Pratt & Whitney Canada PW545A

Service difficulty reports · 594

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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 engine_model_key = 'PW545A'
  ORDER BY difficulty_date DESC"

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SDR DXTA200601625Brake · vibratesEVERY TIME THE BRAKES ARE INITIALLY APPLIED, WILL GET A RUMBLE/VIBRATION FROM BOTH BRAKES FOR 2-3 SECONDS FOLLOWED BY NORMAL BRAKING. IF BRAKE PRESSURE IS RELEASED THEN REAPPLIED, WILL GET THE RUMBLE/VIBRATION. REMOVED LT BRAKE ASSY, 2-1601-, S/N 1303 AND INOct 1, 2006 · N673QS · Cessna 560XL · Landing Gear Brake SystemSDR DXTA200601623Engine · making metalON TAKEOFF ROLL, RT OIL FILTER BYPASS ANNUNCIATOR ILLUMINATED. OIL TEMP AND PRESS INDICATIONS NORMAL. ABORTED TAKEOFF JUST AFTER TAKEOFF ROLL STARTED. REMOVED NR 2 ENGINE, INSTALLED REPAIRED ENGINE IAW MM 71-00-00. PERFORMED GROUND OPERATIONAL CHECKS AND LEASep 30, 2006 · N603QS · Cessna 560XL · Engine (Turbine/Turboprop)SDR CA061006015Engine · leaking(CAN) IN CRUISE, ENGINE OIL PRESSURE WAS SEEN TO DECREASE AND THE LOW OIL PRESSURE WARNING ACTIVATED. THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED EXTERNAL OIL LEAKAGE. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLSep 20, 2006 · Cessna 560XL · Turbine Engine Oil SystemSDR H432006F00000Pin · failedNOSE LANDING GEAR TORQUE LINKS CONNECTED BY QUICK RELEASE PIN. QUICK RELEASE PIN FELL APART WHILE TAXIING ON ACTIVE TAXI WAY DISCONNECTING NOSE WHEEL STEARING. AIRCRAFT TOWED FROM TAXI WAY. NO DAMAGE NOTED. (K)Sep 8, 2006 · N424HH · Cessna 560XL · Nose/Tail Landing GearSDR 2006FA0001002Downlock Switch · failedAFTER TAKEOFF AND GEAR RETRACTION ALL GEAR LIGHTS WENT OUT. APPROX 5-10 INTO FLIGHT, NOTICED RT GREEN GEAR LIGHT WAS ON. NO OTHER ABNORMAL LIGHTS NOTED. 40 MINUTES LATER LIGHT EXTINGUISHED. TROUBLESHOT SYS BY RIGING ALL DOWN LOCK SWITCH WIRING AND SWITCH MSep 6, 2006 · N651QS · Cessna 560XL · Landing Gear Position and WarningSDR CA060704014Fuel Control · malfunctioned(CAN) DURING DESCENT, THE ENGINE WOULD NOT RESPOND TO THROTTLE INPUTS FOR POWER REDUCTION. THE ENGINE WAS SHUT DOWN ON FINAL APPROACH. THE FUEL CONTROL UNIT WAS SUBSEQUENTLY REPLACED. (TC# 20060704014)Jun 18, 2006 · Cessna 560XL · Fuel Control/Turbine EnginesSDR DXTA200601416Engine · oil consumptionLT ENGINE OIL PRESSURE ANNUNCIATOR ILLUMINATED, MASTER WARNING ILLUMINATED. OIL PRESSURE FELL BELOW 20 PSI THEN CAME BACK UP AND HOVERED AT 40 PSI, SHUT ENGINE DOWN NOTICED NO OIL IN SIGHT GAUGE. DETERMINED THAT THE LT ENGINE WAS BURNING OIL INTERNALLY, REPLJun 1, 2006 · N619QS · Cessna 560XL · Engine (Turbine/Turboprop)SDR 2006FA0000566Windshield · crackedPILOTS WINDSHIELD OUTER PANE CRACKED AT 39,000 FT. IT IS BELIEVED THAT A HEATING ELEMENT SHORTED CAUSING THE OUTER PANE TO CRACK. WINDSHIELD