# Service difficulty reports: N812CA, cancelled Oct 29, 2019

A list on [N812CA, cancelled Oct 29, 2019](https://openairdocs.org/deregistered/N812CA-2019-10-29.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 · 54 reports

- [SDR COMA2012030150011](https://openairdocs.org/sdr/COMA2012030150011.md): Stiffener · cracked · Feb 29, 2012 · N812CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > VERTICAL CHANNEL (STIFFENER) WAS FOUND TO BE CRACKED. REPLACED CHANNEL (STIFFENER) IAW CRJ 200 SRM 51-42-06.
- [SDR COMA0212030150010](https://openairdocs.org/sdr/COMA0212030150010.md): Frame · corroded · Feb 29, 2012 · N812CA · Cndair CL6002B19 · Fuselage Main, Frame
  > FUSELAGE FRAME FOUND TO BE CORRODED BEYOND LIMITS. REPAIRED FRAME IAW CRJ 200 SRM 53-00-15 AND CRJ 200 MDTM 51-20-08.
- [SDR COMA2010030150047](https://openairdocs.org/sdr/COMA2010030150047.md): Selector Valve · failed · Feb 25, 2010 · N812CA · Cndair CL6002B19 · Landing Gear Selector
  > ON CLIMBOUT FROM DTW DURING GEAR RETRACTION RECEIVED NOSE GEAR DISAGREE AND GEAR DOOR OPEN WARNING MSG. EMERGENCY DECLARED, A/C RETURNED TO DTW LANDED SAFELY. REMOVED AND REPLACED NOSE LANDING GEAR SELECTOR VALVE.
- [SDR COMA2010012950026](https://openairdocs.org/sdr/COMA2010012950026.md): Angle · cracked · Jan 29, 2010 · N812CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 559 CAP ANGLE CRACKED AT RBL 18.00. REPAIRED FS 559 CAP ANGLE AT RBL 18.00 IAW REO 601R-53-41-260 REV D AND DEVIATION 601R-53-41-609 REV B.
- [SDR COMA2010012650024](https://openairdocs.org/sdr/COMA2010012650024.md): Angle · cracked · Jan 26, 2010 · N812CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 559 LEFT CAP ANGLE CRACKED AT LBL 18.00. REPAIRED CRACK AT LEFT FS 559 IN ACCORDANCE WITH REO 601-53-41-260 REV D DATED 17-SEP-2009.
- [SDR COMA2010012550022](https://openairdocs.org/sdr/COMA2010012550022.md): Bulkhead · cracked · Jan 22, 2010 · N812CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD AT FS 621.00 LINTEL ATTACHMENT FITTING CRACKED. REPAIRED AFT PRESSURE BULKHEAD WEB FS 621.00 LINTEL INSTALLATION IAW REO 601R-53-61-1230.
- [SDR COMA2010012550021](https://openairdocs.org/sdr/COMA2010012550021.md): Bulkhead · cracked · Jan 22, 2010 · N812CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD CRACKED AT FS 621.00 LBL 27.50 ABOVE CARGO DOOR TRACK. REPAIRED AFT PRESSURE BULKHEAD FS 621.00 LBL 27.50 IAW REO 601R-53-61-1541.
- [SDR COMA2010012550020](https://openairdocs.org/sdr/COMA2010012550020.md): Post · cracked · Jan 22, 2010 · N812CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128 CRACKED ON POST AT LBL 18.00 OUTBOARD RADIUS. REPAIRED LOWER OUTBOARD POST LBL 18.00 AT FS 409+128 IAW REO 601R-53-41-056.
- [SDR COMA0760698](https://openairdocs.org/sdr/COMA0760698.md): Anti-Ice Valve · faulty · Dec 7, 2007 · N812CA · Cndair CL6002B19 · Air Intake Anti/De-Ice System
  > FLIGHT 5137 - ON CLIMBOUT FROM CVG TO YYZ RECEIVED LEFT COWL ANTI-ICE INOP MESSAGE. CREW DECLARED EMERGENCY AND RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED LEFT ENGINE COWL ANTI-ICE VALVE.
