Pratt & Whitney Canada PW535A

Service difficulty reports · 251

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE engine_model_key = 'PW535A'
  ORDER BY difficulty_date DESC"

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SDR E07A 392AS 1110Probe · inoperativeON TAKEOFF ROLL CREW HAD CAS MESSAGE INDICATING AP FAIL AND YD FAILED . TAKEOFF WAS ABORTED AND ACFT WAS RETURNED TO FBO. RT SMART PROBE WAS REPLACED AND ACFT WAS RETURNED TO SERVICE.Nov 30, 2010 · N392AS · Emb EMB500 · Pitot/Static SystemSDR DXTA20101104333Warning Light · malfunctionedNOSE GEAR RED UPLOCK LIGHT FAILED TO EXTINGUISH DURING TAKEOFF GEAR RETRACTION.Nov 28, 2010 · N837QS · Cessna 560CESSNA · Landing Gear Position and WarningSDR DXTA2010112904334Warning Light · false activationLEFT ENGINE FUEL FILTER BYPASS ANNUNCIATOR ILLUMINATED OUT OF 27,000 ON CLIMB OUT, SHORTLY AFTER RT SIDE ILLUMINATION. RT FUEL FILTER BYPASS ANNUNCIATOR ILLUMINATED OUT OF 21,000 FT ON CLIMB OUT. REMOVED FUEL FILTER & FUEL SAMPLE. SHIPPED OUT FOR ANALYSIS. Nov 28, 2010 · N822QS · Cessna 560CESSNA · Fuel Indicating SystemSDR DXTA2010110204286Coalescer Bag · odorIMMEDIATELY AFTER TAKEOFF THERE WAS A CHEMICAL OR ELECTRICAL BURNING ODOR THAT LASTED ENTIRE FLIGHT. INCREASING THE TEMP AND OVERHEAD/DEFOG FAN AIRFLOW INCREASED THE ODOR SOURCE. MORE NOTICABLE IN COCKPIT THAN AFT CABIN. REMOVED AND RINSED WITH HOT WATER THENNov 1, 2010 · N827QS · Cessna 560CESSNA · Humidity Control SystemSDR DXTA2010102604272Flap System · malfunctionedFLAPS STOPPED AT 10 WHEN 15 SELECTED, HYD PRESSURE REMAINED ON (MOVED FLAP HANDLE TO MATCH FLAP INDICATOR, HYD PRESS WENT OUT). SELECTED FLAPS 15 AGAIN, FLAP INDICATOR REMAINED 10 WITH HYD PRESS ON. SLOWED PLANE TO 180-185, FLAPS MOVED TO 15 AND HYD PRESS LIGOct 25, 2010 · N808QS · Cessna 560CESSNA · Trailing Edge Flap Control SystemSDR CA101025002Fcu · faultyPOWER ROLL BACK/FLAMEOUT DURING DESCENT TO A CLASSIFIED LOCATION, THE ENG POWER ROLLED BACK BEFORE IT FLAMED OUT. AN UNEVENTFUL SINGLE ENG LANDING WAS MADE AT DESTINATION. THE PROBLEM WAS TRACED BACK TO A FAULTY FUEL CONTROL UNIT (PRE SB 30356/30409) WHICH WSep 27, 2010 · Fuel Control/Turbine EnginesSDR DXTA2010091704241Flap System · frozenDURING FLAP EXTENSION ON APPROACH, THE FLAPS FROZE BETWEEN THE 7 DEGREE DETENT AND THE 15 DEGREE DETENT. RAN FLAPS THUR ALL POSITIONS VARIOUS TIMES - NO DEFECTS NOTED. PLACED LOAD ON FLAPS AND RAN NO DEFECTS. OPEN RT PEDESTAL PANEL. EXAMINED SWITCHES WHILE RSep 16, 2010 · N806QS · Cessna 560CESSNA · Trailing Edge Flap