REMAINS STRUCTURALLY INTERGRAL WITH THE OUTER PANE CRACKED. MFG ENGINEERING IS EVALUATING THE FAILURE. (K)May 24, 2006 · N240B · Cessna 560XL · Flight Compartment WindowsSDR CA060425004Oil System · leakingDURING CRUISE, ENGINE OIL PRESSURE WAS SEEN TO FLUCTUATE ACCOMPANIED BY SMOKE AND ODOR IN THE CABIN AIR. ENGINE OIL PRESSURE SUBSEQUENTLY REDUCED TO ZERO AND THE ENGINE WAS SHUT DOWN IN FLIGHT. PWC WILL INVESTIGATE THE EVENT AND WILL ADVISE OF ROOT CAUSE, ONApr 5, 2006 · Cessna 560XL · Turbine Engine Oil SystemSDR DXTA200601325Engine · low pressureAFTER TAKEOFF AT CLIMB-OUT POWER DETENT, LT LOW OIL PRESSURE ANNUNCIATER ILLUMINATED. LOW PRESSURE WAS VERIFIED ON TAPE, DIGITS WERE RED AND PRESSURE WAS ZERO. REDUCED POWER AND PRESSURE REMAINED ZERO FOR ABOUT 10 SEC THEN RETURNED TO NOMAL. POST FLIGHT INSMar 30, 2006 · N611QS · Cessna 560XL · Engine Oil PressureSDR CA060129004Engine · damaged(CAN) DURING CLIMB, THE CREW OBSERVED ENGINE TEMPERATURE AND FUEL FLOW SPLIT. THE FLIGHT DIVERTED TO POINT OF DEPARTURE AND THE ENGINE WAS SHUT DOWN DURING DESCENT. SUBSEQUENT INSPECTION REVEALED DAMAGE TO THE ENGINE INNER BYPASS DUCTING CONSISTENT WITH AN INJan 23, 2006 · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR DXTA200601189Pump · malfunctionedLEFT FUEL BOOST PUMP CAME ON DURING TAKEOFF ROLL, ABORTED. PERFORMED RUN UP AFTER RESETTING PUMP, CAME ON AGAIN. PERFORMED 3RD RUN UP ON RAMP, DID NOT COME ON. ITEM IS UNDER INVESTIGATION.Jan 10, 2006 · N371QS · Cessna 560CESSNA · Fuel Boost PumpSDR DXTA200601186Fuel Filter · bypassingAT APPROX 30 KNOTS DURING THE TAKEOFF ROLL THE RIGHT FUEL FILTER BYPASS CAUTION LIGHT CAME ON. AFTER THE POWER WAS REDUCED TO IDLE THE LIGHT WENT OUT. REMOVED AND REPLACED WITH NEW FILTER, FILTER HOUSING AND SEALS ON RIGHT ENGINE. GROUND RAN ENGINE AND OPERJan 8, 2006 · N664QS · Cessna 560XL · Aircraft Fuel Filter/StrainerSDR DXTA200501173Brake · vibratesLT AND RT BRAKES ARE CATCHING AND GRABBING ON BRAKE APPLICATION. LOUD CHATTERING CAN BE HEARD AND THE GRABBING SHAKES THE PLANE. BRAKE WEAR PINS SHOW AMPLE BRAKE WEAR AVAILABLE. BLED LT AND RT BRAKE SYSTEM IAW CE 560XLS MM CHP 32-44-00. TAXI CHECKED GOOD.Dec 31, 2005 · N648QS · Cessna 560XL · Landing Gear Brake SystemSDR 122505N508CS1Transducer · failedAFTER DEPARTING LUK, CREW NOTICED RT ENGINE OIL PRESSURE INDICATOR DROPPED TO ZERO PRESSURE WITH NO OTHER FAILURE INDICATIONS. CREW FOLLOWED CHECKLIST PROCEDURES AND ELECTED TO DECLARE EMERGENCY. THE AIRCRAFT WAS DIVERTED TO CVG WHERE IT HAD AN UNEVENTFUL LADec 25, 2005 · N508CS · Cessna 560XL · Engine Oil PressureSDR DXTA200501169Rod · brokenUPON GEAR RETRACTION HEARD A LOUD BANG. NO OTHER INDICATIONS. SHORTLY AFTERWARDS HEARD WHAT SOUNDED LIKE A NOSE GEAR DOOR OPEN. AFTER LANDING LT NOSE GEAR DOOR RETRACTION ROD WAS FOUND BROKEN. INSPECTED NOSE GEAR AND FOUND LT NOSE GEAR DOOR RETRACT ROD BROKEDec 21, 2005 · N675QS · Cessna 560XL · Landing Gear Retraction/Extension SystemSDR DXTA200501137Servo Valve · inoperativeWHEN TAKEOFF POWER APPLIED, L EEC MAN LIGHT ILLUMINATED. TAKEOFF WAS ABORTED. REMOVED AND REPLACED INOP SERVO VALVE IAW PWA 545A M/M 71-00-00. OPS AND LEAK CHECK GOOD.Dec 11, 2005 · N659QS · Cessna 560XL · Power Indicating SystemSDR DXTA200501123Fuel Filter · contaminatedRT ENG FUEL FILTER BYPASS LIGHT ILLUM ON T/O ROLL AT T/O PWR EXTINGUISHED WHEN PWR REDUCED. VERIFIED RT FUEL FILTER BYPASS LIGHT ILLUMIN NEAR T/O PWR SETTINGS. INSTALLED NEW FUEL FILTER & NEW O-RINGS. ALL PARAMETERS NORMAL. INSPECTED FILTER AFTER RUN, NO DENov 17, 2005 · N615QS · Cessna 560XL · Engine Fuel DistributionSDR DXTA200501087Fuel Filter · bypassingRIGHT ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATED ON TAKEOFF ROLL AT TAKEOFF POWER EXTINGUISHED WHEN POWER REDUCED. OPERATED RT ENGINE AND VERIFIED RT FUEL FILTER BYPASS LIGHT ILLUMINATES NEAR TAKEOFF POWER SETTINGS. REMOVED AND INSPECTED FUEL FILTER. FOUNDNov 16, 2005 · N615QS · Cessna 560XL · Fuel Controlling SystemSDR 2005FA0001533Spring · brokenTHE AIRCRAFT RETURNED FROM A FLIGHT WITH NO DEFECTS NOTED. AIRCRAFT WAS MOVED INTO THE HANGAR AND APPROXIMATELY 20 MINUTES LATER A LOUD BANG WAS HERD. THE AIRCRAFT WAS STATIC WITH THE DOOR CLOSED. THE LOUD BANG WAS THE CABIN ENTRY DOOR FORWARD COUNTERBALANCE SNov 11, 2005 · N102FS · Cessna 560XL · Passenger/Crew DoorsSDR 2005FA0001547Spring · brokenTHE AIRCRAFT RETURNED FROM A FLIGHT WITH NO DEFECTS NOTED. AIRCRAFT WAS MOVED INTO THE HANGAR AND APPROXIMATELY 20 MINUTES LATER A LOUD BANG WAS HEARD. THE AIRCRAFT WAS STATIC WITH THE DOOR CLOSED. THE LOUD BANG WAS THE CABIN ENTRY DOOR FORWARD COUNTER BALANCENov 11, 2005 · N102FS · Cessna 560XL · Passenger/Crew DoorsSDR 111105N523CS1Engine · odorAIRCRAFT DEPARTED AND DURING INITIAL CLIMB OUT CREW NOTICED A LOSS OF OIL PRESSURE AND A SLIGHT ODOR FROM RT ENGINE. THE ENGINE WAS SHUT DOWN AND AN EMERGENCY WAS DECLARED. AIRCRAFT WAS REROUTED AND LANDED WITH NO FURTHUR PROBLEMS. THE ENGINE IS BEING REMOVENov 11, 2005 · N523CS · Cessna 560XL · Engine (Turbine/Turboprop)SDR CA051129013Engine · smokeDURING CRUISE, THE ENGINE LOW OIL PRESSURE WARNING ANNUNCIATED ACCOMPANIED BY OIL SMOKE AND ODOR IN THE CABIN AIR. THE ENGINE WAS SHUT DOWN IN FLIGHT AND THE AIRCRAFT DIVERTED FOR AN UNSCHEDULED LANDING. P&WC WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT Nov 10, 2005 · Cessna 560XL · Engine (Turbine/Turboprop)SDR SWIA200515837Carbon Seal · failedRIGHT ENGINE OIL PRESS LOW, RAN QRH MID THRUST KEPT OIL PRESS IN GREEN, THEN PRESS WENT BELOW 25 PSI (RED). RAN SINGLE ENG ABNORMAL QRH. SECURED RIGHT ENG. REPLACED NR 7 CARBON SEAL IAW GEEM SPECIAL PROCEDURES 36A.Nov 9, 2005 · N441SW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR