Canadair CL-601-2A12
Service difficulty reports · 88
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = 'CL6012A12' 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.
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 aircraft_model_key = 'CL6012A12' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CA120928001Heater · failed(CAN) AFT GALLEY WATER TANK HEATING ELEMENT STAYED ON AND CAUSED THE SURROUNDING INSULATION BLANKET TO BURN AND CREATED SMOKE IN CABIN OF ACFT WHICH CAUSED A FLIGHT DIVERSION.SDR CA101108005Tire · failed(CAN) ON POST FLIGHT/DI INSPECTION (NEXT AM) NR 3 MAIN TIRE WAS FOUND TO BE DEFLATED AND ONE INNER RIB/STRIP OF RUBBER MISSING 3/4 AROUND TIRE. APPEARS TO HAVE SEPARATED CLEANLY FROM CARCASS SIGNS OF IMPACT ON TRAILING EDGE OF INBOARD FLAP AND FLAP SEAL AS WESDR DJFA2009006Windscreen · crackedDURING CRUISE, CREW NOTED WHISTILING SOUNDS FROM THE LT WINDSCREEN. AFTER A BRIEF INSP, CREW NOTED (2) VERTICAL CRACKS SPANNING THE WINDSCREEN. AS THE ACFT BEGAN THE INITIAL DESCENT, THE CREW WITNESSED THE OUTER PLY OF THE WINDSCREEN DEPART THE ACFT. THE CRSDR CA081016003O-Ring · failed(CAN) ACFT, PRIOR TO ENG START APU HAD AN UNCOMMANDED SHUTDOWN. WHILE CARRYING OUT COCKPIT TROUBLESHOOTING PILOTS OBSERVED APU BOOST PUMP FAIL LIGHT WAS ILLUMINATED. APU BOOST PUMP WAS SUSPECT BECAUSE IT HAD JUST BEEN CHANGED THE PREVIOUS DAY FOR SAME SNAG. BOSDR CA080806007Gearbox · defective(CAN) DURING FLIGHT, CREW NOTICED THEY LOST THE NR1 ENGINE OIL INDICATION AND GOT THE RED LED. SHUTDOWN ENGINE AND MADE AN UNEVENTFUL LANDING. CREW NOTICED A PUDDLE OF OIL UNDER THE NR1 ENGINE AFTER LANDING. DURING THE TROUBLESHOOTING, THEY REMOVED THE DRAINSDR DJFA2008055Heat Tape · burnedWHILE REFUELING THE AC, THE CREW NOTED A SIGNIFICANT AMOUNT OF SMOKE IN THE COCKPIT. OPEN (A)SDR DJF2008F00004Unknown · smokeWHILE REFUELING THE AC, THE CREW NOTED A SIGNIFICANT AMOUNT OF SMOKE IN THE COCKPIT. (SDR WILL BE COMPLETED AFTER MAINTENANCE/ INSPECTION IS COMPLETE). (K)SDR CA080625008Actuator · malfunctioned(CAN) DURING A FLIGHT, PILOT REPORTED A PITCH TRIM CHANNEL NR1 INOP LIGHT ON. TROUBLESHOOT THE TRIM SYS AND FOUND NR1 TRIM ACTUATOR BRAKE COIL OPEN. HORIZ STAB TRIM ACTUATOR (P/N 600-92301-67/21207-008 S/N Y2003) WAS REPLACED WITH A REPAIRED UNIT WITH TSN 868SDR CA080225005Shaft · broken(CAN) 3 MINUTES AFTER TAKEOFF, GENERATOR FAILED, AC RETURNED TO BASE. GENERATOR REMOVED, FOUND BROKEN SHAFT INSIDE THE IDG (NOT THE MAIN SHAFT). IT BROKE, MELTED THE COVER AND CAME OUT (TC NR 20080225005)SDR DJFA2007133Adg · burnedDURING POST MAINTENANCE CHECK FLIGHT, CREW TESTED THE AIR DRIVEN GENERATOR SYSTEM (ADG). DURING THE TEST THE ADG FAILED LEAVING THE CREW IN COMPLETE ELECTRICAL BLACKOUT. ENGINE DRIVEN