# Service difficulty reports: N952CA, cancelled May 5, 2008

A list on [N952CA, cancelled May 5, 2008](https://openairdocs.org/deregistered/N952CA-2008-05-05.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 · 77 reports

- [SDR COMA0660313](https://openairdocs.org/sdr/COMA0660313.md): Pitot Tube · contaminated · Apr 25, 2006 · N952CA · Cndair CL6002B19 · Airspeed/Mach Indicator
  > FLIGHT 5288 - ON TAKEOFF ROLL OBSERVED NO STANDBY INDICATION. TAKEOFF ABORTED. A/C FERRIED FROM YHZ TO CVG. PURGED WATER FROM STANDBY PITOT SYSTEM.
- [SDR COMA0660232](https://openairdocs.org/sdr/COMA0660232.md): Reducer · faulty · Mar 6, 2006 · N952CA · Cndair CL6002B19 · Waste Disposal System
  > FLIGHT 5145 - EN ROUTE CVG-AVP A NUISANCE SQUEALING NOISE EMITTING FROM GALLEY AREA, FLIGHT RETURNED TO THE FIELD. REPLACED THE GALLEY DRAIN REDUCER.
- [SDR COMA0660139](https://openairdocs.org/sdr/COMA0660139.md): Flap System · malfunctioned · Feb 12, 2006 · N952CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5802 - UPON FLAP RETRACTION DURING PRE-FLIGHT INSPECTION RECEIVED A FLAP FAIL CAUTION MESSAGE. 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 WITH NO FURTHE
- [SDR COMA0560566](https://openairdocs.org/sdr/COMA0560566.md): Wire · broken · Oct 25, 2005 · N952CA · Cndair CL6002B19 · Flight Control System Wiring
  > FLAPS FAIL CAUTION. REPAIRED BROKEN WIRE AT THE LT BPSU.
- [SDR COMA0460611](https://openairdocs.org/sdr/COMA0460611.md): Apu · shutdown · Oct 31, 2004 · N952CA · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) System
  > FLIGHT 5028 APU SHUTDOWN. COULD NOT DUPLICATE. APU OPERATIONAL CHECK SATISFACTORY.
- [SDR COMA0460513](https://openairdocs.org/sdr/COMA0460513.md): Connector · loose · Sep 9, 2004 · N952CA · Cndair CL6002B19 · Emergency Lighting
  > 1ST SEGMENT OF EMERGENCY FLOOR PATH LIGHTING IS INOPERATIVE. SECURED LOOSE CONNECTOR. SYSTEM OPERATION NORMAL.
- [SDR COMA0460063](https://openairdocs.org/sdr/COMA0460063.md): Skin · corroded · Jan 17, 2004 · N952CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > RIGHT SIDE CABIN FLOOR SIL ASSY HAS CORROSION ON TOP SURFACE FROM FS 516 THRU 544. CLEANED CORRODED AREA BY BLENDING OUT CORROSION. CUT OUT AREA THAT WAS OUT OF LIMITS AND FABRICATED AND INSTALLED REPAIR PARTS. TREATED AND PAINTED ENTIRE WORK AEA IAW REO 60
- [SDR COMA0460051](https://openairdocs.org/sdr/COMA0460051.md): Skin · corroded · Jan 15, 2004 · N952CA · Cndair CL6002B19 · Wing, Plate/Skin
  > WHILE PERFORMING TASK 002-57-900-60/601 FOUND CORROSION ON THE LOWER RT WING PLANK ACCESS HOLE CUTOUT (FOR PANEL 640BB) ON THE FORWAD AND AFT CHAMFERS. REMOVED THE CORROSION AND APPLIED SURFACE TREATMENT IAW REO 601R-57-21-030 REV C.
- [SDR COMA0460047](https://openairdocs.org/sdr/COMA0460047.md): Stiffener · cracked · Jan 14, 2004 · N952CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > VERTICAL BEAM CRACKED AT BL 0 BULKHEAD WEB AT FS 409+128 TOP RIVET LOCATION ON REINFORCING PLATE. PERFORMED A MAJOR REPAIR TO CRACKED VERTICAL BEAM, FS 409+128 BL 0 (TOP RIVET ON REINFORCING PLATE) BY TRIMMING OUT CRACKED PORTION OF STIFFENER, FABBING FILLER
- [SDR COMA0460045](https://openairdocs.org/sdr/COMA0460045.md): Floorbeam · corroded · Jan 14, 2004 · N952CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CAP AT FS 559+12 TO 620 AT LBL 27 CORRODED. REMOVED AND REPLACED CAP IAW WVAC EO 601R-53-4581.
