# Service difficulty reports: N960CA, cancelled Feb 12, 2018

A list on [N960CA, cancelled Feb 12, 2018](https://openairdocs.org/deregistered/N960CA-2018-02-12.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 · 96 reports

- [SDR COMA2010100450214](https://openairdocs.org/sdr/COMA2010100450214.md): Hydraulic Line · leaking · Sep 30, 2010 · N960CA · Cndair CL6002B19 · Hydraulic System, Main
  > ON DESCENT INTO DCA RECEIVED HYD 2 LOW PRESS CAUTION MSG, 0 FLUID AND 0 PSI ON EICAS. EMERGENCY DECLARED, A/C DIVERTED TO BWI LANDED SAFELY. REMOVED AND REPLACED NR 2 EDP PRESSURE HOSE IN RT PYLON.
- [SDR COMA2010092050206](https://openairdocs.org/sdr/COMA2010092050206.md): Engine · overtemp · Sep 17, 2010 · N960CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > ON CLIMBOUT FROM BDL TO CVG LEFT ENGINE EXCEEDED ITT LIMITS, REDUCED THRUST TO 85 PERCENT TO MAINTAIN WITH IN LIMITS. EMERGENCY DECLARED, A/C DIVERTED TO ALB LANDED SAFELY. REMOVED AND REPLACED LEFT ENGINE.
- [SDR COMA2010091750204](https://openairdocs.org/sdr/COMA2010091750204.md): Sensing Element · failed · Sep 16, 2010 · N960CA · Cndair CL6002B19 · Pneumatic Indicating System
  > EN ROUTE FROM CMH TO MSP RECEIVED LEFT 14TH STAGE DUCT WARNING MSG. EMERGENCY DECLARED, A/C DIVERTED TO DAY LANDED SAFELY. REMOVED AND REPLACED LEFT PYLON 14TH STAGE SENSING ELEMENT.
- [SDR COMA2009060850152](https://openairdocs.org/sdr/COMA2009060850152.md): Control Handle · failed · Jun 6, 2009 · N960CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > ON FINAL RECEIVED FLAPS FAIL CAUTION MSG. EMERGENCY DECLARED, ACFT LANDED SAFELY. REMOVED AND REPLACED FLAP CONTROL HANDLE.
- [SDR COMA2009050750131](https://openairdocs.org/sdr/COMA2009050750131.md): Bleed Valve · failed · May 5, 2009 · N960CA · Cndair CL6002B19 · Compressor Bleed Valve
  > EN ROUTE FROM JFK TO CLE LEFT 10TH STAGE BLEED VALVE FAILED TO OPEN. EMERGENCY DECLARED, A/C LANDED SAFELY AT CLE. REMOVED AND REPLACED LEFT 10TH STAGE BLEED VALVE.
- [SDR COMA2008120150020](https://openairdocs.org/sdr/COMA2008120150020.md): Skin Panel · damaged · Dec 1, 2008 · N960CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > COMPLIED WITH MODIFICATION K601R36009-3 ON LT FS 640.00 FRAME AND DOUBLER PER S/B601R-53-061 KIT DRWG K601R36009 REV B, 601R-53-61-506 REV C AND 601R53-61-569. REMOVED AND REPLACED SKIN PANEL BETWEEN LT AND RT TRU DOORS IAW CRJ SRM 51-42-06. DAMAGED SKIN JUS
- [SDR COMA0860395](https://openairdocs.org/sdr/COMA0860395.md): Wire Harness · broken · Sep 18, 2008 · N960CA · Cndair CL6002B19 · Door System Wiring
  > ON CLIMBOUT FROM CVG RECEIVED PAX DOOR OUTER HANDLE MSG. A/C RETURNED BACK TO CVG AND LANDED SAFELY. R&R PAX DOOR WIRE HARNESS. OPS CHECK GOOD.
