Canadair CL-604
Service difficulty reports · 220
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 = 'CL604' 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 = 'CL604' 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 CA141217018Connector · damaged(CAN) WHILE CARRYING OUT TASK AMM 27-34-07-000-801. UPON REMOVAL OF THE TRANSMITTER, WE NOTICED A ROLL PIN/STOP WAS BENT, AND HAD INDICATIONS OF CONTACT WITH ANOTHER STOP PIN. WITH THE UNIT PROPERLY INSTALLED, THERE IS NO INDICATION THAT THESE PINS SHOULD BE SDR CA141217014Duct · ruptured(CAN) LT ENGINE ANTI-ICE DUCT RUPTURE. DURING REPOSITION FLIGHT, LH ENGINE ANTI-ICE DUCT RUPTURED. THEY HAD IN FLIGHT "L COWL A/ICE" MESSAGE, SO THEY SWITCHED OFF ENG ANTI ICE AND DIVERTED TO AERODIENST. THE AIRCRAFT LANDED SAFELY BUT THE LEFT THRUST REVERSESDR CA141218023Clamp · deteriorated(CAN) PREMATURE FAILURE OF CUSHION CLAMPS M85052, CLAMP MATERIAL DETERIORATES, WHICH CAN RESULT IN CHAFING & DAMAGE TO HYDRAULIC LINES, ULTIMATELY LEADING TO FAILURE OF THE HYDRAULIC SYSTEM. CUSHION OF CLAMPS ARE DARK BLUE & PURPLE. BLUE CUSHION ON THESE CLASDR CA141128008Shim · misinstalled(CAN) LAMINATED SHIM NOT INSTALLED PER DRAWING. FLOOR/WING TIE BEAM BUMPER PAD LAMINATED SHIMS P/N 600-31143-13 INSTALLED OVER SOLID SHIMS INSTEAD OF UNDER SOLID SHIM AS PER DRAWING REQUIREMENTS. HOWEVER, IT HAS SUBSEQUENTLY BEEN DETERMINED THAT DRAWING ALLOWSSDR CA141105008Connector · leaking(CAN) DURING INSPECTION FOR DAMAGED CABLES ON BOMBARDIER PRODUCTION LINE (REF. CL6-CA-28-36/37), FUEL WAS FOUND IN THE BOOST PUMP CARTRIDGE ELECTRICAL CONNECTORS ON FOUR AIRCRAFT (5941, 5958, 5966 AND 5969). THE CONNECTORS THAT EXPERIENCED LEAKS WERE NOT PART SDR CA141028007Trunnion · corroded(CAN) FOUND CORROSION AROUND FWD AND AFT ATTACHMENT BUSHINGS DURING PERFORMANCE OF SB ON MLG MAIN FITTING ASSEMBLIES. REPAIRED.SDR CA141010018Heater · burned(CAN) WHEN DOING MAINTENACE WITH THE EXTERNAL POWER CONNECTED, THE AVIONIC TECHNICIAN SMELLED SMOKE COMING FROM THE CABIN. AFTER DISCONNECTING THE EXTERNAL POWER AND THE SMOKE WAS GONE, THEY FOUND OUT THAT THE CAUSE WAS THE WATER LINE HEATER AND THE SURROUNDISDR CA140918005Handle · out of tolerance(CAN) AC 5702 TO 5961 INCLUDE SOLID RIVET INSTALLATION FOR BULKHEAD DOOR HANDLE C471142-601, 541 BLKHD, 560 BULKHEAD AND 587 BULKHEAD.THE INSTALLATION OF SOLID RIVET IAW CDP300-03 DOES NOT PROVIDE A TOLERANCE, RIVET SHOP, HEAD TOO SMALL FOR THE ACCEPTABLE LIMISDR CA141202031Gear · fractured(CAN) AT FL360 LEFT ENGINE FLAMED OUT. EMERGENCY LANDING CARRIED OUT. FOUND LEFT ENGINE GEARBOX FAILURE. DECIDED TO BORESCOPE THE RIGHT ENGINE. FOUND CRACK IN AXIS P GEAR. REMOVED GEARBOX.SDR CA140915008Engine · flamed out(CAN) AT FL360 IN CRUISE A NOISE SOUNDING LIKE A FAN WAS HEARD. 