# Service difficulty reports: N956CA, cancelled Apr 18, 2018

A list on [N956CA, cancelled Apr 18, 2018](https://openairdocs.org/deregistered/N956CA-2018-04-18.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 · 100 reports

- [SDR COMA2012011750004](https://openairdocs.org/sdr/COMA2012011750004.md): Bulkhead · cracked · Jan 13, 2012 · N956CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BIRD STRIKE TO FS 169 BULKHEAD, UPPER RT SIDE, AT AFT EDGE OF RADOME. REMOVED AND REPLACED FS 169 BULKHEAD, IAW SRM 53-11-15.
- [SDR COMA2011012050010](https://openairdocs.org/sdr/COMA2011012050010.md): Steering Sys · malfunctioned · Jan 19, 2011 · N956CA · Cndair CL6002B19 · Landing Gear Steering System
  > ON APPROACH INTO ATL RECEIVED STEERING INOP MSG. UNABLE TO RESET. EMERGENCY DECLARED, A/C LANDED SAFELY. PERFORMED SYSTEM RESET FOR THE NOSE WHEEL STEERING SYSTEM AND PERFORMED OPERATIONAL CHECK. OPS CHECK GOOD.
- [SDR COMA2010021650043](https://openairdocs.org/sdr/COMA2010021650043.md): Post · cracked · Feb 15, 2010 · N956CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CRACK IN VERTICAL POST AT FS 409+128, RBL 27.00, IN LOWER RADIUS. TRIMMED OUT DAMAGE AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-41-056 REV E.
- [SDR COMA2010021550042](https://openairdocs.org/sdr/COMA2010021550042.md): Angle · cracked · Feb 13, 2010 · N956CA · Cndair CL6002B19 · Fuselage Main, Frame
  > FOUND CRACK IN FRAME CAP ANGLE AT FS 559.00 LBL 18.00 INBOARD SIDE. REPAIRED CAP ANGLE AT FS 559.00 IAW REO 601R-53-41-260.
- [SDR COMA2010021550041](https://openairdocs.org/sdr/COMA2010021550041.md): Post · cracked · Feb 13, 2010 · N956CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CRACK IN POST AT FS 409+128 LBL 27.00 LOWER RADIUS. REPAIRED POST AT FS 409+128 IAW REO 601R-53-41-056 REV E.
- [SDR COMA2010021550040](https://openairdocs.org/sdr/COMA2010021550040.md): Bulkhead · cracked · Feb 12, 2010 · N956CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING EDDY CURRENT FOUND CRACK IN AFT PRESSURE BULKHEAD FS 621.00 ABOVE CARGO DOOR TRACK. REPAIRED AFT PRESSURE BULKHEAD AT FS 621.00 IAW REO 601R-53-61-1541.
- [SDR COMA2010020950034](https://openairdocs.org/sdr/COMA2010020950034.md): Support · cracked · Feb 7, 2010 · N956CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CRACK IN LOWER END OF FS 409+128 LBL 18 VERTICAL SUPPORT. CUT OUT DAMAGE AND INSTALLED REPAIR ANGLES IAW REO 601R-53-41-056 REV E.
- [SDR COMA2010020550033](https://openairdocs.org/sdr/COMA2010020550033.md): Floor Support · cracked · Feb 5, 2010 · N956CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CRACK IN FS 280.00 FLOOR SUPPORT IN LOWER RADIUS AT RBL 9.00. REPAIRED FLOOR SUPPORT AT FS 280.00 RBL 9.00 IAW REO 601R-53-11-171.
- [SDR COMA2009093050195](https://openairdocs.org/sdr/COMA2009093050195.md): Control Handle · faulty · Sep 30, 2009 · N956CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > ON APPROACH INTO BUF RECEIVED FLAPS FAIL CAUTION MSG WHEN SELECTING FLAPS FROM 20 TO 30 DEG. EMERGENCY DECLARED, A/C LANDED SAFELY. REMOVED AND REPLACED FLAP CONTROL HANDLE.
- [SDR COMA2009032450103](https://openairdocs.org/sdr/COMA2009032450103.md): Apu · malfunctioned · Mar 23, 2009 · N956CA · Cndair CL6002B19 · APU Core Engine
  > DURING TAXI APU MADE A LOUD SQUEAK, A BOOM THEN AUTO SHUTDOWN. SMOKE CAME OUT APU DOOR, NO FLAMES. EMERGENCY DECLARED. DEFERRED APU PER MEL 49-10-01-1.
