N952CA, cancelled May 5, 2008

Service difficulty reports · 77

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR COMA0660313Pitot Tube · contaminatedFLIGHT 5288 - ON TAKEOFF ROLL OBSERVED NO STANDBY INDICATION. TAKEOFF ABORTED. A/C FERRIED FROM YHZ TO CVG. PURGED WATER FROM STANDBY PITOT SYSTEM.Apr 25, 2006 · N952CA · Cndair CL6002B19 · Airspeed/Mach IndicatorSDR COMA0660232Reducer · faultyFLIGHT 5145 - EN ROUTE CVG-AVP A NUISANCE SQUEALING NOISE EMITTING FROM GALLEY AREA, FLIGHT RETURNED TO THE FIELD. REPLACED THE GALLEY DRAIN REDUCER.Mar 6, 2006 · N952CA · Cndair CL6002B19 · Waste Disposal SystemSDR COMA0660139Flap System · malfunctionedFLIGHT 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 FURTHEFeb 12, 2006 · N952CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0560566Wire · brokenFLAPS FAIL CAUTION. REPAIRED BROKEN WIRE AT THE LT BPSU.Oct 25, 2005 · N952CA · Cndair CL6002B19 · Flight Control System WiringSDR COMA0460611Apu · shutdownFLIGHT 5028 APU SHUTDOWN. COULD NOT DUPLICATE. APU OPERATIONAL CHECK SATISFACTORY.Oct 31, 2004 · N952CA · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) SystemSDR COMA0460513Connector · loose1ST SEGMENT OF EMERGENCY FLOOR PATH LIGHTING IS INOPERATIVE. SECURED LOOSE CONNECTOR. SYSTEM OPERATION NORMAL.Sep 9, 2004 · N952CA · Cndair CL6002B19 · Emergency LightingSDR COMA0460063Skin · corrodedRIGHT 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 60Jan 17, 2004 · N952CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR COMA0460051Skin · corrodedWHILE 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.Jan 15, 2004 · N952CA · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA0460047Stiffener · crackedVERTICAL 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 Jan 14, 2004 · N952CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0460045Floorbeam · corrodedFLOORBEAM CAP AT FS 559+12 TO 620 AT LBL 27 CORRODED. REMOVED AND REPLACED CAP IAW WVAC EO 601R-53-4581.Jan 14, 2004 · N952CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR COMA0460044Angle · crackedFS 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.Jan 14, 2004 · N952CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0460043Angle · crackedFS 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.Jan 14, 2004 · N952CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0460042Angle · crackedFS 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.Jan 14, 2004 · N952CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0460041Angle · crackedFS 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.Jan 14, 2004 · N952CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0460040Skin · crackedLEFT 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.Jan 14, 2004 · N952CA · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA0460039Skin · damagedFS 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.Jan 14, 2004 · N952CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR COMA0460038Skin · crackedFS 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 IAJan 14, 2004 · N952CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR COMA0460012Element · unreliableFLIGHT 5874 LEFT 14TH STAGE BLEED LEAK WARNING. REPLACED THE LEFT PYLON BLEED LEAK SENSING ELEMENT.Jan 2, 2004 · N952CA · Cndair CL6002B19 · Overheat DetectionSDR COMA0360382Start Valve · malfunctionedFLIGHT 5868 RT ENGINE STARTER ENGAGED DURING FLIGHT 3 TIMES. REPLACED THE AIR START VALVE.Aug 21, 2003 · N952CA · Cndair CL6002B19 · Engine CrankingSDR COMA0360230Target · out of adjustLANDING GEAR DISAGREE WARNING; NLG DID NOT RETRACT. ADJUSTED THE NLG CENTERED PROXIMITY SENSOR TARGET.May 4, 2003 · N952CA · Cndair CL6002B19 · Landing Gear Position and WarningSDR COMA0360108Shaft · bentFLIGHT 5751 CABIN DOOR WARNING.COULD NOT DUPLICATE. REPLACED INNER HANDLE ROD END ROLLER.Feb 18, 2003 · N952CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0360072Target · looseFLIGHT 5156 GEAR DISAGREE WARNING.TIGHTENED LOOSE TARGET ONTHE L/H MLG UPLOCK.Feb 3, 2003 · N952CA · Cndair CL6002B19 · Landing Gear Position and WarningSDR COMA0360055DoorFLIGHT 5850 DURING T/O A LARGE AMOUNT OF FLUID DRAINED FROM THE LIGHT CONTROL PANEL.RESEALED THE CREW DITCHING HATCH.Jan 26, 2003 · N952CA · Cndair CL6002B19 · Emergency ExitsSDR COMA0260689Door LatchFLIGHT 5103 CABIN DOOR WARNING DURING FLIGHT.ADJUSTED CABIN DOOR LATCH MECHANISM.Dec 2, 2002 · N952CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0260680DoorFLIGHT 5478 CABIN DOOR WARNING MESSAGE.RIGGED/ADJUSTED THE CABIN DORO LATCHING MECHANISM TO M/M SPECIFICATIONS.Nov 29, 