Control SystemSDR DXTA2010091504236Indicator · malfunctionedAT FL410 STBY, GYRO SHOWED 6 DEGREE LT BANK, AND HEADING MISCOMPARE OF APPROX 120 DEGREES. (HEADING OF 330 THEN SLOWY MOVED TO 030). PLANE HEADING WAS 084. ALSO EXT MANUVER ANNUNCIATOR WAS ON. OPS CHECKED NORMAL. PERFORMED RESISTANCE CHECK OF FUSE. FUSE NORMSep 14, 2010 · N818QS · Cessna 560CESSNA · Directional Gyro and Indicating SystemSDR DXTA2010083004211Relay · inoperativeUPON GEAR EXTENSION THE LOW BRAKE PRESS LIGHT ILLUMINATED. ANTI SKID LIGHT CAME ON DURING APPROACH. DID MISSED APPROACH AND HELD TO RUN CHECKLIST. LIGHT STAYED ON DURING SECOND APPROACH; LANDED USING EMERGENCY BRAKE. TROUBLESHOT TO A FAULTY POWER BRAKE MOTORAug 28, 2010 · N808QS · Cessna 560CESSNA · Brake Anti-Skid SectionSDR DXTA2010083004212Seal · tornFOUND DURING MX: EMERGENCY EXIT DOOR WILL NOT OPEN. 2 MEN REQUIRED TO APPLY EXCESSIVE FORCE FROM INSIDE AND OUTSIDE OF ACFT AT SAME TIME, TO OPEN. PERFORMED OPS CHECK OF EMERGENCY EXIT AFTER DOOR SEAL REPLACEMENT OPS CHECK OF EMRGENCY EXIT DOOR GOOD. NO DEFECAug 27, 2010 · N843QS · Cessna 560CESSNA · Emergency ExitsSDR DXTA2010082504206Circuit Board · inoperativeFLAPS INOPERATIVE. CLICKING SOUND HEARD ON TAKEOFF, COMING FROM LT SIDE OF COCKPIT. PLANNED A RETURN TO DEPARTURE; SELECTED FLAPS 15. FLAP HANDLE STOPPED AT THE FLAPS 7 POSITION. R & R HYD, PCB NZ014 IAW WDM 20-10-00. OPS CHECK THE FLAPS, SPEED BRAKES, AND LAug 24, 2010 · N827QS · Cessna 560CESSNA · Trailing Edge Flap Control SystemSDR CA100703006Warning Light · illuminatedABORTED TAKEOFF ON TAKEOFF ROLL AT APPROXIMATELY 70 KTS LEFT ENGINE CONTROL FAULT LIGHT ILLUMINATED WITH MASTER CAUTION. TAKEOFF WAS ABORTED. TROUBLESHOOTING IS ON-GOING. MANUFACTURER WILL INVESTIGATE TO ESTABLISH ROOT CAUSE AND SUPPLEMENT THE REPORT ONCE THEJun 29, 2010 · Engine Indicating SystemSDR DXTA2010061504123Bulb · inoperativeTHE LT MAIN "DOWN AND LOCKED" LIGHT WOULD NOT ILLUMINATE. R & R BULB ON LT GEAR DOWN LOCK ANNUNCIATOR. PERFORMED LANDING GEAR FUNCTIONAL CHECK AND FULL HYD SYS BLEED. SYS CHECKS GOOD. SERVICED GEAR BOTTLE AS REQUIRED. ALL WORK DONE IAW MM 32-01-00.Jun 14, 2010 · N807QS · Cessna 560CESSNA · Landing Gear Position and WarningSDR UG8A051801911UMFire Loop · chafedON DESCENT "FIRE DET SYS R" AMBER CAUTION LIGHT ILLUMINATED FOLLOWED BY RED "RT ENGINE FIRE WARNING". FOUND FIRE LOOP CHAFED.May 18, 2010 · N911U · Cessna 560CESSNA · Fire DetectionSDR WTXR173J01Connector · misinstalledAT THE LT ENGINE FIRE LOOP, IT WAS DISCOVERED THAT BECAUSE THE THREADED