# Service difficulty reports: N965CA, cancelled Apr 15, 2014

A list on [N965CA, cancelled Apr 15, 2014](https://openairdocs.org/deregistered/N965CA-2014-04-15.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 3 · 119 reports

- [SDR COMA2011080850051](https://openairdocs.org/sdr/COMA2011080850051.md): Selector Valve · failed · Aug 6, 2011 · N965CA · Cndair CL6002B19 · Landing Gear Selector
  > ON APPROACH INTO DTW RECEIVED GEAR DISAGREE AFTER SELECTING GEAR DOWN, BOTH MLG FAILED TO EXTEND. EMERGENCY DECLARED, QRH FOLLOWED, A/C LANDED SAFELY AT DTW. REMOVED AND REPLACED MLG SELECTOR VALVE. OPS CHECK GOOD.
- [SDR COMA2010092850209](https://openairdocs.org/sdr/COMA2010092850209.md): Vane · chafed · Sep 27, 2010 · N965CA · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT I/B FLAP VANE LEADING EDGE FOUND TO HAVE CHAFE DAMAGE. REPLACED THE RIGHT I/B FLAP VANE LEADING EDGE IAW CRJ 200 SRM.
- [SDR COMA2010092850208](https://openairdocs.org/sdr/COMA2010092850208.md): Bulkhead · cracked · Sep 27, 2010 · N965CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 559.0 BULKHEAD WEB FOUND TO BE CRACKED. REPAIRED IAW REO 601R-53-41-260 AND DEVIATION REO 601R-53-41-609.
- [SDR COMA2010091650202](https://openairdocs.org/sdr/COMA2010091650202.md): Crossbeam · corroded · Sep 15, 2010 · N965CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 FLOOR SUPPORT CROSSBEAM AT LBL 9 TO RBL 9 IS CORRODED. REPAIRED CROSSBEAM PER SRM 51-42-06.
- [SDR COMA2010091650201](https://openairdocs.org/sdr/COMA2010091650201.md): Bulkhead · corroded · Sep 15, 2010 · N965CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 280 BULKHEAD WEB AT LBL 11 TO LBL 13 IS CORRODED. REPAIRED BULKHEAD WEB AT FS 280 PER SRM 53-11-19.
- [SDR COMA086355](https://openairdocs.org/sdr/COMA086355.md): Skin · damaged · Aug 9, 2008 · N965CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > PASSENGER DOOR CUTOUT AIRFRAME SIDE FWD LOWER CORNER EXISTING REPAIR IS DAMAGED. REPAIRED PASSENGER DOOR CUTOUT AIRFRAME SIDE LOWER FWD CORNER PER CRJ REO 601R-53-21-180 REV (A) AND SR99-5140-0001 SECTION 1. (S)
- [SDR COMA086354](https://openairdocs.org/sdr/COMA086354.md): Floor Skin · cracked · Aug 9, 2008 · N965CA · Cndair CL6002B19 · Fuselage Floor Panel
  > PRESSURE FLOOR SKIN AT STA 460 BETWEEN LBL 9 AND RBL 9 IS CRACKED. REPAIRED PRESSURE FLOOR SKIN WEB AT FS 460.00 WITH TEMPORARY REPAIR PER REO 601R-53-41-103 REV D. (S)
- [SDR COMA086353](https://openairdocs.org/sdr/COMA086353.md): Support Beam · cracked · Aug 9, 2008 · N965CA · Cndair CL6002B19 · Engine Mount Section
  > RT UPPER WEB-ENG SUPPORT BEAM ASSEMBLY CRACKED. COMPLIED WITH REPAIR TO UPPER WEB-ENG SUPPORT. BEAM ASSEMBLY BETWEEN BL 27.5 AND 36.2 PER REO601R-53-61-569. (S)
- [SDR COMA086352](https://openairdocs.org/sdr/COMA086352.md): Support Beam · cracked · Aug 9, 2008 · N965CA · Cndair CL6002B19 · Engine Mount Section
