Cessna 650

Service difficulty reports · 491

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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 = '650'
  ORDER BY difficulty_date DESC"

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SDR FCPR20070006Ballscrew · failedFLAP ACTUATOR DRIVE CARRIAGE BALLSCREW NUT FAILED. FLAPS WOULD NOT MOVE.May 18, 2007 · N651CV · Cessna 650 · Trailing Edge Flap ActuatorSDR 2007FA0000368Doubler · fatiguedTHE 6213011-139 LT DOUBLER AND THE 6213011-140 RT DOUBLER FATIGUE CRACKING ON BOTH. THE 6213011-139 LT DOUBLER AND THE 6213011-140 RT DOUBLER, ON MODEL 650 IS PART OF THE NOSE WHEEL WELL ASSY, HAS BEEN FOUND WITH FATIGUE CRACKING ON MULTIPLE SN. CURRENTLY THApr 20, 2007 · Cessna 650 · Fuselage Main, StructureSDR 2007FA0000367Doubler · fatiguedTHE 6213011139 LT DOUBLER AND THE 6213011140 RT DOUBLER FATIGUE CRACKING ON BOTH. THE 6213011139 LT DOUBLER AND THE 6213011140 RT DOUBLER, ON MODEL 650 IS PART OF THE NOSE WHEEL WELL ASSY, HAS BEEN FOUND WITH FATIGUE CRACKING ON MULTIPLE SN. CURRENTLY THE PAApr 20, 2007 · Cessna 650 · Standard Practices/StructuresSDR BTA2007F00000Unknown · malfunctionedRT ENGINE FIRE LIGHT CAME ON DURING CLIMBOUT, RETARDED THROTTLE LIGHT WENT OUT, ADVANCED THROTTLE LIGHT CAME BACK ON AND LANDED. PERFORMED LEAK CHECKS WITH COWLING OPEN, RAN AT FULL POWER FOR 10 MINUTES, COULD NOT DUPLICATE PROBLEM. FLEW AIRCRAFT BACK TO HOMApr 5, 2007 · N86VP · Cessna 650 · Fire DetectionSDR DXTA200702072Engine · malfunctionedLEFT ENG ROLLED BACK TO 91% N1 ON T/O ROLL (APROX 80 KNOTS). T/O ABORTED. INSP EEC FOR FAULTS NONE NOTED. RAN A/C AT ALL POWER SETTINGS IN AUTO & MANUAL MODES. NO ROLL BACK NOTED SYSTEM OP'S CHECKS SATISFACTORY AT THIS TIME ALL WORK DONE IAW CE 650 M/M 76-10-0Apr 3, 2007 · N713QS · Cessna 650 · Engine (Turbine/Turboprop)SDR 03192007650ZHose · crackedLT UPPER ACTUATOR LINE WAS FOUND TO HAVE A CRACK IN THE ELBOW, CAUSING A HYDRAULIC FLUID LEAK. MATERIAL IN THE ELBOW OF THE HOSE LOOKS GRAINY AS IS STRESSED WHILE FORMING.Mar 19, 2007 · N650Z · Cessna 650 · Hydraulic System, MainSDR DXTA200702018Switch · out of adjustLANDING GEAR WOULD NOT RETRACT. AFTER TAKEOFF. GEAR HANDLE WOULD NOT MOVE. TROUBLESHOT TO NOSE CENTERING SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH IAW 650 MM 32-60-00. OPS CHECK GOOD IAW SAME.Mar 13, 2007 · N715QS · Cessna 650 · Landing Gear Retraction/Extension SystemSDR DXTA200702000Strut · underservicedLANDING GEAR WOULD NOT RETRACT (HANDLE WOULD NOT COME UP) AFTER TAKEOFF. TROUBLESHOT NOSE LANDING GEAR - FOUND NOSE STRUT NOT FULLY SERVICED - SERVICED STRUT WITH FLUID AND NITROGEN IAW CESSNA M/M 12-10-38 FUNCTIONALLY TESTED GEAR - NO DEFECTS NOTED AT THIS TIMar 5, 2007 · N715QS · Cessna 650 · Main Landing Gear Strut/Axle/TruckSDR DXTA200701975Unknown · smokeDISTINCT SMELL OF ELECTRICAL SMOKE IN CABIN AND COCKPIT AND A NOTICEABLE HAZE OF SMOKE VISIBLE. OPERATED GROUND TEST APU TWICE FOR APPROX 20-25 MIN IAW 650 MM 49-10-00. NO NOTICEABLE SIGNS OF SMOKE IN CABIN. RAN CABIN TEMP TO FULL HOT AND COLD. BITE CHECKED Feb 28, 2007 · N795QS · Cessna 650 · Air Distribution SystemSDR DXTA200701933Wire · brokenRT ENGINE FIRE DETECT ANUNCIATOR ILLUMINATED AFTER COCKPIT PREP WAS COMPLETED. T/S TO BROKEN RT FIRE LOOP ON ENG. REMOVED & REPLACED FIRE LOOP. BLEED T/R'S, SYSTEM OP'S CHECKS SATISFACTORY AT THIS TIME. ALL WORK DONE IAW CE 650 M/M 26-10-01Feb 13, 2007 · N791QS · Cessna 650 · Fire Protection System WiringSDR DXTA200701867Control Module · inoperativeLANDING GEAR WOULD NOT RETRACT, AFTER T.O. OUT OF SFO. FINALLY 2-3 SECONDS LATER THE GEAR CAME UP. REMOVED AND REPLACED THE LANDING GEAR CONTROL PERFORMED 10 GEAR SWINGS OSP CHECKS GOOD ALL WORK DONE IAW CE-650 M.M. 32-30-01Jan 19, 2007 · N715QS · Cessna 650 · Landing Gear Retraction/Extension SystemSDR A8J2007F00001Circuit Board · faultyON 1/10-07 AT 1900, AIRCRAFT EXPERIENCED AN AILERON BOOST FAILURE. PILOT DECLEARED AN EMERGENCY AND LANDED AT ITS SCHEDULE DETINATION WITHOUT ANY COMPLICATIONS. AILERON BOOST CIRCUIT BOARD WAS REPLACED AND THE SYSTEM CHECKED GOOD. (K)Jan 10, 2007 · N777XS · Cessna 650 · Aileron Control SystemSDR 01082007650ZUnknown · unknownDISCREPANCY (PRIMARY TRIM INDICATOR DOES NOT MOVE FULL RANGE.) DURING FLIGHT, FLIGHT CREW OBSERVED INTERMITTENT FAILURE OF THE HORIZONTAL STABILIZER PRIMARY TRIM (CLACKER). UPON ARRIVAL, FLIGHT CREW PERFORMED ALL PRE AND POST TAKEOFF OPERATIONAL CHECKS AND OBSJan 8, 2007 · N650Z · Cessna 650 · Stabilizer Position IndicatingSDR DXTA200701837Unknown · unknownAIRCRAFT EXPERIENCED UNCOMMANDED HARD LT YAW CAUSED BY YAW DAMPER. OPERATION CHECK OF A AND B YAW DAMPER SYSTEMS GOOD, SPZ-8000 DIAG. TEST GOOD. RUDDER SERVO OPERATION CHECK GOOD, FLIGHT GUIDANCE, FGC'S, AND AHRS SYSTEMS CHECK GOOD IAW MFG SPZ-8000 AFCD MM SECJan 4, 2007 · N715QS · Cessna 650 · Auto Flight SystemSDR DJFA2007002Computer · odorKLUK-KTUL TRIP 1124319 THE CREW REPORTED A STRONG ELECTRICAL BURNING ODOR IN THE COCKPIT AREA WITH NO SMOKE PRESENT. THEY WERE UNABLE TO ISOLATE IN FLIGHT. MAINTENANCE TROUBLESHOT THE ELECTRICAL SMELL AND ISOLATED IT TO THE STALL WARNING COMPUTER. THE STALLJan 2, 2007 · N364CW · Cessna 650 · Stall Warning SystemSDR 2007F00001Control Unit · defectivePRIMARY TRIM ANNUNCIATOR COMES ON INFLIGHT. SECONDARY TRIM FAIL LIGHT ILLUMINATES ALSO AND STAB TRIM WILL NOT MOVE. TROUBLESHOT STABILIZER SYSTEM; FOUND HORIZONTAL STABILIZER ACTUATOR CONTROL UNIT DEFECTIVE. REPLACED AS REQUIRED; PERFORMED FUNCTIONAL CHECK FLIDec 27, 2006 · N40FC · Cessna 650 · Stabilizer Position IndicatingSDR ZLWA0603Cabin Pressure · uncontrollableCABIN DEPRESSURIZED AT 20,000 FEET, 8500 FT LIGHT ILLUMINATED AND MADE AN EMERGENCY DESCENT. MAINTENANCE INSPECTED SYSTEM COMPONENTS WITH NO DEFECTS NOTED. UNABLE TO DUPLICATE DISCREPANCY.Dec 4, 2006 · N77HF · Cessna 650 · Cabin Pressure Control SystemSDR DXTA200601777Control Module · inoperativeGEAR WOULD NOT RETRACT AFTER TAKE OFF , GEAR HANDLE STUCK IN THE DOWN POSITION. RETURNED TO AIRPORT. REMOVED AND REPLACED LANDING GEAR CONTROL IAW CE 650 M/M CHP 32-30-01, OPS CHECKED AND CYCLED X 10. CHECKS GOODDec 3, 2006 · N715QS · Cessna 650 · Landing Gear SelectorSDR DXTA200601645Annunciator · inoperativeUPON ADVANCING POWER FOR T/O, ENGINE OIL PRESSURE WARNING LIGHT CAME ON. TAPES FOR TEMP AND PRESSURE INDICATED NORMAL. INSTALLED REPAIRED ANNUNCIATOR PANEL IAW CESSNA 650 MM CHAP 31-10-01, OPS CHECK GOOD.Oct 11, 2006 · N710QS · Cessna 650 · Engine Oil Indicating SystemSDR DXTA200601615Link · wornAFTER TAKEOFF GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. CHECKED SYSTEM FOR PROPER OPERATION, COULD NOT DUPLICATE. CHECKED NOSE SQUAT SWITCH FOUND NOSE CENTERING LINK ASSY NOT GRABBING CENTERING SWITCH TO ACTUATE PROPERLY. REMOVED AND REPLACED NOSE CENTSep 25, 2006 · N787QS · Cessna 650 · Landing Gear Retraction/Extension SystemSDR ZLWA0602Cabin Pressure · failedCLIMBING THROUGH FL230, CABIN LOST PRESSURE CONTROL. CABIN WENT TO 20,000, MASK DROPPED. AIRCRAFT WAS INSPECTED AND NUMEROUS TEST RUNS PERFORMED ON AIRCRAFT. ALL SYSTEMS WERE CHECKED AND THE PRESSURIZATION SYSTEM CHECKED GOOD. NO SYSTEM OR COMPONENT FOUND FAULAug 30, 2006 · N650K · Cessna 650 · Cabin Pressure Control SystemSDR CA060822001Bolt · broken(CAN) ON DAILY INSPECTION, FOUND (1) BOLT BROKEN ON NR 4 MAIN WHEEL ASSY. (TC NR 20060822001)Aug 5, 2006 · Cessna 650 · Wheel/Ski/FloatSDR 2006FA0000767Wire Harness · damagedDUAL TRANSPONDER FAILURE IN HEAVY PRECIPITATION. NO FAILURE INDICATION ON SPZ8000 SYSTEM. CENTER REQUESTED RESET OF TRANSPONDER, AND DIRECTED OUT OF RVSM AIRSPACE WHEN UNSUCCESSFUL. HANGAR TESTS OF POWER OUTPUT SHOWED 40WATTS BEFORE CABLES REPLACED, AND 400 WJul 31, 2006 · N96MT · Cessna 650 · Navigation System WiringSDR 2006FA0000766Wire Harness · damagedDUAL TRANSPONDER FAILURE IN HEAVY PRECIPITATION. NO FAILURE INDICATION ON SPZ8000 SYSTEM. CENTER REQUESTED RESET OF TRANSPONDER, AND DIRECTED OUT OF RVSM AIRSPACE WHEN UNSUCCESSFUL. HANGAR TESTS OF POWER OUTPUT SHOWED 40WATTS BEFORE CABLES REPLACED, AND 400 Jul 31, 2006 · N96MT · Cessna 650 · Navigation System WiringSDR 2006FA0000868Switch · mismanufacturedAFTER ARRIVAL, FOUND FUEL LEAK NEAR IB END OF RT WING. INVESTIGATION SHOWED THE LOW LEVEL FUEL LIMIT SWITCH WAS NOT ASSEMBLED. THE FLOAT, PN L15F2, WAS NOT ATTACHED TO THE MOUNT ASSY PN 62266503. THIS ALLOWED FUEL TO LEAK FROM THE WING. SWITCH WAS ASSEMBLEJul 20, 2006 · N993LC · Cessna 650 · Fuel Indicating SystemSDR IJ02006F00000Actuator · crackedAFTER TAKEOFF, THE AIRCRAFT EXPERIENCED A LOSS OF HYDRAULIC PRESSURE, DURING LANDING GEAR RETRACTION. THE CREW RETURNED THE GEAR TO THE EXTENDED POSITION AND DECLARED AN EMERGENCY WITH ATC. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INVESTIGATION REVJul 18, 2006 · N651CV · Cessna 650 · Landing Gear ActuatorSDR DXTA200601472Acm · leakingDURING FLIGHT FROM GSO TO LUK, REAR ACM LEAKING OIL WITH STRONG ODOR IN CABIN. AIRCRAFT CONTINUED AND LANDED AT LUK. REMOVED AND REPLACED REAR ACM, INSTALLED AN OVHD UNIT OF THE SAME P/N WORK DONE IAW HAMILTON STANDARD MM 21-50-03. SERVICED TO PROPER LIMITS.Jul 1, 2006 · N795QS · Cessna 650 · Cabin Cooling SystemSDR 2006FA0000910Shutoff Valve · misinstalledDETERMINED THE PRESSURE REGULATOR SHUTOFF VALVE WAS LEAKING. FOUND THE REGULATOR HAD BEEN INSTALLED WITHOUT GASKETS. THE PARTS MANUAL DOES NOT CLEARLY IDENTIFY THAT GASKETS ARE REQUIRED TO BE INSTALLED WITH THIS SPECIFIC PN OF VALVE. CONTACTED AND CONFIRMEDJun 26, 2006 · N993LC · Cessna 650 · Ice/Rain Protection SystemSDR DXTA200601382Actuator · inoperativePRIMARY AND SECONDARY STAB TRIMS FAILED IN CRUISE FLIGHT (ALTITUDE WAS FL 300 AT MACH .77). REMOVED AND REPLACED HORIZONTAL STABILIZER PRIMARY TRIM ACTUATOR IAW CESSNA 650 MM 27-40-01 AND PERFORMED APPLICABLE CHECKS. OPS CHECKED GOOD.May 6, 2006 · N797QS · Cessna 650 · Stabilizer Position IndicatingSDR DXTA200601366Controller · inoperativePRIMARY TRIM FAIL ENUNCIATOR ILLUMINATED IN FLT. FOLLOWED EMERGENCY CHECKLIST. SECONDARY TRIM FAILED TO MOVE STABILIZER. SEC. TRIM FAULT ENUNCIATOR WAS NOT ILLUMINATED AND NO TRIM CLACKER HEARD. - REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUATOR CONTROLLApr 28, 2006 · N797QS · Cessna 650 · Stabilizer Control SystemSDR LMM2006F00000Switch · defectiveDURING LANDING GEAR RETRACTION, AFTER TAKEOFF. BOTH MAIN GEAR RETRACTED NORMALLY (GREEN LIGHTS OUT). RED TRANSIENT LIGHT REMAINED ON. NOSE GEAR GREEN LIGHT WENT OUT, MOMENTARILY AND THEN CAME BACK ON. (K)Apr 18, 2006 · N650TS · Cessna 650 · Landing Gear Position and WarningSDR DXTA200601352Control Unit · inoperativeGEAR HANDLE WOULD NOT MOVE THEREFORE THAT LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED LANDING GEAR CONTROL DUE TO FAULTY DOWN LOCK SOLENOID, INSTALLED CONTROL. CONTROL AND GEAR OPERATIONAL CHECK NORMAL. WORK PERFORMED IAW THE MM CHAPTER 32-30-01.Apr 15, 2006 · N715QS · Cessna 650 · Landing Gear Retraction/Extension SystemSDR DXTA200601336Control Arm · dirtyLANDING GEAR WOULD NOT RETRACT AFTER DEPARTURE. CLEANED NOSE GEAR CENTERING ARM AND LUBED DUE TO BINDING IAW THE 650 MM CHAPTER 32-20-00. PERFORMED GEAR RETRACTION OPS CHECK. OPS CHECK NORMAL.Apr 8, 2006 · N715QS · Cessna 650 · Landing Gear Retraction/Extension SystemSDR DXTA200601292Disconnect Unit · corrodedBRAKES FADED ON ROLLOUT, TURNED ANTI-SKID OFF BRAKES WORKED NORMAL. BRAKES