- [SDR COMA0460044](https://openairdocs.org/sdr/COMA0460044.md): Angle · cracked · Jan 14, 2004 · N952CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 484 RBL 27, OUTBOARD SUPPORT ANGLE/INTERCOSTAL CRACKED. REMOVED ANGLE FABRICATED REPAIR ANGLE FROM 2024-T3.063 (WVAC PO 32572) AND INSTALLED IAW BOMBARDIER REO 601R-53-41-059.
- [SDR COMA0460043](https://openairdocs.org/sdr/COMA0460043.md): Angle · cracked · Jan 14, 2004 · N952CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 484 LBL 27 OUTBOARD SUPPORT ANGLE/INTERCOSTAL CRACKED. REMOVED ANGLE, FABRICATED REPAIR ANGLE FROM 2024-T3.063 (WVAC PO 32572) AND INSTALLED IAW BOMBARDIER, INC REO 601R-53-41-059.
- [SDR COMA0460042](https://openairdocs.org/sdr/COMA0460042.md): Angle · cracked · Jan 14, 2004 · N952CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 484 RBL 36 INBOARD SUPPORT ANGLE/INTERCOSTAL CRACKED. REMOVED ANGLE, FABRICATED REPAIR ANGLE FROM 2024-T3.063 (WVAC PO 32572) AND INSTALLED IAW BOMBARDIER, INC REO 601R-53-41-059.
- [SDR COMA0460041](https://openairdocs.org/sdr/COMA0460041.md): Angle · cracked · Jan 14, 2004 · N952CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 484 LBL 36 INBOARD SUPPORT ANGLE/INTERCOSTAL CRACKED. REMOVED ANGLE, FABRICATED REPAIR ANGLE FROM 2024-T3.063 (WVAC PO 32572) AND INSTALLED IAW BOMBARDIER, INC. REO601R-53-41-059.
- [SDR COMA0460040](https://openairdocs.org/sdr/COMA0460040.md): Skin · cracked · Jan 14, 2004 · N952CA · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING LOWER WING PLANK SKIN AT WS 148.00 IS CRACKED. REMOVED DAMAGE, FABRICATED REPAIR DOUBLERS FROM 2024-T3.125 (WVAC PO 21137) AND FILLER FROM 2024-T3.100 (WVAC PO 27013), INSTALLED IAW BOMBARDIER, INC REO 601R-57-21-120 REV D.
- [SDR COMA0460039](https://openairdocs.org/sdr/COMA0460039.md): Skin · damaged · Jan 14, 2004 · N952CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FS 310 FUSELAGE SKIN PREVIOUS BETYWEEN STRINGERS 16 AND 17 HAS SUSTAINED FURTHER DAMAGE. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER FROM 2024-T3.063 (WVAC PO 32512) AND 2024-T3.050 (WVAC PO 29669/1), INSTALLED IAW BOMBARDIER, INC REO 601R-53-21-180.
- [SDR COMA0460038](https://openairdocs.org/sdr/COMA0460038.md): Skin · cracked · Jan 14, 2004 · N952CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FS 235 RBL 6 NLG AFT DOOR CUT OUT HAS A.25 INCH CRACK ON FUSELAGE SKIN. REMOVED DAMAGE, FABRICATED REPAIR ANGLE FROM 2024-T42.063 (WVAC PO 169562), FILLER FROM 2024-T3.050 (WVAC PO 32674), FILLER AND DOUBLER FROM 2024-T3.063 (WVAC PO 32572) AND INSTALLED IA
- [SDR COMA0460012](https://openairdocs.org/sdr/COMA0460012.md): Element · unreliable · Jan 2, 2004 · N952CA · Cndair CL6002B19 · Overheat Detection
  > FLIGHT 5874 LEFT 14TH STAGE BLEED LEAK WARNING. REPLACED THE LEFT PYLON BLEED LEAK SENSING ELEMENT.
- [SDR COMA0360382](https://openairdocs.org/sdr/COMA0360382.md): Start Valve · malfunctioned · Aug 21, 2003 · N952CA · Cndair CL6002B19 · Engine Cranking
  > FLIGHT 5868 RT ENGINE STARTER ENGAGED DURING FLIGHT 3 TIMES. REPLACED THE AIR START VALVE.