DXTA200501064Warning Light · illuminatedDURING TAKEOFF ROLL, LEFT EEC LIGHT ILLUMINATED PRIOR TO 70 KTS. DEFERRED IAW NJA CE560XL MEL. MEL 73-3. ITEM IS UNDER INVESTIGATION.Nov 6, 2005 · N604QS · Cessna 560XL · Fuel Controlling SystemSDR DXTA200501048Indicator · malfunctionedLT N1 GAGE INDICATED 0 JUST AFTER POWER UP AT T/O. NO TAPE OR DIGITS. RAN LT ENGINE TO T/O POWER . N1 TAPE HAD NO DEFECTS. REMOVED UPPER AND LOWER LT ENGINE COWLS TO GAIN ACCESS TO N1 SENSOR. RANG OUT SENSOR IAW PWA MM CH. 77-10-01. NO DEFECTS NOTED. COULD Nov 2, 2005 · N684QS · Cessna 560XL · Engine RPM Indicating SystemSDR DXTA200501037Position Switch · inoperativeHYDRAULIC PRESS & UNLOCK LIGHT REMAIN ILLUMINATED ON GEAR RETRACTION. RECYCLED HYD CONTROL PER CK LIST. RECYCLED GEAR & PROBLEM REPEATED ITSELF (SUSPECT NOSE GEAR). - REMOVED AND REPLACED NOSE GEAR UPLOCK SWITCH WITH NEW IAW THE CESSNA 560XL M/M CHAPTER 32-30Oct 27, 2005 · N668QS · Cessna 560XL · Landing Gear Position and WarningSDR DXTA200500962Fuel Filter · cloggedRIGHT SIDE FUEL FILTER BYPASS ANNUNCIATOR AND MASTER CAUTION LIGHT ILLUMINATED DURING TAKEOFF ROLL. LIGHT ILLUMINATED AS THROTTLES WERE PUT IN TO DETENT. THROTTLES BROUGHT UP SLOWLY. LIGHT EXTINGUISHED WHEN THROTTLES BROUGHT BACK TO IDLE. REMOVED AND REPLASep 10, 2005 · N625QS · Cessna 560XL · Aircraft Fuel Filter/StrainerSDR DXTA200500936O-Ring · malfunctionedLEFT FUEL BYPASS ANNUNCIATOR (AMBER) ILLUMINATED ON TAKEOFF ROLL. REMOVED AND REPLACED LT FUEL FILTER AND O-RING'S IAW PWA MM 545A MAINTENANCE MANUAL. RAN A/C LEAK CHECK GOOD FUEL BYPASS AMBER LIGHT DID NOT ILLUMINATE (P/N C31J2404-0R11CA) ASSOCIATED O-RINGSAug 29, 2005 · N604QS · Cessna 560XL · Engine Fuel DistributionSDR CA050824018Line · chafed(CAN) DURING PHASE 5 INSP, 2 HYDRAULIC LINES FOUND CHAFING ON STRUCTURE. P/N 6617077-19 AND 20. REF. AC MFG PROVIDED ENG MFG WITH DRAWING TO INSTALL MISSING LINE SUPPORT HARDWARE TO PREVENT CHAFING.Aug 23, 2005 · Cessna 560XL · Hydraulic System, MainSDR DXTA200500811Actuator · out of adjustAFTER TAKEOFF AND RETRACTING GEAR AND FLAPS-GEAR UNLOCK (RED) LIGHT REMAINED LIT AND STAB MISCOMPARE LIGHT CAME ON. ADJUSTED LT MAIN LANDING GEAR ACTUATOR IAW MM. OPS TESTED LANDING GEAR TEN TIMES WITH NO FAULTS.Jun 29, 2005 · N645QS · Cessna 560XL · Landing Gear ActuatorSDR CA050704009Engine · malfunctioned(CAN) DURING CLIMB, THE ENGINE WOULD NOT RESPOND TO THROTTLE INPUT TO REDUCE POWER. THIS WAS ACCOMPANIED BY AN ELECTRONIC ENGINE CONTROL (EEC) REVERSION. THE FLIGHT WAS DIVERTED AND THE ENGINE WAS SHUT DOWN ON FINAL APPROACH. P&WC WILL INVESTIGATE THE EVENTJun 29, 2005 · Cessna 560XL · Engine (Turbine/Turboprop)SDR DXTA200500809Control Cable · shearedLT RUDDER PEDAL WILL NOT MOVE RUDDER. RT RUDDER PEDAL WILL MOVE RUDDER. LT RUDDER PEDAL MOVES FREELY WITH NO RESISTANCE. ALSO