- [SDR COMA0760697](https://openairdocs.org/sdr/COMA0760697.md): Relief Valve · faulty · Dec 7, 2007 · N812CA · Cndair CL6002B19 · Air Intake Anti/De-Ice System
  > FLIGHT 5137 - ON CLIMBOUT FROM CVG TO YYZ RECEIVED LEFT COWL ANTI-ICE INOP MESSAGE. CREW DECLARED EMERGENCY AND RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED LEFT ENGINE COWL ANTI-ICE PRESSURE RELIEF VALVE.
- [SDR COMA0760543](https://openairdocs.org/sdr/COMA0760543.md): Unknown · malfunctioned · Aug 26, 2007 · N812CA · Cndair CL6002B19 · Aileron Control System
  > FLIGHT 5113 - ON CLIMB, BOX A ON PFD FLASHED 2-3 SECONDS, FOLLOWED BY AUTO-PILOT DISCONNECT. NOTICED STIFFNESS IN CONTROLS WHEN TURNING LEFT. RETURNED TO ATL. LANDED WITHOUT INCIDENT. PERFORMED EO-27-075, AILERON CONTROL PATH INSPECTION. NO FURTHER DEFECT
- [SDR COMA0760290](https://openairdocs.org/sdr/COMA0760290.md): Flapper Valve · obstructed · Mar 26, 2007 · N812CA · Cndair CL6002B19 · Passenger/Crew Doors
  > FLIGHT 5244 - RECEIVED PAX DOOR CAUTION AND CABIN PRESSURE INCREASE ON CLIMBOUT. PERFORMED QRH. RETURNED TO PIT AND LANDED WITHOUT INCIDENT. CLEARED FOD FROM PAX DOOR FLAPPER VALVE. INSPECTED DOOR. NO FURTHER DEFECTS.
- [SDR COMA0760162](https://openairdocs.org/sdr/COMA0760162.md): Bpsu · faulty · Feb 6, 2007 · N812CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5331 - EN ROUTE BOS-YHZ RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT BRAKE POSITION SENSING UNIT.
- [SDR COMA0760161](https://openairdocs.org/sdr/COMA0760161.md): Actuator · faulty · Feb 6, 2007 · N812CA · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLIGHT 5331 - EN ROUTE BOS-YHZ RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT OUTBOARD FLAP OUTBOARD FLAP ACTUATOR.
- [SDR COMA0760149](https://openairdocs.org/sdr/COMA0760149.md): Spoiler Sys · malfunctioned · Feb 6, 2007 · N812CA · Cndair CL6002B19 · Drag Control System
  > FLIGHT 9459 - DURING TAKEOFF ROLL RECEIVED A CONFIG SPOILER MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. PERFORMED SYSTEM RESET WITH NO FURTHER DISCREPANCIES.
- [SDR COMA0760145](https://openairdocs.org/sdr/COMA0760145.md): Flap System · malfunctioned · Feb 5, 2007 · N812CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5567 - DURING BTR APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SY
- [SDR COMA0760091](https://openairdocs.org/sdr/COMA0760091.md): Shaft · damaged · Jan 29, 2007 · N812CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5170 - FLAP FAIL MESSAGE RECEIVED. ABORTED APPROACH, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND WATER IN SYSTEM, REPLACED RIGHT NR 3 FLEX DRIVE SHAFT.
- [SDR COMA0760090](https://openairdocs.org/sdr/COMA0760090.md): Shaft · corroded · Jan 29, 2007 · N812CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5170 - FLAP FAIL MESSAGE RECEIVED. ABORTED APPROACH, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND WATER IN SYSTEM, REPLACED LEFT NR 5 FLEX SHAFT.
- [SDR COMA0760034](https://openairdocs.org/sdr/COMA0760034.md): Bpsu · faulty · Jan 20, 2007 · N812CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5168 - FLAPS FAIL MESSAGE WHEN SELECTING 30 DEGREES. FAILED AT 20 DEGREES. REMOVED AND REPLACED RIGHT BPSU.