CONNECTORS ARE OF THE SAME THREAD TYPE BETWEEN THE WIRING FOR THE FIRE LOOP AND THE FIRE LOOP ITSELF, IT IS VERY EASY FOR THE WIRES AND LOOPS TO BE CONNECTED INCORRECTLY WHICH WOULD PREVENMar 29, 2010 · N166ST · Cessna 560CESSNA · Fire Protection System WiringSDR DXTA2010032904055Master Cylinder · leakingBRAKES IN LT SEAT FEEL MUSHY. THERE IS EXCESSIVE TRAVEL IN THE BRAKE PEDAL BEFORE YOU FEEL BRAKE PRESSURE. FOUND SIGNS OF FLUID LEAKING FROM PILOTS LT BRAKE MASTER CYCLINDER. R&R PILOTS LT MASTER CYLINDER WITH O/H UNIT IAW MM CHAP 32-42-02. OPS CHECK GOOD,Mar 28, 2010 · N699QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR 2010F00060Indicator · malfunctionedCLIMBING THROUGH FL340, 17 MINUTES INTO FLIGHT, AMBER HEADING MISCOMPARE ILLUMINATED RT SIDE WAS 7 DEGREES HIGHER THAN LT. CONTINUED CLIMB TO FL400 WHILE ACCOMPLISHING EVERYTHING ON THE OCF SHEET WITH NO CHANGE TO DISCREPANCY. RT SIDE CONTINUED TO PRECESS AS Mar 5, 2010 · N801QS · Cessna 560CESSNA · Attitude and Direction Data SystemSDR 2010F00049Indicator · malfunctionedHDG MISCOMPARE LIGHT ILLUMINATED CLIMBING THROUGH FL370. DISAGREED BY 35-40 DEGREES. STARTED TO ALIGN IN A TURN, CONTINUED TO DIVERGE AFTER TURN BUT ONLY DISAGREED BY 20 DEGREES UNTIL LANDING. LOGO LIGHTS DID NOT APPEAR TO AFFECT.Feb 25, 2010 · N801QS · Cessna 560CESSNA · Independent Position Determining SystemSDR CA100223003Trim Switch · broken(CAN) PILOT ATTEMPTED TO TRIM ACFT ON CLIMB OUT USING ELECTRIC TRIM TO LEVEL OFF FOR TRAFFIC AVOIDANCE. ACFT FAILED TO RESPOND. EVASIVE ACTION TAKEN AS REQUIRED. FLIGHT CONTINUED USING COPILOT TRIM SWITCH AND/OR MANUAL TRIM AS REQUIRED. ON GROUND PILOT ATTEMPTFeb 22, 2010 · Cessna 560CESSNA · Stabilizer Control SystemSDR 2010F00036Warning Light · illuminatedON APPROACH, EXT FLAPS TO 15, HYD PUMP REMAINED ILLUMINATED. REPOSITIONED FLAPS AND THE LIGHT REMAINED ON. IMMEDIATELY EXT GEAR AND FULL FLAPS. THE HYD LIGHT EXTINGUISHED. FLAP POSITION APPEARED NORMAL. ON SHORT FINAL, TOO LOW FLAPS, TOO LOW TERRAIN SOUNDEFeb 11, 2010 · N844QS · Cessna 560CESSNA · Central WarningSDR CA100203007Engine · surges(CAN) DURING DESCENT, THE PILOT NOTICED THE ENGINE SURGING TWICE BEFORE IT SHUTDOWN BY ITSELF. THE ACFT LANDED SINGLE ENGINE UNEVENTFULLY. GROUND INSP FOUND NO OBVIOUS ENGINE DAMAGE. TROUBLESHOOTING IS ON-GOING. MFG WILL INVESTIGATE TO ESTABLISH ROOT CAUSE ANDJan 28, 2010 · Engine (Turbine/Turboprop)SDR CA100209001Engine · surges(CAN) SURGING/IFSD DURING DESCENT, THE PILOT NOTICED THE ENGINE SURGING TWICE BEFORE IT SHUTDOWN BY