  > LT UPPER WEB-ENG SUPPORT BEAM ASSEMBLY CRACKED. COMPLIED WITH REPAIR TO UPPER WEB-ENG SUPPORT. BEAM ASSEMBLY BETWEEN BL27.5 AND 36.2 PER REO601R-53-51-569. (S)
- [SDR COMA086351](https://openairdocs.org/sdr/COMA086351.md): Doubler · cracked · Aug 9, 2008 · N965CA · Cndair CL6002B19 · Fuselage Main, Frame
  > RT SIDE FUSELAGE FRAME DOUBLER AT FS 640.00 IS CRACKED. COMPLIED WITH MODIFICATION K601R360094 AT FS 640 IAW S/B 601R-53-061. (S)
- [SDR COMA086350](https://openairdocs.org/sdr/COMA086350.md): Frame · cracked · Aug 9, 2008 · N965CA · Cndair CL6002B19 · Fuselage Main, Frame
  > LT SIDE FUSELAGE FRAME DOUBLER AT FS 640.00 IS CRACKED. COMPLIED WITH MODIFICATION K601R36009-R AT FS 640 IAW S/B 601R-53-061. (S)
- [SDR COMA086349](https://openairdocs.org/sdr/COMA086349.md): Doubler · cracked · Aug 9, 2008 · N965CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > RT INTERNAL SKIN DOUBLER AT STA 640 IS CRACKED. FABRICATED PARTS AT STA 640 IAW CRJ REO 601R-53-61-506. (S)
- [SDR COMA086348](https://openairdocs.org/sdr/COMA086348.md): Doubler · cracked · Aug 9, 2008 · N965CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LT INTERNAL SKIN DOUBLER AT STA 640 IS CRACKED. FABRICATED PARTS AT STA 640 IAW CRJ REO 601R-53-61-506. (S)
- [SDR COMA0860321](https://openairdocs.org/sdr/COMA0860321.md): Lamp · burned out · Jul 13, 2008 · N965CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 9422. DURING LINE CHECK FOUND ROW 2-5 EMERGENCY FLOOR LIGHTS INOP. REMOVED AND REPLACED FLOOR EMERGENCY LIGHT STRIP. (A)
- [SDR COMA0860234](https://openairdocs.org/sdr/COMA0860234.md): Inverter · inoperative · Apr 30, 2008 · N965CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5326 - EMERGENCY LIGHTS NOT WORKING FROM ROW 9 AFT. REPLACED NR 4 INVERTER. NO FURTHER DEFECTS.
- [SDR COMA0860213](https://openairdocs.org/sdr/COMA0860213.md): Light · no test · Apr 6, 2008 · N965CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5027 - THE AFT EMERGENCY EXIT FLOOR LIGHTS FAILED TO TEST. DEFERRED PER MEL 33-51-01-6.
- [SDR COMA0860185](https://openairdocs.org/sdr/COMA0860185.md): Relief Valve · faulty · Mar 20, 2008 · N965CA · Cndair CL6002B19 · Air Intake Anti/De-Ice System
  > FLIGHT 5103- RECEIVED RIGHT COWL ANTI-ICE MESSAGE WHEN ANTI-ICE SELECTED ON. RETURNED TO JFK, LANDED WITHOUT INCIDENT. REPLACED PRESSURE RELIEF VALVE. NO FURTHER DEFECTS.
- [SDR COMA0860157](https://openairdocs.org/sdr/COMA0860157.md): Battery Pack · discharged · Mar 4, 2008 · N965CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5479 - FLOOR MOUNTED EMERGENCY STRIP BEHIND ROW 8A IS INOP. REPLACED BATTERY PACK NR 4. NO FURTHER DEFECTS.
- [SDR COMA0760489](https://openairdocs.org/sdr/COMA0760489.md): Bulkhead · cracked · Jul 16, 2007 · N965CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD CRACKED AROUND LINTEL FITTING. PERFORMED PERMANENT REPAIR TO AFT PRESSURE BULKHEAD IAW REO 601R-53-11-563.
