GE CF34-3B

Service difficulty reports · 158

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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 engine_model_key = 'CF343B'
  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 CA120214004Structure · detached(CAN) LOWER LT ENGINE TRANSLATING COWL COME LOOSE IN FLIGHT AND DEPART THE ACFT SHORTLY AFTER DEPARTURE. THE DEPARTING COWL CAUSED DAMAGE TO THE LT LOWER FUSELAGE AREA, AFT OF THE PRESSURE BULKHEAD IN THE APU BAY. DAMAGE INCLUDED DENTED/GOUGED SKIN AND DEFLEFeb 12, 2012 · Cndair CL6002B19 · Engine Thrust ReverserSDR 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 - Nov 24, 2011 · Cndair CL604 · Landing Gear Position and WarningSDR 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 WANov 16, 2011 · Cndair CL604 · Water/Waste System WiringSDR 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 CAUTOct 24, 2011 · Cndair CL604 · AC Generator-AlternatorSDR 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 Oct 9, 2011 · Cndair CL604 · Buffet/GalleysSDR CWQA09202011Wire · chafedNR 1 HYDRAULIC SYSTEM QUANTITY INDICATED 2 PERCENT DURING CLIMB, CHECK LIST FOLLOWED AND UNSCHEDULED LANDING PERFORMED WITHOUT INCIDENT. MAINTENANCE EVALUATION REVEALED NR 1 GENERATOR BLUE WIRE TB209 CHAFED AGAINST, ARCHED, AND BURNED HOLE IN NR 1 HYDRAULIC SSep 19, 2011 · N604GM · Cndair CL6002B16 · Hydraulic Power System WiringSDR CA120111003Pdu · malfunctioned(CAN) ON THEIR WAY BACK TO BASE, PILOTS REPORTED A FLAPS FAIL INDICATION AT 45 DEGREE, AC LANDED WITHOUT INCIDENT AND NO EMERGENCY WAS DECLARED.Aug 24, 2011 · Cndair CL6002B16 · Trailing Edge Flap Control SystemSDR CA110711017Line · chafedTHE CUSHIONING MATERIAL USED ON A SECURING CLAMP FOR THE NR1 ENGINE DRIVEN PUMP HYD PRESSURE LINE HAD DETERIORATED, ALLOWING THE STEEL CLAMP TO CONTACT THE ALUMINUM LINE. THIS CAUSED SIGNIFICANT WEAR TO THE OUTER CIRCUMFERENCE OF THE LINE. NO LEAKAGE WAS NOTEDJul 11, 2011 · Cndair CL6002B16 · Hydraulic System, MainSDR CA120125010Display · malfunctioned(CAN) DURING POWER UP IN THE HANGAR, OR AFTER POWER CYCLE, THE PILOTS OR CO-PILOTS SETTING HAD BEEN RESET TO 22.00 AND THE ON SIDE ALTIMETER INDICATED -1000 FT. DOES NOT MAINTAIN THE PRESELECTED LOCAL AND REVERTS BACK TO 22XX. IN THE EVENT OF A ROLL BACK OR Jun 14, 2011 · Cndair CL6002B16 · Central DisplaySDR 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.May 29, 2011 · Cndair CL604 · Engine ControlsSDR 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.Feb 19, 2011 · Cndair CL604 · APU Core EngineSDR 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 1000Jan 21, 2011 · Cndair CL604 · Cabin Pressure ControllerSDR 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.Dec 31, 2010 · Cndair CL604 · Flight Compartment WindowsSDR 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.Dec 4, 2010 · Cndair CL604 · Air Data ComputerSDR 