N712CA, cancelled Jul 16, 2013

Service difficulty reports · 73

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 = 'N712CA' AND deregistration_id = 'N712CA-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 COMA2010010650009Skin · crackedLEFT LOWER WING PLANK DRAIN VALVE ATTACH HOLE SHOWS DEFECT INDICATION AT WS 65.75, STRINGER 15. OVERSIZED SCREW HOLE TO REMOVE DEFECTS AND INSTALLED A FREEZE PLUG IAW EA 10-5721-02848.Jan 5, 2010 · N712CA · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA2010010650008Skin · gougedLEFT LOWER WING PLANK DRAIN VALVE ATTACH HOLE SHOWS DEFECT INDICATION AT WS 0.0, STRINGER 15. OVERSIZED SCREW HOLE TO REMOVE DEFECTS AND INSTALLED A FREEZE PLUG IAW EA 10-5721-02848.Jan 5, 2010 · N712CA · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA20100650007Skin · crackedRIGHT LOWER WING PLANK DRAIN VALVE ATTACH HOLE SHOWS DEFECT INDICATION AT WS 65.75, STRINGER 15. OVERSIZED SCREW HOLE TO REMOVE DEFECTS AND INSTALLED A FREEZE PLUG IAW EA 10-5721-02848.Jan 5, 2010 · N712CA · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA2010010650006Skin · damagedRIGHT LOWER WING PLANK DRAIN VALVE ATTACH HOLE SHOWS DEFECT INDICATION AT WS 0.0, STRINGER 5. OVERSIZED SCREW HOLE TO REMOVE DEFECTS AND INSTALLED A FREEZE PLUG IAW EA 10-5721-02848.Jan 5, 2010 · N712CA · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA0860322Lamp · burned outFLIGHT 5416. GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMPS. (A)Jul 13, 2008 · N712CA · Cndair CL6002B19 · Emergency LightingSDR COMA0760741Bulkhead · crackedDURING HMV-5 INSPECTION EDDY CURRENT OF AFT PRESSURE BULKHEAD, FOUND 3 CRACKS AROUND LINTEL ATTACHMENT FITTING. REPAIRED CRACKS TO AFT PRESSURE BULKHEAD AROUND LINTEL FITTING AS PER REO 601R-53-61-1230 AND REO 601R-53-61-2463.Dec 21, 2007 · N712CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA0760737Stiffener · crackedDURING HMV-5 INSPECTION, FOUND CRACK AT LOWER END OF VERTICAL STIFFENER. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW BOMBARDIER REO 601R-53-41-056. Dec 19, 2007 · N712CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0760734Beam · crackedCABIN FLOOR LATERAL BEAM CRACKED ON LOWER FLANGE. COMPLIED WITH REO601R-53-11-1308 BY CUTTING OUT DAMAGE AND APPLYING DOUBLER.Dec 18, 2007 · N712CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0760733Web · crackedDURING 559 EDDY CURRENT INSPECTION FOUND A CRACK ON THE 559 WEB. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW SR10-5341-001 REV A SECTION 1 PERMANENT REPAIR.Dec 18, 2007 · N712CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0760730Stiffener · crackedDURING 559 INSPECTION FOUND .6 INCH CRACK ON INBOARD SIDE AND .8 INCH CRACK AT OUTBOARD SIDE OF VERTICAL STIFFENERS. REMOVED DAMAGE AND INSTALLED DOUBLERS PER BOMBARDIER REO 601R-53-41-057.Dec 17, 2007 · N712CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0760711Attach Fitting · crackedLONGITUDINAL FLOORBEAM ATTACH CLIP CRACKED AND HAS LOOSE FASTENERS, INBOARD SIDE OF BEAM FS 280, LBL 9. REMOVED AND REPLACED CLIP IAW CRJ SRM 51-42-21. Dec 11, 2007 · N712CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR COMA0760710Attach Fitting · crackedLONGITUDINAL FLOORBEAM ATTACH CLIP CRACKED FS 280, LBL 10 OUTBOARD SIDE OF BEAM. REMOVED AND REPLACED CLIP IAW CRJ SRM 51-42-21.Dec 11, 2007 · N712CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR COMA0760534Light · inoperativeFLIGHT 5425 - EMERGENCY LIGHT ON CEILING BY LAV INOP. REMOVED AND REPLACED LAMP.Aug 20, 2007 · N712CA · Cndair CL6002B19 · Emergency LightingSDR COMA0760441Seal · missingFLIGHT 4945 - EN ROUTE CVG-OKC RECEIVED A LEFT ENGINE OIL PRESSURE FLUCTUATION WITH INTERMITTENT OIL PRESSURE WARNING. CREW DECLARED AN EMERGENCY AND FLIGHT RETURNED TO CVG LANDING WITHOUT INCIDENT. INSTALLED A STARTER MATING SEAL.Jun 18, 2007 · N712CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR COMA0760289Proximity Sensor · out of adjustFLIGHT 5598 - RECEIVED GEAR DISAGREE WARNING AFTER TAKEOFF. RETURNED TO SAV AND LANDED WITHOUT INCIDENT. FOUND MLG UPLOCK PROXIMITY SENSOR OUT OF ADJUSTMENT AND TARGET LOOSE. ADJUSTED SENSOR AND SECURED TARGET. NO FURTHER DEFECTS.Mar 26, 2007 · N712CA · Cndair CL6002B19 · Landing Gear Position and WarningSDR COMA0760042Drain Line · failedFLIGHT 5385- HYD SYS NR 2 LOW PRESS (SYS QTY SHOWED 5 PERCENT) A/C DIVERTED TO RIC AND LANDED SAFELY. REMOVED AND REPLACED HYD SYS NR 2 CASE DRAIN TUBE ASSY.Jan 19, 2007 · N712CA · Cndair CL6002B19 · Hydraulic System, MainSDR COMA0660388Pseu · malfunctionedFLIGHT 5885 - DURING TAKEOFF ROLL RECEIVED A PROXIMITY SYSTEM FAULT MESSAGE, CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. PERFORMED SYSTEM TEST ON PSEU, DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE.Jun 11, 2006 · N712CA · Cndair CL6002B19 · Landing Gear Position and WarningSDR COMA0660338Caution Message · false activationFLIGHT 5500 - DURING TAKEOFF ROLL RECEIVED A RIGHT AIR CONDITIONING PACK HIGH PRESSURE CAUTION, ABORTED TAKEOFF AND RETURNED TO THE GATE. PERFORMED AN OPERATIONAL CHECK OF THE AIR CONDITIONING PACKS, DISCREPANCY COULD NOT BE DUPLICATED.May 10, 2006 · N712CA · Cndair CL6002B19 · Cabin Cooling SystemSDR COMA0660263Strut · wornFLIGHT 5057 - AFTER TAKEOFF FROM DAY RECEIVED A GEAR DISAGREE/NOSE DOOR OPEN MESSAGE, FLIGHT RETURNED TO THE FIELD. REPLACED THE NLG STRUT LOWER CYLINDER.Mar 18, 2006 · N712CA · Cndair CL6002B19 · Main Landing Gear Strut/Axle/TruckSDR COMA0560730Target · bentFLIGHT 5463 - NLG WILL NOT RETRACT. NLG CENTERED, PROX SWITCH TARGET BENT. C/W TEMPORARY REPAIR TO PROX SWITCH TARGET.Dec 16, 2005 · N712CA · Cndair CL6002B19 · Landing Gear Position and WarningSDR COMA0560436Pump · failedFLIGHT 4998 - NR 2 HYDRAULIC SYSTEM HIGH TEMP AND LOW PRESSURE WARNING. REPLACED THE RT ENGINE HYDRAULIC PUMP.Aug 9, 2005 · N712CA · Cndair CL6002B19 · Engine Fuel PumpSDR COMA0560371Strut · underservicedGEAR DISAGREE. SERVICED NLG SHOCK STRUT, GEAR SWINGS SATISFACTORY.Jun 30, 2005 · N712CA · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR COMA0460679Light · inoperativeFLIGHT 5309 RT OVERWING EMERGENCY LIGHT IS INOP. REPLACED LIGHT BULB.Dec 13, 2004 · N712CA · Cndair CL6002B19 · Emergency LightingSDR COMA0460588Handle · unsecureFLIGHT 5812 CABIN DOOR HANDLE CAUTION MESSAGE. FOUND DOOR HANDLE NOT STOWED. OPERATIONAL CHECK OF DOOR SATISFACTORY. NO DEFECTS FOUND.Oct 28, 2004 · N712CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0460427Acm · malfunctionedFLIGHT 5888 RT AC PACK HIGH PRESSURE CAUTION. COULD NOT DUPLICATE. AIR CONDITION SYSTEM OPERATES NORMAL.Jul 19, 2004 · N712CA · Cndair CL6002B19 · Cabin Cooling SystemSDR COMA0460408Shutoff Valve · malfunctionedFLIGHT 5724 PARKING BRAKE SOV CAUTION MESSAGE. REPLACED THE PARKING BRAKE SOV.Jul 11, 2004 · N712CA · Cndair CL6002B19 · Landing Gear Brake SystemSDR COMA0460405Transducer · malfunctionedFLIGHT 5282 RIGHT ENGINE OIL PRESSURE WARNING DURING T/O. REPLACED THE OIL PRESSURE TRANSDUCER.Jul 2, 2004 · N712CA · Cndair CL6002B19 · Engine Oil Indicating SystemSDR COMA0460004Control Unit · failedFLIGHT 5073 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU.Dec 30, 2003 · N712CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0360575Skin · corrodedFRETTING DAMAGE ON LEFT HAND LOWER WING PLANK FUEL ACCESS HOLE CUTOUT AT 550EB. BLENDED DAMAGE OUT AND ROTO-PEENED AFT OUTBAORD HATCHED AREA IN ACCORDANCE WITH REO 601R-57-21-030.Dec 19, 2003 · N712CA · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA0360499Seal · leakingFLIGHT 5803 RT ENGINE LOST OIL PRESSURE IFSD. REPLACED THE RT ACCESSORY GEAR BOX OIL SEALS.Nov 15, 2003 · N712CA · Cndair CL6002B19 · Turbine Engine Accessory DriveSDR COMA0360466Thrust Reverser · unlockedFLIGHT 5141 RIGHT THRUST REVERSER UNLOCKED CAUTION DURING TAKEOFF. SECURED AND DEFERRED MAINTENANCE ON THRUST REVERSER PER MEL.Oct 22, 2003 · N712CA · Cndair CL6002B19 · Engine Thrust ReverserSDR COMA0360373Reservoir · overtempFLIGHT 9457 NR 2 HYDRAULIC SYSTEM HIGH TEMP CAUTION. REPLACED THE NR 2 HYDRAULIC RESERVOIR.Aug 17, 2003 · N712CA · Cndair CL6002B19 · Hydraulic Reservoir, MainSDR COMA0360329Aileron · bindingFLIGHT 5378 CREW REPORTED "AILERONS BINDING". COULD NOT DUPLICATE - NO AILERON BINDING NOTED - C/W COMAIR EO 27-075 FOR TROUBLESHOOTING.Jul 18, 2003 · N712CA · Cndair CL6002B19 · Aileron Control SystemSDR COMA0360265Pcu · malfunctionedFLIGHT 5686 UNCONTROLLED MOMENTARY ROLL DURING CRUISE FLIGHT, FOLLOWED BY SPOILERONS FAULT MESSAGE. REPLACED THE RT INBOARD SPOILERON PCU.Jun 10, 2003 · N712CA · Cndair CL6002B19 · Drag Control SystemSDR COMA0360006CouplingFLIGHT 5239 LEFT 14TH STAGE BLEED AIR DUCT WARNING.TIGHTENED LOOSE BLEED AIR COUPLING AT THE T/R PDUJan 4, 2003 · N712CA · Cndair CL6002B19 · Pneumatic Distribution SystemSDR COMA0360011EngineFLIGHT 5848 LEFT ENG FAN VIB WARNING, ITT IN RED. IFSDREPLACED THE LEFT ENGINE.Dec 31, 2002 · N712CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA0260463DoorFLIGHT 5575 CABIN DOOR OUTER HANDLE CAUTION MESSAGE.COULD NOT DUPLCITE. OPERATION OF CABIN DORO NORMAL.Jul 30, 2002 · N712CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0260343ApuFLIGHT 5275 SMOKE IN CABIN AND COCKPIT WHEN BLEEDS SOURCE SELECTED TO APU.PLACED APU ON DEFERRED MAINT LIST PER MEL.May 30, 2002 · N712CA · Cndair CL6002B19 · APU Cowling/ContainmentSDR COMA0260282WireFLIGHT 5966 LEFT ENGINE OIL PRESSURE WARNING.REPAIRED CHAFED WIRE AT OIL PRESSURE SWITCH.Apr 23, 2002 · N712CA · Cndair CL6002B19 · Engine Oil Indicating SystemSDR COMA0260234Computer · malfunctionedFLIGHT 5635 UNCOMMANDED RUDDER OSCILLATIONS.REPLACED THE #2 DCU.Apr 5, 2002 · N712CA · Cndair CL6002B19 · Rudder Control SystemSDR COMA0160936Doubler · crackedTHE L/H SIDE FRAME AND AFT DOUBLER AT FS718.0 WERE CRACKED BETWEEN STRINGERS 10 AND 12.REMOVED THE CRACKED AFT DOUBLER AND DAMAGED SECTION OF FRAME. INSTALLED NEW SECTION OF FRAME SPLICE AND NEW AFT DOUBLER I/A/W REO 601R-53-61-193 REV A.Dec 1, 2001 · N712CA · Cndair CL6002B19 · Fuselage Main, FrameSDR COMA0160935Bushing · faultyVERTICAL STABILIZER, L/II HORIZONTAL ATTACH LUG BUSHING MIGRATED.REPLACED BUSHING P/N #600-21061-7 IAW SERVICE BULLETIN 601R-55-007, REF MAINT LOG PAGE #243117 AND COMAIR W/O #169071.Nov 30, 2001 · N712CA · Cndair CL6002B19 · Empennage StructureSDR COMA0160431Pdu · frozenFLAPS FAILED AT 16 DEGREES.REPLACED THE FLAP PDU.Jul 4, 2001 · N712CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0160438Bpsu · malfunctionedFLAP FAILED AT 17 DEGREES.REPLACED THE LEFT HAND BPSU.Jul 3, 2001 · N712CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0160427Actuator · bindingFLAPS FAILED AT 13 DEGREES.REPLACED THE R/H #4 FLAP ACTUATOR.Jun 30, 2001 · N712CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0160411Bpsu · malfunctionedFLAPS FAILED AT 13 DEGREES.REPLACED THE LEFT HAND BPSU.Jun 28, 2001 · N712CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0160412Flap · failedFLAPS FAILED AT 17 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.Jun 28, 2001 · N712CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0160081Access Panel · crackedLOWER WING ACCESS HOLES CRACKED AT 550BB WS 188.040 550CB WS 209.040 AND 550EB WS 253.022. BLENDED DAMAGE AND ROTO-PEENED IAW REO 601R-57-21-030.Jan 7, 2001 · N712CA · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA0060936Engine · vibrationLEFT ENGINE N2 VIB WARNING. REPLACED THE LEFT ENGINE.Nov 22, 2000 · N712CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA0060836Fcu · malfunctionedFLAPS FAILED AT 8 DEGREES. REPLACED THE FECU.Oct 17, 2000 · N712CA · Cndair CL6002B19 · Trailing Edge Flap Control System
Back to N712CA, cancelled Jul 16, 2013