# Service difficulty reports: N975CA, cancelled Jul 16, 2008

A list on [N975CA, cancelled Jul 16, 2008](https://openairdocs.org/deregistered/N975CA-2008-07-16.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 · 57 reports

- [SDR COMA0760107](https://openairdocs.org/sdr/COMA0760107.md): Flap System · malfunctioned · Jan 31, 2007 · N975CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 6056 - FLAPS FAILED AT ZERO 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 COMA0760002](https://openairdocs.org/sdr/COMA0760002.md): Warning Light · illuminated · Jan 1, 2007 · N975CA · Cndair CL6002B19 · Engine Thrust Reverser
  > FLIGHT 5418 - EN ROUTE JAX-LGA RECEIVED A RIGHT THRUST REVERSER UNLOCK MESSAGE, FLIGHT DIVERTED TO CHS. DEFERRED THE RIGHT THRUST REVERSER PER MEL 78-30-01.
- [SDR COMA0660621](https://openairdocs.org/sdr/COMA0660621.md): Probe · failed · Nov 8, 2006 · N975CA · Cndair CL6002B19 · Engine Oil Temperature
  > FLIGHT 5339 - DURING CLIMB LEFT ENGINE OIL TEMP WENT TO AMBER RANGE. AIRCRAFT RETURNED TO CVG AND LANDED WITHOUT INCIDENT. FOUND OIL TANK OVER SERVICED AND PROBE OIL LEVEL INOP. REMOVED EXCESS OIL FROM TANK AND REPLACED PROBE OIL LEVEL.
- [SDR COMA0660598](https://openairdocs.org/sdr/COMA0660598.md): Shutoff Valve · faulty · Nov 2, 2006 · N975CA · Cndair CL6002B19 · Brake Anti-Skid Section
  > FLIGHT 5421- UPON GEAR EXTENSION, INBOARD ANTI-SKID INOP MESSAGE APPEARED. CYCLED GEAR, MESSAGE CLEARED, RE-APPEARED UPON EXTENSION. REPLACED PARKING BRAKE SHUT-OFF VALVE.
- [SDR COMA0660582](https://openairdocs.org/sdr/COMA0660582.md): Control Unit · malfunctioned · Oct 22, 2006 · N975CA · Cndair CL6002B19 · Landing Gear Steering System
  > FLIGHT 5436 - THRUST TO TAKEOFF POWER, AFTER 5 SECONDS STEERING INOP CAUTION MESSAGE AND CONFIG WARNING SPOILER MESSAGE. ABORTED TAKEOFF AT 50 KTS. THRUST LEVERS AT IDLE, CONFIG WARNING WENT AWAY. RESET SPOILERON SYSTEM.
- [SDR COMA0660446](https://openairdocs.org/sdr/COMA0660446.md): Sealant · defective · Jul 22, 2006 · N975CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > ENROUTE, THE MLG INTRANSIT SYMBOLS PULSED APPROXIMATELY 7 TIMES, GEAR LOCKED INTO THE UP POSITION 20 SECONDS LATER. PERFORMED FUNCTIONAL TEST OF LANDING GEAR EXTENSION/RETRACTION SYSTEM, NO DISCREPANCIES NOTED. REPLACED SEALANT FOR THE FORWARD MLG FAIRING.
- [SDR COMA0660277](https://openairdocs.org/sdr/COMA0660277.md): Warning Message · illuminated · Mar 24, 2006 · N975CA · Cndair CL6002B19 · Engine Thrust Reverser
  > FLIGHT 5676 - DURING TAKEOFF ROLL RECEIVED A LEFT THRUST REVERSER UNLOCK MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. DEFERRED THE LEFT THRUST REVERSER PER MEL 78-30-01.
- [SDR COMA0660199](https://openairdocs.org/sdr/COMA0660199.md): Flap System · malfunctioned · Feb 27, 2006 · N975CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5507 - DURING LGA APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE ZERO 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 COMA0660163](https://openairdocs.org/sdr/COMA0660163.md): Flap · malfunctioned · Feb 19, 2006 · N975CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5910 - AFTER LANDING AT MSP AND DURING TAXI TO THE GATE RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 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 WI
- [SDR COMA0560612](https://openairdocs.org/sdr/COMA0560612.md): Indicator · reads low · Nov 16, 2005 · N975CA · Cndair CL6002B19 · Engine Fuel Indicating System
  > FLIGHT 5464 - LEFT ENGINE FUEL FLOW 400 LBS, 1000 LBS NORMAL. OPERATIONAL CHECK OF FUEL FLOW WAS NORMAL.