10 MIN THE ENGINE FLAMED OUT. AIRCRAFT DIVERTED AND LANDED OVERWEIGHT.SDR CA140808002Terminal Block · damaged(CAN) AC SERIAL 5908, 5920 TO 5966 IT HAS BEEN RECENTLY DISCOVERED THAT THE SUBJECT PART NUMBER M81714/17-D31, M81714/17-D32, M81714/17-D33, M81714/17-D34, M81714/17-D35, M81714/17-D37, M81714/17-D38, M81714/17-D44 TERMINAL JUNCTION BLOCK WITH DATE CODES 1233SDR CA140701019Wire Harness · unknown(CAN) ON FUEL BOOST PUMP CANISTER, 601R62181-1, N642-0773, 226115-2). PRODUCTION REMOVED EXISTING PUMP CONNECTOR WIRE ASSY, C93-440 AND RE INSTALL NEW CONNECTOR WIRE KIT, KITC93-440. THOSE NEW CONNECTOR WIRE KIT ARE SUSPECTED TO HAVE THE INSULATION CUT JUST SDR CA140522003Oxygen Mask · mismanufactured(CAN) THE PROBLEM IS WHEN THE OXYGEN MASKS ARE DEPLOYED, THE LANYARD LENGTH IS TOO LONG. THIS LONG LENGTH PREVENTS THE PIN FROM BEING DEPLOYED WHICH IN TURN PREVENTS THE FLOW OF OXYGEN WHEN THE PASSENGER HAS THE MASK ON THEIR FACE. THIS PROBLEM AFFECTS ALL PSDR CA140522009Fuel Line · fouled(CAN) FUEL DRAIN LINE 601-62706-21-01 HARD FOULING WITH WIRES AND BACK SHELL OF CONNECTOR P251.SDR CA140521007Light · burned(CAN) WHILE WORKING ON THE ACFT, MAINTENANCE CREW FOUND THAT THE CIRCUIT BREAKER FOR THE FLOODLIGHTS WAS DISENGAGED, RESETTING THE BREAKER JUST RESULTED IN IT POPPING AGAIN. THE CUSTOMER WAS INFORMED AND THEY GAVE THE GO AHEAD TO FAULT FIND THE PROBLEM. THE SDR CA140227001Flap Track · broken(CAN) DURING A DAILY INSPECTION ON THE 24TH OF FEBRUARY A HEAVY WRINKLE WAS FOUND ON THE LT INBD FLAP. FURTHER INVESTIGATION FOUND THE FAIRING OVER THE FLAP TRACK PULLED DOWN AT THE FRONT. UPON REMOVAL OF THE FLAP TRACK FAIRING THE FORWARD ATTACH BRACKET FORSDR CA140225010Sensor · burned(CAN) THE ACFT WAS POWERED BY APU GENERATOR ONLINE. AFTER 30 MINS, WHEN THE HYDRAULIC PUMP TURNED ON, THE FOLLOWING CIRCUIT BREAKER WAS POPPED OUT, 115 VAC ESS FEED, ESSAC TRANSFER CONT). THE SMOKE CAME FROM BEHIND THE CAPTAIN SIDE CIRCUIT BREAKER PANEL CBP-SDR CA140217020Manifold · failed(CAN) PROXIMITY SYS FAULT, STATUS MESSAGE ON POWER UP. R & R GROUND SPOILER MANIFOLD. PERFORMED BLEED LEAK AND OPS CHECK OF GROUND SPOILER SYSTEM.SDR CA140214001Thrust Reverser · unwanted deploy(CAN) LEFT THRUST REVERSER UNCOMMANDED DEPLOYMENT ON THE TAKEOFF ROLL AT 70 KTS. LT ENGINE OVERHEAT MESSAGE ALSO PRESENT. TAKEOFF ABORTED, ENGINE SHUTDOWN AND ACFT RETURNED TO STAND.SDR CA140120020Wire · failed(CAN) DURING A DAILY INSPECTION, IT WAS NOTED THAT THE TAIL LOGO LIGHTS WOULD NOT ILLUMINATE. INVESTIGATION OF THE SYS FOUND BOTH BULBS SERVICEABLE WITH