- [SDR COMA0760035](https://openairdocs.org/sdr/COMA0760035.md): Flap · malfunctioned · Jan 19, 2007 · N812CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5168 - ON APPROACH FLAPS SELECTED TO 30 BUT REMAINED AT 20 DEGREES. RECEIVED FLAPS FAIL CAUTION MESSAGE. 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 N
- [SDR COMA0660646](https://openairdocs.org/sdr/COMA0660646.md): Windshield · cracked · Nov 20, 2006 · N812CA · Cndair CL6002B19 · Flight Compartment Windows
  > FLIGHT 5584 - DURING DESCENT INTO JAX THE CAPTAIN'S WINDSHIELD CRACKED. REPLACED THE CAPAIN'S WINDSHIELD.
- [SDR COMA0660299](https://openairdocs.org/sdr/COMA0660299.md): Engine · failed · Apr 10, 2006 · N812CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > FLIGHT 9754 - DURING EWR APPROACH AN ABNORMAL NOISE WAS HEARD EMANATING FROM THE RIGHT ENGINE, FOLLOWED BY SLUGGING N1 AND N2 RESPONSE WITH POWER LEVER MOVEMENT. CREW DECLARED AN EMERGENCY AND PERFORMED AN IFSD OF THE RIGHT ENGINE. FLIGHT LANDED WITHOUT INCI
- [SDR COMA0560808](https://openairdocs.org/sdr/COMA0560808.md): Pdu · malfunctioned · Jan 11, 2006 · N812CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5354 - FLAPS FAIL CAUTION. REPLACED THE PDU.
- [SDR COMA0560583](https://openairdocs.org/sdr/COMA0560583.md): Anti-Skid Sys · warning light · Nov 2, 2005 · N812CA · Cndair CL6002B19 · Brake Anti-Skid Section
  > FLIGHT 5904 - PARKING BRAKE SOV AND ANTI/SKID CAUTION. RESET SYSTEM. NO DEFECTS NOTED.
- [SDR COMA0560494](https://openairdocs.org/sdr/COMA0560494.md): Latch · malfunctioned · Sep 11, 2005 · N812CA · Cndair CL6002B19 · Passenger/Crew Doors
  > FLIGHT 5755 - DURING TAKEOFF ROLL RECEIVED A CABIN DOOR HANDLE CAUTION MESSAGE. ABORTED TAKEOFF AND RETURNED TO THE GATE. PERFORMED OPERATIONAL CHECK OF THE CABIN DOOR HANDLE MECHANISM, COULD NOT DUPLICATE DISCREPANCY.
- [SDR COMA0560208](https://openairdocs.org/sdr/COMA0560208.md): Lead · failed · Mar 28, 2005 · N812CA · Cndair CL6002B19 · Ice/Rain Protection System Wiring
  > FLIGHT 5480 RECEIVED A LEFT WINDOW HEAT CAUTION DURING CLIMBOUT OF HSV, AIRCRAFT RETURNED TO THE FIELD. CONNECTED WINDOW ELECTRICAL LEADS TO SPARE TERMINALS.
- [SDR COMA0560203](https://openairdocs.org/sdr/COMA0560203.md): Sensor · malfunctioned · Mar 24, 2005 · N812CA · Cndair CL6002B19 · Overheat Detection
  > FLIGHT 5443 ABORTED TAKEOFF AT 10 KTS DUE TO LEFT JET OVERHEAT CAUTION, AIRCRAFT RETURNED TO THE GATE. DEFERRED JET OVERHEAT CAUTION PER MEL 16-11-02.
- [SDR COMA0560204](https://openairdocs.org/sdr/COMA0560204.md): Controller · faulty · Mar 28, 2004 · N812CA · Cndair CL6002B19 · Windshield/Door Rain/Ice Removal
  > FLIGHT 5480 RECEIVED A LEFT WINDOW HEAT CAUTION DURING CLIMBOUT OF GSO, AIRCRAFT RETURNED TO THE FIELD. FERRIED THE AIRCRAFT TO MCO, REPLACED THE WINDOW HEAT CONTROLLER.