- [SDR COMA0560590](https://openairdocs.org/sdr/COMA0560590.md): Flap System · malfunctioned · Nov 8, 2005 · N975CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5384 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
- [SDR COMA0560551](https://openairdocs.org/sdr/COMA0560551.md): Control Unit · malfunctioned · Oct 12, 2005 · N975CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5033 - FLAPS FAIL CAUTION. REPLACED THE FECU.
- [SDR COMA0560406](https://openairdocs.org/sdr/COMA0560406.md): Flap System · malfunctioned · Jul 24, 2005 · N975CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5497- FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
- [SDR COMA0560241](https://openairdocs.org/sdr/COMA0560241.md): Pump · faulty · Apr 3, 2005 · N975CA · Cndair CL6002B19 · Hydraulic Pressure Indicator
  > FLIGHT 5886 DURING CRUISE FLIGHT RECEIVED A LOW HYDRAULIC NR 3 SYSTEM PRESSURE CAUTION, CREW DECLARED AN EMERGENCY AND LANDED AT JFK WITHOUT INCIDENT. REPLACED HYDRAULIC PUMP 3A.
- [SDR COMA0460695](https://openairdocs.org/sdr/COMA0460695.md): Angle · corroded · Dec 17, 2004 · N975CA · Cndair CL6002B19 · Passenger/Crew Doors
  > FLIGHT DURING HEAVY MAINTENANCE CHECK, (PAX DOOR DETAILED INSPECTION) THE PAX DOOR FORWARD AND AFT BOTTOM CORNERS WERE FOUND TO BE CORRODED. BOTH PARTS WERE REPLACED IN ACCORDANCE WITH SRM STANDARD PROCEDURES.
- [SDR COMA0460629](https://openairdocs.org/sdr/COMA0460629.md): Wire Harness · damaged · Nov 17, 2004 · N975CA · Cndair CL6002B19 · Landing Gear System Wiring
  > FLIGHT 5806 RECEIVED AN ANTI-SKID CAUTION MESSAGE DURING TAKEOFF ROLL. ABORTED AND AIRCRAFT RETURNED TO THE GATE. REPLACED THE RIGHT OUTBOARD ANTI-SKID DETECTOR WIRING HARNESS.
- [SDR COMA0460425](https://openairdocs.org/sdr/COMA0460425.md): Ecu · malfunctioned · Jul 24, 2004 · N975CA · Cndair CL6002B19 · Landing Gear Steering System
  > FLIGHT 5801 NW STEERING INOP MESSAGE. REPLACED THE NWS ECU.
- [SDR COMA0460351](https://openairdocs.org/sdr/COMA0460351.md): Inlet · eroded · Jun 4, 2004 · N975CA · Cndair CL6002B19 · Engine Air Intake System
  > RT HAND ENGINE HEATED IN-LIT LIP ERRODED OUT OF LIMITS. REPAIRED RIGHT HAND ENGINE LIP-SKIN USING SERVICEABLE SKIN, 12.5 SECTION IAW SHORTS CMM 71-61-01.
- [SDR COMA0460144](https://openairdocs.org/sdr/COMA0460144.md): Warning Light · illuminated · Feb 14, 2004 · N975CA · Cndair CL6002B19 · Engine Thrust Reverser
  > FLIGHT 5473 RT THRUST REVERSER UNLOCKED MESSAGE. DEFERRED MAINT. IAW MEL.
- [SDR COMA0360507](https://openairdocs.org/sdr/COMA0360507.md): Actuator · malfunctioned · Nov 18, 2003 · N975CA · Cndair CL6002B19 · Elevator Control System
  > ELEVATOR CONTROLS STIFF. REPLACED THE LEFT ELEVATOR PITCH FEEL ACTUATOR.
- [SDR COMA0360048](https://openairdocs.org/sdr/COMA0360048.md): Light · Jan 23, 2003 · N975CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5530 EMERGENCY FLOOR LIGHTS AT WING EXITS ARE INOP.FOUND LIGHTS DISCONNECTED - RECONNECTED WIRING AT EXIT LIGHTS.
- [SDR COMA0260361](https://openairdocs.org/sdr/COMA0260361.md): Hydraulic Line · leaking · Jun 8, 2002 · N975CA · Cndair CL6002B19 · Hydraulic System, Main
  > FLIGHT 6657 #1 HYDRAULIC SYSTEM INDICATING ZERO PRESSURE AND ZERO QUANTITY.REPLACED THE HYDRAULIC LINES AT THE LT ENGINE TO PYLON INTERFACE.
- [SDR COMA0260358](https://openairdocs.org/sdr/COMA0260358.md): Selector Valve · malfunctioned · Jun 6, 2002 · N975CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > FLIGHT 5882 GEAR DISAGREE WARNING, NLG DID NOT EXTEND - USED MANUAL EXTENSION.REPLACED THE NLG SELECTOR VALVE.