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)Dec 4, 2010 · Cndair CL604 · Central DisplaySDR O2GAN118RHWarning Light · illuminatedSTALL WARNING LIGHT ENROUTE TO DESTINATION, QRH FOLLOWED AND LANDED AT PLANNED DESTINATION, NOT PROBLEMS.Nov 28, 2010 · N118RH · Cndair CL6002B16 · Stall Warning SystemSDR 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 CNov 25, 2010 · Cndair CL604 · Pressure Regulator/Outflow ValveSDR RU3A1021Warning Message · false activationON DESCENT THRU 160 BOTH THROTTLES WERE BROUGHT TO IDLE. NR 2 LOW OIL PRESSURE LIGHT CAME ON, AND LOW OIL PRESSURE TAPE INDICATED LOW. N1 LT 65 PERCENT, RT 34 PERCENT, POWER RE-APPLIED AND ENGINE RECOVERED. MX CHECKED ENGINE ON GROUND AND NO FAULT FOUND.Nov 1, 2010 · N86 · Cndair CL6002B16 · Engine Oil PressureSDR CA101101006Smoke Detector · shorted(CAN) PLEASE BE ADVISED WE HAD AN INCIDENT ABOARD THE ABOVE AIRCRAFT ON APPROACH TO AIRPORT ON THE 1ST OCTOBER 2010. THE FOLLOWING IS THE COMMANDERS REPORT. FL 400 APPROACHING TOD P2 HANDLING, NIGHT, 3 PAX, 2 PILOTS, 1 CABIN ATTENDANT. BAGGAGE BAY SMOKE WAOct 1, 2010 · Cndair CL604 · Smoke DetectionSDR O2GA20100725001Generator · inoperativeNR 1 GENERATOR WENT OFFLINE IN FLIGHT.Jul 25, 2010 · N604GR · Cndair CL6002B16 · AC Generator-AlternatorSDR J7SA5752100528Overheat Loop · out of position'R 14TH STGE DUCT' CAS MESSAGE POSTED. CREW PERFORMED IN-FLIGHT SHUTDOWN OF RT ENGINE AND DECLARED AN EMERGENCY. ACFT LANDING UNEVENTFUL. MX FOUND NO INDICATION OF ACTUAL OVERHEAT OR FIRE. FOUND A GROMMET THAT PLACE THE LOOP IN A BAD ROUTING CONDITION. MOVMay 27, 2010 · N342FX · Cndair CL6002B16 · Overheat DetectionSDR REXA201000055Engine · leakingAT THE 80 KNOT CALL OUT, ON TAKEOFF ROLL FROM KMEM THE F/O ALERTED THE CAPTAIN TO THE LT ENGINE ITT INDICATION BEING APPROXIMATELY 900 DEGREES AND IN THE RED. THE CAPTAIN ABORTED THE TAKEOFF AND CLEARED THE RUNWAY. THE QRH WAS COMPLETED AND THE CAPTAIN ELECTEApr 24, 2010 · N8560F · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CWQA04142010Duct · contaminatedREJECTED TAKEOFF DUE ANTI-ICE FLUID IN APU DUCTS CAUSING SMOKE IN PLANE. RAN ENGINES AT N1 FOR THE DAY TO CLEAR ANY ANTI-ICE FLUID. OPS CHECK GOOD. AIRCRAFT WAS DE-ICED PRIOR AND EMERGENCY EQUIP WAS REQUESTED AFTER EVENT.Apr 14, 2010 · N604B · Cndair CL604 · APU Bleed Air SystemSDR CA100216009Rod · unserviceable(CAN) BOTH THROTTLE ACTUATOR RODS WERE FOUND WITH CHAFING DAMAGE RESULTING FROM CONTACT WITH THE ELEVATOR TORQUE TUBE ASSY PN 600-90410-803. THE CONTACT WAS WHEN THE THROTTLES WERE IN OR BETWEEN IDLE AND CUTOFF. LOCATION DAMAGE ON THE RODS IS AT THE FIRST BEFeb 14, 2010 · Cndair CL604 · Power LeverSDR CA100119002Deice System · failed(CAN) UPON RETURN FROM FLIGHT, HEATED DRAIN MAST WAS COVERED OVER WITH ICE INDICATING THAT IT WAS NOT FUNCTIONING IN FLIGHT. WHEN THE ACFT WAS PLACED IN THE HANGAR, ELECTRICAL POWER APPLIED AND