- [SDR COMA0460175](https://openairdocs.org/sdr/COMA0460175.md): Target · loose · Feb 29, 2004 · N812CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > FLIGHT 5173 GEAR DISAGREE WARNING, LT MLG INDICATES INTRANSIT. TIGHTENED THE PROX SWITCH TARGET ON THE LT MLG UPLOCK.
- [SDR COMA0460057](https://openairdocs.org/sdr/COMA0460057.md): Windshield · failed · Jan 14, 2004 · N812CA · Cndair CL6002B19 · Flight Compartment Windows
  > FLIGHT 5219 COPILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD.
- [SDR COMA0460119](https://openairdocs.org/sdr/COMA0460119.md): Stringer · damaged · Jan 3, 2004 · N812CA · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > CARGO ENTRY WAY FORWARD FRAME AT FS 574.00 APPROXIMATELY STRINGER 15L HAS DAMAGE. COMPLIED WITH REO 601R-53-61-690 TO FACILITATE CARGO ENTRY WAY FORWARD FRAME FS 574.00 REPAIR. PARTIALLY REMOVED FRAME AT FS 574.00 IN ACCORDANCE WITH CRJ SRM 51-40-06. LOCATE
- [SDR COMA0460116](https://openairdocs.org/sdr/COMA0460116.md): Floor Support · cracked · Jan 3, 2004 · N812CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO FLOOR ANGLE AT FS 621.00 BULKHEAD, LEFT AND RIGH SUPPORT, CRACKED. COMPLIED WTIH BOMBARDIER REO 601R-53-61-004. PAINTED REPAIR IN ACCORDANCE WITH CRJ SRM 51-25-00.
- [SDR COMA0460115](https://openairdocs.org/sdr/COMA0460115.md): Plate · cracked · Jan 3, 2004 · N812CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO FOOR LANDING PLATE AT FS 589 CRACKED FROM RIVET HOLE TO EDGE OF PLATE. COMPLIED WITH BOMBARDIER REO 601R-53-61-433.
- [SDR COMA0460114](https://openairdocs.org/sdr/COMA0460114.md): Plate · cracked · Jan 3, 2004 · N812CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO FLOOR LANDING PLATE AT FS 589 CRACKED FROM RIVET HOLE TO EDGE OF PLATE. COMPLIED WITH BOMBARDIER REO 601R-53-61-433.
- [SDR COMA0260708](https://openairdocs.org/sdr/COMA0260708.md): Computer · malfunctioned · Dec 11, 2002 · N812CA · Cndair CL6002B19 · Dependent Position Determining System
  > FLIGHT 5263 AIRCRAFT UNABLE TO TRACK GLIDE SLOPE.REPLACED THE #2 VIR-432
- [SDR COMA0260533](https://openairdocs.org/sdr/COMA0260533.md): Flap · Sep 14, 2002 · N812CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
- [SDR COMA0260228](https://openairdocs.org/sdr/COMA0260228.md): Door · Apr 1, 2002 · N812CA · Cndair CL6002B19 · Service Doors
  > FLIGHT 6152 LOUD SQUEALING AND VIBRATION FROM R/H SIDE OF COCKPIT.GROUND INTERFONE DOOR FOUND OPEN - SECURED DOOR CLOSED - NO DAMAGE TO AIRCRAFT.
- [SDR COMA0160490](https://openairdocs.org/sdr/COMA0160490.md): Actuator · binding · Jul 18, 2001 · N812CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT 43 DEGREES.REPLACED THE RIGHT HAND #1 AND #2 FLAP ACTUATORS.
- [SDR COMA0160487](https://openairdocs.org/sdr/COMA0160487.md): Actuator · binding · Jul 18, 2001 · N812CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT 43 DEGREES.REPLACED THE RIGHT HAND #1 AND #2 FLAP ACTUATORS.
