# Service difficulty reports: N712CA, cancelled Jul 16, 2013

A list on [N712CA, cancelled Jul 16, 2013](https://openairdocs.org/deregistered/N712CA-2013-07-16.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 73 reports

- [SDR COMA2010010650009](https://openairdocs.org/sdr/COMA2010010650009.md): Skin · cracked · Jan 5, 2010 · N712CA · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT 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.
- [SDR COMA2010010650008](https://openairdocs.org/sdr/COMA2010010650008.md): Skin · gouged · Jan 5, 2010 · N712CA · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT 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.
- [SDR COMA20100650007](https://openairdocs.org/sdr/COMA20100650007.md): Skin · cracked · Jan 5, 2010 · N712CA · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT 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.
- [SDR COMA2010010650006](https://openairdocs.org/sdr/COMA2010010650006.md): Skin · damaged · Jan 5, 2010 · N712CA · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT 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.
- [SDR COMA0860322](https://openairdocs.org/sdr/COMA0860322.md): Lamp · burned out · Jul 13, 2008 · N712CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5416. GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMPS. (A)
- [SDR COMA0760741](https://openairdocs.org/sdr/COMA0760741.md): Bulkhead · cracked · Dec 21, 2007 · N712CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING 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.
- [SDR COMA0760737](https://openairdocs.org/sdr/COMA0760737.md): Stiffener · cracked · Dec 19, 2007 · N712CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING HMV-5 INSPECTION, FOUND CRACK AT LOWER END OF VERTICAL STIFFENER. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW BOMBARDIER REO 601R-53-41-056.
- [SDR COMA0760734](https://openairdocs.org/sdr/COMA0760734.md): Beam · cracked · Dec 18, 2007 · N712CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CABIN FLOOR LATERAL BEAM CRACKED ON LOWER FLANGE. COMPLIED WITH REO601R-53-11-1308 BY CUTTING OUT DAMAGE AND APPLYING DOUBLER.
- [SDR COMA0760733](https://openairdocs.org/sdr/COMA0760733.md): Web · cracked · Dec 18, 2007 · N712CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING 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.
- [SDR COMA0760730](https://openairdocs.org/sdr/COMA0760730.md): Stiffener · cracked · Dec 17, 2007 · N712CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING 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.
- [SDR COMA0760711](https://openairdocs.org/sdr/COMA0760711.md): Attach Fitting · cracked · Dec 11, 2007 · N712CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LONGITUDINAL 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.
- [SDR COMA0760710](https://openairdocs.org/sdr/COMA0760710.md): Attach Fitting · cracked · Dec 11, 2007 · N712CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LONGITUDINAL FLOORBEAM ATTACH CLIP CRACKED FS 280, LBL 10 OUTBOARD SIDE OF BEAM. REMOVED AND REPLACED CLIP IAW CRJ SRM 51-42-21.
- [SDR COMA0760534](https://openairdocs.org/sdr/COMA0760534.md): Light · inoperative · Aug 20, 2007 · N712CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5425 - EMERGENCY LIGHT ON CEILING BY LAV INOP. REMOVED AND REPLACED LAMP.
- [SDR COMA0760441](https://openairdocs.org/sdr/COMA0760441.md): Seal · missing · Jun 18, 2007 · N712CA · Cndair CL6002B19 · Turbine Engine Oil System
  > FLIGHT 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.
- [SDR COMA0760289](https://openairdocs.org/sdr/COMA0760289.md): Proximity Sensor · out of adjust · Mar 26, 2007 · N712CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > FLIGHT 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.
- [SDR COMA0760042](https://openairdocs.org/sdr/COMA0760042.md): Drain Line · failed · Jan 19, 2007 · N712CA · Cndair CL6002B19 · Hydraulic System, Main
  > FLIGHT 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.
- [SDR COMA0660388](https://openairdocs.org/sdr/COMA0660388.md): Pseu · malfunctioned · Jun 11, 2006 · N712CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > FLIGHT 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.
- [SDR COMA0660338](https://openairdocs.org/sdr/COMA0660338.md): Caution Message · false activation · May 10, 2006 · N712CA · Cndair CL6002B19 · Cabin Cooling System
  > FLIGHT 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.
- [SDR COMA0660263](https://openairdocs.org/sdr/COMA0660263.md): Strut · worn · Mar 18, 2006 · N712CA · Cndair CL6002B19 · Main Landing Gear Strut/Axle/Truck
  > FLIGHT 5057 - AFTER TAKEOFF FROM DAY RECEIVED A GEAR DISAGREE/NOSE DOOR OPEN MESSAGE, FLIGHT RETURNED TO THE FIELD. REPLACED THE NLG STRUT LOWER CYLINDER.
- [SDR COMA0560730](https://openairdocs.org/sdr/COMA0560730.md): Target · bent · Dec 16, 2005 · N712CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > FLIGHT 5463 - NLG WILL NOT RETRACT. NLG CENTERED, PROX SWITCH TARGET BENT. C/W TEMPORARY REPAIR TO PROX SWITCH TARGET.
