT RETRACT.FOUND NLG FLAT - SERVICED NLG I/A/W M/M INSTRUCTIONS.Feb 13, 2002 · N713CA · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR COMA0260008Bushing · mislocatedTHE R/H SIDE VERTICAL STABILIZER HAS A MIGRATING BUSHING AT HORIZONTAL STABILIZER PIVOT POINT.REMOVED THE MIGRATING BUSHING. MACHINED AND CADMIUM PLATED A NEW NOMINAL SIZE BUSHING I/A/W WVAC EO 601R-55-2910. INSTALLED THE NEW BUSHING I/A/W CRJ AMM 20-26-00-910Dec 28, 2001 · N713CA · Cndair CL6002B19 · Vertical StabilizerSDR COMA0260007Frame · crackedTHE RT SIDE FRAME AND AFT DOUBLER AT FS 718.0 BETWEEN STRINGERS 10 AND 12 WAS CRACKED. REMOVED CRACKED SECTION OF FRAME AND AFT DOUBLER AND INSTALLED A NEW SECTION OF FRAME AND AFT DOUBLER IAW REO 601R-53-61-193 REV A AND WVAC EO 601R-53-2902A.Dec 28, 2001 · N713CA · Cndair CL6002B19 · Fuselage Main, FrameSDR COMA0260006Doubler · crackedTHE L/H SIDE AFT DOUBLER AT FS718.0 WAS CRACKED BETWEEN STRINGERS 10 AND 12.REMOVED CRACKED DOUBLER AND INSTALLED A NEW DOUBLER I/A/W REO 601R-53-61-193 REV A AND WVAC EO 601R-53-2902A.Dec 28, 2001 · N713CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0160206Skin · crackedLT LOWER WING PLANK CRACKED AT ACCESS HOLES, 540 CB WS 76.161, 550 AB WS 163.00 AND 550 FB WS 274.319. BLENDED OUT DAMAGE AND ROTO-PEENED AS REQUIRED IAW REO 601R-57-21-030.Feb 5, 2001 · N713CA · Cndair CL6002B19 · Wing, Plate/Skin
Back to N713CA, cancelled Aug 16, 2013