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 DXTA200702385Brake Assy · malfunctionedON LANDING, CAPTS LT BRAKE PEDAL WENT TO FLOOR WITH NO BRAKING ACTION. REMOVED AND REPLACED PILOTS LT WHEEL BRAKE MASTER CYLINDER. PERFORMED BRAKE BLEED. PERFORMED LEAK CHECK. NO LEAKS NOTED. RAN AIRCRAFT FOR TAXI BRAKE CHECK. NO DISCREPANCYS NOTED. WORK PERAug 6, 2007 · N639QS · Cessna 560XL · Landing Gear Brake SystemSDR DXTA200702360Brake · inoperativeLT MAIN BRAKE SPONGY ON BOTH SIDES OF COCKPIT. BLED LEFT MAIN BRAKE. OPS AND LEAK CHECK GOOD. TAXIED ACFT TO RUN-UP AREA AND BACK. NO DEFECTS NOTED. DONE IN REF. TO CE-560XL MM 32-42-00.Jul 29, 2007 · N639QS · Cessna 560XL · Landing Gear Brake SystemSDR CWQR200704Closeout Panel · crackedDURING A PHASE 5 INSPECTION, FOUND LT WHEEL WELL AFT SPAR CLOSE OUT PANEL CRACKED. (3) CRACKS WERE FOUND BEGINNING FROM THE LOWER SKIN ATTACH FLANGE AND GOES STRAIGHT UP THE PANEL. AN SDR HAS BEEN SUBMITTED TO AIRCRAFT UNDER NR 303303.Jul 16, 2007 · N694QS · Cessna 560XL · