# Service difficulty reports: N721CA, cancelled Aug 26, 2015

A list on [N721CA, cancelled Aug 26, 2015](https://openairdocs.org/deregistered/N721CA-2015-08-26.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 · 67 reports

- [SDR COMA2010071950147](https://openairdocs.org/sdr/COMA2010071950147.md): Hydraulic Line · chafed · Jul 15, 2010 · N721CA · Cndair CL6002B19 · Hydraulic System, Main
  > EN ROUTE FROM BNA TO MSP RECEIVED HYD NR 1 LOW PSI MSG, PRESSURE AND QTY WENT TO ZERO. EMERGENCY DECLARED, A/C DIVERTED TO STL LANDED SAFELY. FOUND HYD LINE FROM TOP OF CASE DRAIN MANIFOLD TO SERVICE PORT CHAFED THROUGH. REMOVED AND REPLACED LINE. NO FURTH
- [SDR COMA2010032950071](https://openairdocs.org/sdr/COMA2010032950071.md): Control Handle · failed · Mar 26, 2010 · N721CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT 30 DEG ON APPROACH INTO JFK. EMERGENCY DECLARED, A/C LANDED SAFELY AT JFK. REMOVED AND REPLACED FLAP CONTROL LEVER.
- [SDR COMA2009121450227](https://openairdocs.org/sdr/COMA2009121450227.md): Bulkhead · cracked · Dec 12, 2009 · N721CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD CRACKED ABOVE CARGO DOOR TRACK. REPAIRED CRACK ABOVE CARGO DOOR TRACK IAW REO 601R-53-61-1541.
- [SDR COMA2009121450226](https://openairdocs.org/sdr/COMA2009121450226.md): Bulkhead · cracked · Dec 12, 2009 · N721CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD CRACKED AROUND LINTEL FITTING. REPAIRED CRACK AT LINTEL FITTING IAW REO 601R-53-61-1230.
- [SDR COMA2009120450221](https://openairdocs.org/sdr/COMA2009120450221.md): Post · cracked · Dec 4, 2009 · N721CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND POST CRACKED AT FS 409.00+128 RBL 27 I/B LOWER CORNER RADIUS. REPAIRED POST IAW REO 601R-53-41-056.
- [SDR COMA2009120350220](https://openairdocs.org/sdr/COMA2009120350220.md): Post · cracked · Dec 3, 2009 · N721CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND POST CRACKED AT FS 409.00+128 LBL 27 I/B LOWER CORNER RADIUS. REPAIRED POST IAW REO 601R-53-41-056.
- [SDR COMA2009040150108](https://openairdocs.org/sdr/COMA2009040150108.md): Engine · vibration · Mar 29, 2009 · N721CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > ON CLIMBOUT FROM BOS RECEIVED LEFT ENGINE VIBE MSG ALONG WITH MAX ITT AND OIL PRESSURE OF 20 PSI. PERFORMED IFSD OF LEFT ENGINE. EMERGENCY DECLARED, A/C RETURNED TO BOS LANDED SAFELY. REMOVED AND REPLACED LEFT ENGINE.
- [SDR COMA2009022450086](https://openairdocs.org/sdr/COMA2009022450086.md): Unknown · smoke · Feb 24, 2009 · N721CA · Cndair CL6002B19 · Air Distribution System
  > EN ROUTE FROM BHM TO LGA, SMOKE IN CABIN WITH APU OFF AND BOTH PACKS RUNNING ON 10TH STAGE BLEED AIR. EMERGENCY DECLARED, A/C RETURNED TO BHM LANDED SAFELY. TRANSFERRED TO DEFERRED LIST PER MEL 21-51-01-2.
- [SDR COMA2009020950078](https://openairdocs.org/sdr/COMA2009020950078.md): Rvdt · failed · Feb 5, 2009 · N721CA · Cndair CL6002B19 · Landing Gear Steering System
  > RECEIVED NWS INOP MSG AFTER SELECTING LANDING GEAR DOWN. WOULD NOT RESET. EMERGENCY DECLARED, A/C LANDED SAFELY. REMOVED AND REPLACED RT NWS POSITION FEEDBACK RVDT.
