# Service difficulty reports: N797CA, cancelled Dec 3, 2022

A list on [N797CA, cancelled Dec 3, 2022](https://openairdocs.org/deregistered/N797CA-2022-12-03.md).

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

- [SDR COMA2011032250030](https://openairdocs.org/sdr/COMA2011032250030.md): Sill · corroded · Mar 22, 2011 · N797CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL IS CORRODED. REPLACED DISCREPANT SILL ANGLE (7075-T6 0.063) AND PART NUMBER 601R38338-2 IAW BOMBARDIER SRM 51-42-13, SRM 51-42-21 AND AMM 20-21-00 PRIMED AND PAINTED IAW SRM 51-25-06 AND SRM 51-25-16, APPLIED AV-8 IAW SRM 51-21-11.
- [SDR COMA2011031650026](https://openairdocs.org/sdr/COMA2011031650026.md): Angle · cracked · Mar 16, 2011 · N797CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 559.00 RT CAP ANGLE CRACKED AT RBL 18.00. REMOVE AND REPLACED DAMAGED AREA OF WEB AND CAP ANGLE AT FS 559.00 RT SIDE IAW COMAIR TASK CARD REO 601R-53-41-260 RT REP, ALSO PERFORMED REO 601R-53-41-609 AROUND SFAR AREA OF WEB.
- [SDR COMA2011031650025](https://openairdocs.org/sdr/COMA2011031650025.md): Angle · cracked · Mar 16, 2011 · N797CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 559 LT CAP ANGLE CRACKED AT RBL 18.00 AND 9.00. REMOVED LT CAP ANGLE AND INSTALLED NEW CAP ANGLE AS PER TASK CARD REO 601R-53-41-260.
- [SDR COMA2011031150024](https://openairdocs.org/sdr/COMA2011031150024.md): Bulkhead · cracked · Mar 11, 2011 · N797CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BULKHEAD WEB CRACKED AROUND LINTEL ATTACH FITTING, TWO PLACES, AT FS 621, LBL 36.2. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1230, REV D.
- [SDR COMA2011031150023](https://openairdocs.org/sdr/COMA2011031150023.md): Angle · cracked · Mar 11, 2011 · N797CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 559 CAP ANGLE CRACKED AT LBL 18. CUT OUT DAMAGED AREA AND INSTALLED NEW CAP ANGLE SECTION IAW REO 601R-53-41-260 LT REP.
- [SDR COMA2010030450053](https://openairdocs.org/sdr/COMA2010030450053.md): Bulkhead · cracked · Mar 4, 2010 · N797CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FORWARD PRESSURE BULKHEAD AT FS 202.75 CRACKED AT CUTOUT FOR PARKING BRAKE CABLE. REPAIRED FWD PRESSURE BULKHEAD AT FS 202.75 IAW REO 601R-53-11-563 AND EA 10-5311-02890.
- [SDR COMA2009012650069](https://openairdocs.org/sdr/COMA2009012650069.md): Door · open · Jan 23, 2009 · N797CA · Cndair CL6002B19 · Accessory Compartment Doors
  > AFTER DEPARTURE FROM LGA LOUD NOISE IN FRONT RIGHT SIDE OF A/C. A/C RETURNED TO LGA, LANDED SAFELY. INSPECTED A/C FOUND COMMUNICATION DOOR LEFT OPEN. INSPECTED DOOR, NO DAMAGE NOTED, SECURED DOOR CLOSED.
- [SDR COMA0860209](https://openairdocs.org/sdr/COMA0860209.md): Sensor · malfunctioned · Apr 4, 2008 · N797CA · Cndair CL6002B19 · Windshield/Door Rain/Ice Removal
  > FLIGHT 5129 - EN ROUTE BUF-CVG RECEIVED A RIGHT WINDSHIELD HEAT CAUTION, FLIGHT RETURNED TO BUF. SWAPPED THE SPARE TEMPERATURE SENSOR ON THE RIGHT WINDSHIELD TO THE SPARE TERMINALS.
- [SDR COMA0860136](https://openairdocs.org/sdr/COMA0860136.md): Selector Valve · failed · Feb 17, 2008 · N797CA · Cndair CL6002B19 · Landing Gear Selector
  > FLIGHT 5386 - LANDING GEAR DISAGREE MESSAGE WHEN SELECTING GEAR DOWN. NOSE GEAR DOWN AND LOCKED MAINS REMAINED UP AND LOCKED. FOLLOWED QRH, PERFORMED MANUAL EXTENSION. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED MAIN LANDING GEAR SELEC
- [SDR COMA0860102](https://openairdocs.org/sdr/COMA0860102.md): Window · cracked · Jan 29, 2008 · N797CA · Cndair CL6002B19 · Flight Compartment Windows
  > FLIGHT 5104 - COCKPIT LEFT SIDE WINDOW CRACKED AT CRUISE. RECEIVED WINDOW HEAT CAUTION MESSAGES. DECLARED EMERGENCY, DIVERTED TO ACY, LANDED WITHOUT INCIDENT. REPLACED COCKPIT LEFT SIDE WINDOW. NO FURTHER DEFECTS.
