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 CA051017004Thermal Barrier · failedDURING FINAL TOP CHARGE CELL NR 19 WENT INTO THERMAL BARRIER BREAKDOWN. HIGH TEMPERATURE LIMIT WAS REACHED AND THE CELL HOUSING MELTED.SDR CA051005006Pin · broken(CAN) DURING A WALK AROUND THE NLG UPLOCK ROLLER PIN WAS FOUND BROKEN AT THE COTTER PIN HOLE.SDR CA050920002Oxygen System · failed(CAN) DURING SCHEDULED MM DEPLOYMENT OF THE PASSENGER OXYGEN MASKS WAS ATTEMPTED. THE CONTROLLER WAS SWITCHED TO THE OVERRIDE POSITION BUT ALL OF THE PASSENGER OXYGEN MASKS FAILED TO DEPLOY. UPON FURTHER INVESTIGATION IT WAS DISCOVERED THAT THERE WAS INSUFICIESDR CA050915005Fitting · loose(CAN) DURING SERVICING A STRONG ODOR OF JET FUEL WAS NOTICED IN THE AFT EQUIPMENT BAY. AFTER INVESTIGATION, THE TRANSFER FUEL LINE FROM THE TAIL TANK TO THE FUSELAGE AUXILIARY TANK WAS FOUND TO BE LEAKING. THE WIGGINS FITTING ON THE TRANSFER ROTOR BURST FUELSDR CA050830003Link · chafed(CAN) DURING AIRCRAFT 1ST 12/24 MONTH INSPECTION, DISCOVERED RT AILERON CABLE FOUND INCORRECTLY ROUTED RESULTING IN CHAFING OF AUTOPILOT SYNCRO INPUT LINK. CABLE INSPECTED NFF AND RE-ROUTED. AREA LAST ACCESSED BY BOMBARDIER SERVICE CENTER, FOR AILERON PCU CHSDR UG82005F00008Probe · dented(REF CNTRL NR: PA 05-004) ALTITUDE SPLIT BETWEEN NR 1 AND NR 2 ALTIMETERS OF 250 FT AT 17000 FT. THE RT PITOT/STATIC PROBE HAS IMPACT DAMAGE. REPLACED THE RT PITPT/STATIC PROBE. COMPLETED ALTITUDE AND LEAK CHECKS IAW MM. RETURNED AIRCRAFT TO SERVICE. (K)SDR 548707212005Terminal Block · burnedCREW SAW WISP OF SMOKE AND BURNING ELECTRICAL ODOR IN COCKPIT. MADE UNSCHEDULED LANDING IN ABQ (EMERGENCY DECLARED FOR CLEARANCE PURPOSES). MAINTENANCE FOUND TERMINAL STRIP ON PILOTS WINDSHIELD BURNED OUT (TERMINAL STRIP IS FOR WINDSHIELD HEAT). NO OTHER DEFESDR CA050617008Engine · flamed out(CAN) RT ENGINE ROLLED BACK, FLAMED OUT DURING CRUISE, AT FL380. NO ABNORMAL INDICATIONS SHOWN. CREW DECLARED EMERGENCY, DESCENDED TO FL210 AND RESTARTED ENGINE USING CROSS BLEED. UNEVENTFUL LANDING AT DIVERSION AIRPORT. NO LEAKS FOUND DURING GROUND RUNS. FUELSDR 548706022005Unknown · odorPILOT REPORTED DURING CLIMB-OUT, PASSING THROUGH FL260, SMELLED STRONG ELECTRICAL ODOR IN COCKPIT. ACCORDING TO PILOT, ODOR WOULD DISSIPATE THEN RETURN STRONG. RAN CHECKLIST AND SHUTOFF LT PACK AND ODOR APPEARED TO DISSIPATE. COPILOT THOUGHT HE SAW PILOTS MSDR CA050509003Line · cracked(CAN) PILOT REPORTED (TAIL TANK AUTO INHIBIT LIGHT ON) BEFORE DEPARTURE. UPON INVESTIGATION, A