- [SDR COMA0860064](https://openairdocs.org/sdr/COMA0860064.md): Outflow Valve · obstructed · Jan 13, 2008 · N956CA · Cndair CL6002B19 · Pressure Regulator/Outflow Valve
  > FLIGHT 5228 - ON CLIMBOUT FROM CVG RECEIVED CABIN ALTITUDE WARNING MESSAGE, WITH PACKS ON, CABIN PRESS RISING. AIRCRAFT RETURNED TO CVG AND LANDED SAFELY. UPON INSPECTION, FOUND A 16" SQUARE PIECE OF INSULATION PROJECTING THROUGH PRIMARY OUTFLOW VALVE. REMO
- [SDR COMA0760674](https://openairdocs.org/sdr/COMA0760674.md): Controller · malfunctioned · Nov 29, 2007 · N956CA · Cndair CL6002B19 · Cabin Pressure Controller
  > FLIGHT 4953 - A/C WILL NOT PRESSURIZE IN FLIGHT. TRIED BOTH CONTROLLERS AND MANUAL MODE WITH NO AFFECT. A/C RETURNED TO DTW AND LANDED SAFELY. TRANSFERRED TO DEFERRED LIST PER MEL 21-31-01-2.
- [SDR COMA0760673](https://openairdocs.org/sdr/COMA0760673.md): Connector · broken · Nov 27, 2007 · N956CA · Cndair CL6002B19 · Landing Gear System Wiring
  > FLIGHT 5594 - RECEIVED ANTI-SKID OUTBOARD CAUTION MESSAGE ON TAKEOFF ROLL. ABORTED TAKEOFF, RETURNED TO GATE WITHOUT INCIDENT. REPLACED BROKEN CONNECTOR ON WHEEL SPEED TRANSDUCER. NO FURTHER DEFECTS.
- [SDR COMA0760640](https://openairdocs.org/sdr/COMA0760640.md): Controller · faulty · Nov 13, 2007 · N956CA · Cndair CL6002B19 · Cabin Pressure Controller
  > FLIGHT 5219 - AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF FROM BOS. AIRCRAFT RETURNED TO BOS AND LANDED SAFELY. FOUND CABIN PRESSURE CONTROLLER FAULTY. DEFERRED PER MEL 21-31-01-1.
- [SDR COMA0760385](https://openairdocs.org/sdr/COMA0760385.md): Reservoir · leaking · May 20, 2007 · N956CA · Cndair CL6002B19 · Hydraulic Reservoir, Main
  > FLIGHT 5661- RECEIVED GEAR DISAGREE MESSAGE. ABORTED APPROACH, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. FOUND NR 3 HYDRAULIC RESERVOIR LEAK DECAY RATE OUT OF LIMITS. REPLACED RESERVOIR. NO FURTHER DEFECTS.
- [SDR COMA0760374](https://openairdocs.org/sdr/COMA0760374.md): Stiffener · cracked · May 16, 2007 · N956CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING 559 INSPECTION FOUND 2 INCH CRACK ON INBOARD SIDE AND.5 INCH CRACK AT OUTBOARD SIDE OF VERTICAL STIFFENER, RBL 9, FS 559. REMOVED DAMAGE AND INSTALLED DOUBLERS PER REO 601R-53-41-520.
- [SDR COMA0760373](https://openairdocs.org/sdr/COMA0760373.md): Stiffener · cracked · May 16, 2007 · N956CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING 559 INSPECTION FOUND.5 INCH CRACK AT BASE OF VERTICAL STIFFENER, FS 559, RBL 18. REMOVED DAMAGE AND INSTALLED DOUBLER PER REO 601R-53-41-067.
- [SDR COMA0760372](https://openairdocs.org/sdr/COMA0760372.md): Stiffener · cracked · May 16, 2007 · N956CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING 559 INSPECTION FOUND.5 INCH CRACK AT LOWER OUTBOARD SIDE OF LBL VERTICAL STIFFENER. REMOVED DAMAGE AND INSTALLED DOUBLER PER BOMBARDIER REO 601R-53-41-057.