NO POWER AT THE LIGHT ASSEMBLIES. FURTHER INVESTIGATION REVEALED A CHAFED WIRE THRU A BULKHEAD GROMMET LOSDR CA131118016Selector Valve · failed(CAN) PILOT REPORT: FUEL ON BOARD DURING OCCURRENCE: 9.100 LBS PAX ON BOARD: 2 CREW ON BOARD: 3 SPEED AT OCCURANCE: 170 KTS WEATHER CONDITIONS DURING OCCURRENCE: 1430Z ILS26 V260-320/1MS 10KM OVC 1200M 5/-1 QNH 1029 NOSIG "GEAR DISAGREE" WHEN CLEARED FOR THSDR CA131113007Selector Valve · failed(CAN) AIRCRAFT COMING IN FOR LANDING, AFTER LANDING, GEAR HANDLE MOVED TO DOWN POSITION, ONLY NLG EXTENDED, DOWN, BOTH MLG REMAIN IN RETRACTED, UP, POSITION. PILOTS FOLLOWED THE CHECKLIST WHERE IT STATES TO CYCLE THE LANDING GEAR HANDLE, BUT IT WAS NOT POSSIBSDR CA130531011Engine · flamed out(CAN) DURING FLIGHT AT CRUISE FL360 .78M, ALL ENGINE INDICATIONS WERE NORMAL WHEN A CLIMB WAS INITIATED TO FL380. CLIMBING THROUGH FL370 THE RIGHT ENGINE ROLLED BACK TO IDLE. CONTINUOUS IGNITION WAS ACTIVATED BUT THE ROLL BACK CONTINUED. IN-FLIGHT ENGINE FAILSDR CA130502007Engine · bird ingestion(CAN) DURING CLIMB, ACFT EXPERIENCED STRONG VIBRATION ON RT ENGINE, CREW RETURN TO GROUND SAFE AND DISCOVER RT ENGINE HAD A BIRD STRIKE.SDR CA130313005Angle · misinstalled(CAN) DURING THE FLIGHT SPOILER SPECIAL DETAILED INSPECTION, PROCEDURE ET-57-70-001, DUE AT 1200 CYCLES IT WAS FOUND THAT THE ANTI-ROTATION PLATE INSTALLED AT APPROXIMATELY RWS 218.00 , THE OTBD BOLT ON THE RT FLIGHT SPOILER WAS THE INCORRECT PN A 600-10343-43SDR CA130118004Oil System · low pressureLEFT ENGINE OIL PRESS, CAS MESSAGE ON THE START OF THE DESCENT A RED, LT ENGINE OIL PRESSURE, CAS MESSAGE POSTED ON EICAS. CREW BROUGHT LT ENGINE BACK TO IDLE AND FOLLOWED THE AFM PROCEDURES. CREW KEEP AN EYE ON THE ENGINE OIL PRESSURE. WHEN OIL PRESSUE DROSDR CA130111002Engine · malfunctioned(CAN) ALTITUDE FL210, AIRSPEED 210 KIAS TEST POINT ATS RELIGHT OF LT ENGINE PREAMBLE: FOLLOWING A SUCCESSFUL WINDMILL RELIGHT OF THE ACFT LT ENGINE IT WAS AGAIN SHUTDOWN IN THE FIRST STEP OF THE ATS RELIGHT PROCEDURE. DURING THE WINDMILL RELIGHT PROCEDURE ITSDR CA121207005Windshield · cracked(CAN) DURING CRUISE WINDSHIELD CRACKED TOP TO BOTTOM.SDR CA130110010Engine · failed(CAN) DURING A QUICK TURN AT THE OPERATORS HOMEBASE, CREW SMELLED SMOKE IN THE CABIN FOLLOWED BY A RED, APU FIRE, CAS MESSAGE ON EICAS. APU AUTO SHUTDOWN AND CREW SET OFF THE APU FIRE BOTTLE. TRIP WAS CANCELLED. TALK WITH MFG, BELIEVE THE APU COMPRESSOR LET SDR CA121019002Spring · broken(CAN) FOUND BROKEN SPRING ON LT AND RT ENGINE THRUST LOWER REVERSER BLOCKER DOOR LINK ASSY DURING 48 MONTHS INSPECTION.SDR CA120921007Lock Fastener · sheared(CAN) INSPECTION REVEALED A SHEARED