CRACK ON THE TAIL TANK PRESSURE FUEL LINE WAS FOUND. IPC 28-13-22 ITEM 115.SDR CA050501001Wire Harness · shortedFUEL QTY IND FOR RT WING TANK INTERMITTENTLY FLICKERED, CHANGED QTY DISPLAYED & OCCASIONALLY ROLLED DOWN TO ZERO POUNDS OF FUEL INDICATED. NO TRUE CONDITION OF FUEL IMBALANCE APPARENT. INVESTIGATION REVEALED THE RED WIRE FOR NR 1 FUEL QTY TRANSMITTER FOR RSDR CA050426006Accelerometer · failedDURING CRUISE, STALL FAIL CAS MESSAGE APPEARED MOMENTARILY. TROUBLESHOOTING OF THE SYSTEM LEAD TO LT ACCELEROMETER INTERMITTENTLY FAILING AFTER BEING POWERED FROM 30 MINUTES TO 3.5 HOURS. LT ACCELEROMETER REPLACED.SDR CA050322004Anti-Ice Valve · closed(CAN) IN CRUISE ENGINE ANTI-ICE WAS SELECTED ON THE NR 2 ENGINE BUT VALVE WOULD NOT OPEN. UPON RETURNING TO BASE VALVE WAS REPLACED AND TESTED FUNCTIONAL.SDR CA050127004Lamp · burned(CAN) UPON LANDING THE CREW WHILE WORKING IN THE GALLEY AREA CLEANING UP NOTICED A BURNING ODOR. AFTER OPENING A SLIDING DOOR IN THE GALLEY THE FUMES BECAME STRONGER. MAINTENANCE REMOVED THE LIGHT COVER AND FOUND THE END OF THE BULB HAD BECOME HOT AND DISCOLSDR CA041101008Bracket · misinstalled(CAN) DURING TAKEOFF ATTEMPT, THE GREEN TAKE-OFF CONFIGURATION WARNING CAME ON.SDR CA041001014Strut · unsecure(CAN) DURING A FLIGHT AFTER MAINTENANCE, AIRCRAFT WAS IN CLIMB TO FL330 WHEN THROTTLES WERE PULLED BACK. CREW WAS UNABLE TO RETARD LT ENGINE THROTTLE. AIRCRAFT DESCENDED TO FL100 WHERE AN EMERGENCY WAS DECLARED AND THE LT ENGINE FIRE SHUTOFF, PBA WAS PUSHEDSDR CA041101005Transducer · out of limits(CAN) WHILE CONDUCTING A LINEARITY CHECK IAW MFG TASK JIC NR 27-35-04-101 (SEE ALSO S/B A604-27-011, REV 1, PART A, B) BOTH LT AND RT AOA TRANSDUCERS WERE FOUND TO BE BEYOND SERVICE LIMITS. BOTH ASSEMBLIES WERE REPLACED WITH IMPROVED TRANSDUCER ASSEMBLIES, PSDR CA040817008Structure · frayed(CAN) DURING THE POST FLIGHT INSPECTION THE RT AND LT WINGLET TIPS WERE FOUND TO BE DAMAGED BY STATIC DISCHARGE. THE RESIN MATERIAL WAS WAS BLOWN AWAY EXPOSING THE CARBON FIBERS AND LEAVING THE TRAILING EDGE FRAYED. CREW DID NOT EXPERIENCE LIGHTNING ON THE LASSDR CA040728002Control Unit · failed(CAN) DISPLAY BLANK. REPAIRED UNIT, INSTALLED F/T, OK (RADIO TUNING UNIT).SDR 54951Adc · failedNR 2 AIR DATA COMPUTER (ADC) FAILED SHOWING ALTITUDE FLAG AND VERTICAL SPEED FLAG. MDC CODES 350-000812 AND 351-080112, 351-0106F2.SDR CA040728001Charger · failed(CAN) MAIN BATTERY CHARGER FAILED, NO FAULT CODES, REPAIRED UNIT, INSTALLED F/T OK.SDR CA040602005Turbine · seized(CAN) DURING INITIAL START AN UNUSUAL NOISE WAS HEARD FROM THE APU. THE UNIT WAS RUN FOR APPROXIMATELY ONE HOUR WITH NO ABNORMAL INDICATIONS. UPON FURTHER INVESTIGATION OF THE NOISE IT WAS DISCOVERED THAT IT WAS NOT POSSIBLE TO ROTATE THE TURBINE WHEEL BY HANDSDR CA040602004Valve · gouged(CAN) THE LOW LIMIT VALVE WAS OBSERVED TO STICK IN AN OPEN POSITION AND WOULD NOT MODULATE. AFTER REMOVAL OF THE VALVE THE BUTTERFLY WAS FOUND TO BE SCRAPING AGAINST THE BODY OF THE VALVE.ANOTHER VALVE WITHTHIS CONDITION HAD PREVIOUSLY BEEN FOUND TO SHEAR THE SDR CA040531007Engine · bird ingestionSHORTLY AFTER TAKEOFF, A BIRD STRIKE OCCURRED ON THE RIGHT ENGINE. CREW CONTINUED CLIMB-OUT AND REDUCED POWER TO IDLE. FLIGHT CONTINUED TO AND MADE AN UNEVENTFUL LANDING. POST FLIGHT INSPECTION REVEALED SEVERAL FAN BLADES DAMAGED BEYOND LIMIT AND DAMAGE TO SDR CA040531006Engine · bird ingestionSHORTLY AFTER TAKEOFF A BIRD STRIKE OCCURRED ON THE RIGHT ENGINE. CREW CONTINUED CLIMB-OUT AND REDUCED POWER TO IDLE. FLIGHT CONTINUED AND MADE AN UNEVENTFUL LANDING. POST FLIGHT INSPECTION REVEALED SEVERAL FAN BLADES DAMAGED BEYOND LIMITS AND DAMAGE TO THESDR CA040514001Shaft · sheared(CAN) AFTER ENGINE START CREW WAS UNABLE TO OBTAIN COLD AIR-CONDITIONED AIR OUT OF THE LT AIR CONDITIONING PACK. ENGINES WERE SHUTDOWN AND MAINTENANCE WAS NOTIFIED OF THE SNAG. MAINTENANCE DISCOVERED THAT THE LOW LIMIT VALVE, BUTTERFLY VALVE WAS NO LONGER ATTSDR 541804062004Relay · failedFLAPS WOULD NOT RETRACT AFTER TAKE-OFF. (FLAPS WERE SET AT 20 DEGREES).MAINTENANCE IN PROGRESS - MAINTENANCE TROUBLESHOOTING CONFIRMED K2CE RELAY WAS AT FAULT. RELAY REPLACED AND OPS CHECKS PERFORMED SATISFACTORILY.SDR CA040413001Spring · missing(CAN) PASSENGER SEATBELT BUCKLE WAS FOUND TO HAVE NO SPRING TENSION IN THE LOCK POSITION. THE DRIVE SCREW PIN HAD BACKED OFF .0312 WHICH ALLOWED TENSION TO RELEASE. BELT ASSEMBLY IS SAFTEY PRODUCTS. THE BUCKLE IS STAMPED. THIS IS A MID COAST STC INTERIOR ISDR CA040511005Engine · fod(CAN) AFTER TAKEOFF THE CREW REPORTED SMOKE IN THE CABIN. AN EMEREGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO BASE AND MADE AN UNEVENTFUL LANDING. BOROSCOPE INSPECTION REVEALED FOD (FOD TYPE WAS NOT IDENTIFIED) FROM 1ST TO 7TH STAGE COMPRESSOR OF LT ENGINSDR CA040316002Control Unit · failed(CAN) BLEED AIR OVERHEAT CONDITION (LT HAND) DOWNSTREAM OF ENG BLEED AIR SHUT OFF VALVE. WARNING WAS INTERMITTENT, BUT REMAINED ON. FOLLOWING AFM PROCEDURES, LT ENG WAS SHUT DOWN IN FLIGHT WHEN