- [SDR COMA0760363](https://openairdocs.org/sdr/COMA0760363.md): Warning System · malfunctioned · May 6, 2007 · N956CA · Cndair CL6002B19 · Engine Thrust Reverser
  > FLIGHT 5280 - LEFT T/R UNLOCK MESSAGE DURING POWER-UP. TROUBLESHOT LEFT T/R SYSTEM AND PERFORMED OPS CHECKS, NO DEFECTS NOTED.
- [SDR COMA0660701](https://openairdocs.org/sdr/COMA0660701.md): Flap System · malfunctioned · Dec 8, 2006 · N956CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED ON FINAL AT 30 DEGREES. 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 COMA0660486](https://openairdocs.org/sdr/COMA0660486.md): Sensor · faulty · Aug 12, 2006 · N956CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > FLIGHT 9459 - DURING CVG APPROACH RECEIVED A LANDING GEAR DISAGREE MESSAGE, ABORTED APPROACH, THEN LANDED WITHOUT INCIDENT. REPLACED MLG UPLOCK PROXIMITY SENSOR.
- [SDR COMA0660439](https://openairdocs.org/sdr/COMA0660439.md): Valve · faulty · Jul 18, 2006 · N956CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > FLIGHT 5117- DURING APPROACH RECEIVED A LANDING GEAR DOWN DISAGREE CAUTION, CREW DECLARED AN EMERGENCY, PERFORMED A MANUAL GEAR EXTENSION AND TOWER FLY-BY. FLIGHT LANDED WITHOUT INCIDENT.
- [SDR COMA0660292](https://openairdocs.org/sdr/COMA0660292.md): Line · leaking · Apr 6, 2006 · N956CA · Cndair CL6002B19 · Hydraulic System, Main
  > FLIGHT 5662- EN ROUTE MCO-RDU, RECEIVED A NR 1 HYDRAULIC SYSTEM LOW PRESSURE CAUTION, FLIGHT DIVERTED TO SAV. REPLACED LEAKING BRAIDED HYDRAULIC LINE.
- [SDR COMA0560619](https://openairdocs.org/sdr/COMA0560619.md): Ejector · malfunctioned · Nov 18, 2005 · N956CA · Cndair CL6002B19 · Cabin Pressure Control System
  > FLIGHT 5440 - RECEIVED A CABIN ALTITUDE MESSAGE DURING CRUISE FLIGHT, DIVERTED TO RDU FOR PRESSURIZATION PROBLEM. REMOVED, INSPECTED AND RE-INSTALLED THE JET PUMP EJECTOR IN THE AFT EQUIPMENT BAY.
- [SDR COMA0560618](https://openairdocs.org/sdr/COMA0560618.md): Seal · damaged · Nov 18, 2005 · N956CA · Cndair CL6002B19 · Cargo/Baggage Doors
  > FLIGHT 9452 - DURING CLIMBOUT OF RDU, CABIN WAS SLOW TO PRESSURIZE. FLIGHT RETURNED TO RDU FOR PRESSURIZATION PROBLEM. FERRIED A/C TO CVG FOR REPLACEMENT OF THE CARGO DOOR SEAL.
- [SDR COMA0560505](https://openairdocs.org/sdr/COMA0560505.md): Actuator · faulty · Sep 16, 2005 · N956CA · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLIGHT 5786 - DURING CLIMBOUT OF JFK RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREE FLAP SETTING. REPLACED FLAP ACTUATOR.
- [SDR COMA0560503](https://openairdocs.org/sdr/COMA0560503.md): Actuator · unreliable · Sep 15, 2005 · N956CA · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLIGHT 5262 - FLAPS FAIL CAUTION. CND, REPLACED 2 FLAP ACTUATORS AND 1 FLEX DRIVE CABLE. RE-RIGGED SYSTEM.
- [SDR COMA0560501](https://openairdocs.org/sdr/COMA0560501.md): Bpsu · malfunctioned · Sep 14, 2005 · N956CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 4960 - FLAPS FAIL CAUTION. REPLACED THE LEFT BPSU.