NOTED RUDDER CABLE BOWS BEHIND PEDAL AND FIREWALL. FOUND RUDDER CONTROL CABLE ASSY (UPPER) BROKEN AT 9 O' CLOCK POSITION. REPLACED RJun 28, 2005 · N695QS · Cessna 560XL · Rudder Control SystemSDR DXTA200500792Engine · malfunctionedON TAKEOFF WITH THROTTLE IN THE T/O DETENT, THE LT ENGINE ITT EXCEEDED 720 DEG CELSIUS WITHIN 10 SECS. THE LT ITT INDICTED 724 DEG CELSIUS AND WAS STILL SLOWLY INCREASING. LT THROTTLE REDUCED TO CLIMB. DETENT AND ITT INDICATION IMMEDIATLY DECREASED BELOW 720Jun 20, 2005 · N624QS · Cessna 560XL · Engine (Turbine/Turboprop)SDR CA050608005Duct · loose(CAN) DEPARTURE AFTER MAINTENANCE, AT FL 22,000 CLIMBING, CREW HEARD A LOUD BANG, THEN THE CABIN ALTITUDE BEGAN TO RISE ( DELTA PRESSURE DROPPED). THE CREW STOPPED CLIMB AND DESCENDED BELOW 10,000 FEET AND ELECTED TO RETURN TO POINT OF DEPARTURE. MAINTENANCE May 24, 2005 · Cessna 560XL · Air Distribution SystemSDR DXTA200500740Wire Harness · faultyDURING TAKEOFF ROLL LEFT ENGINE PRODUCED 80% N1. SCHEDULED TAKEOFF POWER WAS 90.1% - REMOVED AND REPLACED ENGINE WIRING HARNESS PER P&WC M/M CH 76-20-02 OPERATIONAL CHECKS SATISFACTORY. BOTH AUTO AND MANUAL MODES.May 22, 2005 · N617QS · Cessna 560XL · Turbine Engine System WiringSDR CA050518010Uplock Switch · unserviceablePILOT NOTED THAT THE GEAR WOULD NOT RETRACT AFTER TAKEOFF. IT MADE A REPETATIVE CLUNKING SOUND AND THE RED GEAR INDICATION LIGHT FLASHED ON AND OFF. CYCLED THE GEAR BACK DOWN NORMALLY AND LANDED. THE RT MLG UPLOCK SWITCH WAS REPLACED. PERFORMED GEAR EXTENMay 10, 2005 · Cessna 560XL · Landing Gear Position and WarningSDR DXTA200500712Engine · malfunctionedON TAKEOFF , ITT ON LT ENGINE REACHED 725 - 730 INITIALLY DECREASED THROTTLE TO IDLE W/IN 2-3 SECONDS DUPLICATED IN RUN UP PAD ITT ON LT ENGINE REACHED 720 IN CLIMB DETENT DECREASED THROTTLE TO IDLE W/IN 2-3 SECONDS. PERFORMED COMPRESSOR WASH ON LT AND RT ENGMay 8, 2005 · N612QS · Cessna 560XL · Engine EGT/TIT Indicating SystemSDR CA050527008Hmu · failedIN DESCENT, THE ENGINE EXPERIENCED AN UNCOMMANDED SHUTDOWN. A RELIGHT ATTEMPT WAS UNSUCCESSFUL. THE HYDROMECHANICAL FUEL CONTROL UNIT WAS SUBSEQUENTLY REPLACED.May 2, 2005 · Cessna 560XL · Fuel Controlling SystemSDR DXTA200500640Engine · malfunctionedAFTER APPLYING TAKEOFF POWER, RIGHT EEC REVERTED TO MANUAL MODE, ABORTED TAKEOFF. ITEM IS UNDER INVESTIGATION.Mar 21, 2005 · N670QS · Cessna 560XL · Engine (Turbine/Turboprop)SDR 2005FA0000408Relay · failedDURING POST FLIGHT WALK AROUND, PILOT NOTICED THAT THE ROSEMONT SENSOR HAD ICE ON IT. UPON OPERATIONAL CHECK, FOUND THAT THE SENSOR WAS NOT HEATING. TROUBLESHOOTING THE SYSTEM, FOUND THAT THERE WAS NO POWER TO THE HEATING ELEMENT OF THE PROBE. UPON FURTHER Mar 2, 2005 · N1094L · Cessna 560CESSNA · Pitot/Static Anti-Ice SystemSDR 022405N523CS1Engine · malfunctionedDURING CRUISE AT ALTITUDE 40,000 