- [SDR COMA0760302](https://openairdocs.org/sdr/COMA0760302.md): J-Box · loose · Apr 5, 2007 · N797CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE ON T/O, A/C RETURNED BACK TO CVG AND LANDED SAFELY. INSPECTED AND FOUND JB11 LOOSE IN IT'S RACK, RESECURED JB11.
- [SDR COMA0760260](https://openairdocs.org/sdr/COMA0760260.md): Crossbeam · corroded · Mar 15, 2007 · N797CA · Cndair CL6002B19 · Fuselage Main, Structure
  > FS 280 CROSSBEAM CORRODED. REPAIRED CROSSBEAM IAW REO 601R-53-21-069.
- [SDR COMA0760081](https://openairdocs.org/sdr/COMA0760081.md): Shaft · damaged · Jan 27, 2007 · N797CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5421 - FLAP FAIL MESSAGE AT 8 DEGREES. REPLACED NR 1 FLEX DRIVE, LEFT SIDE.
- [SDR COMA0660728](https://openairdocs.org/sdr/COMA0660728.md): Sensing Element · faulty · Dec 22, 2006 · N797CA · Cndair CL6002B19 · Pneumatic Indicating System
  > FLIGHT 5007- EN ROUTE CVG-GSO RECEIVED A LEFT 14TH STAGE DUCT MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT RETURNED TO CVG. REPLACED TEMPERATURE SENSING ELEMENT.
- [SDR COMA0660675](https://openairdocs.org/sdr/COMA0660675.md): Brake Cable · lack of lube · Dec 2, 2006 · N797CA · Cndair CL6002B19 · Landing Gear Brake System
  > FLIGHT 5168 - TAKEOFF ABORTED AT 60 KTS FOR TAKEOFF CONFIG WARNING. TAKEOFF CONFIG OK MESSAGE WAS ON UNTIL TAKEOFF THRUST WAS SET. MAX BTMS WAS 6. ABORTED TAKEOFF WITHOUT INCIDENT. NO FAULTS ON PSEU. CLEANED, LUBRICATED PARKING BRAKE CABLE. SET AND RELEA
- [SDR COMA0660674](https://openairdocs.org/sdr/COMA0660674.md): Brake Cable · out of adjust · Dec 2, 2006 · N797CA · Cndair CL6002B19 · Landing Gear Brake System
  > FLIGHT 5348 - CONFIG BRAKE WARNING MESSAGE WITH THRUST PUSHED UP FOR TAKEOFF. TAKEOFF CONFIG OK ADVISORY APPEARS INTERMITTENTLY. ABORTED TAKEOFF WITHOUT INCIDENT. ADJUSTED PARKING BRAKE CABLE. NO FURTHER DEFECTS NOTED.
- [SDR COMA0660667](https://openairdocs.org/sdr/COMA0660667.md): Control Unit · faulty · Nov 29, 2006 · N797CA · Cndair CL6002B19 · Brake Anti-Skid Section
  > FLIGHT 5002 - ON APPROACH RECEIVED ANTI-SKID INBD AND OUTBD WARNING MESSAGES. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED ASCU, NO FURTHER DEFECTS.
- [SDR COMA0660638](https://openairdocs.org/sdr/COMA0660638.md): Dcu · faulty · Nov 16, 2006 · N797CA · Cndair CL6002B19 · Automatic Data
  > FLIGHT 5195 - EN ROUTE JFK-IAD FLIGHT RETURNED TO JFK DUE TO FLAP INDICATION AND TENDENCY TO ROLL RIGHT. REPLACED THE NR 2 DATA CONCENTRATOR UNIT.
- [SDR COMA0660532](https://openairdocs.org/sdr/COMA0660532.md): Beam · cracked · Sep 7, 2006 · N797CA · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > WHILE PERFORMING EO 57-021 FOUND THE ENGINE BOX BEAM CRACKED ON TIP SKIN. PERFORMED REO 601R-53-61-345/346.
