# Service difficulty reports: N710CA, cancelled Jul 16, 2013

A list on [N710CA, cancelled Jul 16, 2013](https://openairdocs.org/deregistered/N710CA-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 · 94 reports

- [SDR COMA2010061550129](https://openairdocs.org/sdr/COMA2010061550129.md): Pseu · failed · Jun 14, 2010 · N710CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > EN ROUTE FROM MEM TO PIT RECEIVED GROUND PROX SYS CAUTION MSG. EMERGENCY DECLARED, A/C DIVERTED TO CVG LANDED SAFELY. REMOVED AND REPLACED PSEU. OPS CHECK GOOD.
- [SDR COMA2009081050177](https://openairdocs.org/sdr/COMA2009081050177.md): Warning System · activated · Aug 6, 2009 · N710CA · Cndair CL6002B19 · Engine Thrust Reverser
  > ON CLIMBOUT FROM LEX RECEIVED RT REV UNLOCK CAUTION MSG, REV DID NOT DEPLOY AND ATR DID NOT ENGAGE. EMERGENCY DECLARED, A/C RETURNED TO LEX LANDED SAFELY. TRANSFERRED TO DEFERRED LIST PER MEL 78-30-01.
- [SDR COMA2009052750143](https://openairdocs.org/sdr/COMA2009052750143.md): Sill · corroded · May 22, 2009 · N710CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SEVERE CORROSION WAS FOUND ON LEFT FLOOR SILL AFT OF PAX DOOR BETWEEN FS 349.00 AND FS 364.00. REMOVED AND SPLICED IN SERVICEABLE SECTION OF FLOOR SILL IAW EA 10-5320-02609 AND SR 99-5140-0001.
- [SDR COMA2009052750142](https://openairdocs.org/sdr/COMA2009052750142.md): Skin · corroded · May 22, 2009 · N710CA · Cndair CL6002B19 · Wing, Plate/Skin
  > LT WING FUEL ACCESS PANEL CUTOUT AT 540AB HAS FRETTING CORROSION AROUND EDGES. REMOVED CORROSION IN THE CRITICAL AREA AT FUEL ACCESS PANEL 540AB CUTOUT AND FOUND THAT MATERIAL REMOVED WAS WITHIN LIMITS PER REO 601R-57-21-030 REV G.
- [SDR COMA2009052750141](https://openairdocs.org/sdr/COMA2009052750141.md): Skin · corroded · May 22, 2009 · N710CA · Cndair CL6002B19 · Wing, Plate/Skin
  > LT WING FUEL ACCESS PANEL CUTOUT AT 540EB HAS FRETTING CORROSION AROUND EDGES. REMOVED CORROSION IN THE CRITAL AREA AT FUEL ACCESS PANEL 540EB CUTOUT AND FOUND THAT MATERIAL REMOVED WAS WITHIN LIMITS PER REO 601R-57-21-030 REV G.
- [SDR COMA2009052750140](https://openairdocs.org/sdr/COMA2009052750140.md): Skin · corroded · May 22, 2009 · N710CA · Cndair CL6002B19 · Wing, Plate/Skin
  > LT WING FUEL ACCESS PANEL CUTOUT AT 540FB HAS FRETTING CORROSION AROUND EDGES. REMOVED CORROSION IN THE CRITAL AREA AT FUEL ACCESS PANEL 540FB CUTOUT AND FOUND THAT MATERIAL REMOVED WAS WITHIN LIMITS PER REO 601R-57-21-030 REV G.
- [SDR COMA2009052750139](https://openairdocs.org/sdr/COMA2009052750139.md): Skin · corroded · May 22, 2009 · N710CA · Cndair CL6002B19 · Wing, Plate/Skin
  > LT WING FUEL ACCESS PANEL CUTOUT AT 550BB HAS FRETTING CORROSION AROUND EDGES. REMOVED CORROSION IN THE CRITICAL AREA AT FUEL ACCESS PANEL 550BB CUTOUT AND FOUND THAT MATERIAL REMOVED WAS WITHIN LIMITS PER REO 601R-57-21-030 REV G.