WOULD NOT HOLD DURING STATIC THRUST CK ABOVE 61 PERCENT N1, WITH ANTI SKID ON. ANTI SKID OFF BRAKES ARE NORMAL. REMOVED AND REPLACED CORRODED RT WHEEL WELL CONNECTOR JW18 IAW 650 WM Mar 12, 2006 · N710QS · Cessna 650 · Brake Anti-Skid SectionSDR 2006FA0000214Windshield · crackedPILOT'S GLASS WINDSHIELD SHOWED SIGNS OF OVERHEATING AT UPPER CENTER EDGE CAUSING COMPLETE CRACKING OF WINDSHIELD IN A SPIDER WEB FASHION. THE WINDSHIELD REMAINED STRUCTURALLY SOUND AND THE AIRCRAFT WAS ABLE TO LAND WITHOUT INCIDENT.Mar 8, 2006 · N430SA · Cessna 650 · Flight Compartment WindowsSDR CA060224008Turnbuckle · chafedDURING A SCHEDULED PHASE 5 INSPECTION ON CESSNA 650 C-FIMO, THE TECHNICIAN DISCOVERED THAT THE LT AND RT AILERON OUTBOARD AFT CABLE CHAFED THROUGH THE LOKCLAD AND THE TURNBUCKLE WAS DAMAGED.Feb 24, 2006 · Cessna 650 · Aileron Control SystemSDR DXTA200601245Gearbox · frozenFLAPS INOP, WOULD NOT EXTEND. FLAP INOP LIGHT ILLUM, WOULD NOT RESET. CHK`D FLAP CONTROLLER. NONE FOUND GAINED ACCESS TO FLAP PDU. DISCONNECTED RT FLAP DRIVE CABLE FROM PDU. UPON REMOVAL, DRIVESHAFT OF FLEX CABLE REMAINED IN PDU & CABLE SEPARATED FROM PDU.Feb 14, 2006 · N713QS · Cessna 650 · Trailing Edge Flap Control SystemSDR 2006FA0000159Water Separator · separatedEXPERIENCED AN ABRUPT CABIN PRESS FLUCTUATION DURING FLT. FLT CREW REPORTED, ABLE TO MAINTAIN CABIN ALT WITHIN LIMITS AFTER NOTICED PROBLEM. AFTER THIS A/C LANDED MX PERSONNEL DISCOVERED ONE OF THE ENVIRONMENTAL CONTROL SYS WATER SEPARATOR UNITS HAD SEPARATEJan 30, 2006 · N766MH · Cessna 650 · Humidity Control SystemSDR ZN3R556712Stator · separatedENGINE 4TH LPC STATOR HAD INNER RING FRACTURE, LEADING TO A SINGLE VANE SEPARATING FROM THE STATOR ASSEMBLY. THE VANE CAUSED DAMAGE TO THE HPC AREA OF THE ENGINE. AIRCRAFT DID NOT EXPERIENCE ANY PROBLEMS WITH ENGINE DURING FLIGHT, AND PERFORMED SCHEDULED LANJan 3, 2006 · N650TA · Cessna 650 · Turbine Engine Compressor SectionSDR DXTA200601182Squat Switch · intermittentDURING ROLL OUT (AT APPROXIMATELY 20 - 30 KNOTS) THE BRAKES RELEASED EVEN THOUGH THE BRAKING PRESSURE WAS NOT REDUCED. THE AIRPLANE CONTINUED ROLLING FOR APPROXIMATELY 15-30 YARDS THEN THE BRAKES KICKED BACK IN AGAIN. TROUBLESHOT BRAKE CONTROL SYSTEM, FOUND Jan 3, 2006 · N710QS · Cessna 650 · Landing Gear Position and WarningSDR DXTA200501126Coalescer Bag · contaminatedHOT OIL SMELL CAME INTO CABIN DURING CLIMB. INDICATED AIRSPEED 215 KNOTS, CLIMBING 100 FT PER MINUTE THRU 41,700 FT. ALL INDICATIONS NORMAL (OIL, HYDRAULIC AND ELECTRICAL). INSPECTED ENGINE, APU, AND ACM OIL LEVELS. ALL INDICATE FULL. REMOVED PLUMBING FRODec 3, 2005 · N790QS · Cessna 650 · Humidity Control SystemSDR DXTA200501100Control Panel · hotAT FL390 RIGHT REAR PASSENGER AUDIO & LIGHTING PANELS WERE VERY HOT TO THE TOUCH. PANELS COOLED OFF ONCE AIRCRAFT WAS ON THE