THE SKIN REMAINED BELOW 45 DEG AND ALLOWED ELECTRICAL CURRENT TO Jan 18, 2010 · Cndair CL604 · Water Line Anti-Ice SystemSDR CA091218003Power Lever · stiff(CAN) CAPTAIN REPORTED THE NR 1 THRUST LEVER WAS STIFF TO OPERATE AND GETTING WORSE AS FLIGHT CONTINUED. A RETURN TO THE FIELD OF DEPARTURE WAS CARRIED OUT. (TC NR 20091218003)Dec 17, 2009 · Cndair CL604 · Power LeverSDR CA091201001Oil System · low pressure(CAN) DURING THE TAKEOFF ROLL, THE RT ENG LOW OIL PRESS INDICATION CAME ON THE CREW REDUCED ENGINE POWER TO IDLE AND THE ENGINE SHUT DOWN UNCOMMANDED AIRCRAFT RETURNED TO PARKING POSITION. INVESTIGATION ON GOING, FIRST CHECK OF OIL LEVEL SHOWED SUFFICIENT OILNov 30, 2009 · Cndair CL604 · Turbine Engine Oil SystemSDR CA091202015Solenoid · open(CAN) MLG FAILED TO DEPLOY. QRH PROCEDURES FOLLOWED, ALT EXTENSION CARRIED OUT. T/S DISCOVERED OPEN CIRCUIT ON EXTEND SOLENIOD OF MLG SELECTOR VALVE. VALVE CHANGED AND GEAR SWINGS COMPLETED PER AMM. A/C RETURNED TO SERVICE. (TC NR 20091202015)Nov 25, 2009 · Cndair CL604 · Landing Gear Retraction/Extension SystemSDR CA091201004Transmitter · malfunctioned(CAN) CADOR 2009C3326 ON TAKEOFF WHEN THE PILOT ADVANCED THE THRUST LEVERS HE GOT A CONFIGURATION SPOILER WARNING MESSAGE. THE TAKEOFF WAS REJECTED AND THE AIRCRAFT RETURNED TO BASE. UPON INVESTIGATION IT WAS FOUND THAT MAINTENANCE WAS PERFORMED ON THE RT FLIGNov 24, 2009 · Cndair CL604 · Drag Control SystemSDR CA091105001Fcu · obstructed(CAN) ON DESCENT LT ENG PWR LEVER COULD NOT BE RETRACTED. AN IN FLIGHT SHUTDOWN WAS CARRIED OUT. ACFT LANDED AT DESTINATION WITHOUT FURTHER INCIDENT. SUBSEQUENT INVESTIGATION FOUND THE LT ENG UPPER CORE COWL STAY OUT OF PLACE AND INTERFERING WITH THE FCU. THENov 4, 2009 · Cndair CL604 · Fuel Controlling SystemSDR CA091120002Rod · loose(CAN) DURING FLIGHT THE CREW COULD NOT RETARD THE LT THROTTLE. ENG WAS SHUTDOWN AND AN UNEVENTFUL LANDING MADE. IT WAS SUBSEQUENTLY FOUND THE UPPER COWL SUPPORT ROD HAD COME OUT OF ITS STORAGE CLIP AND FALLEN ONTO THE THROTTLE LINKAGE.Nov 1, 2009 · Cndair CL604 · Nacelle/Pylon Miscellaneous StructureSDR CA090924008Case · cracked(CAN) UPON CLEANING OF FAN ASSY. DURING MX EVENT, IT WAS NOTICED THAT A 3 INCH CRACK AFT OF THE FAN STATOR RING WAS PRESENT. FURTHER INVESTIGATION REVEALED A CRACK PROPOGATING ALONG 2 BOLT HOLES THAT ATTACH THE FAN CASE TO THE THRUST REVERSER DEFLECTOR RING.Sep 21, 2009 · Cndair CL604 · Turbine Engine Compressor SectionSDR CA091020004Case · cracked(CAN) CRACKS TO THE AFT FAN CASE PN 6052T01G08 WERE DISCOVERED PRIOR TO SCHEDULED ACFT ENG WATER WASH. 2 CRACKS ALONG THE HORIZONTAL AXIS OF THE FAN CASE CONTINUING DOWNWARD ALONG THE FLANGE. ENG HASE BEEN REMOVED FOR FAN CASE REPAIR.Sep 21, 2009 · Cndair CL604 · Turbine Engine Compressor SectionSDR CA090731005Sensing Element · chafedCREW REPORT AT 14,000 FT GOT RT ENGINE FIRE WARNING. WARNING WENT OUT WHEN