# Service difficulty reports: N709CA, cancelled Apr 12, 2012

A list on [N709CA, cancelled Apr 12, 2012](https://openairdocs.org/deregistered/N709CA-2012-04-12.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 · 55 reports

- [SDR COMA0860092](https://openairdocs.org/sdr/COMA0860092.md): Flap · malfunctioned · Jan 21, 2008 · N709CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5620 - FLAPS FAIL CAUTION MESSAGE, FLAPS FAILED AT 0 DEGREES. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I0001, FLAPS FAIL FIRST EVENT MAINTENANCE ACTION.
- [SDR COMA0760509](https://openairdocs.org/sdr/COMA0760509.md): Oil System · low · Aug 1, 2007 · N709CA · Cndair CL6002B19 · Turbine Engine Oil System
  > FLIGHT 5387 - DURING CLIMBOUT RECEIVED LEFT ENGINE LOW OIL PRESS WARNING MESSAGE. AIRCRAFT RETURNED BACK TO CID AND LANDED SAFELY. INSPECTED LEFT ENGINE AND FOUND IT TO BE LOW ON OIL. SERVICED ENGINE AND PERFORMED GROUND RUNS.
- [SDR COMA0760417](https://openairdocs.org/sdr/COMA0760417.md): Spring · out of rig · May 31, 2007 · N709CA · Cndair CL6002B19 · Aileron Control System
  > FLIGHT 5503 - LEFT AND RIGHT AILERON MORE STIFF THAN NORMAL. -A- ON PFD WITH AUTO-PILOT ON, IN TURNS. HYD PUMP 1A SQUEALING. AILERONS FELT NORMAL WHEN DISCONNECTED. FOUND BOTH CENTERING MECHANISMS FORCE TOO HIGH. RIGGED LEFT AND RIGHT AILERON CENTERING ME
- [SDR COMA0760322](https://openairdocs.org/sdr/COMA0760322.md): Flap · malfunctioned · Apr 16, 2007 · N709CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION MSG. 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 CAUTION MESSAGES.
- [SDR COMA0660648](https://openairdocs.org/sdr/COMA0660648.md): Anti-Ice Valve · warning message · Nov 22, 2006 · N709CA · Cndair CL6002B19 · Air Intake Anti/De-Ice System
  > FLIGHT 5380 - EN ROUTE TYS-CHS RECEIVED A LEFT COWL ANTI-ICE CAUTION MESSAGE, FLIGHT RETURNED TO TYS. RESET THE LEFT ENGINE COWL ANTI-ICE VALVE.
- [SDR COMA0660562](https://openairdocs.org/sdr/COMA0660562.md): Actuator · faulty · Sep 30, 2006 · N709CA · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLIGHT 5008 - FLAPS FAIL MESSAGE, FLAPS FAILED AT ZERO DEGREES. REMOVED AND REPLACED LEFT INBOARD FLAP INBOARD ACTUATOR.
- [SDR COMA0660561](https://openairdocs.org/sdr/COMA0660561.md): Actuator · faulty · Sep 30, 2006 · N709CA · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLIGHT 5008 - FLAPS FAIL CAUTION MESSAGE, FLAPS FAILED AT ZERO DEGREES. REMOVED AND REPLACED LEFT INBOARD FLAP OUTBOARD ACTUATOR.
- [SDR COMA0660554](https://openairdocs.org/sdr/COMA0660554.md): Flap System · malfunctioned · Sep 27, 2006 · N709CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5423 - EN ROUTE CVG-PWM RECEIVED A FLAP FAIL CAUTION AT ZERO DEGREES, CREW DECLARED AN EMERGENCY AND DIVERTED TO BGR. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS
- [SDR COMA0660535](https://openairdocs.org/sdr/COMA0660535.md): Flap System · malfunctioned · Sep 8, 2006 · N709CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5253 - DURING TUL APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT ZERO DEGREES, CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C).