- [SDR COMA086345](https://openairdocs.org/sdr/COMA086345.md): Flux Detector · failed · Aug 11, 2008 · N960CA · Cndair CL6002B19 · Directional Gyro and Indicating System
  > EFIS COMP MON MSG, FIRST OFFICER`S HEADING DIFFICULT TO RIGHT. ACFT RETURNED BACK TO CVG, LANDED SAFELY. REMOVED AND REPLACED NR 2 FLUX DETECTOR. (S)
- [SDR COMA0860297](https://openairdocs.org/sdr/COMA0860297.md): Floorbeam · cracked · Jun 22, 2008 · N960CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > DURING HMV NR 6 INSPECTION, NDT INSPECTION FOUND A CRACK ON THE FS 559 LBL 18, LOWER CAP ANGLE. CUT OUT DAMAGE SECTION OF CAP ANGLE AND SPLICED IN NEW SECTION WITH DOUBLERS IN ACCORDANCE WITH REO 601R 53-41-260. (S)
- [SDR COMA0860293](https://openairdocs.org/sdr/COMA0860293.md): Bulkhead · cracked · Jun 17, 2008 · N960CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACK ON REAR PRESSURE BULKHEAD AT LBL 36.20 WL 80. REPAIRED REAR PRESSURE BULKHEAD IAW REO 601R-53-61-1285. (S)
- [SDR COMA0860292](https://openairdocs.org/sdr/COMA0860292.md): Post · cracked · Jun 16, 2008 · N960CA · Cndair CL6002B19 · Fuselage Main, Structure
  > DURING HMV-6, EDDY CURRENT INSPECTION FOUND CRACK ON LOWER POST, FS 409+128, LBL 18, OUTBOARD SIDE. CUT OUT DAMAGE AND INSTALLED A DOUBLER IN ACCORDANCE WITH REO 601R-53-41-056 REV E. (S)
- [SDR COMA0860291](https://openairdocs.org/sdr/COMA0860291.md): Stringer Clip · cracked · Jun 16, 2008 · N960CA · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > DURING HMV-6, INSPECTION FOUND FRAME 625 TO STRINGER 15L ATTACH CLIP CRACKED. REMOVED AND REPLACED CLIP IN ACCORDANCE WITH SRM 51-42-20. (S)
- [SDR COMA0860288](https://openairdocs.org/sdr/COMA0860288.md): Bulkhead · cracked · Jun 15, 2008 · N960CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD CRACKED AT THE TOP OF LINTEL FITTING. REPAIRED REAR PRESSURE BULKHEAD AROUND LINTEL FITTING IAW REO 601R-53-61-1230. (S)
- [SDR COMA0860281](https://openairdocs.org/sdr/COMA0860281.md): Frame · cracked · Jun 11, 2008 · N960CA · Cndair CL6002B19 · Fuselage Main, Frame
  > DURING HMV-6, INSPECTION FOUND FLANGE OF FS 640 FRAME CRACKED BETWEEN STRINGERS 13R AND 14R. DAMAGED PORTION OF FLANGE CUT OUT AND REPAIR DOUBLER INSTALLED PER REO 601R-53-61-691. (S)
- [SDR COMA0860283](https://openairdocs.org/sdr/COMA0860283.md): Frame · cracked · Jun 10, 2008 · N960CA · Cndair CL6002B19 · Fuselage Main, Frame
  > LT FUSELAGE FRAME CRACKED AT FS 640 BETWEEN STRINGERS 9 & 10. PERFORMED MODIFICATION K601R36009-3 AS PER PART C OF SB 601R-53-061E. (S)
- [SDR COMA0860282](https://openairdocs.org/sdr/COMA0860282.md): Stiffener · cracked · Jun 10, 2008 · N960CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING HMV-6, EDDY CURRENT INSPECTION FOUND VERTICAL WEB STIFFENER CRACKED ON FWD SIDE OF FS 280, RBL 12, AT AND ABOVE CABIN FLOOR LINE. REMOVED AND REPLACED DAMAGED ANGLE IN ACCORDANCE WITH SRM 51-42-06 AND 51-42-13. (S)
- [SDR COMA0860280](https://openairdocs.org/sdr/COMA0860280.md): Bulkhead · cracked · Jun 10, 2008 · N960CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACK ON REAR PRESSURE BULKHEAD ABOVE CARGO DOOR TRACK. REPAIRED REAR PRESSURE BULKHEAD IAW REO 601R-53-61-1541. (S)