PWR LEVER WAS PULLED TO IDLE. SECURED ACFT VIA CHECKLIST. DID NOT USE ENG FIRE EXTINGUISHERS. RT ENG COMBUSTION SECTION FIRE DETECTION SENSE ELEMENT, PN:244-10457 SN:9724 REMOVED DJul 28, 2009 · Cndair CL604 · Fire DetectionSDR CA090728002Heater · overheated(CAN) OPERATOR REPORTED AFTER A 4 HR FLIGHT THAT SUITCASES STORED IN BAGGAGE COMPARTMENT ON THE FLOOR JUST INSIDE CARGO NET (RT SIDE) ARE TOO HOT TO TOUCH. ONE SUITCASE HAS SUFFERED HEAT DAMAGE (DAMAGE TO THE CREW SUITCASE HANDLE). MX WIRING VERIFICATION DONJul 27, 2009 · Cndair CL604 · Heating SystemSDR 2009FA0000895Pressure Switch · failedDID THE NEW FULL FUNCTIONAL CHECK OF OUR SENSORS ON OUR CF343B AND IT TOOK SOME TIME TO GET THE ONE SENSOR TO PASS AND THE OTHER ENGINE SENSOR NEEDED TO BE REPLACED. ON THAT SENSOR YOU COULD HEAR THE MECHANICAL HALF OF THE SENSOR ACTUATING BUT THE CONTACTS INJul 2, 2009 · N43R · Cndair CL6002B16 · Engine Oil Indicating SystemSDR CA090629006Apu · failed(CAN) WHILE THE ACFT WAS TAXIING TO FBO RAMP, SMOKE AND FLAMES WERE COMING OUT OF THE APU INLET. APU WAS SHUTDOWN. APU ENCLOSER AND INTAKE WAS INSPECTED, CHECKED OIL LEVEL AND CHIP DETECTOR. FOUND TO BE OK. TRIED TO START THE APU, IT WOULD ACCELERATE TO 14Jun 23, 2009 · Cndair CL604 · APU Core EngineSDR CA090716001Bearing · failed(CAN) THE APU WAS STARTED IN FLIGHT AND ACFT LANDED. WHEN IT GOT TO FBO SMOKE STARTED TO COME INTO CABIN. IT WAS NOT BAD ENOUGH TO WARRANT AN EMERGENCY EVACUATION AND AS APU SHUT ITSELF DOWN IT DID NOT GET ANY WORSE. IT WAS OBSERVED BY FBO THAT AT THE SAME Jun 23, 2009 · Cndair CL604 · APU Core EngineSDR CA090614001Unknown · smoke(CAN) AFTER TAKEOFF ON RUNWAY 06R AT APPROX 500 FEET AGL BLUE SMOKE WAS OBSERVED COMING OUT BETWEEN GLARESHIELD AND WINDSHIELD CTR POST. ACRID ODOR. ELECTRICAL IN NATURE. EMERGENCY DECLARED AND IMMEDIATE RETURN REQUESTED TO ATC. LANDING WAS PERFORMED ON 24Jun 12, 2009 · Cndair CL6002B16 · Air Distribution SystemSDR CA090401011Holder · melted(CAN) NEON LIGHT, PLASTIC HOLDING CLAMP MELTED DOWN. THIS NEON IS LOCATED IN THE CABIN GALLEY. IT HAS BEEN DETECTED BY THE ODOR (SMELL IN THE CABIN). MFG HAS BEEN ADVISED AND THEY WILL WRITE A CONDITION REPORT. AT THE TIME OF THE SNAG, ACFT WAS ON EXTERNAL Apr 1, 2009 · Cndair CL604 · Passenger Compartment LightingSDR CA090318002Balance Tube · blocked(CAN) FOLLOWING RECEPTION OF ADVISORY WIRE NR AW604-28-0082, BORESCOPE INSP HAS BEEN PERFORMED IN THE 1 AND 3 INCHES FUEL BALANCE TUBES OF BOTH WINGS. THE RESULT IS, ALL TUBES SEALED WITH PRC ARE PARTIALLY BLOCKED (ESTIMATED AVERAGE BLOCKAGE 10 TO 20 PERCENT, Mar 5, 2009 · Cndair CL604 · Aircraft Fuel Distribution SystemSDR CA090202007Duct · dented(CAN) WHILE IN SCOTTSDALE, ARIZONA, DURING THE PREFLIGHT CHECK THE CREW NOTICED THE APU INLET WAS DENTED AND APU INLET BELLOWS WAS RIPPED. NO OPERATIONAL ABNORMALITY WERE NOTICED BY THE CREW PRIOR TO THE