- [SDR COMA0560488](https://openairdocs.org/sdr/COMA0560488.md): Control System · failed · Sep 5, 2005 · N956CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLT 5805 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
- [SDR COMA0560437](https://openairdocs.org/sdr/COMA0560437.md): Wire Harness · chafed · Aug 11, 2005 · N956CA · Cndair CL6002B19 · Turbine Engine System Wiring
  > FLIGHT 5164 - EN ROUTE FSD - CVG RECEIVED A NR 2 ENGINE FIRE MESSAGE, SHUTDOWN NR 2 ENGINE. FLIGHT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 ENGINE ASSEMBLY AND IDG HARNESS ASSEMBLY DUE TO CHAFED BLUE WIRE ARCING AGAINST THE FUEL CONTROL.
- [SDR COMA0560099](https://openairdocs.org/sdr/COMA0560099.md): Proximity Sensor · malfunctioned · Jan 30, 2005 · N956CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > FLIGHT 5443 GEAR DISAGREE WARNING AFTER T/O. REPLACED THE LT NLG DOWNLOCK PROXIMITY SENSOR.
- [SDR COMA0560008](https://openairdocs.org/sdr/COMA0560008.md): Door · open · Dec 21, 2004 · N956CA · Cndair CL6002B19 · Air Conditioning Doors
  > FLIGHT 5315, 02 SERVICE DOOR LEFT OPEN. INSPECTED FOR DAMAGE AND SECURED DOOR IN CLOSED POSITION.
- [SDR COMA0460618](https://openairdocs.org/sdr/COMA0460618.md): Warning Light · activated · Nov 13, 2004 · N956CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > FLIGHT 5316 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. LANDING GEAR EXTENSION AND RETRACTION CHECKS WERE NORMAL AND SATISFACTORY.
- [SDR COMA0460001](https://openairdocs.org/sdr/COMA0460001.md): Skin · corroded · Dec 31, 2003 · N956CA · Cndair CL6002B19 · Wing, Plate/Skin
  > THE LEFT AND RIGHT LOWER WING TANK ACCESS PANEL CUTOUTS HAD CORROSION AT PANELS 640AB, 640CB, 640DB, 640FB, 640BB, 540BB, 540FB, 550AB AND 550BB. REMOVED CORROSION AND RESTORED THE FINISH IAW REO 601R-57-21-030 REV C.
- [SDR COMA0360581](https://openairdocs.org/sdr/COMA0360581.md): Hinge Fitting · chafed · Dec 30, 2003 · N956CA · Cndair CL6002B19 · Elevator Miscellaneous Structure
  > RIGHT ELEVATOR NR 1 HINGE POINT ON THE HORIZONTAL IS CHAFED. REPAIRED BY BLENDING CHAFED AREA SMOOTH, PERFORMED LIQUID PENETRANT INSPECTION, ROTO/FLAP PEEN REWORKED AREA IAW CNDAIR SRM 51-24-11, AND TREATED AREA WITH ALODINE, ALL WORK PERFORMED IAW WVAC EO 60
- [SDR COMA0360579](https://openairdocs.org/sdr/COMA0360579.md): Skin · dented · Dec 27, 2003 · N956CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT.018 DEEP IN LEFT FUSELAGE LOWER SKIN AT FS 580.00 + 30 BELOW STR 20 L. RECONTOURED SKIN DAMAGE AREA IAW WVAC EO NR 601R-53-4489.
- [SDR COMA0360577](https://openairdocs.org/sdr/COMA0360577.md): Skin · cracked · Dec 27, 2003 · N956CA · Cndair CL6002B19 · Wing, Plate/Skin
  > THE LEFT LOWER WING PLANK FUEL DRAIN FORWARD SCREW HOLE AT WS 85.5 HAD AN INDICATION WHILE PERFORMING EDDY CURRENT INSPECTION (FUEL BOOST PUMP DRAIN VALVE FORWARD SCREW HOLE). DRILLED THE SCREW HOLE TO.3125 INCH TO REMOVE THE INDICATION. FABRICATED AND INST
- [SDR COMA0360576](https://openairdocs.org/sdr/COMA0360576.md): Floorbeam · corroded · Dec 27, 2003 · N956CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > THE FLOORBEAM CAP BETWEEN FS 559+12 TO FS 620, LBL 27 WAS CORRODED. REMOVED THE CORRODED FLOORBEAM CAP AND INSTALLED A NEW BEAM CAP IAW WVAC EO 601R-53-4501.