- [SDR COMA0860274](https://openairdocs.org/sdr/COMA0860274.md): Doubler · cracked · Jun 8, 2008 · N960CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > RT FS 718.00 FRAME DOUBLER CRACKED ON THE AFT SIDE AT STRINGERS 10 AND 11. REMOVED AND REPLACED FRAME DOUBLER IAW BOMBARDIER REO 601R-53-61-243. (S)
- [SDR COMA0860273](https://openairdocs.org/sdr/COMA0860273.md): Bulkhead · cracked · Jun 8, 2008 · N960CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FORWARD PRESSURE BULKHEAD CRACKED AT PARKING BRAKE CABLE AT FS 202.75. REPAIRED FORWARD PRESSURE BULKHEAD AT FS 202.75 IAW CRJ REO 601R-53-11-563. (S)
- [SDR COMA0860272](https://openairdocs.org/sdr/COMA0860272.md): Pan · cracked · Jun 8, 2008 · N960CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR BELOW TRUSS CRACKED ON LT SIDE BELOW ACCUMULATOR GAUGE AT FS 193.00. REPAIRED FLOOR IAW REO 601R-53-11-081. (S)
- [SDR COMA0860271](https://openairdocs.org/sdr/COMA0860271.md): Floorbeam · cracked · Jun 8, 2008 · N960CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280 FLOORBEAM (GALLEY SIDE) CRACKED. REPAIRED FS 280 FLOORBEAM IAW REO 601R-53-11-136. (S)
- [SDR COMA0860159](https://openairdocs.org/sdr/COMA0860159.md): Bracket · bent · Mar 5, 2008 · N960CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > FLIGHT 5458 - RECEIVED GEAR DISAGREE MESSAGE AND NOSE DOOR WARNING. NOSE GEAR DID NOT INDICATE UP. COMPLIED WITH QRH. RETURNED TO ATL, LANDED WITHOUT INCIDENT. FOUND NLG OLEO SENSOR BRACKET BENT, INCREASING SENSOR GAP BEYOND LIMIT. REWORKED BRACKET. NO F
- [SDR COMA0760656](https://openairdocs.org/sdr/COMA0760656.md): Anti-Ice System · malfunctioned · Nov 20, 2007 · N960CA · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > FLIGHT 5181 - DURING TAKEOFF ROLL RECEIVED A WING OVERHEAT WARNING MESSAGE, ABORTED T/O AND RETURNED TO THE GATE. DEFERRED WING ANTI-ICE SYSTEM PER MEL 30-12-03.
- [SDR COMA0760434](https://openairdocs.org/sdr/COMA0760434.md): None · none · Jun 13, 2007 · N960CA · Cndair CL6002B19 · Standard Practices/Structures
  > TEMPORARY REPAIR INCORPORATED FOR LEFT LOWER WING PLANK CRACK AT WS 148.019 IAW REO 601R-57-21-138. COMPLIED WITH PERMANENT REPAIR OF THE LEFT LOWER WING PLANK CRACK IAW REO 601R-57-21-130 REV G AND CRJ REO 601R-57-21-829.
- [SDR COMA0760433](https://openairdocs.org/sdr/COMA0760433.md): None · none · Jun 13, 2007 · N960CA · Cndair CL6002B19 · Standard Practices/Structures
  > TEMPORARY REPAIR INCORPORATED FOR RIGHT LOWER WING PLANK CRACK AT WS 148.019 IAW REO 601R-57-21-138. COMPLIED WITH PERMANENT REPAIR OF THE RIGHT LOWER WING PLANK CRACK IAW REO 601R-57-21-130 REV G AND CRJ REO 601R-57-21-829.
- [SDR COMA0760344](https://openairdocs.org/sdr/COMA0760344.md): Pressure Switch · faulty · Apr 28, 2007 · N960CA · Cndair CL6002B19 · Engine Oil Pressure
  > FLIGHT 5637 - RIGHT ENGINE OIL PRESSURE WARNING DURING CLIMBOUT, AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED RIGHT ENGINE OIL PRESSURE SWITCH. OPS CHECK GOOD.
- [SDR COMA0760061](https://openairdocs.org/sdr/COMA0760061.md): Trim Switch · faulty · Jan 25, 2007 · N960CA · Cndair CL6002B19 · Stabilizer Control System
  > FLIGHT 5078 - DURING CLIMBOUT CAPTAIN SIDE STAB TRIM WOULD NOT MOVE IN THE DOWN POSITION. AIRCRAFT RETURNED BACK TO BOS AND LANDED SAFELY. REMOVED AND REPLACED CAPTAIN SIDE PITCH TRIM SWITCH.