- [SDR COMA0260291](https://openairdocs.org/sdr/COMA0260291.md): Skin · cracked · Apr 29, 2002 · N975CA · Cndair CL6002B19 · Wing, Plate/Skin
  > CRACK FOUND ON RT LOWER WING PLANK AT PANEL 650GB.REPAIRED IAW 601R-57-21-030.
- [SDR COMA0260113](https://openairdocs.org/sdr/COMA0260113.md): Landing Gear · Feb 19, 2002 · N975CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > FLIGHT 5032 NLG DID NOT EXTEND, GEAR DISAGREE WARNING. USED MANUAL EXTENSION SYSTEM.COULD NOT DUPLICATE - INSPECTED NLG AND FOUND NO DEFECTS.
- [SDR COMA0160972](https://openairdocs.org/sdr/COMA0160972.md): Proximity Switch · Dec 17, 2001 · N975CA · Cndair CL6002B19 · Nose/Tail Landing Gear
  > FLIGHT 5970 - CONFIG OK MESSAGE WENT OUT DURING T/O.REMOVED DIRT FROM NLG PROX SWITCHES.
- [SDR COMA0160579](https://openairdocs.org/sdr/COMA0160579.md): Web · cracked · Aug 8, 2001 · N975CA · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > CRACKS FOUND ON LEFT HAND AND RIGHT HAND LOWER WEBS OF ENGINE SUPPORT BEAM F.S. 625.30.REPAIRED LEFT HAND AND RIGHT HAND LOWER WEBS OF ENGINE SUPPORT BEAM I/A/W CANADAIR REO 601R-53-61-366 REV C.
- [SDR COMA0160568](https://openairdocs.org/sdr/COMA0160568.md): Angle · corroded · Aug 6, 2001 · N975CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THE FWD J ANGLE AT F.S. 280 BETWEEN LBL9.0 AND RBL9.0 IS CORRODED.REMOVED AND REPLACED THE FWD J ANGLE AT FS 280 BETWEEN LBL9.0 AND RBL9.0 P/N 600-34017-351 I/A/W WVAC E.O. 601R-53-2624.
- [SDR COMA0160161](https://openairdocs.org/sdr/COMA0160161.md): Computer · malfunctioned · Jan 24, 2001 · N975CA · Cndair CL6002B19 · Stall Warning System
  > STALL FAIL CAUTION DURING T/O. RESET THE STALL COMPUTER.
- [SDR COMA0160158](https://openairdocs.org/sdr/COMA0160158.md): Computer · malfunctioned · Jan 23, 2001 · N975CA · Cndair CL6002B19 · Stall Warning System
  > STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER.
- [SDR COMA0160061](https://openairdocs.org/sdr/COMA0160061.md): Computer · malfunctioned · Jan 3, 2001 · N975CA · Cndair CL6002B19 · Stall Warning System
  > STALL FAIL CAUTION DURING T/O. RESET THE STALL COMPUTER.
- [SDR COMA0160035](https://openairdocs.org/sdr/COMA0160035.md): Computer · malfunctioned · Dec 30, 2000 · N975CA · Cndair CL6002B19 · Stall Warning System
  > STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER.
- [SDR COMA0061056](https://openairdocs.org/sdr/COMA0061056.md): Pump · failed · Dec 14, 2000 · N975CA · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main
  > Left engine low hydraulic pressure message. Replace the left engine hydraulic pump.
- [SDR COMA0061016](https://openairdocs.org/sdr/COMA0061016.md): Angle · cracked · Dec 6, 2000 · N975CA · Cndair CL6002B19 · Fuselage Main, Structure
  > FS 621.00 FLOOR ATTACHMENT ANGLE IS CRACKED ON RIGHT HAND SIDE. PERFORMED A MAJOR REPAIR BY REPLACING CRACKED FLOOR SUPPORT ANGLE AT FS 621.0 RIGHT HAND SIDE IAW CRJ REO 601R-53-61-004B.
- [SDR COMA0061009](https://openairdocs.org/sdr/COMA0061009.md): Floorbeam · cracked · Dec 6, 2000 · N975CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > F.S. 621.00 FLOOR ATTACH ANGLE IS CRACKED RT SIDE. REMOVE AND REPLACED RT SIDE F.S. 621.00 FLOOR ATTACH ANGLE I/A/W CANADAIR S/B 601R-53-018.
- [SDR COMA0061010](https://openairdocs.org/sdr/COMA0061010.md): Angle · cracked · Dec 2, 2000 · N975CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR SEAL STRIKER AT F.S. 349.00 CRACKED. FURTHER INVESTIGATION FOUND PREVIOUS REPAIR AND ONLY SEALANT TO BE CRACKED. REMOVED OLD SEALANT AND REAPPLIED AERODYNAMIC FILLER EO 1751 B/A IAW REO 601R-52-11-008 REV B PART 4.