- [SDR COMA2009022450085](https://openairdocs.org/sdr/COMA2009022450085.md): Wire Harness · faulty · Feb 23, 2009 · N710CA · Cndair CL6002B19 · Door System Wiring
  > EN ROUTE FROM YYZ TO JFK RECEIVED PAX DOOR WARNING, CARGO DOOR AND SERVICE DOOR CAUTION MSG'S, WITH NO LOSS OF CABIN PRESSURE. A/C DIVERTED TO SYR LANDED SAFELY. FOUND PAX DOOR WIRE HARNESS TO BE FAULTY. REPLACED PAX DOOR WIRE HARNESS.
- [SDR COMA086359](https://openairdocs.org/sdr/COMA086359.md): Line · chafed · Aug 17, 2008 · N710CA · Cndair CL6002B19 · Hydraulic System, Main
  > EN ROUTE FROM JAX TO LGA RECEIVED HYD SYS NR 1 LOW PRESS CAUTION MSG. FOLLOWED QRH, HYD QTY SHOWED, PRESS DROPPED TO 0 PSI. ACFT DIVERTED TO RIC AND LANDED SAFELY. FOUND LT ENG EDP SUPPLY LINE CHAFED. REPAIRED EDP SUPPLY LINE IAW CRJ AMM TASK 20-22-00-910-
- [SDR COMA0860176](https://openairdocs.org/sdr/COMA0860176.md): Uplock · out of rig · Mar 14, 2008 · N710CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > FLIGHT 5653 - GEAR DISAGREE MESSAGE ON APPROACH INTO MCI. AIRCRAFT LANDED SAFELY. FOUND NLG UPLOCK PIN OUT OF RIG. PERFORMED RIGGING OF NLG UPLOCK PIN, OPS CHECK GOOD.
- [SDR COMA0760539](https://openairdocs.org/sdr/COMA0760539.md): Selector Valve · faulty · Aug 21, 2007 · N710CA · Cndair CL6002B19 · Landing Gear Selector
  > FLIGHT 5258 - DURING LANDING GEAR EXTENSION, RECEIVED GEAR DISAGREE MESSAGE. NOSE GEAR DID NOT COME DOWN. REPLACED NOSE GEAR SELECTOR VALVE. NO FURTHER DEFECTS.
- [SDR COMA0760531](https://openairdocs.org/sdr/COMA0760531.md): Priority Valve · faulty · Aug 16, 2007 · N710CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > FLIGHT 5376 - NOSE GEAR WOULD NOT EXTEND. CYCLED GEAR, ON SECOND ATTEMPT GEAR EXTENDED NORMALLY. LANDED WITHOUT INCIDENT. REPLACED MAIN AND NOSE LANDEING GEAR PRIORITY VALVES. NO FURTHER DEFECTS.
- [SDR COMA0760175](https://openairdocs.org/sdr/COMA0760175.md): Oxygen System · leaking · Feb 11, 2007 · N710CA · Cndair CL6002B19 · Crew Oxygen System
  > FLIGHT 4941- EN ROUTE YYZ-JFK DISCOVERED A CREW OXYGEN SUPPLY LEAK, FLIGHT DIVERTED TO AVP. SERVICED THE CREW OXYGEN SYSTEM.
- [SDR COMA0660323](https://openairdocs.org/sdr/COMA0660323.md): Skin Panel · cracked · May 2, 2006 · N710CA · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING LEADING EDGE HAS CRACK PROPAGATING FROM RIVET AT WS 199. REMOVED AND REPLACED LEFT WING CENTER LEADING EDGE IAW CRJ AMM 57-41-01-400-804. INSTALLED P/N 601R1204403 PER EA 10-5741-01196.
- [SDR COMA0560831](https://openairdocs.org/sdr/COMA0560831.md): Trim System · malfunctioned · Jan 27, 2006 · N710CA · Cndair CL6002B19 · Stabilizer Position Indicating
  > FLIGHT 5442 - DURING TAKEOFF ROLL, BOTH STAB TRIM AND MACH TRIM DISENGAGED, ABORTED TAKEOFF AND RETURNED TO GATE. PERFORMED AN OPERATIONAL CHECK OF THE HSTCU AND GROUND RUNS, DISCREPANCIES COULD NOT BE DUPLICATED.