WARNING PERSISTED AFTER AFFECTED BLEED VALVE WAS CLOSED. AC WAS SDR SVU2004F00001Control Unit · failedSTAB CHANNEL NR 1 FAILED. (WO NR 33978)SDR CA040123002Strut · unsecure(CAN) SHORTLY AFTER TAKEOFF, THE CREW NOTED THAT LT ENGINE THROTTLE COULD NOT BE RETARDED FROM 92 PERCENT. CREW ELECTED TO SHUT ENGINE DOWN WITH FIRE/PUSH PBA. A/C MADE AN UNEVENTFUL LANDING. SUBSEQUENT INSPECTION REVEALED THAT THE CORE COWL SUPPORT STRUT HSDR SVU2004F00004Transformer · defectiveCHANNEL NR 1 DISENGAGES DURING FLIGHT. (WO NR 34166)SDR WVE2004F00000Carbon Seal · leakingDURING 400/800/12 MO INSPECTION THE RT ENGINE NR 1 CARBON SEAL WAS FOUND TO BE LEAKING OIL EXCESSIVELY. THE NR 1 CARBON SEAL WAS CHANGED THREE TIMES PREVIOUSLY: AT 1/22/00 TT: 1274:44 TC: 663, AT 8/3/00 TT: 1902:37 TC:953: AND 1/25/02 TT: 3448:35 TC: 1805SDR CA031110008Controller · burned(CAN)AFTER T/O, CREW NOTICED OVERHEATING ELECTRONIC SMELL, SMALL AMOUNT OF SMOKE FROM PASSENGER'S OXY CNTL PANEL. CREW DIVERTED AC, HEADED BACK TO AIRPORT OF ORIGIN. LIGHT DIMMER ASSY (PS1LN) WIRE LN15C22 FEEDING 5 VAC TO OXYGEN CTRL PANEL (P/N 6044441011, WISDR 2003F00271Switch · malfunctionedRIGHT THRUST REVERSER UNLOCKED ON ENGINE START. BOTH THRUST REVERSER STOW SWITCHES WERE LEFT IN THE DEPRESSED POSITION. PLACED BOTH THRUST REVERSER STOW SWITCHES IN THE NORMAL POSITION. THRUST REVERSERS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR CA030401007Line · chafed(CAN) NR 1 EDP HYDRAULIC CASE DRAIN LINE WAS CHAFING AGAINST NR 1 EDP HYDRAULIC PX LINE, DUE TO INSUFFICIENT CLEARANCE/SYSTEM VIBRATION. CHAFING OCCURRED OVER A LENGTH OF APPROXIMATELY 4 INCHES, AND WAS BEYOND ALLOWABLE LIMITS.SDR CA030328002Display · failed(CAN) ON AIRCRAFT POWER UP CDU NR 3 SHOWED A BLACK SCREEN. THE MAINTENANCE DIAGNOSTIC COMPUTOR (MDC) LINE REPLACEABLE UNIT (LRU) STATUS INDICATED CODE: CDU 3 FAILED - NO CDU-2OUT. MDC LRU DIAGNOSTICS INDICATED CODE: CDU 3 354 - FAILED. NEW CDU INSTALLED AND SSDR 2003F00212Spoiler · inoperativeGROUND SPOILERS DID NOT DEPLOY AT KPTK. NONE, EXTENSIVE TROUBLESHOOTING IN WORK. (M)SDR 2003F00229Controller · failedGROUND SPOILERS DID NOT DEPLOY AT KPTK. NO DISCREPANCIES WERE DISCOVERED DURING TROUBLESHOOTING, AND SEVERAL OPERATIONAL CHECKS PER THE CL604 MM TASK 27-61-00-720-802. THE PSEU (CONTROLLER) WAS CHANGED AS A PRECAUTION PER BOMBARDIER RECOMMENDATION. THE AIRCSDR CA030212005Seal · leaking(CAN) EVIDENCE OF HYDRAULIC FLUID LEAKING FROM PCU SHAFT SEAL AREA.SUSPECT LEAKING IS WORSE AT ALTITUDE ORIN EXTREME COLD