ITSELF. THE ACFT LANDED SINGLE ENGINE UNEVENTFULLY. GROUND INSP FOUND NO OBVIOUS ENGINE DAMAGE. TROUBLESHOOTING IS ON-GOING. MFG WILL INVESTIGATE TO ESTABLISH RJan 28, 2010 · Engine (Turbine/Turboprop)SDR 10P012701911UMCable · brokenFOLLOW-UP CABLE WAS FOUND TO HAVE OVER 50 PERCENT OF ITS DIAMETER BROKEN AT THE SWEDGED BALL. POSSIBLE IMPROPER SWEDGING OF THE BALL ON THE CABLE. COMPLY WITH SB560-27-19 FLIGHT CONTROLS FLAP FOLLOW-UP CABLE IMPROVEMENT. COMPLIED WITH SB 27-19. REPLACEMENTJan 27, 2010 · N911UM · Cessna 560CESSNA · Trailing Edge Flap Control SystemSDR DXTA2009122103903Fuel Control · malfunctionedAPPROX 1 HR INTO FLT AT FL410, RT N1 READ 2 % LOWER THAN LT N1. RT ENG N1 DID NOT RESPOND TO THROTTLE. RT N1 ROLLED BACK TO 55 %, WITH FURTHER REDUCTION TO 35 %. ALL ENG INDICATIONS LOW BUT WITHIN LIMITS. AT APPROX 18600 FT-7 RAT RT ENG SPOOLED UP/ BACK TO NDec 20, 2009 · N810QS · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR CA100117002Fuel Control · malfunctioned(CAN) DURING CRUISE AT FL410, THE RT ENGINE N1 SPEED WAS READING 2 PERCENT LOWER THAN THE LT ENGINE. THE ENGINE N1 WOULD NOT RESPOND TO THROTTLE MOVEMENT AND N1 STARTED TO ROLL BACK TO 55 PERCENT WITH FURTHER ROLL BACK TO 35 PERCENT IN DESCENT. AT FL 186, THDec 20, 2009 · Fuel Control/Turbine EnginesSDR 2009FA0000771Valve · inoperativePRESSURIZATION INOPERATIVE AT ALTITUDE, THE ACFT GOT RED "ALT" ANNUNCIATOR, EMER PRESSURIZATION DID NOT KICK ON. DIFFERENTIAL PRESSURE GAUGE STUCK AT 12,000 FT. REPLACED PRIMARY OUT FLOW VALVE. OPS CHECK STILL BAD ON CHECK FLIGHT. NOTED CABIN ALTITUDE UNCOJul 16, 2009 · N557PG · Cessna 560CESSNA · Cabin Pressure Control SystemSDR DXTA2009060803680Fuel Control · inoperativeON TAKEOFF, LT ENG SLOW TO ACCELERATE. NORMAL CLIMB OUT, N1 SYNC ON FL 180. LEVELED FL 390 N1 MATCHED 90 % ACCELERATING TO CRUISE. LESS THAN 2 MIN INTO ACCELERATION N1 DROPPED TO 60 % & FUEL FLOW DROPPED TO 220 PPH. DESCENDED TO FL 290. MOVING THROTTLE DID NOTJun 7, 2009 · N812QS · Cessna 560CESSNA · Fuel Control/Turbine EnginesSDR DXTA2009051303648Spring · brokenENGINE SHUTS OFF WHEN BROUGHT BACK TO IDLE, ON GROUND. REMOVED & REPLACED THROTTLE SPRING RAN FOR OP'S AND SLAM CHECKS. SYSTEM OP'S CHECKS SATISFACTORY AT THIS TIME. ALL WORK DONE IAW MM 76-10-00May 12, 2009 · N820QS · Cessna 560CESSNA · Power LeverSDR DXTA2009041703604Engine · undamagedDURING POST FLIGHT, FOUND EVIDENCE OF BIRD STRIKE INTO RT ENGINE. COMPLIED WITH BIRD STRIKE INSPECTION ON AIRFRAME IAW M.M. CH 5-10-00, NO DAMAGE FOUND. COMPLIED WITH BIRD STRIKE