- [SDR COMA0660367](https://openairdocs.org/sdr/COMA0660367.md): Transducer · faulty · May 31, 2006 · N709CA · Cndair CL6002B19 · Engine Oil Pressure
  > FLIGHT 5262 - EN ROUTE RIC-CVG RECEIVED A RIGHT ENGINE HIGH OIL PRESSURE WARNING, CREW DECLARED AN EMERGENCY, RETURNED TO RIC AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT ENGINE OIL PRESSURE TRANSDUCER.
- [SDR COMA0660201](https://openairdocs.org/sdr/COMA0660201.md): Flap System · malfunctioned · Feb 27, 2006 · N709CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5187 - DURING BTV APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 8 DEGREES, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C
- [SDR COMA0560813](https://openairdocs.org/sdr/COMA0560813.md): Warning Light · illuminated · Jan 16, 2006 · N709CA · Cndair CL6002B19 · Electrical Power System
  > FLIGHT 5151- GENERATOR NR 2 CAUTION. SERVICED THE IDG OIL SYSTEM.
- [SDR COMA0560698](https://openairdocs.org/sdr/COMA0560698.md): Coupling · damaged · Dec 8, 2005 · N709CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 4989 - FLAPS FAIL CAUTION. REPLACED THE NR 5 FLEX SHAFT.
- [SDR COMA0560687](https://openairdocs.org/sdr/COMA0560687.md): Bpsu · unreliable · Dec 6, 2005 · N709CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5399 - FLAPS FAIL CAUTION. REPLACED THE LT BPSU.
- [SDR COMAO560319](https://openairdocs.org/sdr/COMAO560319.md): Pseu · malfunctioned · May 24, 2005 · N709CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > FLT 5183 - DISPLAY COOL CAUTION, CABIN ALTITUDE WARNING AND BURNING ODOR IN COCKPIT. REPLACED THE PSEU.
- [SDR COMA0560316](https://openairdocs.org/sdr/COMA0560316.md): Warning Light · illuminated · May 23, 2005 · N709CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > FLIGHT 9483 GEAR DISAGREE WARNING. FOUND NLG REQUIRED SERVICED. SERVICED NLG IAW MM.
- [SDR COMA0560309](https://openairdocs.org/sdr/COMA0560309.md): Shutoff Valve · malfunctioned · May 14, 2005 · N709CA · Cndair CL6002B19 · Cabin Cooling System
  > FLIGHT 4987 - LT AND RT AIR CONDITIONING PACKS FAILED. REPLACED THE LEFT AND RIGHT 10TH STAGE PRSOV.
- [SDR COMA0560223](https://openairdocs.org/sdr/COMA0560223.md): Bpsu · faulty · Apr 3, 2005 · N709CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5446 RECEIVED A FLAP FAIL CAUTION AFTER LANDING WHEN FLAPS WERE RETRACTED. REPLACED THE LEFT BPSU.
- [SDR COMA0560101](https://openairdocs.org/sdr/COMA0560101.md): Window · cracked · Jan 30, 2005 · N709CA · Cndair CL6002B19 · Flight Compartment Windows
  > FLIGHT 5530 PILOTS SIDE WINDOW CRACKED. REPLACED WINDOW.
- [SDR COMA0560020](https://openairdocs.org/sdr/COMA0560020.md): Warning System · malfunctioned · Jan 1, 2005 · N709CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > FLIGHT 5316, GEAR DISAGREE WARNING. COULD NOT DUPLICATE. FUNCTIONAL TEST OF LANDING GEAR EXTENSION AND RETRACTION SYSTEM NORMAL, NO DEFECTS FOUND.
- [SDR COMA0460356](https://openairdocs.org/sdr/COMA0460356.md): Priority Valve · unreliable · Jun 8, 2004 · N709CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > FLIGHT 5156 GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE.
- [SDR COMA0460366](https://openairdocs.org/sdr/COMA0460366.md): Landing Gear · lack of lube · Jun 7, 2004 · N709CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > FLIGHT 5334 GEAR DISAGREE WARNING, WHEN SELECTED DOWN. CLEAN AND LUBED LANDING GEAR.