- [SDR COMA0660302](https://openairdocs.org/sdr/COMA0660302.md): Flap System · malfunctioned · Apr 12, 2006 · N797CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5603 - DURING TAXI RECEIVED A FLAP FAIL CAUTION MESSAGE AT 27 DEGREES, AIRCRAFT 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 COMA0660131](https://openairdocs.org/sdr/COMA0660131.md): Flap System · malfunctioned · Feb 9, 2006 · N797CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5000 - DURING YUL APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT ZERO 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 CAUTIO
- [SDR COMA0560663](https://openairdocs.org/sdr/COMA0560663.md): Check Valve · malfunctioned · Dec 1, 2005 · N797CA · Cndair CL6002B19 · Cabin Cooling System
  > FLIGHT 5153 - RIGHT AC PACK HIGH TEMP AND SMOKE TOILET WARNING WITH VISIBLE SMOKE. REPLACED THE FAN BYPASS CHECK VALVE.
- [SDR COMA0560357](https://openairdocs.org/sdr/COMA0560357.md): Pcu · leaking · Jun 16, 2005 · N797CA · Cndair CL6002B19 · Drag Control System
  > RECEIVED HYDRAULIC NR 2 LOW PRESSURE CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND DIVERTED TO IAD. ACFT LANDED WITHOUT INCIDENT. REPLACED LEAKING FLIGHT SPOILER PCU.
- [SDR COMA0560356](https://openairdocs.org/sdr/COMA0560356.md): Pump · faulty · Jun 16, 2005 · N797CA · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main
  > RECEIVED HYDRAULIC NR 2 LOW PRESSURE CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND DIVERTED TO IAD. ACFT LANDED WITHOUT INCIDENT. REPLACED RT ENGINE HYDRAULIC.
- [SDR COMA0560355](https://openairdocs.org/sdr/COMA0560355.md): Line · leaking · Jun 16, 2005 · N797CA · Cndair CL6002B19 · Hydraulic System, Main
  > RECEIVED A HYDRAULIC NR 2 LOW PRESSURE CAUTION MESSAGE. CREW DECLARED EMERGENCY AND DIVERTED TO IAD. ACFT LANDED WITHOUT INCIDENT. REPLACED LEAKING NR 2 EDP PRESSURE LINE.
- [SDR COMA0560294](https://openairdocs.org/sdr/COMA0560294.md): Warning System · activated · May 1, 2005 · N797CA · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLIGHT 5605 FLAPS FAIL CAUTION. RESET FLAPS SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
- [SDR COMA0560225](https://openairdocs.org/sdr/COMA0560225.md): Computer · faulty · Apr 2, 2005 · N797CA · Cndair CL6002B19 · Stall Warning System
  > FLIGHT DURING TAKEOFF ROLL RECEIVED A STALL FAIL CAUTION MESSAGE, AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED THE STALL PROTECTION COMPUTER.
- [SDR COMA0560070](https://openairdocs.org/sdr/COMA0560070.md): Valve · faulty · Jan 20, 2005 · N797CA · Cndair CL6002B19 · Ice Detection
  > FLIGHT 4983, DURING CLIMB-OUT OF ATL, RECEIVED A LEFT COWL ANTI-ICE CAUTION, FLIGHT DIVERTED BACK TO ATL. REPLACED THE ANTI-ICE VALVE.
- [SDR COMA0560065](https://openairdocs.org/sdr/COMA0560065.md): Warning Light · illuminated · Jan 20, 2005 · N797CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5790 RECEIVED A FLAP FAIL CAUTION MESSAGE AFTER PUSHBACK FROM ATL GATE. AIRCRAFT 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 COMA0460575](https://openairdocs.org/sdr/COMA0460575.md): Warning Light · illuminated · Oct 21, 2004 · N797CA · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLIGHT 5376 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
- [SDR COMA0460584](https://openairdocs.org/sdr/COMA0460584.md): Bpsu · faulty · Oct 15, 2004 · N797CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5222 FLAPS FAIL CAUTION MESSAGE. REMOVED AND REPLACED BPSU.
- [SDR COMA0460571](https://openairdocs.org/sdr/COMA0460571.md): Control Unit · failed · Oct 12, 2004 · N797CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5370 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU.
- [SDR COMA0460573](https://openairdocs.org/sdr/COMA0460573.md): Warning Light · false activation · Oct 11, 2004 · N797CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 4943 FLAPS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE. INSPECTED FLAP SYSTEM AND FOUND NO DEFECTS.
- [SDR COMA0460570](https://openairdocs.org/sdr/COMA0460570.md): Warning System · activated · Oct 11, 2004 · N797CA · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLIGHT 5011 FLAPS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE. INSPECTED FLAP SYSTEM, FOUND NO DEFECTS.