- [SDR COMA0360230](https://openairdocs.org/sdr/COMA0360230.md): Target · out of adjust · May 4, 2003 · N952CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > LANDING GEAR DISAGREE WARNING; NLG DID NOT RETRACT. ADJUSTED THE NLG CENTERED PROXIMITY SENSOR TARGET.
- [SDR COMA0360108](https://openairdocs.org/sdr/COMA0360108.md): Shaft · bent · Feb 18, 2003 · N952CA · Cndair CL6002B19 · Passenger/Crew Doors
  > FLIGHT 5751 CABIN DOOR WARNING.COULD NOT DUPLICATE. REPLACED INNER HANDLE ROD END ROLLER.
- [SDR COMA0360072](https://openairdocs.org/sdr/COMA0360072.md): Target · loose · Feb 3, 2003 · N952CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > FLIGHT 5156 GEAR DISAGREE WARNING.TIGHTENED LOOSE TARGET ONTHE L/H MLG UPLOCK.
- [SDR COMA0360055](https://openairdocs.org/sdr/COMA0360055.md): Door · Jan 26, 2003 · N952CA · Cndair CL6002B19 · Emergency Exits
  > FLIGHT 5850 DURING T/O A LARGE AMOUNT OF FLUID DRAINED FROM THE LIGHT CONTROL PANEL.RESEALED THE CREW DITCHING HATCH.
- [SDR COMA0260689](https://openairdocs.org/sdr/COMA0260689.md): Door Latch · Dec 2, 2002 · N952CA · Cndair CL6002B19 · Passenger/Crew Doors
  > FLIGHT 5103 CABIN DOOR WARNING DURING FLIGHT.ADJUSTED CABIN DOOR LATCH MECHANISM.
- [SDR COMA0260680](https://openairdocs.org/sdr/COMA0260680.md): Door · Nov 29, 2002 · N952CA · Cndair CL6002B19 · Passenger/Crew Doors
  > FLIGHT 5478 CABIN DOOR WARNING MESSAGE.RIGGED/ADJUSTED THE CABIN DORO LATCHING MECHANISM TO M/M SPECIFICATIONS.
- [SDR COMA0260678](https://openairdocs.org/sdr/COMA0260678.md): Roller · worn · Nov 27, 2002 · N952CA · Cndair CL6002B19 · Passenger/Crew Doors
  > FLIGHT 5465 CABIN DOOR LATCH CAUTION MESSAGE.REPLACED THE INNER HANDLE LATCH ROLLER.
- [SDR COMA0260672](https://openairdocs.org/sdr/COMA0260672.md): Proximity Switch · malfunctioned · Nov 26, 2002 · N952CA · Cndair CL6002B19 · Door Warning System
  > FLIGHT 5863 CABIN DOOR WARNING.REPLACED PROXIMITY SWITCH 546.
- [SDR COMA0260649](https://openairdocs.org/sdr/COMA0260649.md): Rod · broken · Nov 16, 2002 · N952CA · Cndair CL6002B19 · Main Landing Gear
  > FLIGHT 5459 CABIN ALTITUDE CAUTION MESSAGE - CABIN WOULD NOT PRESSURIZE.REPLACED BROKEN ROD ON CABIN DOOR VENT VALVE.
- [SDR COMA0260355](https://openairdocs.org/sdr/COMA0260355.md): Landing Gear · Jun 4, 2002 · N952CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > FLIGHT 5494 NOSE GEAR DISAGREE WARNING. NLG UNSAFE INDICATION.INSPECTED NLG AND PERFORMED EXT AND RETRACTION CHECKS. NO FAULTS FOUND.
- [SDR COMA0260245](https://openairdocs.org/sdr/COMA0260245.md): Igniter · inoperative · Apr 10, 2002 · N952CA · Cndair CL6002B19 · Spark Plug/Igniter
  > FLIGHT 5877 LEFT ENGINE IGNITION STATUS MESSAGE.REPALCED THE ENGINE IGNITERS.
- [SDR COMA0260239](https://openairdocs.org/sdr/COMA0260239.md): Aileron · Apr 6, 2002 · N952CA · Cndair CL6002B19 · Aileron Control System
  > FLIGHT 6066 AILERON CONFIG WARNING DURING T/O.COULD NOT DUPLICATE. INSPECTED AILERON SYSTEM - NO ABNORMALTY FOUND.