- [SDR COMA0760488](https://openairdocs.org/sdr/COMA0760488.md): Bulkhead · cracked · Jul 16, 2007 · N965CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FORWARD PRESSURE BULKHEAD CRACKED AT PARKING BRAKE CABLE. REPAIRED IAW REO 601R-53-11-563.
- [SDR COMA0670390](https://openairdocs.org/sdr/COMA0670390.md): Engine · overtemp · May 21, 2007 · N965CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > FLIGHT 4988 - DURING TAKEOFF ROLL THE RIGHT ENGINE ITT INDICATED 905C, ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED THE RIGHT ENGINE ASSEMBLY.
- [SDR COMA0760386](https://openairdocs.org/sdr/COMA0760386.md): Pump · malfunctioned · May 20, 2007 · N965CA · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main
  > FLIGHT 5389 - HYD PUMP 1B CIRCUIT BREAKER POPPED WHILE STARTING NR 1 ENGINE. RETURNED TO GATE. RESET BREAKER, PERFORMED OPS CHECK, NO FURTHER DEFECTS.
- [SDR COMA0760359](https://openairdocs.org/sdr/COMA0760359.md): Bulkhead · cracked · May 3, 2007 · N965CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING FS 559 INSPECTION FOUND SEMI-BULKHEAD CRACKED AT RBL 18. STOP DRILLED CRACK AND INSTALLED DOUBLER IAW REO 601R-53-41-353.
- [SDR COMA076027](https://openairdocs.org/sdr/COMA076027.md): Wire · faulty · Jan 14, 2007 · N965CA · Cndair CL6002B19 · Ice/Rain Protection System Wiring
  > FLIGHT 5342 - RECEIVED ANTI-ICE DUCT WARNING MESSAGE IN FLIGHT. FOLLOWED QRH AND DIVERTED TO GSO. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THERMAL SWITCH WIRE AT LEFT WING STATION 250. NO FURTHER DEFECTS.
- [SDR COMA0660734](https://openairdocs.org/sdr/COMA0660734.md): Actuator · failed · Dec 27, 2006 · N965CA · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLIGHT 5206 - RECEIVED A FLAP FAIL CAUTION MESSAGE DURING BGR APPROACH AT 30 DEGREE FLAP SETTING. REPLACED THE LEFT OUTBOARD FLAP INBOARD ACTUATOR.
- [SDR COMA0660733](https://openairdocs.org/sdr/COMA0660733.md): Actuator · failed · Dec 27, 2006 · N965CA · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLIGHT 5206 - RECEIVED A FLAP FAIL CAUTION MESSAGE DURING BGR APPROACH AT 30 DEGREE FLAP SETTING. REPLACED THE LEFT INBOARD FLAP INBOARD ACTUATOR.
- [SDR COMA0660732](https://openairdocs.org/sdr/COMA0660732.md): Flap · malfunctioned · Dec 27, 2006 · N965CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5206 - RECEIVED A FLAP FAIL CAUTION MESSAGE DURING BGR APPROACH AT 30 DEGREE FLAP SETTING. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP
- [SDR COMA0660720](https://openairdocs.org/sdr/COMA0660720.md): Wire Harness · chafed · Dec 21, 2006 · N965CA · Cndair CL6002B19 · Ice/Rain Protection System Wiring
  > FLIGHT 5323 - DURING CLIMBOUT RECEIVED AN ANTI-ICE DUCT CAUTION MESSAGE, FLIGHT RETURNED TO CVG. REPAIRED CHAFED WIRING ON THE LEFT WING LEADING EDGE AT STA 330.25 AND 377.40.
- [SDR COMA0660512](https://openairdocs.org/sdr/COMA0660512.md): Support Beam · cracked · Aug 25, 2006 · N965CA · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > DURING INSPECTION OF THE ENGINE SUPPORT BEAM IAW EO 53-021 (AD 2004-10-03) FOUND CRACK AT LOCATION FS 640, LBL 9.0, WL 119.12 (UPPER BOX BEAM SKIN).PERFORMED REPAIR IAW REO 601R-53-61-345.