- [SDR COMA2009010550055](https://openairdocs.org/sdr/COMA2009010550055.md): Angle · cracked · Jan 4, 2009 · N721CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FS 559.00 CAP ANGLE CRACKED AT LBL 9.00 AND LBL18.00. REPAIRED IAW REO 601R-53-41-260.
- [SDR COMA2009010550054](https://openairdocs.org/sdr/COMA2009010550054.md): Angle · cracked · Jan 2, 2009 · N721CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT FS 559.00 CAP ANGLE CRACKED AT LBL 9.00 AND LBL 18.00. REPAIRED CAP ANGLE IAW REO 601R-53-41-260.
- [SDR COMA2008121650025](https://openairdocs.org/sdr/COMA2008121650025.md): Alternator · failed · Dec 11, 2008 · N721CA · Cndair CL6002B19 · AC Generator-Alternator
  > ON CLIMBOUT FROM CVG, NR 2 ENGINE N2 SHOWS 0 RPM. A/C RETURNED TO CVG LANDED SAFELY. REMOVED AND REPLACED NR 2 ENGINE ALTERNATOR STATOR. OPS CHECK GOOD.
- [SDR COMA0860232](https://openairdocs.org/sdr/COMA0860232.md): Indicator · unknown · Apr 22, 2008 · N721CA · Cndair CL6002B19 · Engine Fuel Indicating System
  > FLIGHT 4972 - ON TAKEOFF ROLL NR 2 ENGINE FUEL FLOW READ OUT WAS 1300 LBS. ABORTED TAKEOFF SAFELY. TRANSFERRED TO DMI LIST PER 73-31-01.
- [SDR COMA0860128](https://openairdocs.org/sdr/COMA0860128.md): Flap · malfunctioned · Feb 11, 2008 · N721CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5190 - FLAPS FAIL CAUTION MESSAGE ON APPROACH. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. COMPLIED WITH SI-2-2710001 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES.
- [SDR COMA0860125](https://openairdocs.org/sdr/COMA0860125.md): Actuator · faulty · Feb 11, 2008 · N721CA · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLIGHT 5532 - FLAPS FAIL CAUTION MESSAGE AT 0 DEGREES WHEN SELECTING 8 DEGREES. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED RIGHT O/B FLAP O/B ACTUATOR.
- [SDR COMA0860124](https://openairdocs.org/sdr/COMA0860124.md): Actuator · faulty · Feb 11, 2008 · N721CA · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLIGHT 5532 - FLAPS FAIL CAUTION MESSAGE AT 0 DEGREES WHEN SELECTING TO 8 DEGREES. EMERGENCY DECLARED, A/C LANDED SAFELY. REMOVED AND REPLACED RIGHT O/B FLAP I/B ACTUATOR.
- [SDR COMA0760497](https://openairdocs.org/sdr/COMA0760497.md): Flap System · malfunctioned · Jul 23, 2007 · N721CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5120 - FLAPS FAIL AT 30 DEGREES ON APPROACH, AIRCRAFT LANDED SAFELY. 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 COMA0760420](https://openairdocs.org/sdr/COMA0760420.md): A/C Pack · uncontrollable · Jun 1, 2007 · N721CA · Cndair CL6002B19 · Cabin Cooling System
  > FLIGHT 5228 - LEFT A/C PACK UNCONTROLLABLE IN AUTO OR MANUAL. RETURNED TO OMA, LANDED WITHOUT INCIDENT. INSPECTED LEFT PACK AND DUCTS FOR DAMAGE, PERFORMED TEMP CONTROL CHECK. NO FURTHER DEFECTS.
- [SDR COMA0760220](https://openairdocs.org/sdr/COMA0760220.md): Control Handle · faulty · Mar 1, 2007 · N721CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5686 - FLAP FAIL MESSAGE AFTER LANDING. REPLACED FLAP CONTROL HANDLE AS INDICATED BY FECU INTERROGATION. ALSO PERFORMED EO 27-046AD. NO FURTHER DEFECTS.