- [SDR COMA0360468](https://openairdocs.org/sdr/COMA0360468.md): Engine · failed · Oct 23, 2003 · N956CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > FLIGHT 5308 LOUD BANG FOLLOWED BY LEFT ENGINE FAILURE. REPLACED LEFT ENGINE.
- [SDR COMA0360240](https://openairdocs.org/sdr/COMA0360240.md): Switch · failed · May 16, 2003 · N956CA · Cndair CL6002B19 · Stabilizer Position Indicating
  > FLIGHT 5575 DURING TAKE OFF ROLL RECEIVED A STABILIZER TRIM CAUTION, ABORTED T/O AND RETURNED TO THE GATE. REPLACED THE LEFT AND RIGHT PITCH TRIM DISCONNECT SWITCHES.
- [SDR COMA0360144](https://openairdocs.org/sdr/COMA0360144.md): Flap · Mar 11, 2003 · N956CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5103 FLAPS FAILED AT 20 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
- [SDR COMA0260696](https://openairdocs.org/sdr/COMA0260696.md): Apu · Dec 6, 2002 · N956CA · Cndair CL6002B19 · APU Cowling/Containment
  > FLIGHT 5169 FUEL FUMES IN FWD SECTION OF AIRCRAFT AFTER APU START.COULD NOT DUPLICATE, OPERATIONAL CHECK OF APU WAS NORMAL.
- [SDR COMA0260523](https://openairdocs.org/sdr/COMA0260523.md): Wire · failed · Sep 10, 2002 · N956CA · Cndair CL6002B19 · Landing Gear Steering System
  > FLIGHT 5975. AFTER DEPARTING CVT RECEIVED A STEERING IMPERATIVE MESSAGE AFTER GEAR RETRACTION. FLIGHT RETURNED TO THE FIELD.REPLACED THE STEERING WIRING HARNESS.
- [SDR COMA0260494](https://openairdocs.org/sdr/COMA0260494.md): Door Latch · Aug 22, 2002 · N956CA · Cndair CL6002B19 · Cargo/Baggage Doors
  > FLIGHT 5622 CARGO DOOR OPEN CAUTION MESSAGE.FOUND HANDLE UNLATCHED - CLOSED AND LATCHED HANDLE.
- [SDR COMA0260487](https://openairdocs.org/sdr/COMA0260487.md): Target · loose · Aug 14, 2002 · N956CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > FLIGHT 5787 GEAR DISAGREE MESSAGE, R/H MLG DID NOT INDICATE UPLOCK.TIGHTENED LOOSE PROXIMITY SENSOR TARGET ON R/H MLG UPLOCK.
- [SDR COMA0260287](https://openairdocs.org/sdr/COMA0260287.md): Fcu · malfunctioned · Apr 28, 2002 · N956CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL MESSAGE. REPLACED THE FECU.
- [SDR COMA0260286](https://openairdocs.org/sdr/COMA0260286.md): Flap · Apr 28, 2002 · N956CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT 20 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
- [SDR COMA0260175](https://openairdocs.org/sdr/COMA0260175.md): Cable · loose · Mar 9, 2002 · N956CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5010 EMERGENCY FLOOR PATH LIGHTING INOP.SECURED LOOSE WIRE CONNECTION AT ROW 11.
- [SDR COMA0260025](https://openairdocs.org/sdr/COMA0260025.md): Switch · malfunctioned · Dec 31, 2001 · N956CA · Cndair CL6002B19 · Pneumatic Distribution System
  > FLIGHT 5527 - AFTER T/O, L/H AC PACK HIGH PRESSURE MESSAGE, FOLLOWED BY BLEED AIR DUCT MESSAGE, FOLLOWED BY L/H JET PIPE OVERHEAT, FOLLWOED BY R/H AC PACK HIGH PRESSURE.REPLACED THE L/H AC PACK PRESSURE SWITCH.
- [SDR COMA0160902](https://openairdocs.org/sdr/COMA0160902.md): Plank · cracked · Nov 15, 2001 · N956CA · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT LOWER WING CUT OUT AT 640 C B CRACKED.BLENDED OUT DAMAGE AND ROTO-PEENED I/A/W REO 601R-57-21-030.

Next page: https://openairdocs.org/deregistered/N956CA-2018-04-18/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 = 'N956CA' AND deregistration_id = 'N956CA-2018-04-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N956CA-2018-04-18/reports

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