2002 · N952CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0260678Roller · wornFLIGHT 5465 CABIN DOOR LATCH CAUTION MESSAGE.REPLACED THE INNER HANDLE LATCH ROLLER.Nov 27, 2002 · N952CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0260672Proximity Switch · malfunctionedFLIGHT 5863 CABIN DOOR WARNING.REPLACED PROXIMITY SWITCH 546.Nov 26, 2002 · N952CA · Cndair CL6002B19 · Door Warning SystemSDR COMA0260649Rod · brokenFLIGHT 5459 CABIN ALTITUDE CAUTION MESSAGE - CABIN WOULD NOT PRESSURIZE.REPLACED BROKEN ROD ON CABIN DOOR VENT VALVE.Nov 16, 2002 · N952CA · Cndair CL6002B19 · Main Landing GearSDR COMA0260355Landing GearFLIGHT 5494 NOSE GEAR DISAGREE WARNING. NLG UNSAFE INDICATION.INSPECTED NLG AND PERFORMED EXT AND RETRACTION CHECKS. NO FAULTS FOUND.Jun 4, 2002 · N952CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA0260245Igniter · inoperativeFLIGHT 5877 LEFT ENGINE IGNITION STATUS MESSAGE.REPALCED THE ENGINE IGNITERS.Apr 10, 2002 · N952CA · Cndair CL6002B19 · Spark Plug/IgniterSDR COMA0260239AileronFLIGHT 6066 AILERON CONFIG WARNING DURING T/O.COULD NOT DUPLICATE. INSPECTED AILERON SYSTEM - NO ABNORMALTY FOUND.Apr 6, 2002 · N952CA · Cndair CL6002B19 · Aileron Control SystemSDR COMA0260120Pylon · corrodedDURING 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.Feb 26, 2002 · N952CA · Cndair CL6002B19 · Nacelle/Pylon, Attach FittingsSDR COMA0260083Bushing · scoredTHE 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 BFeb 1, 2002 · N952CA · Cndair CL6002B19 · Vertical StabilizerSDR COMA0160933Switch · malfunctionedFLIGHT #5843. COPILOTS STABILIZER TRIM IS INTERMITTENT.REPLACED THE COPILOTS TRIM SWITCH.Nov 27, 2001 · N952CA · Cndair CL6002B19 · Stabilizer Control SystemSDR COMA0160709RadomeFLIGHT #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.Sep 10, 2001 · N952CA · Cndair CL6002B19 · Fuselage Structure (General)SDR COMA0160329Skin · crackedRT 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.Mar 18, 2001 · N952CA · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA0061074Harness · failedDURING 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.Dec 26, 2000 · N952CA · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR COMA0060983Seal · damagedPAX 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.Dec 2, 2000 · N952CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0060873Computer · false activationSTALL FAIL MESSAGE DURING TAKEOFF. RESET THE STALL COMPUTER.Oct 31, 2000 · N952CA · Cndair CL6002B19 · Stall Warning SystemSDR COMA0060834Control Unit · malfunctionedCONFIG AILERON WARNING MESSAGE DURING T/O. RESET SECU, COULD NOT DUPLICATE. RESET SECU NR 1 AND 2.Oct 14, 2000 · N952CA · Cndair CL6002B19 · Aileron Control SystemSDR COMA0060624Strut · dischargedGEAR DISAGREE WARNING. WOW CAUTION MESSAGE. FOUND NLG SHOCK STRUT IMPROPERLY SERVICED. SERVICED STRUT IAW M/M.Aug 4, 2000 · N952CA · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR COMA0060565Angle · corrodedTHE 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.Jul 12, 2000 · N952CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0060566Doubler · corrodedTHE 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.Jul 11, 2000 · N952CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR COMA0060554Beam · corrodedTRANSVERSE BEAM AT FS 349 CORRODED BETWEEN LBL 9 AND LBL 27. REPAIRED TRANSVERSE BEAM AT FS 349 IAW WVAC EO 601R-53-1491A.Jul 8, 2000 · N952CA · Cndair CL6002B19 · Fuselage Main, StructureSDR COMA0060478Aileron · sluggishA/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 DEFECTSJun 6, 2000 · N952CA · Cndair CL6002B19 · Aileron Control SystemSDR COMA0060290Lead · defectiveEMERGENCY FLOOR PATH LIGHTING AT ROW 8 IS INOPERABLE. REPLACED POWER LEAD.Mar 26, 2000 · N952CA · Cndair CL6002B19 · Emergency LightingSDR COMA0060264Latch · out of adjCABIN DOOR LATCH CAUTION MESSAGE. ADJUSTED CABIN DOOR LATCH MECHANISM.Mar 12, 2000 · N952CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0060191Computer · cockpitSTALL FAIL CAUTION MESSAGE. RESET STALL COMPUTER, SYSTEM TEST NORMAL.Feb 22, 2000 · N952CA · Cndair CL6002B19 · Stall Warning SystemSDR COMA9960744Skin · crackLOWER HORIZONTAL SURFACE OF RIGHT LOWER WING ACCESS HOLE AT 640DB CRACKED. BLENDED OUT DAMAGE, ROTO-PEENED, AND ALODINED IAW REO 601R-57-21-030.Dec 5, 1999 · N952CA · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA9960681Doubler · crackedFS 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.Nov 6, 1999 · N952CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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