- [SDR COMA0560436](https://openairdocs.org/sdr/COMA0560436.md): Pump · failed · Aug 9, 2005 · N712CA · Cndair CL6002B19 · Engine Fuel Pump
  > FLIGHT 4998 - NR 2 HYDRAULIC SYSTEM HIGH TEMP AND LOW PRESSURE WARNING. REPLACED THE RT ENGINE HYDRAULIC PUMP.
- [SDR COMA0560371](https://openairdocs.org/sdr/COMA0560371.md): Strut · underserviced · Jun 30, 2005 · N712CA · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > GEAR DISAGREE. SERVICED NLG SHOCK STRUT, GEAR SWINGS SATISFACTORY.
- [SDR COMA0460679](https://openairdocs.org/sdr/COMA0460679.md): Light · inoperative · Dec 13, 2004 · N712CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5309 RT OVERWING EMERGENCY LIGHT IS INOP. REPLACED LIGHT BULB.
- [SDR COMA0460588](https://openairdocs.org/sdr/COMA0460588.md): Handle · unsecure · Oct 28, 2004 · N712CA · Cndair CL6002B19 · Passenger/Crew Doors
  > FLIGHT 5812 CABIN DOOR HANDLE CAUTION MESSAGE. FOUND DOOR HANDLE NOT STOWED. OPERATIONAL CHECK OF DOOR SATISFACTORY. NO DEFECTS FOUND.
- [SDR COMA0460427](https://openairdocs.org/sdr/COMA0460427.md): Acm · malfunctioned · Jul 19, 2004 · N712CA · Cndair CL6002B19 · Cabin Cooling System
  > FLIGHT 5888 RT AC PACK HIGH PRESSURE CAUTION. COULD NOT DUPLICATE. AIR CONDITION SYSTEM OPERATES NORMAL.
- [SDR COMA0460408](https://openairdocs.org/sdr/COMA0460408.md): Shutoff Valve · malfunctioned · Jul 11, 2004 · N712CA · Cndair CL6002B19 · Landing Gear Brake System
  > FLIGHT 5724 PARKING BRAKE SOV CAUTION MESSAGE. REPLACED THE PARKING BRAKE SOV.
- [SDR COMA0460405](https://openairdocs.org/sdr/COMA0460405.md): Transducer · malfunctioned · Jul 2, 2004 · N712CA · Cndair CL6002B19 · Engine Oil Indicating System
  > FLIGHT 5282 RIGHT ENGINE OIL PRESSURE WARNING DURING T/O. REPLACED THE OIL PRESSURE TRANSDUCER.
- [SDR COMA0460004](https://openairdocs.org/sdr/COMA0460004.md): Control Unit · failed · Dec 30, 2003 · N712CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5073 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU.
- [SDR COMA0360575](https://openairdocs.org/sdr/COMA0360575.md): Skin · corroded · Dec 19, 2003 · N712CA · Cndair CL6002B19 · Wing, Plate/Skin
  > FRETTING 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.
- [SDR COMA0360499](https://openairdocs.org/sdr/COMA0360499.md): Seal · leaking · Nov 15, 2003 · N712CA · Cndair CL6002B19 · Turbine Engine Accessory Drive
  > FLIGHT 5803 RT ENGINE LOST OIL PRESSURE IFSD. REPLACED THE RT ACCESSORY GEAR BOX OIL SEALS.
- [SDR COMA0360466](https://openairdocs.org/sdr/COMA0360466.md): Thrust Reverser · unlocked · Oct 22, 2003 · N712CA · Cndair CL6002B19 · Engine Thrust Reverser
  > FLIGHT 5141 RIGHT THRUST REVERSER UNLOCKED CAUTION DURING TAKEOFF. SECURED AND DEFERRED MAINTENANCE ON THRUST REVERSER PER MEL.
- [SDR COMA0360373](https://openairdocs.org/sdr/COMA0360373.md): Reservoir · overtemp · Aug 17, 2003 · N712CA · Cndair CL6002B19 · Hydraulic Reservoir, Main
  > FLIGHT 9457 NR 2 HYDRAULIC SYSTEM HIGH TEMP CAUTION. REPLACED THE NR 2 HYDRAULIC RESERVOIR.
- [SDR COMA0360329](https://openairdocs.org/sdr/COMA0360329.md): Aileron · binding · Jul 18, 2003 · N712CA · Cndair CL6002B19 · Aileron Control System
  > FLIGHT 5378 CREW REPORTED "AILERONS BINDING". COULD NOT DUPLICATE - NO AILERON BINDING NOTED - C/W COMAIR EO 27-075 FOR TROUBLESHOOTING.