- [SDR COMA0560745](https://openairdocs.org/sdr/COMA0560745.md): Priority Valve · faulty · Dec 22, 2005 · N710CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > FLIGHT 9644 - DURING FERRY FLIGHT 9644 CLE-MCO, RECEIVED A GEAR DISAGREE MESSAGE. FLIGHT DIVERTED TO CAK. REPLACED THE NLG PRIORITY VALVE.
- [SDR COMA0560741](https://openairdocs.org/sdr/COMA0560741.md): Priority Valve · unreliable · Dec 20, 2005 · N710CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > FLIGHT 5274 - GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE.
- [SDR COMA0560574](https://openairdocs.org/sdr/COMA0560574.md): Trim Switch · malfunctioned · Oct 27, 2005 · N710CA · Cndair CL6002B19 · Stabilizer Position Indicating
  > FLIGHT 5116 - STAB TRIM 1 AND 2 DISCONNECT AND MACH TRIM INOPERABLE. REPLACED THE CO-PILOT TRIM DISCONNECT SWITCH.
- [SDR COMA0560326](https://openairdocs.org/sdr/COMA0560326.md): Frame · cracked · Jun 1, 2005 · N710CA · Cndair CL6002B19 · Fuselage Main, Frame
  > LT 621.00 FRAME CRACKED. REPAIRED IAW REO 601R-53-61-117.
- [SDR COMA0560327](https://openairdocs.org/sdr/COMA0560327.md): Frame · cracked · Jun 1, 2005 · N710CA · Cndair CL6002B19 · Fuselage Main, Frame
  > LT FRAME CRACKED AT STR 10. REPAIRED IAW REO 601R-53-61-487.
- [SDR COMA0560328](https://openairdocs.org/sdr/COMA0560328.md): Door Frame · cracked · Jun 1, 2005 · N710CA · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR FRAME CRACKED AT FS 320 AND 338. REPAIRED IAW REO 601R-52-11-402.
- [SDR COMA0560332](https://openairdocs.org/sdr/COMA0560332.md): Frame · cracked · Jun 1, 2005 · N710CA · Cndair CL6002B19 · Fuselage Main, Frame
  > LT AND RT FS 718 FRAME CRACKED. REPAIRED IAW EO 53-027.
- [SDR COMA0560331](https://openairdocs.org/sdr/COMA0560331.md): Support Beam · cracked · Jun 1, 2005 · N710CA · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > CENTER ENGINE SUPPORT BEAM (LOWER WEB) CRACKED. REPAIRED IAW REO 601R-53-61-1353.
- [SDR COMA0560330](https://openairdocs.org/sdr/COMA0560330.md): Drag Angle · cracked · Jun 1, 2005 · N710CA · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > LT MLG DRAG ANGLE INBOARD OF BATTERY RIB CRACKED. REPAIRED IAW CRJ SRM 51-42-21.
- [SDR COMA0560329](https://openairdocs.org/sdr/COMA0560329.md): Rib · cracked · Jun 1, 2005 · N710CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > RT BATT RIB CRACKED. REPAIRED IAW REO 601R-57-51-046.
- [SDR COMA0560230](https://openairdocs.org/sdr/COMA0560230.md): Engine · out of tolerance · Apr 5, 2005 · N710CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > FLIGHT 5267 DURING CLIMBOUT OF CVG THE RIGHT ENGINE WOULD NOT ACHIEVE CHARTED RATED THRUST. AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT ENGINE ASSEMBLY.
- [SDR COMA0560148](https://openairdocs.org/sdr/COMA0560148.md): Wire Harness · faulty · Feb 28, 2005 · N710CA · Cndair CL6002B19 · Landing Gear System Wiring
  > FLIGHT 5153 AFTER TAKEOFF FROM CVG RECEIVED A GEAR UP DISAGREE MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. REPLACED THE NLG WIRING HARNESS ASSEMBLY.
- [SDR COMA0460446](https://openairdocs.org/sdr/COMA0460446.md): Sensor · malfunctioned · Aug 3, 2004 · N710CA · Cndair CL6002B19 · Engine Oil Quantity
  > FLIGHT 5492, RT ENGINE HIGH OIL TEMP. REPLACED THE OIL TEMP SENSOR.