- [SDR COMA0760121](https://openairdocs.org/sdr/COMA0760121.md): Fcu · faulty · Jan 29, 2007 · N721CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5524 - DURING ROC APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE FLAP CONTROL UNIT.
- [SDR COMA0760084](https://openairdocs.org/sdr/COMA0760084.md): Flap System · malfunctioned · Jan 28, 2007 · N721CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5529 - DURING CMH APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 8 DEGREE FLAP SETTING, 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,
- [SDR COMA0760050](https://openairdocs.org/sdr/COMA0760050.md): Actuator · failed · Jan 23, 2007 · N721CA · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLIGHT 5156 - FLAPS FAIL MESSAGE APPEARED WHEN FLAPS WERE SELECTED TO 8 DEGREES. LANDED WITHOUT INCIDENT. REPLACED LEFT INBOARD FLAP OUTBOARD ACTUATOR.
- [SDR COMA0760049](https://openairdocs.org/sdr/COMA0760049.md): Actuator · failed · Jan 23, 2007 · N721CA · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLIGHT 5156 - FLAPS FAIL MESSAGE APPEARED WHEN FLAPS WERE SELECTED TO 8 DEGREES. LANDED WITHOUT INCIDENT. REPLACED LEFT INBOARD FLAP INBOARD ACTUATOR.
- [SDR COMA0760048](https://openairdocs.org/sdr/COMA0760048.md): Flex Drive · twisted · Jan 23, 2007 · N721CA · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLIGHT 5156 - FLAPS FAIL MESSAGE APPEARED WHEN FLAPS WERE SELECTED TO 8 DEGREES. LANDED WITHOUT INCIDENT. REPLACED LEFT WING NR 5 FLAP FLEX DRIVE SHAFT.
- [SDR COMA0760047](https://openairdocs.org/sdr/COMA0760047.md): Flex Drive · twisted · Jan 23, 2007 · N721CA · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLIGHT 5156 - FLAPS FAIL MESSAGE APPEARED WHEN FLAPS WERE SELECTED TO 8 DEGREES. LANDED WITHOUT INCIDENT. REPLACED LEFT WING NR 3 FLAP FLEX DRIVE SHAFT.
- [SDR COMA0760046](https://openairdocs.org/sdr/COMA0760046.md): Flex Drive · twisted · Jan 23, 2007 · N721CA · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLIGHT 5156 - FLAPS FAIL MESSAGE APPEARED WHEN FLAPS WERE SELECTED TO 8 DEGREES. LANDED WITHOUT INCIDENT. REPLACED LEFT WING NR 2 FLAP FLEX DRIVE SHAFT.
- [SDR COMA0660238](https://openairdocs.org/sdr/COMA0660238.md): Accelerometer · faulty · Mar 10, 2006 · N721CA · Cndair CL6002B19 · Engine Vibration Analyzer
  > FLIGHT 5199 - EN ROUTE GSO-LGA THE LEFT ENGINE N1 FLUCTUATED FROM 1.8, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE ENGINE ACCELEROMETER.
- [SDR COMA0660224](https://openairdocs.org/sdr/COMA0660224.md): Drive Shaft · worn · Mar 3, 2006 · N721CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5882 - AFTER TAKEOFF FROM JFK RECEIVED A FLAP FAIL CAUTION MESSAGE AT ZERO DEGREES, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT WING NR 3 FLEX DRIVE SHAFT.
- [SDR COMA0660158](https://openairdocs.org/sdr/COMA0660158.md): Flap System · malfunctioned · Feb 18, 2006 · N721CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5334 - AFTER LANDING AT SDF AND DURING RETRACTION OF THE FLAPS RECEIVED A FLAP CAUTION MESSAGE AT 27 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
- [SDR COMA0560716](https://openairdocs.org/sdr/COMA0560716.md): Bulkhead · damaged · Dec 13, 2005 · N721CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > HOLE IN AFT PRESSURE BULKHEAD FS 621 AND LBL 45. INSTALLED RIVET IN FS 621 AND LBL 45 AFT PRESSURE BULKHEAD IAW SRM 51-12-00 PG 21, SMALL HOLE REPAIR.
