N964CA, cancelled Dec 5, 2020

Service difficulty reports · 93

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 = 'N964CA' AND deregistration_id = 'N964CA-2020-12-05'
  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 COMA2012031950015Pump · failedON CLIMBOUT FROM DTW RECEIVED GEAR DISAGREE MSG WHEN GEAR WAS SELECTED UP. EMERGENCY DECLARED, A/C RETURNED TO DTW LANDED SAFELY. REMOVED AND REPLACED ACMP 3B. OPS CHECK GOOD.Mar 16, 2012 · N964CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA2011102850088Warning System · activatedEN ROUTE FROM DTW TO MSN RECEIVED RT THRUST REV UNLOCKED CAUTION MSG, FOLLOWED QRH. EMERGENCY DECLARED, A/C DIVERTED TO LAN LANDED SAFELY. TRANSFERRED TO DEFERRED LIST PER MEL 78-30-01.Oct 27, 2011 · N964CA · Cndair CL6002B19 · Engine Thrust ReverserSDR COMA2011102450083Warning System · activatedEN ROUTE FROM DTW TO RIC AT 31000FT RECEIVED RT THRUST REV UNLOCK CAUTION MSG. FOLLOWED QRH PROCEDURES, EMERGENCY DECLARED. A/C DIVERTED TO IAD, LANDED SAFELY. TRANSFERRED TO DEFERRED LIST PER MEL 78-30-01.Oct 21, 2011 · N964CA · Cndair CL6002B19 · Engine Thrust ReverserSDR COMA2010091350195Wire Harness · failedON T/O FROM CVG RECEIVED ANTISKID I/B CAUTION MSG. EMERGENCY DECLARED, A/C DIVERTED BACK TO CVG LANDED SAFELY. REMOVED AND REPLACED RIGHT MLG I/B HARNESS SUB ASSY FOR WHEEL SPEED TRANSDUCER.Sep 10, 2010 · N964CA · Cndair CL6002B19 · Landing Gear System WiringSDR COMA2010083050186Floor Skin · crackedPRESSURE FLOOR SKIN IS CRACKED AT FS 461.00 BETWEEN LBL 9 AND RBL 9. CUT OUT DAMAGED AREA AND INSTALLED TEMPORARY REPAIR DOUBLER IAW REO 601R-53-41-103, REV A.Aug 29, 2010 · N964CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA2010082650185Post · crackedFOUND FS 409+128 LOWER BULKHEAD OUTBOARD RBL 18 POST CRACKED AT LOWER RADIUS. REPAIRED FS 409+128 RBL 18 POST ON OUTBOARD LOWER PART OF BULKHEAD IAW BOMBARDIER REO 601R-53-41-056.Aug 26, 2010 · N964CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA2010082650183Angle · crackedFOUND FS 409 INBOARD ANGLE AT LBL 27 CRACKED. REPAIRED IAW REO601R-53-41-056.Aug 26, 2010 · N964CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA2010082550184Angle · crackedFOUND CAP ANGLE CRACKED AT FS 559.00, LBL 18.00. COMPLIED WITH REPAIR TO PRESSURE BULKHEAD STRUCTURE FS 559.00 23L-23R IAW REO 601R-53-41-260 AND DEVIATION REO 601R-41-609.Aug 25, 2010 · N964CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA2010082550182Angle · crackedFOUND CAP ANGLE CRACKED IN RADIUS AT FS 559.00, RBL 18.00. COMPLIED WITH REPAIR TO PRESSURE BULKHEAD STRUCTURE FS 559.00 23L-23R IAW REO 601R-53-41-260 AND DEVIATION REO 601R-41-609.Aug 25, 2010 · N964CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA2010082450181Bulkhead · crackedBULKHEAD WEB CRACKED ABOVE CARGO DOOR TRACK, AT FS 621, LBL 27.50, WL 130. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1541, REV B.Aug 23, 2010 · N964CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA2010082450180Bulkhead · crackedBULKHEAD WEB CRACKED AROUND LINTEL ATTACH FITTING AT FS 621, LBL 36.2. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1230 REV D.Aug 23, 2010 · N964CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA2009050450126Warning System · malfunctionedON CLIMBOUT FROM JFK RECEIVED ANTI-ICE DUCT WARNING MSG. EMERGENCY DECLARED, A/C RETURNED TO JFK LANDED SAFELY. PERFORMED OPS CHECK OF ANTI-ICE SYSTEM, NO DEFECTS NOTED.May 4, 2009 · N964CA · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR COMA2009012050064Oil Cooler · leakingEN ROUTE FROM BHM TO LGA RECEIVED APU OIL PRESSURE MSG. A/C DIVERTED TO TRI, LANDED SAFELY. FOUND APU OIL COOLER LEAKING. R&R APU OIL COOLER.Jan 14, 2009 · N964CA · Cndair CL6002B19 · APU Oil SystemSDR COMA086358Floorbeam · corrodedFOUND CORROSION ON UNDER FLOOR FRAME AT FS 280 BETWEEN LBL 9.00 AD RBL 9.00. REMOVED AND REPLACED FLOOR SUPPORT IAW CRJ SRM 51-42-06. (S)Aug 17, 2008 · N964CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR COMA0860071Engine · failedFLIGHT 5341 - EN ROUTE FROM MKE TO CVG SEVERE ENGINE NOISE AND SHUDDER ON LEFT ENGINE. PERFORMED IFSD. EMERGENCY DECLARED AND AIRCRAFT DIVERTED TO ORD AND LANDED SAFELY. REMOVED AND REPLACED LEFT ENGINE.Jan 16, 2008 · N964CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA0760736Hydraulic Line · defectiveFLIGHT 5483 - RECEIVED HYD 2 LOW PRESSURE CAUTION MESSAGE, FOLLOWED BY ED2 CAUTION. ALL NR 2 FLUID LOST. LANDED IAD WITHOUT INCIDENT. REPLACED RIGHT ENGINE HYDRAULIC CROSSOVER LINE. NO FURTHER DEFECTS. Dec 19, 2007 · N964CA · Cndair CL6002B19 · Hydraulic System, MainSDR COMA0760396Stiffener · crackedDURING FS 559 INSPECTION FOUND CRACKS AT LOWER END OF VERTICAL BOX STIFFENER, FS 559 RBL 9 INBOARD AND OUTBOARD SIDE. CUT OUT DAMAGE AND INSTALLED DOUBLERS IAW CRJ REO 601R-53-41-057.May 24, 2007 · N964CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0760395Stiffener · crackedDURING FS 559 INSPECTION FOUND CRACKS AT BASE OF VERTICAL BOX STIFFENER, FS 559, LBL 0 INBOARD AND OUTBOARD SIDE. CUT OUT DAMAGE AND INSTALLED DOUBLERS IAW REO 601R-53-41-057.May 24, 2007 · N964CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0760008Duct · failedFLIGHT 4935 - AT CRUISE RECEIVED CABIN ALT WARNING MESSAGE. AIRCRAFT DIVERTED TO IND AND LANDED SAFELY. FOUND LEFT PACK ACM COMPRESSOR OUTLET DUCT DISCONNECTED, REPLACED DUCT.Jan 5, 2007 · N964CA · Cndair CL6002B19 · Air Distribution SystemSDR COMA0660632Transducer · faultyFLIGHT 5576 - DURING CLIMBOUT OF CVG THE LEFT ENGINE OIL PRESSURE FLUCTUATED BETWEEN 64 AND 79 PSI. REPLACED THE OIL PRESSURE TRANSDUCER.Nov 14, 2006 · N964CA · Cndair CL6002B19 · Engine Oil Indicating SystemSDR COMA0660387Priority Valve · faultyFLIGHT 5141- DURING CVG APPROACH WHEN GEAR WAS SELECTED DOWN, RECEIVED A DISAGREE MESSAGE, NOSE GEAR DID NOT EXTEND. CYCLED LANDING GEAR AND MESSAGE CLEARED. REPLACED THE PRIORITY VALVE.Jun 9, 2006 · N964CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA0660386Selector Valve · faultyFLIGHT 5141 - DURING CVG APPROACH WHEN GEAR WAS SELECTED DOWN, RECEIVED A DISAGREE MESSAGE, NOSE GEAR DID NOT EXTEND. CYCLED LANDING GEAR AND MESSAGE