INSPECTION ON LEFT AND RIGHT ENGINES IAW MM 72-00-00, NO DAMAGE FOUND.Apr 17, 2009 · N825QS · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR CA090403003Fuel Control · malfunctioned(CAN) WHILE AT FL 280, THE PILOT RETARDED THE THROTTLES TO SLOW DOWN THE ACFT. WHEN LATER ADVANCING THE THROTTLES, THE LT ENGINE WOULD NOT RESPOND AND BEGAN SPOOLING BACK. IT WAS SHUTDOWN AND SECURED BEFORE LANDING. THE PROBLEM WAS TRACED TO FUEL SYS COMPONENFeb 24, 2009 · Cessna 560CESSNA · Fuel Control/Turbine EnginesSDR ZESA2008014Sensor · out of limitsCREW IDENTIFIED DURING TAKEOFF THAT THE THROTTLE POSITION WHEN MATCHED SHOWED THE LT ENGINE AT 88 PERCENT AND THE RT ENGINE AT 37 PERCENT. RT ENGINE TOOK APPX 4-5 SECONDS TO CATCH UP TO THE LT. MAINT TROUBLESHOT AND REPLACED THE RT ENGINE T1 SENSOR. OPS CHESep 25, 2008 · N511TH · Cessna 560CESSNA · Engine BMEP/Torque IndicatingSDR CA080814008Engine · malfunctioned(CAN) WHILE ON APPROACH, THE LT ENGINE ROLLED BACK AND WOULD NOT RESPOND TO THROTTLE MOVEMENTS. WHILE CREW WAS PERFORMING EMERGENCY CHECKLIST FOR ENGINE SHUTDOWN. THE LT ENGINE SHUTDOWN ON ITS OWN. ACFT LANDED WITHOUT INCIDENT. MFG WILL CONTINUE INVESTIGATINAug 2, 2008 · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR DXTA200803069Pressure Switch · inoperativeWHILE TAKING THE RUNWAY FOR DEPARTURE THE LOW BRAKE PRESSURE - ANTI-SKID ANNUNCIATOR LIGHT ILLUMINATED. REMOVED DEFECTIVE PUMP MOTOR PRESSURE SWITCH AND INSTALLED REPAIRED SWITCH. SYSTEM CHECKS GOOD REF MM 32-20-00. TAXI CHECKED GOOD IAW PILOTS HANDBOOK.May 19, 2008 · N814QS · Cessna 560CESSNA · Brake Anti-Skid SectionSDR DXTA200803063Bracket · bentAFTER TAKEOFF AND GEAR RETRACTION, RED, GEAR UNLOCK LIGHT REMAINED ILLUMINATED. FOUND NOSE UPLOCK CATCH ROD BRACKETS BENT. REMOVED OLD BRACKETS AND INSTALLED NEW BRACKETS REF MM 32-20-01. OPS CHECKED GOOD.May 16, 2008 · N677QS · Cessna 560XL · Landing Gear Position and WarningSDR DXTA200803059Lamp · inoperativeON ARRIVAL, THE "LT" GEAR DOWN INDICATION LIGHT DID NOT ILLUMINATE. JACKED ACFT, RESET EMERGENCY BLOW-DOWN BOTTLE. REMOVED AIR FROM SYSTEM. FOUND ROTARY KNOB WOULD NOT TEST. REPLACED ALL (4) LAMPS. SWITCH TEST NORMAL. PERFORMED GEAR SWINGS SEVERAL TIMES.May 14, 2008 · N818QS · Cessna 560CESSNA · Landing Gear Position and WarningSDR DXTA200803045Controller · failedAT FL300 THE CABIN RATE STARTED CLIMBING ABNORMALLY TILL IT REACHED 6000 FT IAW MINT THE 10,000 FT CABIN ENUNCIATORS ILLUMINATED AND THE EMER PRESS CAME ON. OXYGEN MASKS DROPPED IN THE CABIN. DECLARED AN EMERGENCY AND