- [SDR COMA0460487](https://openairdocs.org/sdr/COMA0460487.md): Engine · failed · Aug 24, 2004 · N797CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > FLIGHT 4990 LT ENGINE ROLLBACK TO 50 PERCENT AFTER T/O. REPLACED LEFT ENGINE.
- [SDR COMA0360306](https://openairdocs.org/sdr/COMA0360306.md): Windshield · cracked · Jun 29, 2003 · N797CA · Cndair CL6002B19 · Flight Compartment Windows
  > FLIGHT 5620 THE LEFT WINDSHIELD SHATTERED DURING CLIMBOUT OF ATL, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. REPLACED THE LEFT WINDSHIELD.
- [SDR COMA0160608](https://openairdocs.org/sdr/COMA0160608.md): Computer · Aug 18, 2001 · N797CA · Cndair CL6002B19 · Stall Warning System
  > FLIGHT #5235. DURING TAXI OUT RECEIVED A STALL FAIL CAUTION MESSAGE, AIRCRAFT RETURNED TO THE GATE.RESET THE STALL PROTECTION COMPUTER.
- [SDR COMA0160545](https://openairdocs.org/sdr/COMA0160545.md): Computer · malfunctioned · Jul 30, 2001 · N797CA · Cndair CL6002B19 · Rudder Control System
  > YAW DAMPNER DROPPED OFF LINE DURING TAXI CHECKS.REPLACED THE #1 FCC-4000.
- [SDR COMA0160538](https://openairdocs.org/sdr/COMA0160538.md): Rudder · Jul 27, 2001 · N797CA · Cndair CL6002B19 · Rudder Control System
  > VERY NOTICEABLE YAWING MOTION INFLIGHT.COULD NOT DUPLICATE. CHEDCKED YAW DAMPNERS AND RUDDER SYSTEM. NO DEFECTS FOUND.
- [SDR COMA0160338](https://openairdocs.org/sdr/COMA0160338.md): Cap · chafed · Mar 24, 2001 · N797CA · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBOARD FLAP HAS CHAFED VANE CAP ON INBOARD END. BLENDED CHAFED AREA IAW CANADAIR REO 601R-57-52-004 AND PAINTED IAW CRJ SRM 51-21-16.
- [SDR COMA0160336](https://openairdocs.org/sdr/COMA0160336.md): Bushing · worn · Mar 23, 2001 · N797CA · Cndair CL6002B19 · Horizontal Stabilizer, Attach Fittings
  > HORIZONTAL STAB LEFT OUTBOARD PIVOT POINT BUSHING WORN. REMOVED AND REPLACED BUSHING IAW CRJ AMM 20-26-00-910-803. REAMED BUSHING IAW REO 601R-55-11-022 REV A.
- [SDR COMA0160335](https://openairdocs.org/sdr/COMA0160335.md): Bushing · worn · Mar 23, 2001 · N797CA · Cndair CL6002B19 · Vertical Stabilizer
  > LEFT VERTICAL STAB PIVOT POINT BUSHING WORN. REMOVED AND REPLACED BUSHING IAW CRJ AMM 20-26-00-910-803, REAMED BUSHING IAW CRJ DRAWING 600-21061. MACHINED FLANGE IAW WVAC EO 601R-55-2325.
- [SDR COMA0160102](https://openairdocs.org/sdr/COMA0160102.md): Element · malfunctioned · Jan 12, 2001 · N797CA · Cndair CL6002B19 · Overheat Detection
  > RT 14TH STAGE BLEED AIR LEAK WARNING. REPLACED THE PYLON LEAK SENSE ELEMENT.
- [SDR COMA0061035](https://openairdocs.org/sdr/COMA0061035.md): Warning System · malfunctioned · Dec 12, 2000 · N797CA · Cndair CL6002B19 · Door Warning System
  > CABIN DOOR HANDLE CAUTION MESSAGE. COULD NOT DUPLICATE. CLEANED WIRING CONNECTION, OPERATIONAL CHECK SATISFACTORY.
- [SDR COMA0060124](https://openairdocs.org/sdr/COMA0060124.md): Fcu · malfunctioned · Jan 29, 2000 · N797CA · Cndair CL6002B19 · Fuel Control/Turbine Engines
  > RIGHT ENGINE OVER SPEED. REPLACED RIGHT ENGINE FUEL CONTROL.
- [SDR COMA0060016](https://openairdocs.org/sdr/COMA0060016.md): Actuator · malfunctioned · Dec 28, 1999 · N797CA · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLAPS FAILED AT 37 DEGREES DURING LANDING APPROACH. REPLACED LEFT WING NR 3 FLAP ACTUATOR.

## 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 = 'N797CA' AND deregistration_id = 'N797CA-2022-12-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N797CA-2022-12-03/reports

---
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