GROUND. BURNING WIRING ODOR IN A/C REAR, NO SMOKE OBSERVED. ITEM IS UNDER INVESTIGATION.Nov 22, 2005 · N782QS · Cessna 650 · Communications SystemSDR DXTA200501099Position Switch · out of adjustCAB DOOR UNLOCK LIGHT WAS FLICKERING ON TAKEOFF ROLL, AFTER THE ABORT THE ANNUNCIATOR EXTINGUISHED. REPEAT WRITE UP. ADJUSTED UPPER FWD DOOR PIN SWITCH, OPERATIONAL CHECKS SATISFACTORY. ALL WORK IAW CE-650 M/M CHPT 52-70-00.Nov 21, 2005 · N782QS · Cessna 650 · Door Warning SystemSDR DJFA2005163Spar · corrodedDURING AN UNSCHEDULED MAINTENANCE VISIT, WHILE INVESTIGATING A FUEL LEAK, CORROSION WAS DISCOVERED ON BOTH FORWARD AND BOTH AFT WING SPAR SPLICES ON THE UNDERSIDE OF THE WING DIRECTLY ABOVE THE SKID RAILS.Nov 10, 2005 · N384CW · Cessna 650 · Wing SparSDR CA051018001Turnbuckle · chafedDURING PHASE 1-5 INSPECTION ON AIRCRAFT, TECHNICIANS DISCOVERED THAT THE LT AND RT AILERON CABLES WERE FOULING. THE RESULT WAS THAT THE LT TURNBUCKLE WAS CHAFED AND THE RT SIDE THE SAFETY CLIP WAS GONE AND THE TURNBUCKLE WAS ALSO CHAFED.Oct 17, 2005 · Cessna 650 · Aileron Control SystemSDR DXTA200501018Control Panel · hotBURNT WIRING SMELL WAS NOTICED AFTER ENGINE SHUTDOWN. HEADING AD SELECTION CONTROL PANEL WAS EXTREMELY HOT SO COMPLETE SHUTDOWN WAS INITIATED. - TROUBLESHOT TO BAD REMOTE INSTRUMENT CONTROLLER, REPLACED BAD R.I.C. IAJ CE 650MM CH 34-21-00 + OPS CHECK GOOD.Oct 11, 2005 · N787QS · Cessna 650 · Instrument PanelSDR DJFA2005148Line · leakingCREW REPORTED THAT RT ENGINE OIL LOW PRESSURE ANNUNCIATOR HAD ILLUMINATED WHILE IN CRUISE FLIGHT APPROX AN HOUR AND A HALF AFTER TAKE OFF. RT ENGINE OIL PRESSURE INDICATED BETWEEN 38 - 25 PSI. POWER TO RT ENGINE WAS REDUCED TO FLIGHT IDLE, AND AN EMERGENCY WOct 6, 2005 · N397CW · Cessna 650 · Turbine Engine Oil SystemSDR JDW2005F00000Pin · looseRT MAIN GEAR OLEO STRUT WOULD NOT COMPRESS AFTER LANDING, MORE THAN 50 PERCENT OF NORMAL. AC WAS JACKED, SERVICE OF THE STRUT WAS CHECKED NORMALLY. NEX LANDING, STRUT WOULD AGAIN NOT COMPRESS. OLEO WAS REMOVED FROM AC AND DISASSEMBLED. METERING PIN INSIDE Oct 5, 2005 · N650DA · Cessna 650 · Landing Gear Retraction/Extension SystemSDR DXTA200500988Smoke Detector · faultyDURING THE TAKEOFF ROLL, THE RED "SMOKE DETECT" LIGHT CAME ON TRIGGING THE MASTER WARNING, DURING THE TAXI BACK TO THE FBO THE LIGHT AND MASTER WARNING KEPT ON ILLUMINATING AND FLASHING. TROUBLESHOT SYSTEM AND FOUND SMOKE DETECTOR BOX FAULTY. REMOVED DEFECTISep 28, 2005 · N795QS · Cessna 650 · Smoke DetectionSDR DXTA200500973Fire Detector · malfunctionedAPU FIRELIGHT CAME ON IN FLIGHT, PUSH THE LIGHT AND BLEW THE BOTTLE AS PER CHECKLIST, INSPECTED APU AND SURROUNDING AREA NO DAMAGE NOTED, MEL PER CE-650 NJA MEL MANUAL. ITEM IS UNDER INVESTIGATION.Sep 17, 2005 · N710QS · Cessna 650 · Fire Detection
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