CONDITIONS.SDR CA030131006Feel Unit · rough(CAN) CREW STATED THAT ON TAKEOFF, EXCESSIVE FORCE ( AS COMPARED TO NORMAL TAKEOFF FORCE) WAS REQUIRED TO PULL THE YOKE BACK FOR TAKEOFF. CREW STATED THAT THE REQUIRED FORCE WAS SUCH THAT THEY CONSIDERED ABORTING TAKEOFF, BUT DID NOT. CREW ALSO NOTED THAT THE SDR CA030117004Pcu · leaking(CAN) WHILE IN THE HANGAR, HYDRAULIC FLUID WAS NOTICED ON THE WING UNDERSIDE LEAKING FROM THE AILERON PCU DRAIN HOLES. DURING SUBSEQUENT LEAK CHECKS WITH THE PCU INSPECTION PANEL REMOVED NO SIGNIFICANT LEAKAGE NOTICED. DURING SHORT TURN AROUND FLIGHTS NO EVIDSDR CA030116002Pump · failed(CAN) PRODUCTION FLIGHT TEST NR 4 DATED 8 JAN 03, HYDRAULIC NR 2 HI TEMP CAUTION POSTED JUST AFTER LEVELING ATF 410 TEMP MAXIMUM 104C, RT ENGINE SHUTDOWN, TEMP DECREASE TO NORMAL LIMIT. ENGINE RELIT PRIOR TO LANDING. EDP REMOVED AND INSTALLED. GROUND RUN CARRISDR O2G2003F00000Ram Air Turb · inoperativeAUTOMATIC DEPLOYMENT OF ADG OCCURRED AT ALTITUDE WHILE ENROUTE. NO ADVANCE WARNING OR INDICATION WAS GIVEN PRIOR TO DEPLOYMENT. CREW PROCEEDED WITHOUT FURTHER INCIDENT. MAINTENANCE CREW STOWED AND PERFORMED OPERATIONAL CHECKS IAW MM. NO DEFECTS NOTED. AIRSDR CA020830019Key · failed(CAN) BRAKE UNIT WAS APPROACHING WEAR LIMIT IAW AMM, AND AS A RESULT ELECTED TO CHANGE THE ASSEMBLY. UPON REMOVAL OF THE ASSOCIATED MAIN WHEEL, 5 OF THE CENTRE ROTOR DRIVE KEYS WERE FOUND SHEARED FROM THE ROTOR ITSELF. MINOR DAMAGE WAS NOTED ON THE MAIN WHEELSDR O2G2002F00000Control Unit · failedMACH TRIM FAILURE BY AUTOPILOT PITCH TRIM. SHORTLY AFTER THE STABILIZER CHANNEL NR1 TRIM FAILED RESULTING IN A LOSS OF ALL PITCH TRIM. REMOVED AND REPLACED HSTCU BOX, SYSTEM OPS CHECKED GOOD.SDR CA020705001Line · chafed(CAN) RT ENGINE OIL REPLENISH LINE WHERE IT EXITS THE AFT EQUIPMENT BAY AND ENTERS THE RT ENGINE PYLON WAS FOUND CHAFED AGAINST A STEEL BRAIDED HYD LINE. OIL LINE REPLACEDSDR 2002FA0000928Line · chafedLOST ALL NR 2 HYDRAULIC FLUID AT CRUISE FL 37 AFTER 3 HOURS IN FLIGHT. LEAK TRACED TO NR 2 EDB CASE DRAIN RETURNED LINE TUBE ASSEMBLY. REPLACED LINE, BLED AND LEAK CHECKED, NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE.SDR CA020408016Controller · failed(CAN) IT HAS BEEN FOUND DURING DEVELOPMENT OF A CABIN MANAGEMENT SYSTEM. IT DID NOT MEET THE MANUFACTURER'S SPECIFICATIONS. THE UNIT IS USED TO SWITCH CABIN LIGHTS. THE SPECIFICATION WAS MENTIONING CAPACITY FOR MAX CONTINUOUS RATING OF 7.5 AMPS, THE CONTROLLED
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