SYSTEM WAS BROUGHT BACK ON-LINE AND AIRCRAFT LANDED SAFELY. MAINTENANCE FSDR CA070328003Line · failed(CAN) DURING ROUTINE SERVICING AFTER A/C ARRIVAL, HYD FLUID WAS NOTICED LEAKING OUT OF THE BOTTOM OF THE RUDDER AND RUNNING DOWN THE TAILCONE AND TO THE GROUND. PANELS WERE REMOVED TO LOCATE THE LEAK, FIGURING THAT THERE WAS A BAD RUDDER PCU LEAKING. WHAT WAS SDR CA070301004Rod · corroded(CAN) DURING THE PILOT PRE-FLIGHT CHECKS THE LT FLIGHT SPOILER INDICATED DEPLOYED WHEN STOW WAS SELECTED. THE FLIGHT SPOILER STOW/DEPLOY HANDLE WAS STIFF AT THE STOW EXTREMELY. VISUAL CONFIRMATION REVEALED THAT THE FLIGHT SPOILER WAS NOT FULLY STOWED BUT THE RSDR CA070221001Bushing · failed(CAN) DURING FLIGHT THE CO-PILOTS RUDDER PEDAL ADJUSTMENT MECHANISM FAILED ALLOWING THE RUDDER PEDALS TO FALL FORWARD TO THE LIMIT OF THEIR TRAVEL. INSPECTION REVEALED THAT THE THREADED BUSHING IN THE ADJUSTMENT MECHANISM HAD FAILED ALLOWING THE SYSTEM TO DICOSDR CA070125001Actuator · inoperative(CAN) RT MAIN LANDING GEAR UNLOCK INDICATION APPROX. 15 - 20 MIN. AFTER ARRIVAL, NO PUMP, NO GEAR COMMAND, LOCK PARTIALLY MOVED TO UNLOCK POSITION. RETRACTING ACTUATOR REPLACED AND AC RETURNED TO SERVICE.SDR CA061010005Flap System · malfunctioned(CAN) FLAP FAIL BETWEEN 20 DEGREES TO 0 DEGREE DURING RETRACTION OF THE FLAPS AT TAKEOFF , FLAPS RESET ON GROUND IAW OPERATING MANUAL NR 1 ABNORMAL PROCEDURE SECTION 10 P3-4. A/C RETURN TO SERVICE. NO SNAG. FLAP FAIL BETWEEN 20 DEGREES TO 0 DEGREE DURING RETSDR CA060918001Flap System · malfunctioned(CAN) FLAP FAILED ON TAKEOFF, A/C RETURNED AND LANDED SAFELY AT QB MAIN BASE, BREAKER WAS RESET IAW OPERATING MANUAL, COULDN`T DUPLICATED THE SNAG. A/C DID ONE FLIGHT AND RETURN TO BASE WITHOUT ANY SNAG.SDR CA060828001Pump · broken(CAN) LT MAIN AND SCAVENGE EJECTOR FAILURE (MOTIVE FLOW FAILURE). FUEL PUMP SHAFT FOUND BROKEN. FUEL PUMP REPLACED AND AIRCRAFT RETURNED TO SERVICE. A/C HOURS; 25194:25 CYCLES; 29896 (TC NR 20060828001)SDR CA070720009Windshield · cracked(CAN) LT WINDSHIELD OUTER PANE CRACKED IN FLIGHT WITH NO LOSS OF PRESSURIZATION. FLIGHT CONTINUED NORMALLY. NEW WINDSHIELD INSTALLED AND AIRCRAFT RETURNED TO SERVICE. (TC NR 20070720009)SDR CA060728006Engine · oil consumption(CAN) AIRCRAFT HAD TO SHUTDOWN THE RT ENGINE DURING FLIGHT, DUE TO LOW OIL PRESSURE. APPROX 3 HOURS INTO THE FLIGHT, THE PILOT REPORTED THE OIL PRESSURE WAS FLUCUTATING BETWEEN 45 AND 65 PSI, THEN DROPPED AGAIN TO 35 AND 55 PSI, AND FINALLY GOT A STEADY LOW OISDR CA060515003Vent Line · corroded(CAN) REFUELLING WAS C/O, MASTER REFUEL PANEL CHECK C/O TO CHECK VALVE FOR OPERATION, WHAT WAS NOTICED, FUEL CAME OUT OUT OF THE LT NACA SCOOP APPROXIMATE 2 GALLON, THEN STOP. MAINT WAS ADVISED,THIS WAS ONLY HAPPENING WHEN