- [SDR COMA0660662](https://openairdocs.org/sdr/COMA0660662.md): Warning System · malfunctioned · Nov 27, 2006 · N960CA · Cndair CL6002B19 · Door Warning System
  > FLIGHT 5056 - DURING CLIMBOUT OF BNA RECEIVED A CABIN DOOR OUTER HANDLE MESSAGE, FLIGHT RETURNED TO BNA. PERFORMED AN OPERATIONAL CHECK OF THE CABIN DOOR OUTER HANDLE AND INDICATION, DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE.
- [SDR COMA0660534](https://openairdocs.org/sdr/COMA0660534.md): Window · cracked · Sep 8, 2006 · N960CA · Cndair CL6002B19 · Flight Compartment Windows
  > FLIGHT 5674 - DURING CRUISE FLIGHT, THE LEFT SIDE COCKPIT WINDOW CRACKED. REPLACED THE LEFT COCKPIT SIDE WINDOW.
- [SDR COMA0660485](https://openairdocs.org/sdr/COMA0660485.md): Control Handle · faulty · Aug 11, 2006 · N960CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 9482 - DURING APPROACH, FLAPS FAILED AT 30 DEGREES. CREW LANDED WITHOUT INCIDENT. REPLACED FLAP CONTROL HANDLE.
- [SDR COMA0660296](https://openairdocs.org/sdr/COMA0660296.md): Windshield · failed · Apr 10, 2006 · N960CA · Cndair CL6002B19 · Flight Compartment Windows
  > FLIGHT 5301 - CAPTAIN'S WINDSHIELD SHATTERED. REMOVED AND REPLACED CAPTAIN'S WINDSHIELD.
- [SDR COMA0560483](https://openairdocs.org/sdr/COMA0560483.md): Reservoir · malfunctioned · Sep 2, 2005 · N960CA · Cndair CL6002B19 · Hydraulic Reservoir, Main
  > FLIGHT 5064 - GEAR DISAGREE WARNING. REPLACED THE NR 3 HYDRAULIC RESERVOIR.
- [SDR COMA0560385](https://openairdocs.org/sdr/COMA0560385.md): Selector Valve · malfunctioned · Jul 9, 2005 · N960CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > FLIGHT 5521 - GEAR DISAGREE WARNING. REPLACED THE MLG SELECTOR VALVE.
- [SDR COMA0560023](https://openairdocs.org/sdr/COMA0560023.md): Warning System · malfunctioned · Jan 2, 2005 · N960CA · Cndair CL6002B19 · Pitot/Static Anti-Ice System
  > FLIGHT 5164, LEFT AND RIGHT AOA HEAT CAUTION. RESET SYSTEM. COULD NOT DUPLICATE.
- [SDR COMA0460385](https://openairdocs.org/sdr/COMA0460385.md): Battery · malfunctioned · Jun 19, 2004 · N960CA · Cndair CL6002B19 · Battery/Charger System
  > FLIGHT 5721 DURING CRUISE FLIGHT APU BATTERY INDICATED 99 AMPS, AIRCRAFT DIVERTED TO CLE. DEFERRED THE APU BATTERY PER MEL 24-32-03.
- [SDR COMA0460341](https://openairdocs.org/sdr/COMA0460341.md): Warning Light · illuminated · May 27, 2004 · N960CA · Cndair CL6002B19 · Engine Thrust Reverser
  > FLIGHT 5399 LEFT THRUST REVERSER UNLOCKED CAUTION MESSAGE. DEFERRED MAINT ON T/R PER MEL.
- [SDR COMA0460217](https://openairdocs.org/sdr/COMA0460217.md): Oxygen Mask · activated · Mar 20, 2004 · N960CA · Cndair CL6002B19 · Passenger Oxygen System
  > FLIGHT 5118 02 MASK AT ROW 9 DROPPED DURING T/O. RESTOWED 02 MASKS AT ROW 9.
- [SDR COMA0360164](https://openairdocs.org/sdr/COMA0360164.md): Proximity Sensor · out of adjust · Mar 21, 2003 · N960CA · Cndair CL6002B19 · Door Warning System
  > FLIGHT 9492 AVIONICS DOOR CAUTION MESSAGE AT 8000 FT. ADJUSTED THE AVIONICS DOOR PROXIMITY SENSOR.