- [SDR COMA0260120](https://openairdocs.org/sdr/COMA0260120.md): Pylon · corroded · Feb 26, 2002 · N952CA · Cndair CL6002B19 · Nacelle/Pylon, Attach Fittings
  > DURING REMOVAL OF THE RIGHT ENGINE ASSEMBLY, DISCOVERED FRETTING/PITTING CORROSION ON THE AFT ENGINE PYLON THRUST FITTING MOUNTING VIB.REPAIRED IN ACCORDANCE WITH REO 601R-54-50-036.
- [SDR COMA0260083](https://openairdocs.org/sdr/COMA0260083.md): Bushing · scored · Feb 1, 2002 · N952CA · Cndair CL6002B19 · Vertical Stabilizer
  > THE R/H VERTICAL STABILIZER BUSHING WAS SCORED AT HORIZONTAL STABILIZER PIVOT POINT.REMOVED THE SCORED BUSHING. MACHINED FLANGE OF NEW BUSHING P/N 600-21061-7S/B I/A/W WVAC EO 601R-55-2952.INSTALLED THE NEW BUSHING I/A/W CRJ AMM 20-26-00-910-803. REAMED THE B
- [SDR COMA0160933](https://openairdocs.org/sdr/COMA0160933.md): Switch · malfunctioned · Nov 27, 2001 · N952CA · Cndair CL6002B19 · Stabilizer Control System
  > FLIGHT #5843. COPILOTS STABILIZER TRIM IS INTERMITTENT.REPLACED THE COPILOTS TRIM SWITCH.
- [SDR COMA0160709](https://openairdocs.org/sdr/COMA0160709.md): Radome · Sep 10, 2001 · N952CA · Cndair CL6002B19 · Fuselage Structure (General)
  > FLIGHT #5420. DURING TAKE OFF AT CVG AIRCRAFT ENCOUNTERED MULTIPLE BIRD STRIKES ON RADOME, TAKE OFF WAS ABORTED AND RETURNED TO THE GATE.PERFORMED BIRD STRIKE AND HIGH ENERGY STOP INSPECTION, NO DEFECTS NOTES.
- [SDR COMA0160329](https://openairdocs.org/sdr/COMA0160329.md): Skin · cracked · Mar 18, 2001 · N952CA · Cndair CL6002B19 · Wing, Plate/Skin
  > RT LOWER WING PLANK CRACKED AT 2 LOCATIONS: 640 DB WS 95.950 AND 640 FB WS 136.676. BLENDED OUT DAMAGED AREAS AND ROTO-PEENED IAW REO 601R-57-21-030.
- [SDR COMA0061074](https://openairdocs.org/sdr/COMA0061074.md): Harness · failed · Dec 26, 2000 · N952CA · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > DURING CLIMB-OUT OF CVG, THE NR 1 AND 3 HYDRAULIC LOW PRESSURE CAUTION MESSAGES ACTIVATED, AIRCRAFT RETURNED TO THE FIELD. REPLACED THE FLAP POSITION HARNESS.
- [SDR COMA0060983](https://openairdocs.org/sdr/COMA0060983.md): Seal · damaged · Dec 2, 2000 · N952CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR LEAKS DURING PRESURIZATION. RECONTOURED ADHESIVE FILLER AT PREVIOUS REPAIR ON PAX DOOR SEAL STRIKER FS 349 IAW REO 601R-52-11-008 REV B.
- [SDR COMA0060873](https://openairdocs.org/sdr/COMA0060873.md): Computer · false activation · Oct 31, 2000 · N952CA · Cndair CL6002B19 · Stall Warning System
  > STALL FAIL MESSAGE DURING TAKEOFF. RESET THE STALL COMPUTER.
- [SDR COMA0060834](https://openairdocs.org/sdr/COMA0060834.md): Control Unit · malfunctioned · Oct 14, 2000 · N952CA · Cndair CL6002B19 · Aileron Control System
  > CONFIG AILERON WARNING MESSAGE DURING T/O. RESET SECU, COULD NOT DUPLICATE. RESET SECU NR 1 AND 2.