A/C WAS PARK OVERNIGHT. SO MAINT CREWSDR CA060428002Transformer · inoperative(CAN) LOSS OF NR 1 MASI, NR 1 ALTIMETER, FDR, NR 1 ADI PITCH AND ROLL INFO, COMPASS INFO, NR 1 ESSENTIAL BUS AND LOSS 26 VAC. CAUSE OF FAULT FOUND TO BE BROKEN WIRES AT T2XD POST NR 3. TRANSFORMER LOCATED ON BACK OF C/B PANEL C. (TC NR 20060428002)SDR CA060407005Hinge Fitting · crackedLHS MAIN LANDING GEAR (MLG) P/N CC670-10520-965, S/N 15042 AND RT MLG DOOR P/N CC670-10520-966, S/N (SAME AS RHS) WERE CRACKED AT THE AFT HINGE FITTING P/N CC670-10571-13 (SEE PIX.1) AND AT FORWARD HINGE FITTING P/N CC670-10570-5 (SEE PIX.2). LOOSE FASTERNERSSDR DJFA2005179Bulkhead · crackedDURING A SCHEDULED MAINTENANCE VISIT, A CRACK WAS DISCOVERED IN THE PRESSURE BULKHEAD WEB AT FUSELAGE STATION 409.00 WHILE PERFORMING AIRWORTHINESS DIRECTIVE 97-24-02, SERVICE BULLETIN 601-0501. THE CRACK IS LOCATED AT THE CORNER OF THE KEEL BEAM LINK CUTOUT SDR CA051121001Fuel Heater · cracked(CAN) FUEL LEAK AS BEEN FOUND ON SEVEN DAYS INSPECTION, TECHNICIAN HAS FOUND A CRACK IN A SOLDERED JOINT ON FUEL HEATER. THE FUEL HEATER HAS BEEN REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR DJFA2005159Bulkhead · crackedDURING A ROUTINE MAINTENANCE VISIT, A CRACK WAS DISCOVERED IN THE PRESSURE BULKHEAD WEB AT FUSELAGE STATION 409.00 WHILE PERFORMING AD 97-24-02. THE CRACK WAS REPAIRED IAW EO NR 601-53-10-266, AND IN CONJUNCTION WITH DRAWING K600-31904. THE AIRCRAFT WAS RETUSDR CA050826001Heat Exchanger · leaking(CAN) DURING TROUBLESHOOTING TO FIND CAUSE FOR LOW OIL PRESSURE AT HIGH POWER IT WAS DISCOVERED THAT THE OIL HAD BECOME CONTAMINATED WITH FUEL AND SUBSEQUENTLY LOWERED IN VISCOSITY CAUSING LOW OIL PRESSURE READINGS. THE OIL TO FUEL HEAT EXCHANGER, FUEL HEATER/SDR DJFA2005111Selector Valve · inoperativeTHE CREW REPORTED THAT DURING A NORMAL GEAR EXTENSION, THE NOSE WHEEL WOULD NOT EXTEND. THE LANDING GEAR WAS CYCLED TWICE, AND THE NOSE GEAR REMAINED RETRACTED. A MANUAL EXTENSION WAS PERFORMED, AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SDR DJFA2005104Controller · brokenAFTER MLG SELECTED DOWN, LT MLG INDICATOR LIGHTS DID NOT ILLUMINATE. CREW TESTED BULBS AND PERFORMED A FLY-BY PAST TOWER. CONTROLLER REPORTED THAT MLG APPEARED TO BE DOWN AND LOCKED. A MANUAL MLG EXTENSION PERFORMED AND AIRCRAFT LANDED WITHOUT FURTHER INCIDESDR CA050413003Element · broken(CAN) DURING A SCHEDULED 1200-HOUR CHECK, A FUNCTIONAL TEST OF THE RIGHT THRUST REVERSER AUTO THROTTLE RETARDER WAS CARRIED OUT. THE RIGHT THROTTLE FAILED TO RETURN TO IDLE POSITION WITH THE THRUST REVERSERMANUAL DEPLOYMENT. UPON INVESTIGATION IT WAS DISCOVERESDR CA050406005Actuator · leaking(CAN) NOSE LANDING GEAR ACTUATOR LEAKING AT ROD END PISTON. LIFE LIMITED PART AT 