N949CA, cancelled Oct 19, 2007

Service difficulty reports · 90

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 = 'N949CA' AND deregistration_id = 'N949CA-2007-10-19'
  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 COMA0660588Anti-Ice System · warning lightFLIGHT 5644 - ANTI-ICE DUCT MESSAGE AFTER TAKEOFF FROM CVG. AIRCRAFT RETURNED TO CVG AND LANDED WITHOUT INCIDENT. INSPECTED FORWARD FUSELAGE LOOPS AND PERFORMED OPS CHECK, CHECKS GOOD (CND).Oct 27, 2006 · N949CA · Cndair CL6002B19 · Ice/Rain Protection SystemSDR COMA0660490Circuit Breaker · malfunctionedFLIGHT 5470 - DURING FLAP SELECTION FROM 8 DEGREES, RECEIVED 3B HYD PUMP CAUTION MESSAGE. CREW DECLARED AN EMERGENCY, LANDED WITHOUT INCIDENT. FOUND 3B CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER, PERFORMED OPS CHECK PER AMM, NO FURTHER DEFECTS NOTED.Aug 14, 2006 · N949CA · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR COMA0660370Flap · malfunctionedFLIGHT 5480 - FLAP FAIL MESSAGE AFTER LANDING IN HSV, FAILED 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 WITH NO FURTHER FLAP CAUTION MESSAGES.Jun 1, 2006 · N949CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0660357Flap · malfunctionedFLIGHT 4997 - FLAP FAIL CAUTION MESSAGE WHILE IN CRUISE FLIGHT. 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 FURTHER FLAP CAUTION MESSAGES.May 23, 2006 · N949CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0660353Flap · malfunctionedFLIGHT 5296 - DURING APPROACH RECEIVED FLAP FAIL MESSAGE AT 20 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 AND E). FLAMay 19, 2006 · N949CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0660318Caution Message · illuminatedFLIGHT 5581 - FLAP FAIL CAUTION MESSAGE WHILE SITTING AT GATE. 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 FURTHER FLAP CAUTION MESSAGES.Apr 30, 2006 · N949CA · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR COMA0660306Flap System · malfunctionedFLIGHT 5199 - FLAP FAIL CAUTION MESSAGE CAME ON DURING TAXI. 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 FURTHER FLAP CAUTION MESSAGES.Apr 17, 2006 · N949CA · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR COMA0560685Flap System · malfunctionedFLIGHT 5130- DURING LANDING AT MSG RECEIVED A FLAP FAIL MESSAGE AT 45 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 WITH NO FURTHER FLAP CAUTION MESSAGESDec 12, 2005 · N949CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0560544Battery · dischargedFLIGHT 5903 - EMERGENCY FLOOR LIGHTNING INOPERABLE ROWS 9 TO 13. REPLACED THE EMERGENCY BATTERY.Oct 10, 2005 · N949CA · Cndair CL6002B19 · Emergency LightingSDR COMA0560515Bulkhead · crackedWHILE PERFORMING TASK CRJ-2-162014, DETAILED INSPECTION OF THE PRESSURE BULKHEAD WEBS AND VERTICAL BEAMS AT FS 559.0, TWO CRACKS WERE DISCOVERED IN THE BULKHEAD WEB RADIATING FROM THE HOLES FOR THE ATTACH BOLTS OF THE RIGHT AILERON CONTROL CABLE REAR QUADRANT Sep 21, 2005 · N949CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA0560049Controller · malfunctionedFLIGHT 5147 WING OVERHEAT MESSAGE. REPLACED