Canadair CL-604

Service difficulty reports · 220

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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.

SDR CA020326007Control Cable · failed(CAN) DURING ROUTINE INSPECTION FOUND RT WING OUTBOARD AILERON CONTROL CABLE RUBBING AGAINST TOP AILERON FUEL SYNC TRANSMITTER LINK. FURTHER DETAIL INSPECTION DISCOVERED AILERON DUAL SYNC TRANSMITTER LEVER INSTECTED APPROX 180 DEG. OUT OF NORMAL POS. PERFORMEMar 7, 2002 · Cndair CL604 · Aileron Control SystemSDR CA020226009Windshield · failed(CAN) ENROUTE TO KINGSTON, JAMAICA, FROM TORONTO, A CRACK OCCURRED IN THE FACEPLY OF THE CO-PILOT'S WINDSCREEN. ON DESCENT INTO KINGSTON, THE PLY BEGAN TO DELAMINATE. APPROXIMATELY 2/3'S OF THE FACE PLY DEPARTED THE AIRCRAFT PRIOR TO TOUCHDOWN IN JAMAICA.Feb 13, 2002 · Cndair CL604 · Flight Compartment WindowsSDR CA020215001Wire Harness · chafed(CAN) DURING TAKE-OFF ROLL, THE POWER SET TO TAKE OFF N1, THE SPEED WERE JUST CALLED ALIVE, WHEN THE LEFT ENGINE ROLLED BACK TO IDLE. THE AIRCRAFT WAS TAXIED CLEAR AND WHILE TAXIING BACK TO FBO LEFT ENGINE SHUT DOWN. THE CAS MESSAGE INDICATED HYD SOV 1 AND ENGFeb 11, 2002 · Cndair CL604 · Fire DetectionSDR CA020201014Nut · missing(CAN) DURING A PRE-DELIVERY INSPECTION A NUT WAS DISCOVERED MISSING ON BOLT ON CONTROL ROD ASSEMBLY AND TORQUE TUBE AFFECTING THE PCU RUDDER TORQUE TUBE ASSEMBLY. A FLEET INSPECTION WAS CARRIED OUT AND NO OTHER AIRCRAFT FOUND WITH SIMILAR PROBLEM.Jan 28, 2002 · Cndair CL604 · Rudder Control SystemSDR CA020402008Bolt · broken(CAN) IN THE PROCESS OF PERFORMING A D.I. THE ENGINEER FOUND A MISSING BOLT ON THE NR 4 MAIN WHEEL ASSY. UPON REMOVAL OF THE WHEEL THE HEAD OF THE BOLT AND HALF OF THE SHANK WHERE STILL IN THE INBOARD WHEEL HALF. THE THREADED END OF THE BOLT AND NUT WERE LATERDec 13, 2001 · Cndair CL604 · Wheel/Ski/FloatSDR CA011121011Windshield · cracked(CAN) IN CRUISE, OUTER LAYER OF LEFT WINDSHIELD CRACKED - COMPLETED UNEVENTFUL LANDING. TEMPORARY REPAIR CARRIED OUT ON WINDSHIELD FACE PLY AS PER CH 56-10-00A-205. AIRCRAFT FERRIED BACK TO YYZ BASE AND WINDSHIELD REPLACED AND AIRCRAFT RETURNED BACK TO SERVICNov 6, 2001 · Cndair CL604 · Flight Compartment WindowsSDR 2002F00003Support · crackedTHE FLANGE OF THE WATER SEPARATOR SUPPORT ASSEMBLY WAS CRACKED IN TWO PLACES.Sep 11, 2001 · Cndair CL604 · Fuselage Miscellaneous StructureSDR CA011005005Brace · loose(CAN) AFTER TAKEOFF, AT 700 FEET AGL, CREW THROTTLED BACK & FOUND THAT LEFT THROTTLE WAS STIFF. THEY ATTEMPTED TO REDUCE POWER FURTHER, BUT IT COULD NOT BE REDUCED ANY LOWER THAN 90 PERCENT. THROTTLE COULD BE ADVANCED SLIGHTLY BUT WOULD ONLY OPERATE BETWEEN 90Aug 21, 2001 · Cndair CL604 · Nacelle/Pylon, Plate/SkinSDR TJ42001F00000Static Port · damagedWHILE TROUBLESHOOTING A STATIC LEAK ON THE EMERGENCY STATIC SYSTEM, I FOUND A PIN HOLE IN THE CASTING OF THE STATIC PORT. THIS PIN HOLE WAS INSIDE THE PRESSURE VESSLE AND WAS LEAKING AT A RATE OF 200 FPM. THIS PROBLEM IS NOT DETECTABLE UNLESS ONE IS CHECKING Jun 20, 2001 · N15SP · Cndair CL604 · Pitot/Static SystemSDR 2001FA0000214Interphone · unserviceableON TAXI IN, CREW EXPERIENCED A LOUD CONTINUOUS SQUEAL IN THEIR HEADSETS AND ALSO OVER THE COCKPIT SPEAKERS. COMMUNICATION WAS IMPOSSIBLE WITH THE