- [SDR COMA0560680](https://openairdocs.org/sdr/COMA0560680.md): Intercostal · cracked · Dec 12, 2005 · N721CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED AT FS 484 BL27.00-36.00 RIGHT SIDE BELOW FLOOR AFT OF EMERGENCY EXIT. REPAIRED CRACK IAW BRAS EO 601R-53-41-059.
- [SDR COMA0560404](https://openairdocs.org/sdr/COMA0560404.md): Overheat Sensor · malfunctioned · Jul 23, 2005 · N721CA · Cndair CL6002B19 · Landing Gear Brake System
  > FLIGHT 5580- BRAKE OVERHEAT MESSAGE. INSPECTED BRAKE AND FOUND NO DEFECTS.
- [SDR COMA0560340](https://openairdocs.org/sdr/COMA0560340.md): Warning System · activated · Jun 7, 2005 · N721CA · Cndair CL6002B19 · Engine Thrust Reverser
  > RT THRUST REVERSER UNLOCK CAUTION. DEFERRED MAINTENANCE ON RIGHT THRUST REVERSER PER MEL.
- [SDR COMA0560314](https://openairdocs.org/sdr/COMA0560314.md): Line · leaking · May 20, 2005 · N721CA · Cndair CL6002B19 · Hydraulic System, Main
  > FLIGHT 5088 HYDRAULIC SYSTEM NR 1 LOW PRESSURE CAUTION, QUANTITY INDICATED 0. REPLACED HIGH PRESSURE LINE IN LEFT HAND ENGINE PYLON.
- [SDR COMA0560245](https://openairdocs.org/sdr/COMA0560245.md): Control Panel · failed · Apr 7, 2005 · N721CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5315 DURING CLIMBOUT OF CVG WITH FLAPS RETRACTED THE STAB AND MACH TRIM MASTER CAUTION MESSAGES ACTIVATED, CREW FOLLOWED QRH PROCEDURES, RE-ENGAGED STAB/MACH TRIM AND LANDED AT SAV WITHOUT INCIDENT. CLEANED STAB/MACH TRIM ENGAGE PANEL SWITCHES AND RE-R
- [SDR COMA0560032](https://openairdocs.org/sdr/COMA0560032.md): Lamp · inoperative · Jan 7, 2005 · N721CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5681 EMERGENCY FLOOR LIGHTS INOP AT ROW 1 AND 2. REPLACED THE FLEXIBLE LIGHT STRIP.
- [SDR COMA0470032](https://openairdocs.org/sdr/COMA0470032.md): Engine · overheated · Apr 19, 2004 · N721CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > FLIGHT 5711 DURING TAKEOFF ROLL AT 80 KNOTS NR 2 ENGINE ITT REACHED 906C DEGREES, ABORTED T/O AND RETURNED TO THE GATE. REPLACED THE RIGHT ENGINE.
- [SDR COMA0460240](https://openairdocs.org/sdr/COMA0460240.md): Warning Light · illuminated · Apr 4, 2004 · N721CA · Cndair CL6002B19 · Engine Temperature Indicating System
  > FLIGHT 5390 RIGHT ENGINE ITT OVERTEMP DURING T/O. COULD NOT DUPLICATE. GROUND RUN SATISFACTORY. NO DEFECT FOUND.
- [SDR COMA0460215](https://openairdocs.org/sdr/COMA0460215.md): Seal · leaking · Mar 19, 2004 · N721CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FLIGHT 5892 WATER LEAKING FROM CABIN CEILING. RESEALED AROUND ADF ANTENNA.
- [SDR COMA0460157](https://openairdocs.org/sdr/COMA0460157.md): Pdu · malfunctioned · Feb 21, 2004 · N721CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5108 FLAPS FAIL MESSAGE DURING TAXI. REPLACED THE PDU.