STARTED AN EMERGENCY DESCENT TO 10,000. May 5, 2008 · N825QS · Cessna 560CESSNA · Cabin Pressure ControllerSDR CA080424005Ignition Lead · defective(CAN) DURING ROUTINE INSP OF THE ENGINE, THE LT ENG OB IGNITER LEAD WAS FOUND DEFECTIVE. UPON REMOVAL OF IGNITER FROM LEAD, FOUND THE LEAD`S CENTER ELECTRICAL POST LOOSE AT IGNITER END. APPROX ONE INCH OF THE CENTER POST OF LEAD FEEL OUT WITH CERAMIC INSULATOApr 23, 2008 · Cessna 560CESSNA · Ignition Harness (Distribution)SDR DXTA20082983Warning Light · illuminatedAFTER SELECTING GEAR DOWN, RT MAIN GREEN LIGHT AND GEAR UNLOCKED RED LIGHT BEGAN TO FLICKER INTERMITTENT (3 GREEN NO RED).Apr 6, 2008 · N806QS · Cessna 560CESSNA · Landing Gear Position and WarningSDR DXTA200802983Actuator · malfunctionedAFTER SELECTING GEAR DOWN, RT MAIN GREEN LIGHT AND GEAR UNLOCKED RED LIGHT BEGAN TO FLICKER INTERMITTENT (3 GREEN NO RED). TROUBLESHOT TO FAULTY RT MLG ACTUATOR DOWNLOCK SWITCH. REMOVED AND REPLACED RT MLG ACTUATOR. LEAK AND OPERATIONAL CHECKS NORMAL IAW MM 3Apr 6, 2008 · N806QS · Cessna 560CESSNA · Landing Gear ActuatorSDR DXTA20082950Pitot System · contaminatedON TAKEOFF ROLL F/O AIRSPEED MISCOMPAIRED WITH CAPT A/S, TAKEOFF WAS ABORTED. DRAINED OUT EXCESS WATER FROM THE PITOT PROBES AND STATIC PROBES, AND PERFORMED AN AIR DATA SYSTEMS - INSPECTION/ CHECK. SYSTEMS CHECKED NORMAL IAW MM REV. 23, 34-11-10 & 34-11-26.Mar 19, 2008 · N834QS · Cessna 560CESSNA · Pitot/Static SystemSDR DXTA20082939Pcb · inoperativeLANDING GEAR DID NOT EXTEND WHEN GEAR HANDLE WAS PUT DOWN. REPLACED PCB NZ014 PER CE560 ENCORE & MM 24-51-01, REPLACED LANDING GEAR CONTROL HANDLE ASSY. PER CE560 ENCORE & MM 32-31-01. FUNCTIONAL CHECKED GOOD PER 560 ENCORE & MM 32-01-00.Mar 14, 2008 · N814QS · Cessna 560CESSNA · Landing Gear Retraction/Extension SystemSDR DXTA20082912Indicator · looseELEVATOR TRIM POSITION INDICATOR INOP. INDICATES INCORRECT TRIM POSITION. FOUND TRIM LOOSE. SHIMMED & RESECURED INDICATOR IAW MM 27-31-00. OPERATIONAL AND TRAVEL CHECK NORMAL.Mar 3, 2008 · N814QS · Cessna 560CESSNA · Elevator Tab Control SystemSDR DXTA20082897Anti-Skid Sys · malfunctionedON TAXI OUT LOW BRAKE PRESS AND ANTI-SKID INOP LIGHT ILLUMINATED. NORMAL BRAKING WAS INEFFECTIVE. EMERGENCY BRAKE WAS USED TO STOP THE AC. GAINED ACCESS TO ANTI-SKID CONTROLLER AND FOUND NO FAULTS. EMERGENCY PNEUMATIC BOTTLE IS SERVICED TO TOP OF GREEN ARC. Feb 24, 2008 · N814QS · Cessna 560CESSNA · Brake Anti-Skid SectionSDR DXTA20082890Landing Gear · malfunctionedDURING NORMAL GEAR EXTENISON ON FINAL APPROACH, LT