- [SDR COMA0660383](https://openairdocs.org/sdr/COMA0660383.md): Pressure Valve · malfunctioned · Jun 8, 2006 · N965CA · Cndair CL6002B19 · Passenger/Crew Doors
  > FLIGHT 5063 - DURING CLIMBOUT OF GSO RECEIVED A CABIN DOOR OUTER HANDLE CAUTION MESSAGE, FLIGHT RETURNED TO THE FIELD. RE-RIGGED THE CABIN DOOR PRESSURE VALVE VENT FLAP.
- [SDR COMA0660381](https://openairdocs.org/sdr/COMA0660381.md): Warning System · malfunctioned · Jun 6, 2006 · N965CA · Cndair CL6002B19 · Door Warning System
  > FLIGHT 5063 - AFTER TAKEOFF FROM GSO RECEIVED A CABIN DOOR OUTER HANDLE CAUTION MESSAGE, FLIGHT RETURNED TO THE FIELD. DEFERRED THE CABIN DOOR INDICATION PER MEL 52-70-01-1.
- [SDR COMA0660351](https://openairdocs.org/sdr/COMA0660351.md): Ecu · faulty · May 18, 2006 · N965CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5285 - RECEIVED A FLAP FAIL CAUTION MESSAGE AT ZERO DEGREES DURING TAXI AT DCA. REPLACED THE FLAP ELECTRONIC CONTROL UNIT.
- [SDR COMA0660348](https://openairdocs.org/sdr/COMA0660348.md): Caution Message · false activation · May 15, 2006 · N965CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5719 - FLAP FAIL MESSAGE AT GATE. 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 FURTHER FLAP CAUTION MESSAGES.
- [SDR COMA0660322](https://openairdocs.org/sdr/COMA0660322.md): Flap System · out of rig · May 1, 2006 · N965CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5450 - FLAP FAIL CAUTION MESSAGE. FLAPS WILL NOT COME OUT OF ZERO POSITION. FOUND LEFT SIDE FLAP SYSTEM OUT OF RIG. MECHANICALLY AND ELECTRICALLY RIGGED LEFT SIDE FLAP SYSTEM.
- [SDR COMA0660317](https://openairdocs.org/sdr/COMA0660317.md): Flap System · malfunctioned · Apr 28, 2006 · N965CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5049 - FLAP FAIL MESSAGE ON GROUND AT 0 DEGREES. 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 FURTHER FLAP CAUTION MESSAGES.
- [SDR COMA0660310](https://openairdocs.org/sdr/COMA0660310.md): Flap System · malfunctioned · Apr 22, 2006 · N965CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5381 - DURING PUSHBACK RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREES, FLIGHT RETURNED TO THE GATE. 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 N
- [SDR COMA0660223](https://openairdocs.org/sdr/COMA0660223.md): Latch · damaged · Mar 2, 2006 · N965CA · Cndair CL6002B19 · Passenger/Crew Doors
  > FLIGHT 5701 - EN ROUTE BTV-ATL RECEIVED A CABIN DOOR LATCH CAUTION MESSAGE, FLIGHT DIVERTED TO SYR. ADJUSTED ROD-END OF CABIN DOOR LATCH ROLLER ASSEMBLY.
- [SDR COMA0660118](https://openairdocs.org/sdr/COMA0660118.md): Pressure Switch · faulty · Feb 7, 2006 · N965CA · Cndair CL6002B19 · Ice Detection
  > FLIGHT 5093 - DURING CLIMB-OUT OF EVV RECEIVED A LEFT ENGINE COWL A/ICE CAUTION MESSAGE, FLIGHT RETURNED TO EVV. REPLACED THE LEFT ENGINE COWL ANTI ICE PRESSURE SWITCH.