- [SDR COMA0360265](https://openairdocs.org/sdr/COMA0360265.md): Pcu · malfunctioned · Jun 10, 2003 · N712CA · Cndair CL6002B19 · Drag Control System
  > FLIGHT 5686 UNCONTROLLED MOMENTARY ROLL DURING CRUISE FLIGHT, FOLLOWED BY SPOILERONS FAULT MESSAGE. REPLACED THE RT INBOARD SPOILERON PCU.
- [SDR COMA0360006](https://openairdocs.org/sdr/COMA0360006.md): Coupling · Jan 4, 2003 · N712CA · Cndair CL6002B19 · Pneumatic Distribution System
  > FLIGHT 5239 LEFT 14TH STAGE BLEED AIR DUCT WARNING.TIGHTENED LOOSE BLEED AIR COUPLING AT THE T/R PDU
- [SDR COMA0360011](https://openairdocs.org/sdr/COMA0360011.md): Engine · Dec 31, 2002 · N712CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > FLIGHT 5848 LEFT ENG FAN VIB WARNING, ITT IN RED. IFSDREPLACED THE LEFT ENGINE.
- [SDR COMA0260463](https://openairdocs.org/sdr/COMA0260463.md): Door · Jul 30, 2002 · N712CA · Cndair CL6002B19 · Passenger/Crew Doors
  > FLIGHT 5575 CABIN DOOR OUTER HANDLE CAUTION MESSAGE.COULD NOT DUPLCITE. OPERATION OF CABIN DORO NORMAL.
- [SDR COMA0260343](https://openairdocs.org/sdr/COMA0260343.md): Apu · May 30, 2002 · N712CA · Cndair CL6002B19 · APU Cowling/Containment
  > FLIGHT 5275 SMOKE IN CABIN AND COCKPIT WHEN BLEEDS SOURCE SELECTED TO APU.PLACED APU ON DEFERRED MAINT LIST PER MEL.
- [SDR COMA0260282](https://openairdocs.org/sdr/COMA0260282.md): Wire · Apr 23, 2002 · N712CA · Cndair CL6002B19 · Engine Oil Indicating System
  > FLIGHT 5966 LEFT ENGINE OIL PRESSURE WARNING.REPAIRED CHAFED WIRE AT OIL PRESSURE SWITCH.
- [SDR COMA0260234](https://openairdocs.org/sdr/COMA0260234.md): Computer · malfunctioned · Apr 5, 2002 · N712CA · Cndair CL6002B19 · Rudder Control System
  > FLIGHT 5635 UNCOMMANDED RUDDER OSCILLATIONS.REPLACED THE #2 DCU.
- [SDR COMA0160936](https://openairdocs.org/sdr/COMA0160936.md): Doubler · cracked · Dec 1, 2001 · N712CA · Cndair CL6002B19 · Fuselage Main, Frame
  > THE 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.
- [SDR COMA0160935](https://openairdocs.org/sdr/COMA0160935.md): Bushing · faulty · Nov 30, 2001 · N712CA · Cndair CL6002B19 · Empennage Structure
  > VERTICAL 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.
- [SDR COMA0160431](https://openairdocs.org/sdr/COMA0160431.md): Pdu · frozen · Jul 4, 2001 · N712CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT 16 DEGREES.REPLACED THE FLAP PDU.
- [SDR COMA0160438](https://openairdocs.org/sdr/COMA0160438.md): Bpsu · malfunctioned · Jul 3, 2001 · N712CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAILED AT 17 DEGREES.REPLACED THE LEFT HAND BPSU.
- [SDR COMA0160427](https://openairdocs.org/sdr/COMA0160427.md): Actuator · binding · Jun 30, 2001 · N712CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT 13 DEGREES.REPLACED THE R/H #4 FLAP ACTUATOR.
- [SDR COMA0160411](https://openairdocs.org/sdr/COMA0160411.md): Bpsu · malfunctioned · Jun 28, 2001 · N712CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT 13 DEGREES.REPLACED THE LEFT HAND BPSU.
- [SDR COMA0160412](https://openairdocs.org/sdr/COMA0160412.md): Flap · failed · Jun 28, 2001 · N712CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT 17 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
- [SDR COMA0160081](https://openairdocs.org/sdr/COMA0160081.md): Access Panel · cracked · Jan 7, 2001 · N712CA · Cndair CL6002B19 · Wing, Plate/Skin
  > LOWER 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.
- [SDR COMA0060936](https://openairdocs.org/sdr/COMA0060936.md): Engine · vibration · Nov 22, 2000 · N712CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > LEFT ENGINE N2 VIB WARNING. REPLACED THE LEFT ENGINE.
- [SDR COMA0060836](https://openairdocs.org/sdr/COMA0060836.md): Fcu · malfunctioned · Oct 17, 2000 · N712CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT 8 DEGREES. REPLACED THE FECU.

Next page: https://openairdocs.org/deregistered/N712CA-2013-07-16/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N712CA-2013-07-16/reports

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