DISCOVERY. MAINTENANCE TECHNICIAN WAS DISPATCHED AND BJan 29, 2009 · Cndair CL604 · APU Cowling/ContainmentSDR CA090127005Butterfly Valve · brokenPILOT REPORTED LEFT AIR CONDITIONING PACK BLOWS HOT AIR REGARDLESS OF TEMPERATURE SELECTION. SYSTEM INTERROGATED AND DETERMINED THE LOW PRESSURE MODULATING AND SHUTOFF VALVE DEFECTIVE. CLOSE INSPECTION OF VALVE PLENUM DETERMINED BUTTERFLY VALVE HAD BEEN EJECJan 20, 2009 · Cndair CL604 · Air Distribution SystemSDR CA090116015Control System · malfunctioned(CAN) RT ENGINE WAS SHUTDOWN IN PREPARATION FOR WINDMILL RELIGHT. DURING THE DESCENT AT 320 KTS TO DETERMINE UNLOCKING OF THE ENGINE N2 REACHED 13.6% BY APPROX 24000 FEET. N2 WAS 12.6% AT 21000 FT. SUBSEQUENT ATTEMPT TO ATS RELIGHT THE ENGINE WAS NOT SUCCESJan 16, 2009 · Cndair CL6002B19 · Fuel Controlling SystemSDR CA090102002Flap System · malfunctioned(CAN) ON APPROACH THE FLAP FAILED TO EXTEND AND THE AIRCRAFT DIVERTED WHERE THEY LANDED WITH THE FLAPS UP. UPON INSPECTION FOUND THE FLAPS WOULD NOT MOVE AND WERE IN ASYMMETRIC CONDITION. BOTH THE LT AND RT BDU WERE REPLACED AND THE FLAP SYSTEM TESTED SERVICDec 24, 2008 · Cndair CL604 · Trailing Edge Flap Control SystemSDR CA081218003Display · malfunctioned(CAN) IN CRUISE FL 380, 3.5 HOURS IN FLIGHT, THE MFD NR 2 LOWER WINDOW STARTED TO CYCLE BETWEEN THE DIFFERENT FORMATS (PPOS, PLAN, TCAS ECT) AT FEW SECONDS INTERVAL WITH UNDEFINED SYMBOLS/TEXT LINE (HIEROGLYPH). AT THAT TIME THE PFDS 1 AND 2, MFD 1 SHOWED NORDec 16, 2008 · Cndair CL604 · Central DisplaySDR CA081205002Display · inoperative(CAN) 30 MINUTES PRIOR TO LANDING, THE PILOT PRIMARY FLIGHT DISPLAY(PFD 1) WENT BLANK. THEN IAW AFM (SECTION 05-15-1) THE CREW SELECTED THE REVERSION MODE TO HAVE THE MULTIFUNCTION DISPLAY (MFD 1) IN COMPRESSED MODE, AT THAT TIME THE MFD 1 ALSO WENT BLANK. THENov 23, 2008 · Cndair CL604 · Navigation SystemSDR SWIA200820187Carbon Seal · leakingFLT 3799 - AFTER TAKEOFF AIRCRAFT FILLED WITH SMOKE AND WE RECEIVED THE TOILET SMOKE CAUTION. FOUND NR 3 CARBON SEAL LEAK LEFT ENGINE. REPLACED ENGINE. Oct 16, 2008 · N455SW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA080923002Window · cracked(CAN) WHILE IN CRUISE, CREW EXPERIENCED THE FAILURE OF THE COCKPIT LT SIDE WINDOW OUTER MAIN PLY. A CRACK SPANNED FROM THE LOWER FWD FRAME, TO THE FWD SECTION OF THE UPPER FRAME OF THE WINDSHIELD. THE ACFT HAD DEPARTED AND WAS ENROUTE SOUTHBOUND WHEN THE FAISep 22, 2008 · Cndair CL604 · Flight Compartment WindowsSDR CA080903006O-Ring · deteriorated(CAN) DEPARTING, EN ROUTE, NR3 HYDR SYS LO PRESS. LIGHT CAME (ON) AND QTY READ 2 PERCENT. ACFT RETURNED TO BASE. INVESTIGATION SHOWED A (BLOWN) SEAL ON PRIORITY VALVE IN THE LANDING GEAR WHEEL WELL. O-RING FOUND DETERIORATED. REPLACED O-RING, FUNCTION TESTEDAug 31, 2008 · Cndair CL604 · Landing Gear Retraction/Extension System
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