LOCK FASTENER PIN ON THE FWD ROW OF FASTENERS OF THE INBD FLAP HINGE FITTING 600-10317-6, INSTALLED AT WS 76.50.SDR CA120607006Heater · burned(CAN) HAVE JUST ATTENDED THE SUBJECT ACFT AFTER THE CREW REPORTED A BURNING ODOR FROM THE GALLEY AREA. UPON INVESTIGATION A SMALL HOLE HAD BEEN BURNED IN THE CARPET ADJACENT TO THE SINK AREA. THE CARPET HAS BEEN REMOVED AND THE CAUSE OF THE ISSUE HAS BEEN IDESDR CA130131001Wire Harness · exposed(CAN) THE COCKPIT TOUCH SCREEN SUPPLIES THE ELECTRONIC CHARTS, AIRPLANE DOCUMENTATION AND MANUALS, WEATHER INFORMATION, AND ACCESS TO THE CABINS ELECTRONICS SYSTEM CONTROLS. ELECTRICAL HARNESS IS DAMAGED AT INSTALLATION OR/IN SERVICE. THE HARNESS WAS CRUSHEDSDR CA120404001Compressor · stalled(CAN) DURING CLIMB, FROM FL380 TO FL400, THE RT ENGINE BEGAN TO COMPRESSOR STALL 5-6 TIMES QUICKLY AND BRIEFLY, AS THE CREW, INCREASING POWER AT A SLOW RATE PROPORTIONAL TO THE CLIMB RATE OF THE ACFT. THEIR INDICATED MACH NR WAS APPROXIMATELY .80 AND ENGINES WSDR CA120426012Fitting · leaking(CAN) THE FLIGHT CREW REPORTED THAT THE AMBER, HYD 2 LO PRESS, MESSAGE ILLUMINATED ON THE ENGINE INDICATION AND CREW ALERTING SYSTEM, EICAS, THEY ACCESSED THE HYD SYNOPTIC PAGE AND NOTED THAT THE HYD SYS NR 2 QTY DECREASED TO 0 PERCENT IN A RELATIVELY SHORT PESDR CA120227015Hose · leaking(CAN) WAS FLYING WHEN THE FLIGHT CREW REPORTED THAT THE AMBER HYD 2 LO PRESS MSG ILLUMINATED ON THE ENG INDICATION & CREW ALERTING SYS, EICAS. THEY ACCESSED THE HYD SYNOPTIC PAGE & NOTED THAT THE HYD SYS NR 2 QTY DECREASED TO 0% IN A RELATIVELY SHORT PERIOD OSDR CA120113008Switch · failed(CAN) DURING PRODUCTION FLIGHT TEST, PILOTS DECLARED THAT NOSE LANDING GEAR DIDN"T RETRACT AFTER TAKE OFF. A/C LANDED WITHOUT INCIDENT AND NO EMERGENCY WAS DECLARED. - MICROSWITCH FOUND OUT OF TOLERANCE ON NOSE LG.DOORS - MICROSWITCH RE ADJUSTED AND TESTED - SDR CA120222005Connector · melted(CAN) THE WATER STERILIZER "FAILURE CHAN 1" LIGHT WAS ILLUMINATED. ACCESS TO THE NPS-A2 POTABLE WATER TRAETMENT UNIT, P/N: 9-10001-06 , S/N:1495MOD2.2 GAINED AND GALLEY CB PANEL B-8, PURIFIER WAS OPENED. THE CB WAS RESET AND VERIFIED THAT THE CHAMBER 1 LAMP WASDR CA111202004Idg · failed(CAN) DURING THE CRUISE AT F350, THE RT PILOT`S SCREENS BLANKED INTERMITTENTLY COMBINED WITH A MASTER CAUTION AURAL WARNING WITH ASSOCIATED GENERATOR 2 OFF MESSAGE. CYCLED EVERY 5-10 SECONDS. STAB CHANNEL 2 AND YAW DAMPER 2 STATUS MESSAGES AND MACH TRIM CAUTSDR CA111207002Dcu · damaged(CAN) IMMEDIATELY AFTER ROTATE, AN AURAL `BLEED AIR DUCT` AND ASSOCIATED RED CAS MESSAGE ACTIVATED - SOON TO BE FOLLOWED BY VARYING AMOUNTS OF AMBER CAS MESSAGES. AUTOFLIGHT SYSTEMS, GEAR