- [SDR COMA0060986](https://openairdocs.org/sdr/COMA0060986.md): Angle · cracked · Dec 2, 2000 · N975CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > UNDER FLOOR ANGLES ARE CRACKED AT RBL27 AND LBL27 F.S. 484.0 REMOVED CRACKED ANGLES. FABRICATED NEW ANGLES FROM S6144-4 AND INSTALLED NEW ANGLES IAW WVAC EO 601R-53-1978.
- [SDR COMA0060984](https://openairdocs.org/sdr/COMA0060984.md): Angle · cracked · Dec 2, 2000 · N975CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR SEAL STRIKER AT F.S. 349.00 CRACKED. REMOVED OLD SEALANT AND REAPPLIED AERODYNAMIC FILLER EC 1751 B/A IAW REO 601R-52-11-008 REV B PART 4.
- [SDR COMA0060794](https://openairdocs.org/sdr/COMA0060794.md): Controller · malfunctioned · Oct 1, 2000 · N975CA · Cndair CL6002B19 · Detection System
  > CARGO SMOKE WARNING FIRE BOTTLES DISCHARGED. REPLACED FIRE DETECTION CONTROLLER.
- [SDR COMA0060387](https://openairdocs.org/sdr/COMA0060387.md): Warning System · activated · Apr 27, 2000 · N975CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
- [SDR COMA0060298](https://openairdocs.org/sdr/COMA0060298.md): Sign · inoperative · Mar 30, 2000 · N975CA · Cndair CL6002B19 · Emergency Lighting
  > EXIT SIGN AT CABIN DOOR IS INOPERABLE. REPLACED EXIT SIGN.
- [SDR COMA0060007](https://openairdocs.org/sdr/COMA0060007.md): Warning System · illuminated · Dec 27, 1999 · N975CA · Cndair CL6002B19 · Central Warning
  > LEFT WINDOW HEAT CAUTION MESSAGE. COULD NOT DUPLICATE, OPERATIONAL CHECK OF WINDOW HEAT SATISFACTORY.
- [SDR COMA9960727](https://openairdocs.org/sdr/COMA9960727.md): Frame · cracked · Nov 27, 1999 · N975CA · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 718.00 LEFT HAND AND RIGHT HAND FRAMES AND AFT DOUBLERS WERE CRACKED STR 10-12. REPAIRED LEFT HAND AND RIGHT HAND FRAMES AND AFT DOUBLER IAW CANADAIR REO 601R-53-61-193A.
- [SDR COMA9960495](https://openairdocs.org/sdr/COMA9960495.md): Bulb · failed · Sep 8, 1999 · N975CA · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT ROW 2 IS INOPERABLE. REPLACED LIGHT BULB.
- [SDR COMA9960450](https://openairdocs.org/sdr/COMA9960450.md): Actuator · malfunctioned · Aug 11, 1999 · N975CA · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLAPS FAILED AT 8 DEGREES. REPLACED THE RIGHT OUTBOARD FLAP ACTUATORS.
- [SDR COMA9960439](https://openairdocs.org/sdr/COMA9960439.md): Pdu · malfunction · Aug 10, 1999 · N975CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL MESSAGE. REPLACED THE PDU.
- [SDR COMA9960420](https://openairdocs.org/sdr/COMA9960420.md): Fail Message · activated · Aug 8, 1999 · N975CA · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLAPS FAIL MESSAGE. RESET FLAP SYSTEM IAW AD 98 20 01.
- [SDR COMA9960417](https://openairdocs.org/sdr/COMA9960417.md): Bpsu · out of adjust · Aug 3, 1999 · N975CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL MESSAGE. C/W RIGGING OF LEFT AND RIGHT BPSU.
- [SDR COMA9960333](https://openairdocs.org/sdr/COMA9960333.md): Pseu · malfunctioned · Jun 29, 1999 · N975CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE AND PROX SYSTEM FAULT MESSAGE. REPLACED THE PSEU.
- [SDR COMA9960276](https://openairdocs.org/sdr/COMA9960276.md): Valve · malfunctioned · Jun 15, 1999 · N975CA · Cndair CL6002B19 · Landing Gear Brake System
  > LOUD SQUEAL FROM NOSE AREA WHEN RIGHT BRAKE APPLIED. REMOVED AND REPLACED NR 2 BRAKE CONTROL VALVE.

Next page: https://openairdocs.org/deregistered/N975CA-2008-07-16/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 = 'N975CA' AND deregistration_id = 'N975CA-2008-07-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N975CA-2008-07-16/reports

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