- [SDR COMA0160324](https://openairdocs.org/sdr/COMA0160324.md): Warning System · false activation · Mar 19, 2001 · N812CA · Cndair CL6002B19 · Integrated Flight System
  > EFIS COMP MON CAUTION DURING T/O. REPLACED THE NR 2 AHARS.
- [SDR COMA0160299](https://openairdocs.org/sdr/COMA0160299.md): Computer · malfunctioned · Mar 5, 2001 · N812CA · Cndair CL6002B19 · Stall Warning System
  > STALL FAIL CAUTION MESSAGE DURING T/O. RESET THE STALL COMPUTER.
- [SDR COMA0160261](https://openairdocs.org/sdr/COMA0160261.md): Bpsu · failed · Feb 17, 2001 · N812CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU.
- [SDR COMA0160051](https://openairdocs.org/sdr/COMA0160051.md): Warning System · false activation · Jan 2, 2001 · N812CA · Cndair CL6002B19 · Door Warning System
  > CABIN DOOR OUTER HANDLE CAUTION MESSAGE. COULD NOT DUPLICATE. DOOR LATCH MECHANISM OPERATES NORMALLY.
- [SDR COMA0160050](https://openairdocs.org/sdr/COMA0160050.md): Smoke Detector · false indication · Jan 2, 2001 · N812CA · Cndair CL6002B19 · Smoke Detection
  > SMOKE TOILET CAUTION MESSAGE, F/A REPORTS SMOKE AND ELECTRIC SMELL IN CABIN.COULD NOT DUPLICATE. REPLACED LAV SMOKE DETECTOR.
- [SDR COMA0160045](https://openairdocs.org/sdr/COMA0160045.md): Warning System · false activation · Dec 31, 2000 · N812CA · Cndair CL6002B19 · Smoke Detection
  > SMOKE TOILET CAUTION MESSAGE. COULD NOT DUPLICATE. INSPECTED TOILET AND FOUND NO DISCREPANCY.
- [SDR COMA0160018](https://openairdocs.org/sdr/COMA0160018.md): Skin · damaged · Dec 28, 2000 · N812CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > RT SIDE FUSELAGE SKIN WAS DAMAGED BETWEEN F.S. 700.0 AND 718.0 AT STR 18R.REPAIRED FUSELAGE DAMAGE BETWEEN F.S. 700.0 AND 718.0 AT STR 18R IAW WVAC EO 601R-53-2054.
- [SDR COMA0061033](https://openairdocs.org/sdr/COMA0061033.md): Handle · broken · Dec 12, 2000 · N812CA · Cndair CL6002B19 · Landing Gear Selector
  > LANDING GEAR SELECTOR HANDLE BROKE OFF, WHEN GEAR SELECTED UP. REPLACED THE GEAR SELECTOR ASSY.
- [SDR COMA0060961](https://openairdocs.org/sdr/COMA0060961.md): Amplifier · malfunctioned · Nov 23, 2000 · N812CA · Cndair CL6002B19 · Power Lever
  > POWER LEVER SPLIT IN FLIGHT. REPLACED THE N1 CONTROL AMPLIFIER.
- [SDR COMA0060920](https://openairdocs.org/sdr/COMA0060920.md): Warning System · malfunctioned · Nov 13, 2000 · N812CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE, PARKING BRAKE SOV, ANTI-SKID MESSAGE AND VIBRATION AFTER GEAR RETRACTION. COULD NOT DUPLICATE. OPERATIONAL TEST OF LANDING GEAR WAS SATISFACTORY.
- [SDR COMA0060757](https://openairdocs.org/sdr/COMA0060757.md): Computer · failed · Sep 15, 2000 · N812CA · Cndair CL6002B19 · Stall Warning System
  > STALL FAIL CAUTION MESSAGE DURING TAKEOFF ROLL, AIRCRAFT RETURNED TO GATE. RESET THE STALL COMPUTER.

Next page: https://openairdocs.org/deregistered/N812CA-2019-10-29/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 = 'N812CA' AND deregistration_id = 'N812CA-2019-10-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N812CA-2019-10-29/reports

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