AND FLAP APPEARED TO OPERATE NORMALLY, SO THE SID WAS CONTINUED (MARUB SDR CA110615002Throttle · bindingAFTER TAKEOFF THE CREW UNABLE TO MOVE LEFT THROTTLE LEVER TO REDUCE ENGINE POWER. THE ENGINE EXCEED THE ITT TARGET BUT STAY WITHIN LIMIT. THIS WAS THE SECOND FLIGHT AFTER MX.SDR CA110222009Turbine Nozzle · crackedDISASSEMBLY OF THE APU FOR A CRACKED SCROLL ASSY REVEALED A CRACKED TURBINE NOZZLE ASSY. THE TURBINE NOZZLE HAD 389 HRS SINCE NEW.SDR CA111111006Controller · inoperative(CAN) AS REPORTED BY FLIGHT CREW: THE ACFT DEPARTED UNTIL THE ACFT HAD TO LEVEL OF AT 19.000 FT, THE PRESSURIZATION SEEMED TO BE WORKING FINE AND THE CABIN ALTITUDE DISPLAYED 4.000 FT. ONCE THE ACFT STARTED TO CLIMB FURTHER, THE CABIN RATE OF CLIMB WAS 1000SDR CA110120001Servo · failedDURING CLIMB OUT, A MASTER CAUTION KEPT APPEARING SAYING "AUTOPILOT AILERON TRIM LT WING LOW". THIS CAME ON AND OFF SEVERAL TIMES. QRH WAS RUN AND IT ORDERED THE DISCONNECTION OF AUTOPILOT WHICH WAS DONE. SO THE PILOT IS IN A POSITION WHERE THE MEL FOR THE FSDR CA110106007Windshield · crackedWINDSHIELD OUTER HEATED PLY CRACKED IN CRUISE PHASE OF FLIGHT. WINDSHIELD HEAT TURNED OFF AS PER CHECKLIST. FLIGHT CONTINUED TO DESTINATION WITHOUT FURTHER INCIDENT.SDR CA101227002Unknown · odor(CAN) COCKPIT AND CABIN FULL OF SMOKE AFTER TAKE OFF AND ROTATION BECAUSE OF HEAVY SNOW A/C WAS DEICED WITH A LOT OF DE-ICING FLUID. AFTER TAKE OFF THE COCKPIT AND PASSENGER CABIN FILLED WITH SMOKE (NO BURN ODOR), NO VISIBILITY AT ALL. EMERGENCY DECLARED WITH SDR CA101213008Unknown · smoke(CAN) DUE TO A HEAVY SNOW A/C WAS DEICED WITH A LOT OF DE-ICING FLUID CONSUMPTION. AFTER A/C ROTATE AND TAKE OFF THE COCKPIT AND PASSENGER CABIN WAS FULL OF SMOKE (NO BURN SMELL), NO VISIBILITY AT ALL. CREW DECLARED EMERGENCY AND LANDED BACK UNEVENTFULLY. IN FSDR CA101208008Display · failed(CAN) IN CRUISE, THE #1 ADAPTIVE FLIGHT DISPLAY WENT BLANK BRIEFLY AND THEN RETURN TO NORMAL FOR THE DURATION OF THE FLIGHT. AFD HAS BEEN REPLACED WITH AN OVERHAULED UNIT. (TC# 20101208008)SDR CA101208007Adc · failed(CAN) SHORLTY AFTER TAKE OFF THE NR 2 ALTIMETER BAROMETRIC SETTING ROLLED BACK TO THE PREVIOUS INPUT SETTING. BAROMETRIC PRESSURE WAS RESET AND REMAIN NORMAL FOR THE DURATION OF THE FLIGHT. AIR DATA COMPUTER WAS REPLACED WITH A SERVICEABLE UNIT.SDR CA101206012Outflow Valve · failedACFT EXPERIENCED AN UNCOMMANDED DEPRESSURIZATION IN FLIGHT WITH PRESSURIZATION SYS OPERATING IN AUTO MODE. WHEN THE PILOTS NOTICED A RAPID CHANGE IN THE RATE OF PRESSURIZATION, THEY IMMEDIATELY SWITCHED TO MANUAL MODE OF OPERATION. IN MANUAL MODE, THE ACFT C
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