- [SDR COMA0460231](https://openairdocs.org/sdr/COMA0460231.md): Smoke Detector · false activation · Mar 29, 2004 · N709CA · Cndair CL6002B19 · Smoke Detection
  > FLIGHT 5226 CARGO SMOKE WARNING, DISCHARGED CARGO FIRE BOTTLES. INSPECTED AND FOUND NO EVIDENCE OF OR CONDITION TO CAUSE SMOKE. REPLACED SMOKE DETECTORS.
- [SDR COMA0460071](https://openairdocs.org/sdr/COMA0460071.md): Control Unit · malfunctioned · Jan 19, 2004 · N709CA · Cndair CL6002B19 · Stabilizer Control System
  > FLIGHT 5839 STAB TRIM AND MACH TRIM DISENGAGED DURING FLIGHT. COULD NOT DUPLICATE. NO FAULT CODES IN COMPUTER. OPERATIONAL CHECK NORMAL.
- [SDR COMA0360485](https://openairdocs.org/sdr/COMA0360485.md): Computer · faulty · Nov 5, 2003 · N709CA · Cndair CL6002B19 · Fuel Indicating System
  > FLIGHT 5485 - DURING CLIMBOUT OF MCO RECEIVED A FUEL IMBALANCE CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIELD. REPLACED THE FUEL COMPUTER.
- [SDR COMA0360484](https://openairdocs.org/sdr/COMA0360484.md): Connector · contaminated · Nov 5, 2003 · N709CA · Cndair CL6002B19 · Fuel Indicating System
  > FLIGHT 5484 DURING CLIMBOUT OF MCO RECEIVED A FUEL IMBALANCE CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIELD. CLEANED MOISTURE FROM CONNECTOR J425/P425.
- [SDR COMA0360455](https://openairdocs.org/sdr/COMA0360455.md): Computer · malfunctioned · Oct 9, 2003 · N709CA · Cndair CL6002B19 · Fuel Indicating System
  > FLIGHT 5557 LEFT FUEL INDICATION INOP. REPLACED THE FUEL COMPUTER.
- [SDR COMA0360360](https://openairdocs.org/sdr/COMA0360360.md): Thrust Reverser · malfunctioned · Aug 11, 2003 · N709CA · Cndair CL6002B19 · Engine Thrust Reverser
  > FLIGHT 5229 LT THRUST REVERSER UNLOCKED MESSAGE DURING FLIGHT. DEFERRED MAINT PER MEL.
- [SDR COMA0360113](https://openairdocs.org/sdr/COMA0360113.md): Capacitor · malfunctioned · Feb 22, 2003 · N709CA · Cndair CL6002B19 · Fuel Quantity Sensor
  > FLIGHT 5022 FUEL QUANTITY INDICATION IS ERRATIC.REPLACED THE #6 FUEL QUANTITY PROBE.
- [SDR COMA0360081](https://openairdocs.org/sdr/COMA0360081.md): Computer · malfunctioned · Feb 4, 2003 · N709CA · Cndair CL6002B19 · Fuel Indicating System
  > FLIGHT 5543 LEFT FUEL PUMP CAUTION AND FUEL IMBALANCE CAUTION MESSAGE.REPLACED THE FUEL COMPUTER.
- [SDR COMA0260308](https://openairdocs.org/sdr/COMA0260308.md): Bellcrank · dirty · May 8, 2002 · N709CA · Cndair CL6002B19 · Aileron Control System
  > FLIGHT 5883 A/P TRIM LWD CAUTION MESSAGE. AILERONS VERY STIFF.COULD NOT DUPLICATE PROBLEM ON GROUND - AILERON AFT BELLCRANK ASSY WERE DETERMINED TO BE MOST PROBABLE CAUSE AND WERE REPLACED.