- [SDR COMA0060624](https://openairdocs.org/sdr/COMA0060624.md): Strut · discharged · Aug 4, 2000 · N952CA · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > GEAR DISAGREE WARNING. WOW CAUTION MESSAGE. FOUND NLG SHOCK STRUT IMPROPERLY SERVICED. SERVICED STRUT IAW M/M.
- [SDR COMA0060565](https://openairdocs.org/sdr/COMA0060565.md): Angle · corroded · Jul 12, 2000 · N952CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THE FORWARD J-ANGLE AT FS 280 BETWEEN LBL 9.0 AND RBL 9.0 IS CORRODED. PERFORMED A MAJOR REPAIR BY REPLACING CORRODED FORWARD J-ANGLE AT FS 280 BETWEEN LBL 9.0 AND RBL 9.0 IAW WVAC EO 601R-53-1489.
- [SDR COMA0060566](https://openairdocs.org/sdr/COMA0060566.md): Doubler · corroded · Jul 11, 2000 · N952CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > THE DOUBLER (P/N 601R38669-49) FORWARD OF THE SERVICE DOOR IS CORRODED. PERFORMED A MAJOR REPAIR BY REPLACING CORRODED DOUBLER (P/N 601R38669-49) FORWARD OF THE SERVICE DOOR IAW WVAC EO 601R-53-1504.
- [SDR COMA0060554](https://openairdocs.org/sdr/COMA0060554.md): Beam · corroded · Jul 8, 2000 · N952CA · Cndair CL6002B19 · Fuselage Main, Structure
  > TRANSVERSE BEAM AT FS 349 CORRODED BETWEEN LBL 9 AND LBL 27. REPAIRED TRANSVERSE BEAM AT FS 349 IAW WVAC EO 601R-53-1491A.
- [SDR COMA0060478](https://openairdocs.org/sdr/COMA0060478.md): Aileron · sluggish · Jun 6, 2000 · N952CA · Cndair CL6002B19 · Aileron Control System
  > A/P TRIM CAUTION MESSAGE. LITTLE TO NO CONTROL OF AILERONS. ELEVATORS ALSO EXTREMELY DIFFICULT TO MOVE. COULD NOT DUPLICATE. INSPECTED ALL FLIGHT CONTROLS AND CABLE RUNS. COMPLIED WITH FUNCTIONAL AND OPERATIONAL TEST OF AILERONS AND ELEVATORS. NO DEFECTS
- [SDR COMA0060290](https://openairdocs.org/sdr/COMA0060290.md): Lead · defective · Mar 26, 2000 · N952CA · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY FLOOR PATH LIGHTING AT ROW 8 IS INOPERABLE. REPLACED POWER LEAD.
- [SDR COMA0060264](https://openairdocs.org/sdr/COMA0060264.md): Latch · out of adj · Mar 12, 2000 · N952CA · Cndair CL6002B19 · Passenger/Crew Doors
  > CABIN DOOR LATCH CAUTION MESSAGE. ADJUSTED CABIN DOOR LATCH MECHANISM.
- [SDR COMA0060191](https://openairdocs.org/sdr/COMA0060191.md): Computer · cockpit · Feb 22, 2000 · N952CA · Cndair CL6002B19 · Stall Warning System
  > STALL FAIL CAUTION MESSAGE. RESET STALL COMPUTER, SYSTEM TEST NORMAL.
- [SDR COMA9960744](https://openairdocs.org/sdr/COMA9960744.md): Skin · crack · Dec 5, 1999 · N952CA · Cndair CL6002B19 · Wing, Plate/Skin
  > LOWER HORIZONTAL SURFACE OF RIGHT LOWER WING ACCESS HOLE AT 640DB CRACKED. BLENDED OUT DAMAGE, ROTO-PEENED, AND ALODINED IAW REO 601R-57-21-030.
- [SDR COMA9960681](https://openairdocs.org/sdr/COMA9960681.md): Doubler · cracked · Nov 6, 1999 · N952CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 718 RH5 AFT DOUBLER IS CRACKED BETWEEN STR 11-12. REPLACED CRACKED DOUBLER AT FS 718 RHS BETWEEN STR 11 AND 12 WITH NEW DOUBLERS IAW CRJ REO 601R-53-61-193.

Next page: https://openairdocs.org/deregistered/N952CA-2008-05-05/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 = 'N952CA' AND deregistration_id = 'N952CA-2008-05-05'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N952CA-2008-05-05/reports

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