TOWER. OUR CUSTOMER SERVICE REP HAD US DISCONNECT THE HEADPHONE/MIC JACK ASSEMBLY IN THE AFT EQUIPMENT BAY. THEJun 6, 2001 · N15SP · Cndair CL604 · Interphone/Passenger Announcement (PA) SystemSDR CA010511026Actuator · failed(CAN) OVERHEAT OF THE ACCUMULATOR, THE ELECTRIC WIING, LOWER ENGINE FAIRING AND THE LOWER CENTRAL PART OF THE NACELLE DUE TO DE-COUPLING OF THE COMPRESSED AIR INTAKE AND THE 10TH STAGE HOT AIR PORTION. THIS COUPLING IS IN A HARD TO READ AREA AND IS HARD TO TIGApr 21, 2001 · Cndair CL604 · Engine Bleed Air SystemSDR CA010426026Tire · failed(CAN) A/C DEPARTED TOLUCA, MENCO & LANDED AT TORONTO. UPON ARRIVAL IT NOTED THAT NR 3 MAIN WHEEL TIRE MISSING ITS TREAD. GTAA OPS STAFF RPTED NO DEBRIS ON LDG RWY. THEREFORE SEPARATION, MOST LIKELY OCCURRED ON TAKEOFF FROM TOLUCA. BASED ON ATMOSPHERIC CONDITIOApr 3, 2001 · Cndair CL604 · TireSDR CA010205028Pump · leaking(CAN) FUEL FOUND IN BOTH STANDBY AND APU FUEL BOOST PUMPS UNDER PLUG (REF CMM 28-20-78 PAGE 1010, ITEM 100).FUEL WAS FOUND ON BOTH SIDE OF PLUG AND ALSO FOUND IN CONDUIT WHERE WIRING FOR PUMP RUNS TO FRONT SPAR. LOCATION OF LEAK UNKNOWN AT THIS TIME.SEE ATTACHDec 11, 2000 · Cndair CL604 · Fuel Boost PumpSDR CA001229014O-Ring · leaking(CAN) FUEL WAS FOUND POOLED IN LEFT HAND ENGINE COWLING DURING POST FLIGHT INSPECTION. ENGINE RUN CARRIED OUT FOR LEAK CHECK PURPOSES AND FOUND FUEL STREAMING FROM MFC. MFC REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2001-01-03TC: MANUFACTURE OF AIRCRAFT AND EDec 7, 2000 · Cndair CL604 · Fuel Control/Turbine EnginesSDR CA001129036Pin · failed(CAN) DURING DISASSEMBLY OF THROTTLE QUADRANT TO COMPLY WITH BOMBARDIER SB 604-76-001/RATHER FIGEAL SB FE210-76-01 IT WAS FOUND THAT PIN 160 HAD MIGRATED OUT OF LATCH ASSEMBLY. THIS PIN IS A PRESS FIT AND WE FOUND IT COULD BE REMOVED BY HAND. IF THIS PIN IS RENov 2, 2000 · Cndair CL604 · Power LeverSDR 20000601SH001Plug · damagedSHANK OF FUSE PLUG DEFLECTS FROM PLUG CENTER AXIS ENOUGH TO ALLOW PACKING TO ESCAPE FROM ITS GROOVE IN THE PLUG SHANK AND THE RECESS IN THE WHEEL TUBE WELL. RESULT IS LOSS OF NITROGEN PRESSURE IN TIRE. SUSPECT HEAT AFFECTS PLUG MATERIAL CAUSING MOVEMENT (DEFFeb 7, 2000 · Cndair CL604 · Landing Gear Retraction/Extension SystemSDR CA000120032Pump · failed(CAN) PRODUCTION AIRCRAFT EXPERIENCED LT ENGINE OIL PRESSURE WARNING WAS POSTED DURING FLIGHT TEST.Jan 7, 2000 · Cndair CL604 · Engine Oil PressureSDR CA991231002Clamp · broken(CAN) V-BAND CLAMP HOLDING THE FCU AND FUEL PUMP FOUND PARTIALLY BROKEN.SB73-003 8 NOT COMPLIED WITH.Nov 15, 1999 · Cndair CL604 · Engine Fuel DistributionSDR CA981019007Bushing · damaged(CAN) COUNTERSUNK WASHER FOUND INSTALLED UPSIDE DOWN ON BOLT P/N NAS6712D52 IN OTHER WORDS, THE COUNTERSINK IS FACING AWAY FROM HEAD OF BOLT. COUNTERSINK BEARING AGAINST THE BUSHING DAMAGING IT.Oct 7, 1998 · Cndair CL604 · Wing, Attach FittingsSDR CA980721019Wire · chafed(CAN) YAW DAMPER NR 2 FAILED. STABILIZER AUGMENTATION COMPUTER REPLACED. ONE HOUR INTO FLIGHT, NR 2 YAW DAMPER FAILED AGAIN. LOW RESISTANCE READINGS ON 26 VAC AND LVDT EXC YDZ OUTPUT FROM STABILIZER COMPUTER WAS TRACED TO A SHORTED WIRE IN THE LEFT WING LEAJul 17, 1998 · Cndair CL604 · Auto Flight System Wiring
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