THE CONTROLLER.Jan 11, 2005 · N949CA · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR COMA0560026Connector · defectiveFLIGHT 5198, EMERGENCY FLOOR PATH LIGHTING INOP AT ROW 2 THRU 5. REPLACED WIRE CONNECTOR.Jan 3, 2005 · N949CA · Cndair CL6002B19 · Emergency LightingSDR COMA0460568Selector Valve · unreliableFLIGHT 5994 GEAR DISAGREE WARNING. REPLACED THE NLG SELECTOR VALVE.Oct 3, 2004 · N949CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA0460528Reservoir · inoperativeFLIGHT 5492 GEAR DISAGREE WARNING. REPLACED THE SYSTEM 3 HYDRAULIC RESERVOIR.Sep 11, 2004 · N949CA · Cndair CL6002B19 · Hydraulic Reservoir, MainSDR COMA0460392Computer · malfunctionedFLIGHT 5546 STAB TRIM AND MACH TRIM CAUTION. RESET HSTCU, COULD NOT DUPLICATE, OPERATIONAL CHECK NORMAL.Jun 28, 2004 · N949CA · Cndair CL6002B19 · Drag Control SystemSDR COMA0460011Warning Light · illuminatedFLIGHT 5682 RIGHT THRUST REVERSER UNLOCK INFLIGHT. SECURED AND DEFERRED MAINT PER MEL.Jan 2, 2004 · N949CA · Cndair CL6002B19 · Engine Thrust ReverserSDR COMA0360564Windshield · crackedFLIGHT 5815 CO-PILOTS WINDSHIELD CRACKED. REPLACED WINDSHIELD.Dec 18, 2003 · N949CA · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA0360537Wire · looseTHE AFT SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOP. SECURED LOOSE WIRING CONNECTION.Dec 6, 2003 · N949CA · Cndair CL6002B19 · Emergency LightingSDR COMA0360504Frame · crackedRT 718 FRAME FLANGE CRACKED BELOW STRINGER 10. REPAIRED FRAME IN ACCORDANCE WITH REO 601R-53-61-193.Nov 13, 2003 · N949CA · Cndair CL6002B19 · Fuselage Main, FrameSDR COMA0460314Skin Panel · crackedPRESSURE FLOOR SKIN HAS CRACK AT FS 461.00. REPAIRED IN ACCORDANCE WITH REO 601R-53-41-102.Nov 6, 2003 · N949CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR COMA0360502Floor Panel · crackedPRESSURE FLOOR SKIN HAS CRACK AT FS 461.00. REPAIRED IN ACCORDANCE WITH REO 601R-53-41-102.Nov 6, 2003 · N949CA · Cndair CL6002B19 · Fuselage Floor PanelSDR COMA0360289Idg · malfunctionedFLIGHT 5304 LEFT IDG CAUTION MESSAGE DURING T/O. DEFERRED MAINT PER MEL.Jun 24, 2003 · N949CA · Cndair CL6002B19 · Alternator-Generator DriveSDR COMA0260711Power Cable · inoperativeFLIGHT 5893 EMERGENCY FLOOR PATH LIGHTING IS INOP.REPLACED TRACK LIGHTING POWER STRIPS.Dec 12, 2002 · N949CA · Cndair CL6002B19 · Emergency LightingSDR COMA0260591LampFLIGHT 5480 EMERGENCY FLOOR LIGHT AT ROW 3 IS INOP.DEFERRED MAINT PER MELOct 15, 2002 · N949CA · Cndair CL6002B19 · Emergency LightingSDR COMA0260538LampFLIGHT 5284 1 SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOP.DEFERRED MAINT PER MEL.Sep 18, 2002 · N949CA · Cndair CL6002B19 · Emergency LightingSDR COMA0260501CartA/C FUSELAGE STRUCK BY BAGGAGE CART AND SUSTAINED MAJOR DAMAGE BETWEEN F.S. 654 AND 672, AND STRINGERS 21L TO 23L.C/W REPAIR TO SKIN AND STRINGERS I/A/W SRM 53-00-31 AND 53-00-03 AND REO 601R 53-61-577 AND 579.Aug 29, 2002 · N949CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR COMA0260393Seal · leakingFLIGHT 5298 LEFT ENGINE OIL PRESSURE WARNING AFTER T/O, AIRCRAFT RETURNED TO