FEET, THE RIGHT ENGINE DID A UNCOMMANDED SHUTDOWN. THE CREW PUT THE AIRCRAFT INTO THE RESTART ENVELOPE AND ATTEMPTED TWO INFLIGHT RESTARTS. THE ENGINE WOULD NOT START SO AN EMERGENCY WAS DECLARED AND THE AIRCRAFT SAFELY LANDEFeb 24, 2005 · N523CS · Cessna 560XL · Engine (Turbine/Turboprop)SDR CA050224008Engine · shutdown(CAN) THE ENGINE EXPERIENCED AN UNCOMMANDED SHUTDOWN IN CRUISE. SUBSEQUENT RELIGHT ATTEMPTS WERE UNSUCCESSFUL. THE CREW DECLARED AN EMERGENCY AND THE FLIGHT DIVERTED. MFG WILL INVESTIGATE THE EVENT AND SUPPLEMENT THIS REPORT TO REFLECT ROOT CAUSE ONCE ESTABFeb 24, 2005 · Cessna 560XL · Engine (Turbine/Turboprop)SDR DXTA200500601Engine · leakingDURING FLIGHT CREW & PASSENGERS NOTICED FUMES IN CABIN. AFTER LANDING FOUND OIL LEAKING FROM NR 1 ENGINE & NO OIL SHOWING ON SIGHT GAUGE. ENGINE CHANGE CURRENTLY IN WORK.Feb 19, 2005 · N670QS · Cessna 560XL · Engine (Turbine/Turboprop)SDR 2005FA0000276Heat Shield · contaminatedAFTER LANDING, SMOKE AND SMALL FLAME OBSERVED FROM LT MAIN GEAR WHEEL. FIRE WAS EXTINGUISHED, NO DAMAGE TO LANDING GEAR OR AIRCRAFT. LT MAIN GEAR WHEEL ASSEMBLY WAS REPLACED AS A PRECAUTION. THE LT WHEEL HAD BEEN RECENTLY CLEANED WITH A WATER BASED SOLVENT IAWFeb 11, 2005 · N404BT · Cessna 560XL · Wheel/Ski/FloatSDR CA050120006Line · cracked(CAN) AIRCRAFT DEPARTED. AS THE AIRCRAFT ACCELERATED THE CREW BECAME CONCERNED DUE TO A VIBRATION. THE AIRCRAFT WAS DIVERTED TO INTERNATIONAL AIRPORT. INVESTIGATION FOUND A CRACK IN THE HYDRAULIC LINE FROM THE LT ENGINE DRIVEN HYDRAULIC PUMP WHERE IT CONNECTJan 9, 2005 · Cessna 560XL · Hydraulic System, MainSDR DXTA200400461Fuel Filter · warning lightDURING TAKEOFF ROLL FUEL FILTER L-ANNUNCIATOR ILLUMINATED. TAKEOFF ABORTED, ANNUNCIATOR EXTINGUISHED DURING ABORT. REPLACED LEFT AND RIGHT ENGINE FUEL FILTER AND ASSOCIATED PACKING. PERFORMED SATISFACTORY ENGINE RUNS AND LEAK CHECKS. REFERENCE P + W 545 AMNov 30, 2004 · N670QS · Cessna 560XL · Engine Fuel DistributionSDR DXTA200400460Filter · warning lightDURING TAKEOFF ROLL MASTER CAUTION ILLUMINATED TRIGGERED BY RIGHT ENGINE FUEL FILTER BY-PASS ANNUNCIATOR. REMOVED AND REPLACED RT FUEL FILTER IAW P&W 545 MM CHAPTER 73-10-07. LEAK CHECK GOOD, FILTER INSTALLED IS NEW. OPERATIONAL CHECK SATISFACTORY.Nov 29, 2004 · N621QS · Cessna 560XL · Engine Fuel DistributionSDR CA050107001Hmu · failed(CAN) RT ENGINE WOULD NOT START.Nov 28, 2004 · Cessna 560XL · Fuel Controlling SystemSDR CA041202004Control Cable · broken(CAN) DUE TO THE RISK ASSOCIATED TO BROKEN MAIN CONTROL CABLES, FOLLOWING THE BROKEN RT WING DOWN OB AILERON CABLE P/N 6660001-62 AT RWS 54 (REF. SDR NR 20031113014), WE DECIDED TO INSPECT THE AILERON WING CABLES MORE FREQUENTLY THAN THE 1200 HRS REQUIRED BY Nov 26, 2004 · Cessna 560XL · Aileron Control System
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