19480 CYCLES. A/C RETURN TO BASE ON SPECIAL FLIGHT PERMIT WITH GEAR DOWN.SDR CA050222008Gcu · inoperative(CAN) A FEW MINUTES AFTER TAKE-OFF FROM AIRPORT WHILE SHUTTING DOWN THE APU, THE FLIGHT CREW HAD A SEVERE ELECTRICAL SMELL IN THE COCKPIT, BUT NO SMOKE APPEARS. THE FLIGHT CREW DECLARED AN EMERGENCY LANDING AT THE SAME AIRPORT. BACK TO THE MAINTENANCE FACILITSDR CA050215012Connector · loose(CAN) ON APPROACH, NLG WOULD NOT DEPLOY UPON NORMAL SELECTION OF LANDING GEAR DOWN. EMER EXTENSION WAS COMPLETED, AC LANDED WITHOUT FURTHER INCIDENT, FOUND THAT (NLG) SELECTOR VALVE WAS AT FAULT. PINS IN CONNECTION TO EXTEND SOLENOID WHICH CONTROLS DOWN SELESDR CA050120008Anti-Ice Valve · failed(CAN) FOLLOWING AN FAA, SUSPECTED UNAPPROVED PART REPORT, FOR A COWL ANTI ICE VALVE P/N: 300013000-002 S/N: 1596, MFG P/N: 601-97097-5, AN ADDITIONAL VALVE S/N:691, WAS FOUND TO HAVE BEEN REPAIRED AND CERTIFIED WITHOUT THE USE OF A PROPER CMM.SDR CA050125009Access Door · distorted(CAN) THIS AIRCRAFT WAS INSPECTED AND TESTED AND FOUND TO EXHIBIT UNACCEPTABLE NOSE AVIONICS ACCESS DOOR DEFORMATION IN EXTREME COLD CONDITIONS. THE DEGREE OF DOOR CORNER CURLING EXCEEDS THE MANUFACTURERS LIMIT FOR SKIN WAVINESS FOR RVSM CERTIFICATION. THIS CSDR CA050125008Access Door · distorted(CAN) THIS AIRCRAFT WAS INSPECTED AND TESTED AND FOUND TO EXHIBIT UNACCEPTABLE NOSE AVIONICS ACCESS DOOR DEFORMATION IN EXTREME COLD CONDITIONS. THE DEGREE OF DOOR CORNER CURLING EXCEEDS THE MANUFACTURERS LIMITS FOR SKIN WAVINESS FOR RVSM CERTIFICATION. (THIS SDR CA050119002Access Panel · distorted(CAN) AC REMOVED FROM HEATED HANGAR (20 DEG C) TO RAMP (-27 DEG C) T/E OF UPPER ELEC BAY ACCESS PANEL DEFLECTED .345 FROM AIRFRAME. FURTHER INVESTIGATION SHOWED DISTORTION THROUGHOUT PANEL WITH GREATEST DISTORTION AT CORNERS RANGING FROM .100IN TO .345 IN. SISDR CA050119001Valve · improper part(CAN) FOLLOWING AN FAA, SUSPECTED UNAPPROVED PART REPORT, FOR A COWL ANTI-ICE VALVE PN 300013000-002, SN 1596, THREE (3) ADDITIONAL VALVES WERE FOUND TO HAVE BEEN REPAIRED AND CERTIFIED WITHOUT THE USE OF PROPER CMM. THE VALVES INVOLVED ARE S/N: 133R, 867, 691SDR CA040729002Generator · failedDURING A ROUTINE POST MAJOR MAINTENANCE FLIGHT CHECK OF THE AIR DRIVEN TURBINE GENERATOR SYSTEM, THE SYSTEM FAILED TO TAKE THE ELECTRICAL LOAD, AS INDICATED BY THE AMMETER AND THE VOLTMETER, WHEN THE TURBINE WAS MANUALLY DEPLOYED. MAINTENANCE FINDINGS:- ADG OSDR CA040603004Aileron · mismanufactured(CAN) WHILE INVESTIGATING A SNAG, DISCOVERED AN AILERON A/P QUADRANT ASSEMBLY P/N 40E22-84-1069-1 WHICH DID NOT MEET THE MANUFACTURER'S DRAWING IN THE INSTALLATION OF THE NR 1 COLLINS A/P SERVO, LOCATED IN THE LT MLG WHEEL WELL. FOR THE DISABLING OF THE NR1 SDR CA040423007Potentiometer · intermittent(CAN) DURING TAKEOFF ROTATION, THE STICK SHAKER ACTIVATED ON THE LOW LEVEL, THE STALL PROTECT SYSTEM (SPS) WARBLER SOUNDED, THE SPS FAIL LIGHTS WENT TO A FLASH CYCLE AND THE STALL PUSH LIGHTS ACTIVATED. THE LT SPS NEEDLE WAS SWINGING BACK AND FORTH INTO THE SSDR CA031113001Engine · shutdown(CAN) DURING CRUISE AT FL 390, THE RT ENGINE SHUTDOWN. THE CREW REPORTED ALL ENGINE PARAMETERS WERE NORMAL AT THE TIME AND NO MESSAGES OR CAUTIONS WERE POSTED. THE CREW DECENDED AND PERFORMED A SUCCESSFUL WINDMILL RELIGHT AT 10,000 FT. FOLLOWED BY AN UNEVENTSDR CA030903006Actuator · failed(CAN) ATTEMPT TO TRIM AIRCRAFT NOSE UP OR NOSE DOWN CAUSED BOTH PITCH TRIM CHANNELS TO INDICATE (OFF). THUS HORIZONTAL PITCH TRIM SYSTEM DE-ACTIVATED.SDR CA030724002Battery Pack · overheated(CAN) THE BATTERY ASSEMBLY FOR NR 4 EMERGENCY LIGHTING POWER SUPPLY WAS REMOVED FOR BENCH CHECK. THE ASSEMBLY WAS INSPECTED AND FOUND THAT THE CELL TABS HAD BEEN OVERHEATED, INSULATION HAD BEEN MELTED OFF AND THE PLASTIC ENCLOSURE WAS ALSO DAMAGED. AN OPERATIOSDR CA030731005Bushing · failed(CAN) AFTER COMPLETION OF TASK, INSPECT ELEVATOR ATTACH BOLTS, VISUAL AND NDT INSPECTION, AND DURING POST INSTALLATION/INDEPENDENT INSPECTION, INSPECTOR NOTICED CLICKING NOISE, FOLLOWING INVESTIGATION FOUND (LT ELEVATOR): LT ELEVATOR ATTACH FITTING CRACKED, DUSDR CA030122001Fitting · broken(CAN) DOOR TENSION FITTING (UPPER FORWARD) BROKEN IN FLIGHT.SDR CA021217006Bearing · broken(CAN) DURING 300-600 HOUR INSPECTION AILERON PCU OPERATION TEST. FOUND AILERON QUADRANT IN RT WHEEL WELL IS NOISY (SNAPPING). AFTER REMOVING RT AILERON QUADRANT ASS FOR INVESTIGATION, FOUND RT QUADRANT ITEM 57 PAGE 27-11-00 FGURE 3 IN IPC BEARING IS DAMAGE (RASDR CA021125002Bearing · broken(CAN) DURING 300-600 HOURS INSPECTION AILERON PCU OPERATION TEST, FOUND AILERON QUADRANT IN RT WHEEL WELL IS NOISY (SNAPPING).AFTER REMOVING RT/ AILERON QUADRANT ASSEMBLY FOR INVESTIGATION, FOUND RT/ QUADRANT, BEARING IS DAMAGED (RACES HALF WAY ROUND). CHANGESDR CA020926001Wire · exposed(CAN) WIRING HARNESS FOR THE ENGINE FIRE BOTTLE SQUIBS LOCATED IN THE APU AREA HAD EXPOSED WIRES WHERE THEHARNESS ENTERS THE CONNECTOR PLUG FOR THE SQUIB.SDR CA020925003Wire Harness · exposed(CAN) WIRING HARNESS FOR THE ENGINE FIRE BOTTLE SQUIBS LOCATED IN THE APU AREA HAD EXPOSED WIRES WHERE THEHARNESS ENTERS THE CONNECTOR PLUG FOR THE SQUIB.SDR CA020913010Wire · shorted(CAN) ON A SCHEDULED MAINTENANCE INSPECTION OF THE FIRE BOTTLES, MECHANIC FOUND ON RT BOTTLE LT SQUIB WIRING TO BE EXPOSED AND TOUCHING EACH OTHER IN THE APU AREA. ANOTHER CL601 A/C INSPECTED AND FOUND SIMILAR PROBLEM WITH SQUIB WIRING (SAME BOTTLE AND SQUIB)
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