- [SDR COMA0460347](https://openairdocs.org/sdr/COMA0460347.md): Reservoir · malfunctioned · Jun 2, 2004 · N710CA · Cndair CL6002B19 · Hydraulic Reservoir, Main
  > FLIGHT 5556 LANDING GEAR DISAGREE WARNING. REPLACED THE NR 3 SYSTEM HYDRAULIC RESERVOIR.
- [SDR COMA0460242](https://openairdocs.org/sdr/COMA0460242.md): Receiver · malfunctioned · Apr 1, 2004 · N710CA · Cndair CL6002B19 · Glide Slope System
  > FLIGHT 5837 COPILOTS GLIDESLOPE FLAG ON APPROACH. REPLACED THE NR 2 NAV RECEIVER.
- [SDR COMA0360490](https://openairdocs.org/sdr/COMA0360490.md): Flap · malfunctioned · Nov 8, 2003 · N710CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5144 FLAPS FAIL WARNING MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
- [SDR COMA0360428](https://openairdocs.org/sdr/COMA0360428.md): Light · defective · Sep 24, 2003 · N710CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5601 DURING INSPECTION FOUND THE FLOOR EMERGENCY LIGHTING INOPERATIVE AT ROWS 8 THROUGH 13. REPLACED SECTION OF THE FLOOR EMERGENCY LIGHTING STRIP.
- [SDR COMA0360257](https://openairdocs.org/sdr/COMA0360257.md): Pump · failed · May 30, 2003 · N710CA · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main
  > FLIGHT 5830 GEAR DISAGREE WARNING DURING GEAR EXTENSION AND RETRACTION. REPLACED HYDRAULIC PUMP 3B.
- [SDR COMA0360174](https://openairdocs.org/sdr/COMA0360174.md): Control Panel · malfunctioned · Mar 30, 2003 · N710CA · Cndair CL6002B19 · Extinguishing System
  > FLIGHT 5843 CARGO FIRE BOTTLE "LOW" CAUTION MESSAGE. REPLACED THE FIRE PANEL.
- [SDR COMA0360173](https://openairdocs.org/sdr/COMA0360173.md): Fire Bottle · discharged · Mar 30, 2003 · N710CA · Cndair CL6002B19 · Fire Bottle, Fixed
  > FLGIHT 5198 - CARGO FIRE BOTTLE "LOW" CAUTION MESSAGE. REPLACED THE CARGO FIRE BOTTLES
- [SDR COMA0360172](https://openairdocs.org/sdr/COMA0360172.md): Bottle · discharged · Mar 30, 2003 · N710CA · Cndair CL6002B19 · Fire Bottle, Fixed
  > FLIGHT 5198 CARGO FIRE BOTTLE "LOW" CAUTION MESSAGE. REPLACED THE CARGO FIRE BOTTLES.
- [SDR COMA0360047](https://openairdocs.org/sdr/COMA0360047.md): Fire Bottle · Jan 23, 2003 · N710CA · Cndair CL6002B19 · Extinguishing System
  > FLIGHT 5292 CARGO FIRE BOTTLE LOW MESSAGE.COULD NOT DUPLICATE. INPSECTED BOTTLE AND WIRING - NO DEFECTS.
- [SDR COMA0260681](https://openairdocs.org/sdr/COMA0260681.md): Pdu · malfunctioned · Nov 30, 2002 · N710CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5238 FLAPS FAILED AT 8 DEGREES.REPLACED THE PDU.
- [SDR COMA0260677](https://openairdocs.org/sdr/COMA0260677.md): Flap · Nov 27, 2002 · N710CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 6009 FLAPS FAILED AT ZERO DEGREES.COULD NOT DUPLICATE. C/W EO 27-045 AND 27-046. NO DEFECTS FOUND.
- [SDR COMA0260670](https://openairdocs.org/sdr/COMA0260670.md): Flap · Nov 26, 2002 · N710CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5371 FLAPS FAILED AT 0 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01.
- [SDR COMA0260603](https://openairdocs.org/sdr/COMA0260603.md): Door · Oct 22, 2002 · N710CA · Cndair CL6002B19 · Service Doors
  > FLIGHT 5670 LOUD SQUEAL AND VIBRATION IN FLIGHT.FOUND AIRCRAFT EXTERNAL SERVICE PANEL OPEN. INPSPECTED FOR DAMAGE AND SECURED DOOR.