- [SDR COMA0360147](https://openairdocs.org/sdr/COMA0360147.md): Pump · malfunctioned · Mar 15, 2003 · N960CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > FLIGHT 5510 GEAR DISAGREE WHEN GEAR SELECTED DOWN.REPLACED THE #3A ACMP
- [SDR COMA0260426](https://openairdocs.org/sdr/COMA0260426.md): Cowling · cracked · Jul 15, 2002 · N960CA · Cndair CL6002B19 · Engine Cowling System
  > RIGHT ENGINE FIXED CORE COWL IS CRACKED IN AFT CHANNEL APPROX 1/5 INCH. REPAIRED CRACK BY STOP DRILLING AND INSTALLING A DOUBLER IAW SHORTS CMM 71-13-01 REPAIR SRS 065 AND REO 601R-71-13-1989.
- [SDR COMA0260425](https://openairdocs.org/sdr/COMA0260425.md): Bushing · damaged · Jul 15, 2002 · N960CA · Cndair CL6002B19 · Horizontal Stabilizer Miscellaneous Structure
  > THE RIGHT VERTICAL STABILIZER HINGE BUSHING WAS DAMAGED AND REQUIRES REPLACEMENT. REMOVED AND REPLACED BUSHING IAW WVAC EO 601R-55-3359 CRJ AMM 20-26-00-910-803.
- [SDR COMA0260414](https://openairdocs.org/sdr/COMA0260414.md): Flap · Jul 5, 2002 · N960CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED MESSAGE AFTER LANDING.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
- [SDR COMA0260192](https://openairdocs.org/sdr/COMA0260192.md): Computer · malfunctioned · Mar 14, 2002 · N960CA · Cndair CL6002B19 · Stabilizer Control System
  > FLIGHT 5860 MACH TRIM/STAB TRIM CAUTION MESSAGE.REPLACED THE HSTCU.
- [SDR COMA0260063](https://openairdocs.org/sdr/COMA0260063.md): Spring · stuck · Jan 24, 2002 · N960CA · Cndair CL6002B19 · Door Warning System
  > FLIGHT 5602 AVIONICS BAY DOOR WARNING DURING T/O.FOUND AVIONICS DOOR SWITCH JAMMED. REPLACED SWITCH SPRING.
- [SDR COMA0260044](https://openairdocs.org/sdr/COMA0260044.md): Flap · Jan 13, 2002 · N960CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5553 FLAPS FAILED AT 30 DEGREES DURING APPROACH.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01.
- [SDR COMA0260048](https://openairdocs.org/sdr/COMA0260048.md): Computer · Jan 11, 2002 · N960CA · Cndair CL6002B19 · Central Warning
  > FLIGHT 5285 CONFIG AILERONS AND CONFIG TRIM AURAL WARNING DURING T/O.COULD NOT DUPLICATE. TEST OF AILERON TRIM SYSTEM WAS NORMAL.
- [SDR COMA0260003](https://openairdocs.org/sdr/COMA0260003.md): Plank · cracked · Dec 24, 2001 · N960CA · Cndair CL6002B19 · Wing, Plate/Skin
  > EDDY CURRENT INDICATES CRACKS.BLENDED OUT DAMAGE AND ROTO-PEENED I/A/W REO 601R-57-21-030.
- [SDR COMA0260005](https://openairdocs.org/sdr/COMA0260005.md): Beam · cracked · Dec 22, 2001 · N960CA · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > ENGINE SUPPORT BEAM CRACKED.REPAIRED DAMAGE I/A/W REO601R-53-61-345.
- [SDR COMA0260001](https://openairdocs.org/sdr/COMA0260001.md): Beam · cracked · Dec 22, 2001 · N960CA · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > ENGINE SUPPORT BEAM CRACKED.REPAIRED DAMAGE I/A/W REO 601R-53-61-366.
- [SDR COMA0160853](https://openairdocs.org/sdr/COMA0160853.md): Switch · faulty · Oct 24, 2001 · N960CA · Cndair CL6002B19 · Autopilot System
  > FLIGHT #5570. DURING TEST OF THE YAW DAMPER SYSTEM THE #2 WOULD NOT ENGAGE.REPLACED THE YAW DAMPER SWITCH.

Next page: https://openairdocs.org/deregistered/N960CA-2018-02-12/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 = 'N960CA' AND deregistration_id = 'N960CA-2018-02-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N960CA-2018-02-12/reports

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