MSP. (IFSD)REPLACED ACCESSORY GEAR BOX OIL SEALS AT AXIS D&F.Jun 28, 2002 · N949CA · Cndair CL6002B19 · Engine Oil System (Airframe Furnished)SDR COMA0260220DoorFLIGHT 5472 CABIN DOOR WARNING.COULD NOT DUPLICATE OPERATIONAL CHECK OF DOOR NORMAL. NO FAULT CODES IN COMPUTER.Mar 31, 2002 · N949CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0160825Window · fracturedFLIGHT 5903. PILOT'S SIDE WINDOW SHATTERED AT 29,000 FT.REPLACED THE PILOT'S SIDE WINDOW.Oct 16, 2001 · N949CA · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA0160729Angle · crackedLEFT SIDE INBOARD ANGLE AT F.S. 484.0 LBL 9 UNDER FLOOR PANEL 261CLF IS CRACKED.REPAIRED THE ANGLE AT FS 484.0 LBL9 I/A/W WVAC EO 601R-53-2711A.Sep 14, 2001 · N949CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR COMA0160728Angle · crackedLEFT SIDE INBOARD ANGLE AT F.S. 484.0 LBL 27 UNDER FLOOR PANEL 261DLF IS CRACKED.REPAIRED THE ANGLE AT F.S. 484.0 LBL27 I/A/W WVAC EO 601R-53-2711A.Sep 14, 2001 · N949CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR COMA0160727Angle · crackedRIGHT SIDE ELEVATER AND RUDDER PULLEY SUPPORT BRACKET AT F.S. 484.0 UNDER FLOOR PANEL 262DRF IS CRACKED.REPAIRED THE RIGHT SIDE ELEVATER AND RUDDER SUPPORT BRACKET AT F.S. 484.0 I/A/W WVAC EO 601R-53-2711A.Sep 14, 2001 · N949CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR COMA0160708Cap · chafedTHE L/H AND R/H INBOARD FLAP LEADING EDGE INBOARD VANE CAPS ARE CHAFED WHERE THEY CONTACT THE TEFLON BUMPER PADS.REMOVED THE CHAFED INBOARD VANE CAPS. INSTALLED NEW VANE CAPS L/H (601R14303-53S) AND R/H (601R14303-54) IAW WVAC EO 601R-57-2706.Sep 11, 2001 · N949CA · Cndair CL6002B19 · Leading Edge Slat Control SystemSDR COMA0160707Cap · chafedTHE R/H INBOARD FLAP LEADING EDGE VANE CAP MIDDLE SKIN IS CHAFED WHERE THE FLAP CONTACTS THE TEFLON BUMPER PAD.REMOVED THE CHAFED MIDDLE VANE CAP. INSTALLED A NEW CAP (P/N 601R14303-10) IAW AERODESIGN ENGINEERING REPORT NO. 1286-1.Sep 11, 2001 · N949CA · Cndair CL6002B19 · Leading Edge Slat Control SystemSDR COMA0160706Bushing · wornHORIZONTAL STABILIZER RHS VERTICLE BUSHING WORN.REMOVED R/H VERTICAL STAB BUSHING P/N 600-21061 INSTALLED NEW BUSHING ALT P/N 600-21061-7/SB I/A/W CRJ MM 20-26-00-910-803 FINAL REAMED BUSHING 1.50 I/A/W CANADAIR REO 601R-55-11-022 MACHINED BUSHING HAT I/A/W WVSep 10, 2001 · N949CA · Cndair CL6002B19 · Vertical Stabilizer, Attach FittingsSDR COMA0160552Web · crackedENGINE SUPPORT BEAM LOWER WEB CRACKED ON LEFT SIDE.PERFORMED A MAJOR REPAIR TO ENGINE SUPPORT BEAM LOWER NIB I/A/W CANADAIR REO 601R-53-61-366 REV C.Aug 5, 2001 · N949CA · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR COMA0160554Web · crackedENGINE SUPPORT BEAM LOWER WEB CRACKED ON RIGHT SIDE.PERFORMED A MAJOR REPAIR TO ENGINE SUPPORT BEAM LOWER WEB I/A/W CANADAIR REO 601R-53-61-366 REV C.Aug 5, 2001 · N949CA · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR COMA0160553Web · crackedENGINE SUPPORT BEAM IS CRACKED ON CENTER OF TOP WEB.PERFORMED A TEMPORARY MAJOR REPAIR TO CRACKED ENGINE SUPPORT BEAM I/A/W CANADAIR REO 601R-53-61-315 REV B.Aug 5, 2001 · N949CA · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR COMA0160210Warning Light · illuminatedFLAP FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE IAW AD 98-20-01.Feb 6, 2001 · N949CA · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR COMA0160128Carbon Seal · leakingLEFT ENGINE OIL PRESSURE FLUCTUATING BETWEEN 30 AND 48 PSI. REPLACED THE ACCESSORY DRIVES CARBON SEALS.Jan 17, 2001 · N949CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR COMA0160092Bulb · burned outEMERGENCY LIGHT AT ROW 5 IS INOP. REPLACED LIGHT BULB.Jan 8, 2001 · N949CA · Cndair CL6002B19 · Emergency LightingSDR COMA0061023Warning System · malfunctionedSTANDBY PITOT HEAT CAUTION MESSAGE. REPLACED THE NR 3 ADSHC.Dec 7, 2000 · N949CA · Cndair CL6002B19 · Pitot/Static Anti-Ice SystemSDR COMA0060897Seal · damagedLOUD SQUEAL FROM CABIN DOOR AREA. REPAIRED DOOR SEAL NIB DAMAGE I/A/W REO 601R-5211-108.Nov 8, 2000 · N949CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0060868Frame · damagedFRAME WEB DAMAGED AT FS 654.5 BETWEEN STRINGER 21B AND 22B LEFT HAND. CAUSED BY ELECTRICAL ARCING AT APU GROUND CABLE (N1232) . REMOVED DAMAGED FRAME SECTION AND SPLICED IN A NEW SECTION IAW REO 601R-53-61-301.Nov 1, 2000 · N949CA · Cndair CL6002B19 · Fuselage Main, FrameSDR COMA0060874Battery · dischargedAPU BATTERY AT ZERO VOLTS, APU BATTERY CHARGER IS INTERMITTENT. APU GROUND CABLE ARCHING AT GROUND STUD N1232, WHICH CAUSED SUBSTANTIAL DAMAGE AT FRAME 654.5. REPAIRED DAMAGED FRAME AND RELOCATED GROUND STUD IAW S/B 601R-49-014.Oct 28, 2000 · N949CA · Cndair CL6002B19 · Battery/Charger SystemSDR COMA0060792Connector · looseSEVERAL EMERGENCY LIGHTS AND SIGNS ARE INOP, FWD CABIN AREA. SECURED LOOSE CONNECTION AT FLOOR TRACK LIGHTING.Oct 2, 2000 · N949CA · Cndair CL6002B19 · Emergency LightingSDR COMA0060754Transducer · failedSTALL FAIL CAUTION MESSAGE DURING TAKEOFF, AIRCRAFT RETURNED TO THE GATE. REPLACED THE NR 1 AOA TRANSDUCER.Sep 15, 2000 · N949CA · Cndair CL6002B19 · Stall Warning SystemSDR COMA0060720Angle · corrodedTHE FWD J ANGLE AT FS 280 BETWEEN LBL 9.0 AND RBL 9.0 IS CORRODED. PERFORMED A MAJOR REPAIR BY REPLACING CORRODED FWD J ANGLE AT FS 280 BETWEEN LBL 9.0 AND RBL 9.0 IAW WVAC EO 601R-53-1681.Sep 10, 2000 · N949CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0060719Floorbeam · damagedTHE OUTBOARD FLANGE OF THE BEAM AT RBL 9.0 AND FS 409 + 8 WAS PREVIOUSLY REPAIRED. THIS EO PROVIDES FOR MODIFYING THE SPLICE ANGLE TO ACCOMODATE THE REPAIR. PERFORMED A MAJOR REPAIR TO THE OUTBOARD FLANGE OF THE BEAM AT RBL 9.0 AND FS 409 + 8 IAW WVAC EO 601Sep 10, 2000 · N949CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR COMA0060718Floorbeam · damagedDURING ACCOMPLISHMENT OF SB 601R-53-037 REV A, THE I/B FLANGE OF THE FLOORBEAM AT RBL 27.0 FS 409 + 8 WAS FOUND TO HAVE A PREVIOUS REPAIR. PERFORMED A MAJOR REPAIR BY REMOVING EXISTING REPAIR AND INSTALLING A SPLICE ANGLE ON FLOORBEAM RBL 27.0 FS 409 + 8 IAW Sep 10, 2000 · N949CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
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