- [SDR COMA0560815](https://openairdocs.org/sdr/COMA0560815.md): Windshield · cracked · Jan 17, 2006 · N965CA · Cndair CL6002B19 · Flight Compartment Windows
  > FLIGHT 5701- PILOT'S WINDSHIELD SHATTERED. REPLACED WINDSHIELD.
- [SDR COMA0560652](https://openairdocs.org/sdr/COMA0560652.md): Flap System · malfunctioned · Nov 27, 2005 · N965CA · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLIGHT 5850 - RECEIVED A FLAP FAIL CAUTION MESSAGE AFTER LANDING WHEN FLAPS WERE SELECTED TO 20 DEGREES. 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 FURTHER
- [SDR COMA0560490](https://openairdocs.org/sdr/COMA0560490.md): Light · inoperative · Sep 6, 2005 · N965CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5565 - EMERGENCY FLOOR LIGHTING INOPERATIVE FROM ROWS 2 THROUGH 5. CLEANED CONTACTORS ON EMERGENCY FLOOR TRACK LIGHT STRIP.
- [SDR COMA0560484](https://openairdocs.org/sdr/COMA0560484.md): Lamp · inoperative · Sep 2, 2005 · N965CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5387 - EMERGENCY LIGHTS ROW 1-5 INOPERABLE. RESECURED LIGHT STRIP.
- [SDR COMA0560458](https://openairdocs.org/sdr/COMA0560458.md): Bpsu · out of rig · Aug 21, 2005 · N965CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5858 - FLAPS FAIL CAUTION. ADJUSTED THE RIGGING OF THE RT BPSU.
- [SDR COMA0560435](https://openairdocs.org/sdr/COMA0560435.md): Element · malfunctioned · Aug 8, 2005 · N965CA · Cndair CL6002B19 · Detection System
  > FLIGHT 5105 - LT 14TH STAGE DUCT WARNING. REPLACED THE PYLON DUCT LEAK SENSING ELEMENT.
- [SDR COMA0460603](https://openairdocs.org/sdr/COMA0460603.md): Bulkhead · corroded · Sep 16, 2004 · N965CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 280 HAS CORROSION ON WEB AT CBP WALLS. REPAIRED IAW REO 601R-53-11-584.
- [SDR COMA0460519](https://openairdocs.org/sdr/COMA0460519.md): Skin · corroded · Sep 16, 2004 · N965CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FS 574 LEFT HAND SIDE HAS TWO CORRODED FASTENERS AT 8 POSITION ABOVE FLOOR. REPAIRED IAW REO 601R-53-61-1135.
- [SDR COMA0460522](https://openairdocs.org/sdr/COMA0460522.md): Floorbeam · cracked · Sep 16, 2004 · N965CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CARGO FLOOR CAP CRACKED. IAW SRM 51-42-06, 51-42-13, 51-42-21 AND 51-42-26.
- [SDR COMA0460521](https://openairdocs.org/sdr/COMA0460521.md): Web · cracked · Sep 16, 2004 · N965CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO CAP WEB AT LIGHTING HOLE IB SIDE CRACKED FROM EXCESSIVE STRESS.IAW SRM 51-42-06, 51-42-13.
- [SDR COMA0460520](https://openairdocs.org/sdr/COMA0460520.md): Skin · cracked · Sep 16, 2004 · N965CA · Cndair CL6002B19 · Wing, Plate/Skin
  > RT WING PLANK AT VS 148 IS CRACKED. IAW EO 57-020.
- [SDR COMA0460518](https://openairdocs.org/sdr/COMA0460518.md): Bulkhead · corroded · Sep 16, 2004 · N965CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 280 HAS CORROSION ON WEB AT BL AFT SIDE AND CRACKS LOCATED OUTBOARD OF LBL/RBL 9. REPAIRED IAW REO 601R-53-11-136.

Next page: https://openairdocs.org/deregistered/N965CA-2014-04-15/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 = 'N965CA' AND deregistration_id = 'N965CA-2014-04-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N965CA-2014-04-15/reports

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