CLEARED. REPLACED THE NLG SELECTOR VALVE.Jun 9, 2006 · N964CA · Cndair CL6002B19 · Landing Gear SelectorSDR COMA0560479Flap System · malfunctionedFLIGHT 5874 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.Sep 1, 2005 · N964CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0460249Frame · crackedRIGHT HAND 718.00 FRAME HAS CRACK IN RADIUS OF ATTACH FLANGE AT TOP OF STRINGER 11R. REPAIRED IN ACCORDANCE WITH REO 601R-53-61.969.Mar 25, 2004 · N964CA · Cndair CL6002B19 · Fuselage Main, FrameSDR COMA0460122Selector Valve · malfunctionedFLIGHT 5351 NOSE DOOR OPEN WARNING DURING GEAR RETRACTION. REPLACED THE NLG DOOR SELECTOR VALVE.Feb 3, 2004 · N964CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA0460065Warning Light · illuminatedFLIGHT 5339 LEFT THRUST REVERSER UNLOCK CAUTION DURING T/O. SECURED THRUST REVERSER AND DEFERRED MAINT PER MEL.Jan 18, 2004 · N964CA · Cndair CL6002B19 · Engine Thrust ReverserSDR COMA0360477Doubler · dentedPREVIOUS REPAIR OF FUSELAGE SKIN LHS FS 310.00 BETWEEN STR 16-17 HAS SUSTAINED FURTHER DAMAGE DUE TO CONTACT WITH DOOR PINS. PERFORMED A MAJOR REPAIR BY REMOVING DAMAGED REPAIR DOUBLERS AND FILLER. FABED NEW DOUBLERS AND FILLER WITH 2024T3.063 AND 2024T3.050Nov 3, 2003 · N964CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR COMA0360469Window · crackedFLIGHT 5441 CO-PILOT SIDE WINDSHIELD SHATTERED. REPLACED SIDE WINDOW.Oct 24, 2003 · N964CA · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA0360212Strut · flatFLIGHT 5758 LANDING GEAR DISAGREE WARNING, NOSE LANDING GEAR DID NOT RETRACT. REPLACED THE NOSE LANDING GEAR STRUT PISTON ASSEMBLY.Apr 22, 2003 · N964CA · Cndair CL6002B19 · Nose/Tail Landing GearSDR COMA0360202Warning Light · illuminatedFLIGHT 5715 RT THRUST REVERSER UNLOCK CAUTION MESSAGE. SECURED T/R AND DEFERRED MAINT PER MEL.Apr 16, 2003 · N964CA · Cndair CL6002B19 · Engine Thrust ReverserSDR COMA0360015Coalescer BagFLIGHT 5716 TOILET SMOKE WARNING.CLEANED COALESCER SOCKS AND RAN SYSTEM TO CLEAR OIL FUMES FROM PREVIOUS APU FAILURE.Jan 8, 2003 · N964CA · Cndair CL6002B19 · Cabin Cooling SystemSDR COMA0260663Throttle Control · malfunctionedFLIGHT 5273 R/H THRUST REVERSER UNLOCKED MESSAGE.REPLACED THE THROTTLE GEAR BOX.Nov 23, 2002 · N964CA · Cndair CL6002B19 · Engine Thrust ReverserSDR COMA0260610Apu · smokeFLIGHT 5426 SMOKE TOILET CAUTION MESSAGE.REPLACED THE APU.Oct 25, 2002 · N964CA · Cndair CL6002B19 · APU Cowling/ContainmentSDR COMA0260581Element · defectiveFLIGHT 5071 - MLG BAY OVERHEAT WARNING.REPLACED OVERHEAT SENSING ELEMENT R/H WHEEL WELL.Oct 14, 2002 · N964CA · Cndair CL6002B19 · Detection SystemSDR COMA0260510Element · malfunctionedFLIGHT 5983 L/H 14TH STAGE BLEED AIR DUCT WARNING. IFSD.REPLACED THE BLEED AIR LEAK SENSOR ELEMENT IN L/H ENGINE PYLON.Sep 3, 2002 · N964CA · Cndair CL6002B19 · Pneumatic Indicating SystemSDR COMA0260385Landing GearFLIGHT 5858 GEAR DISAGREE WARNING DURING EXTENSION.COULD NOT DUPLICATE GEAR EXTENSION AND RETRACTION CHECKS WERE NORMAL.Jun 23, 2002 · N964CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA0260351Thermocouple · faultyFLIGHT 5640 LT ENG ITT HOT WARNING - ITT FLUCTUATED FROM NORMAL TO OVER 900 DEGREES.REPLACED THE LOW PRESSURE TURBINE ASSY DUE TO DEFECTIVE THERMOCOUPLE ASSY.Jun 2, 2002 · N964CA · Cndair CL6002B19 · Engine Temperature Indicating SystemSDR COMA0260227Strap · corrodedTWO FLOOR SUPPORT STRAPS CORRODED TO THE POINT THAT REPLACEMENT IS REQUIRED.REPAIRED I/A/W REO 601R-53-41-080.Apr 2, 2002 · N964CA · Cndair CL6002B19 · Fuselage Main, StructureSDR COMA0260226Angle · corroded65 FASTENERS REMOVED FROM LT AND RT FLOOR SUPPORT ANGLES BETWEEN FS 409.0+128 AND FS559.0.REPAIRED I/A/W REO 601R-53-41-081.Apr 2, 2002 · N964CA · Cndair CL6002B19 · Fuselage Main, StructureSDR COMA0260225Angle · corrodedAREAS OF CORROSION NOTED ON LT AND RT FLOOR SUPPORT ANGLES BETWEEN FS 409.0+128 AND FS 559.0. REPAIRED IAW REO 601R-53-41-079.Apr 2, 2002 · N964CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0260224Plank · crackedCRACK FOUND ON RT LOWER WING PLANK AT PANEL 610AB.REPAIRED I/A/W 601R-57-21-030.Apr 2, 2002 · N964CA · Cndair CL6002B19 · Fuselage Main, StructureSDR COMA0260223Plank · crackedCRACK FOUND ON RT LOWER WING PLANK AT PANEL 640DB.REPAIRED I/A/W 601R-57-21-030.Apr 2, 2002 · N964CA · Cndair CL6002B19 · Fuselage Main, StructureSDR COMA0260222Plank · crackedCRACK FOUND ON LT LOWER WING PLANK AT PANEL 550BB.REPAIRED I/A/W 601R-57-21-030.Apr 2, 2002 · N964CA · Cndair CL6002B19 · Fuselage Main, StructureSDR COMA0260221Plank · crackedCRACK FOUND ON LT LOWER WING PLANK AT PANEL 550GB.REPAIRED I/A/W 601R-57-21-030.Apr 2, 2002 · N964CA · Cndair CL6002B19 · Fuselage Main, StructureSDR COMA0260053Charger · inoperativeFLIGHT 5492 MAIN BATTERY CHARGER MESSAGE.REPLACED BATTERY CHARGER.Jan 15, 2002 · N964CA · Cndair CL6002B19 · Alternator-Generator DriveSDR COMA0160952Fitting · corrodedDURING REMOVAL OF THE RIGHT ENGINE ASSEMBLY, DISCOVERED PITTING CORROSION ON THE AFT ENGINE PYLON THRUST FITTING MOUNTING RIB. REPAIRED IAW REO 601R-54-50-040.Dec 9, 2001 · N964CA · Cndair CL6002B19 · Nacelle/Pylon, Attach FittingsSDR COMA0160805Wire · faultyFLIGHT 5354, FLOOR PATCH EMERGENCY LIGHTING, ROWS 2 THROUGH 5, ARE INOPERATIVE. REPLACED POWER WIRES FOR INOP SECTION OF LIGHTING.Oct 12, 2001 · N964CA · Cndair CL6002B19 · Light System WiringSDR COMA0160620Web · crackedR/H AND L/H SIDES OF THE ENGINE SUPPORT BEAM ASSY ARE CRACKED ON THE LOWER WEB.REPAIRED R/H AND L/H OUTBD LOWER ENGINE SUPPORT BEAM WEB I/A/W CANADAIR REO 601R-53-61-366.Aug 18, 2001 · N964CA · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR COMA0160621Web · crackedUPPER CENTER ENGINE SUPPORT BEAM HAS 1/2 CRACK (CENTER AFT).PERFORMED A TEMPORARY REPAIR I/A/W CANADAIR REO 601R-53-61-345 REV B.Aug 17, 2001 · N964CA · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR COMA0160584Angle · corrodedTHE FWD J-ANGLE AT FS280 BETWEEN LBL9.0 AND RBL 9.0 IS CORRODED.REPLACED FWD J-ANGLE AT FS280.0 BETWEEN LBL9.0 AND RBL9.0 I/A/W WVAC EO 601R-53-2641.Aug 13, 2001 · N964CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
Back to N964CA, cancelled Dec 5, 2020