- [SDR COMA0260247](https://openairdocs.org/sdr/COMA0260247.md): Skin · damaged · Apr 15, 2002 · N709CA · Cndair CL6002B19 · Wing, Plate/Skin
  > WHILE AIRCRAFT WAS AT HANGAR FOR OVERNIGHT, MAINTENANCE NOTICED EVIDENCE OF A LIGHTNING STRIKE ON RIGHT WING LOWER SKIN TOWARD TIP AT W.S.401.COMPLIED WITH LIGHTNING STRIKE INSPECTION PER CHECKLIST AND PERFORMED TEMPORARY REPAIR PER BOMBARDIER REO 601R-57-31-
- [SDR COMA0260207](https://openairdocs.org/sdr/COMA0260207.md): Flap · Mar 23, 2002 · N709CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5820 FLAPS FAILED AT 0 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
- [SDR COMA0160841](https://openairdocs.org/sdr/COMA0160841.md): Wheel · cracked · Oct 23, 2001 · N709CA · Cndair CL6002B19 · Wheel/Ski/Float
  > DURING N.D.T. INSPECTION OF THE MLG WHEEL INBOARD SUB ASSEMBLY, DISCOVERED A CRACK AT THE SPOKE AREA.WHEEL WAS REMOVED FROM SERVICE AND SCRAPPED.
- [SDR COMA0160831](https://openairdocs.org/sdr/COMA0160831.md): Control Column · Oct 21, 2001 · N709CA · Cndair CL6002B19 · Control Column Section
  > FLIGHT #5260. WHILE MOVING AILERONS THRU FULL RANGE OF TRAVEL, A SLIGHT BINDING CAN BE FELT AT FULL TRAVEL AND AT NEUTROL.RETROQUED THE NUT HOLDING YOKE TO CONTROL COLUMN.
- [SDR COMA0160797](https://openairdocs.org/sdr/COMA0160797.md): Web · cracked · Oct 9, 2001 · N709CA · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > ENGINE SUPPORT BEAM LOWER WEB CRACKED BETWEEN FS 625.30 AND FS 640.00 AT WL 111.09, BL37 LT AND RT.PERFORMED TEMPORARY REPAIR I/A/W BOMBARDIER REO 601R-53-61-366 REV. C.
- [SDR COMA0160794](https://openairdocs.org/sdr/COMA0160794.md): Doubler · cracked · Oct 6, 2001 · N709CA · Cndair CL6002B19 · Fuselage Main, Frame
  > F.S.718 FRAME DOUBLER CRACKED ON LEFT SIDE OF FUSELAGE.REPAIRED LEFT SIDE DOUBLER I/A/W REO 601R-53-61-193 REV A.
- [SDR COMA0160093](https://openairdocs.org/sdr/COMA0160093.md): Engine · vibration · Jan 7, 2001 · N709CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > RT ENGINE VIB INDICATION AT.7, ENGINE FAILED. REPLACED ENGINE.
- [SDR COMA0060975](https://openairdocs.org/sdr/COMA0060975.md): Warning System · activated · Nov 30, 2000 · N709CA · Cndair CL6002B19 · Door Warning System
  > CABIN DOOR HANDLE CAUTION MESSAGE. COULD NOT DUPLICATE. DOOR AND DOOR WARNING SYSTEM OPERATION SATISFACTORY.
- [SDR COMA0060884](https://openairdocs.org/sdr/COMA0060884.md): Panel · cracked · Nov 5, 2000 · N709CA · Cndair CL6002B19 · Wing, Plate/Skin
  > CRACK IN LOWER HORIZONTAL SURFACE OF LT AND RT LOWER WING ACCESS HOLES.540FB WS 136.676, 540DB WS 95.950 AND 640 FB WS 136.676. BLENDED OUT DAMAGE, ROTO PEENED AND ALODINED IAW BOMBARDIER REO 601R-57-21-030.