- [SDR COMA0360532](https://openairdocs.org/sdr/COMA0360532.md): Frame · cracked · Dec 7, 2003 · N721CA · Cndair CL6002B19 · Fuselage Main, Frame
  > CRACK NOTED AT FS 718.00 RT BETWEEN STRINGER 11 - 12. REPAIRED PER SERVICE BULLETIN 601R-53-055 PART B PER EA 10-5320-00242.
- [SDR COMA0360531](https://openairdocs.org/sdr/COMA0360531.md): Doubler · cracked · Dec 7, 2003 · N721CA · Cndair CL6002B19 · Fuselage Main, Frame
  > CRACK NOTED AT FS 718.00 LT AND DOUBLER BETWEEN STRINGER 10 -12. REPAIRED PER EO 53 027 AND SERVICE BULLETIN 601R-53-055 PD.
- [SDR COMA0360530](https://openairdocs.org/sdr/COMA0360530.md): Doubler · cracked · Dec 7, 2003 · N721CA · Cndair CL6002B19 · Fuselage Main, Frame
  > CRACK NOTED AT FS 718.00 RIGHT HAND DOUBLER BETWEEN STRINGER 10 - 12. REPAIRED PER EO 53-027 AND SERVICE BULLETIN 601R-53-055 PE.
- [SDR COMA0360215](https://openairdocs.org/sdr/COMA0360215.md): Warning Light · illuminated · Apr 24, 2003 · N721CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > FLIGHT 5083 ANTI-SKID CAUTION MESSAGE WHEN LANDING GEAR EXTENDED. COULD NOT DUPLICATE, SYSTEM TEST NORMAL.
- [SDR COMA0360200](https://openairdocs.org/sdr/COMA0360200.md): Generator · inoperative · Apr 16, 2003 · N721CA · Cndair CL6002B19 · AC Generation System
  > FLIGHT 5261 GENERATOR NR 2 OFF-LINE DURING T/O. DEFERRED MAINT PER MEL.
- [SDR COMA0360142](https://openairdocs.org/sdr/COMA0360142.md): Pump · leaking · Mar 9, 2003 · N721CA · Cndair CL6002B19 · Engine Fuel Pump
  > FOUND SMALL PIN HOLE IN RT ENG FUEL PUMP HOUSING, FOUND DURING A LEAK CHECK FOR A NON RELATED ITEM. REPLACED FUEL PUMP.
- [SDR COMA0260728](https://openairdocs.org/sdr/COMA0260728.md): Transducer · malfunctioned · Dec 20, 2002 · N721CA · Cndair CL6002B19 · Engine Oil Pressure
  > LEFT ENGINE OIL PRESSURE INDICATED 157 PSI. REPLACED THE OIL PRESSURE TRANSDUCER.
- [SDR COMA0260417](https://openairdocs.org/sdr/COMA0260417.md): Priority Valve · malfunctioned · Jul 7, 2002 · N721CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > FLIGHT 5222 GEAR DISAGREE WARNING DURING GEAR EXTENSION.REPLACED THE NLG PRIORITY VALVE.
- [SDR COMA0260389](https://openairdocs.org/sdr/COMA0260389.md): Door · Jun 26, 2002 · N721CA · Cndair CL6002B19 · Passenger/Crew Doors
  > FLIGHT 5726 CABIN DOOR WARNING AFTER T/O.OUTER HANDLE NOT STOWED PROPERLY - INSPECTED AND OPERATED DOOR - FOUND NO DEFECT.
- [SDR COMA0160951](https://openairdocs.org/sdr/COMA0160951.md): Pin · Dec 9, 2001 · N721CA · Cndair CL6002B19 · Nose/Tail Landing Gear
  > FLIGHT #5686 NLG DOES NOT RETRACT WHEN LANDING GEAR SELECTED UP.FOUND NLD DOWN LOCK SAFETY PIN INSTALLED. - REMOVED PIN AND AIRCRAFT RETURNED TO SERVICE.

Next page: https://openairdocs.org/deregistered/N721CA-2015-08-26/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 = 'N721CA' AND deregistration_id = 'N721CA-2015-08-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N721CA-2015-08-26/reports

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