MAIN GEAR WOULD NOT INDICATE DOWN AND LOCKED BY THE GEAR INDICATOR LIGHT. CLEAN AND LUBRICATED LT AND RT MLG UPLOCKS. COMPLETED LANDING GEAR HYD SYS FUNCTIONAL TEST IAW MM CHAPTER 32-01 WITH NO DEFECTS AT THFeb 19, 2008 · N806QS · Cessna 560CESSNA · Landing Gear Retraction/Extension SystemSDR DXTA20082884Engine · power lossATTEMPTED A STATIC T/O AND THE RT ENG DIDN'T MAKE THE COMPUTED T/O PWR WITH FULL THROTTLE TRAVEL. IT WAS 2 PERCENT SHORT OF THE REQUIRED 92.2 PERCENT AT 0 DEG C. PERFORMED TAXI/ POWER OF THE DAY CHECKS WITH CREW AT 5 DEGREES C. POWER NEEDED WAS 91.5 PERCENT Feb 16, 2008 · N807QS · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR DXTA200802862Engine · overtempRT ENG WOULD NOT ATTAIN POWER WITHOUT EXCEEDING ITT AND N2 LIMITS. TAKE OFF ABORTED. REPLACED RT ENGINE WITH REPAIRED UNIT AND REPLACED RT BDV CONTROLLER WITH REPAIRED UNIT. PERFORMED IAW MM CHAP 75-30-01 AND MM CHAP 71-01-05. PERFORMED ALL ENGINE ADJUSTMENTS Feb 10, 2008 · N807QS · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR DXTA200802824Gasket · leakingDURING TAKEOFF ROLL, RT ENGINE ITT CLIMBED TO 700 DEG WHERE AS LT ENGINE STABILILZED AT 650 DEG ABORTED TO ROLL. CONFIRMED RT ENGINE TO GO UP TO 700 DEGREES AND T/O POWER. PERFORMED ALL ELECTRICAL CHECKS TO DETERMINE NR2 ITT INDICATION SYSTEM IS READING TRUEFeb 3, 2008 · N807QS · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR CWQR200801Skin · crackedDURING A PHASE 1-4 INSPECTION THE TECHNICIAN NOTICED A SMALL CRACK IN THE PAINT UNDER THE RT ENGINE PYLON. REMOVED THE PAINT AND FOUND A 1.5 INCH CRACK. STARTING AT THE FWD BOTTOM CUT OUT FOR THE FWD SUPPORT BEAM. APPEARS THAT THERE WAS NOT ENOUGH CLEARANCE INJan 29, 2008 · N839QS · Cessna 560CESSNA · Fuselage Main, Plate/SkinSDR DXTA200802788Actuator · malfunctionedON APPROACH AT 4000 FT AND 180 KIAS THE RT MAIN GREEN GEAR INDICATOR ILLUMINATED STEADY. JACKED AIRCRAFT AND T/S TO DEFECTIVE RT DOWNLOCK SWITCH. REMOVED & REPLACED RT MLG ACTUATOR AND ADJUSTED. OPS AND LEAK CHECKED GOOD IAW MM 32-01-00 DOWN JACKED AIRCRAFT.Jan 22, 2008 · N839QS · Cessna 560CESSNA · Landing Gear ActuatorSDR DXTA200802784Indicator · inoperativeON TAKEOFF CAPT'S AIRSPEED GAVE NO INDICATION, RED AIRSPEED ENUNCIATION SHOWED ON AIRSPEED INDICATOR. SIMULATED AIRSPEED WITH PITOT/STATIC TEST SET AND COULD NOT DUPLICATE DISCREPANCY. CHECKED NR 1 PITOT HOSE FOR MOISTURE, NO MOISTURE FOUND. BLEW OUT NR 1 PIJan 21, 2008 · N834QS · Cessna 560CESSNA · Airspeed/Mach Indicator
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