- [SDR COMA0060436](https://openairdocs.org/sdr/COMA0060436.md): Intercostal · cracked · May 17, 2000 · N709CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THE INTERCOSTAL BETWEEN LBL 9 AND LBL 18 AT FS 484.0 HAS A CRACK EXTENDING FROM THE RADIUS AT LBL 18. PERFORMED A MAJOR REPAIR TO CRACKED INTERCOSTAL AT LBL 18 FS 484.0 IAW WVAC EO 601R-53-1331.
- [SDR COMA0060435](https://openairdocs.org/sdr/COMA0060435.md): Skin · dented · May 17, 2000 · N709CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN IS DENTED AFT OF THE CARGO DOOR AT FS 650 AND STRINGERS 20 - 21 LHS. PERFORMED A MAJOR REPAIR TO FUSELAGE SKIN AT FS 650 STR 20 - 21 LHS IAW WVAC EO 601R-53-1329.
- [SDR COMA0060425](https://openairdocs.org/sdr/COMA0060425.md): Floor Support · cracked · May 17, 2000 · N709CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FS 621 FLOOR SUPPORT ANGLE IS CRACKED. PERFORMED A MAJOR REPAIR AT FS 621 RIGHT FLOOR SUPPORT ANGLE IAW CANADAIR REO 601R-53-61-117.
- [SDR COMA0060097](https://openairdocs.org/sdr/COMA0060097.md): Warning System · activated · Jan 26, 2000 · N709CA · Cndair CL6002B19 · Door Warning System
  > CABIN DOOR WARNING. ADJUSTED DOOR LATCH MECHANISM.
- [SDR COMA0060096](https://openairdocs.org/sdr/COMA0060096.md): Warning System · activated · Jan 26, 2000 · N709CA · Cndair CL6002B19 · Door Warning System
  > CABIN DOOR WARNING COULD NOT DUPLICATE. OPERATION OF DOOR AND WARNING SYSTEM WAS NORMAL.
- [SDR COMA9960707](https://openairdocs.org/sdr/COMA9960707.md): Vane Cap · chafed · Nov 22, 1999 · N709CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT HAND AND RIGHT HAND INBOARD CAPS CHAFED LEFT HAND.027 RIGHT HAND.028. REMOVED CHAFED INBOARD FLAP VANE INBOARD CAPS AND INSTALLED NEW CAPS IAW WVAC EO 601R-57-0632A.
- [SDR COMA9960704](https://openairdocs.org/sdr/COMA9960704.md): Doubler · cracked · Nov 20, 1999 · N709CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AFT DOUBLER (P/N 600-36030-32) AT FS 718 RWS STR 11-12 WAS CRACKED. PERFORMED A MAJOR REPAIR BY REPLACING AFT DOUBLER (P/N 600-36030-32) AT FS 718 RHS STR 11-12 IAW CRJ REO 601R-53-61-193 REV A.
- [SDR COMA9960701](https://openairdocs.org/sdr/COMA9960701.md): Te Flap · failed · Nov 18, 1999 · N709CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS WILL NOT RETRACT, FLAPS STUCK AT 26 DEGREES. RESET FLAP SYSTEM PER AD 98-20-01.
- [SDR COMA9960683](https://openairdocs.org/sdr/COMA9960683.md): Panel · chafed · Nov 14, 1999 · N709CA · Cndair CL6002B19 · Ailerons
  > RIGHT HAND OUTBOARD LOWER COVER PANEL ON RIGHT HAND AILERON CHAFED BEYOND LIMITS. FABRICATED NEW PANEL AND INSTALLED AN AILERON IAW WVAC EO 601R-57-0619.
- [SDR COMA9960471](https://openairdocs.org/sdr/COMA9960471.md): Pack · malfunctioned · Aug 24, 1999 · N709CA · Cndair CL6002B19 · Cabin Cooling System
  > STRONG SULFURIC SMELL IN AIRCRAFT. DEFERRED LEFT HAND AIR CONDITIONING SYSTEM.

Next page: https://openairdocs.org/deregistered/N709CA-2012-04-12/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 = 'N709CA' AND deregistration_id = 'N709CA-2012-04-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N709CA-2012-04-12/reports

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