- [SDR COMA0260422](https://openairdocs.org/sdr/COMA0260422.md): Check Valve · worn · Jul 10, 2002 · N710CA · Cndair CL6002B19 · Engine Oil Indicating System
  > FLIGHT 5703 R/H ENGINE OIL TEMP INDICATED 165 DEGREES C DURING CLIMBFOUND ENGINE OIL OVER SERVICED - DRAINED EXCESS OIL AND REPLACED LUBE PUMP OIL FILTER CHECK VALVE.
- [SDR COMA0260235](https://openairdocs.org/sdr/COMA0260235.md): Bpsu · malfunctioned · Apr 5, 2002 · N710CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5297 FLAPS FAILED AT 0 DEGREES.REPLACED THE R/H BPSU.
- [SDR COMA0260205](https://openairdocs.org/sdr/COMA0260205.md): Control Unit · malfunctioned · Mar 20, 2002 · N710CA · Cndair CL6002B19 · Pneumatic Indicating System
  > FLIGHT 5279 R/H 14TH STAGE BLEED AIR DUCT WARNING IFSD.REPLACED THE BLEED AIR CONTROL UNIT.
- [SDR COMA0260017](https://openairdocs.org/sdr/COMA0260017.md): Computer · Dec 27, 2001 · N710CA · Cndair CL6002B19 · Central Warning
  > FLIGHT 5371 T/O CONFIG OK MESSAGE WENT OUT DURING T/O.COULD NOT DUPLICATE, ALL T/O CONFIG MESSAGE NORMAL DURING TEST.
- [SDR COMA0160885](https://openairdocs.org/sdr/COMA0160885.md): Web · cracked · Nov 10, 2001 · N710CA · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > THE ENGINE SUPPORT BEAM LOWER WEB WAS CRACKED AT L/H AND R/H SIDES.REMOVED THE CRACKED PORTIONS OF THE LOWER WEB AND PERFORMED A MAJOR REPAIR I/A/W REO 601R-53-61-366 REV D.
- [SDR COMA0160882](https://openairdocs.org/sdr/COMA0160882.md): Frame · cracked · Nov 9, 2001 · N710CA · Cndair CL6002B19 · Fuselage Main, Frame
  > DISC CRACKED FRAME FLANGE @F.S.718 R/H SIDE.CORRECTIVE ACTION; CUT OUT DAMAGED FRAME, FABRICATED AND INSTALLED REPAIR SECTION MADE FROM P/N 600-36030-24. ALL WORK PERFORMED I/A/W WVAC EO 601R-53-2828, CANADAIR CRJ REO 601R-53-61-193 AND CRJ SRM REF LOG PAGE
- [SDR COMA0160657](https://openairdocs.org/sdr/COMA0160657.md): Door · Aug 29, 2001 · N710CA · Cndair CL6002B19 · Flight Compartment Equipment
  > FLIGHT #5967. DURING TAXI OUT DISCOVERED THAT THE COCKPIT DOOR WOULD NOT LATCH, AIRCRAFT RETURNED TO THE GATE.REPLACED THE COCKPIT DOOR ASSEMBLY.
- [SDR COMA0160463](https://openairdocs.org/sdr/COMA0160463.md): Fcu · failed · Jul 11, 2001 · N710CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > AFTER T/O FROM CVG FLAP FAULT CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIELD.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "SECOND EVENT" MAINTENANCE ACTION, PARAGRAPH (B)3(D AND E)4. REPLACED THE FLAP ELECTRONIC CONTROL UNIT.
- [SDR COMA0160466](https://openairdocs.org/sdr/COMA0160466.md): Bpsu · failed · Jul 11, 2001 · N710CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAIL CAUTION FLIGHT TEST OF FLAP SYSTEM, AIRCRAFT RETURNED TO CVG AND LANDED SAFETY.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "SECOND EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 3 AND (D AND E) 4. REPLACED THE RIGHT BRAKE POSITIONING SENSING UNIT.

Next page: https://openairdocs.org/deregistered/N710CA-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 = 'N710CA' AND deregistration_id = 'N710CA-2013-07-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N710CA-2013-07-16/reports

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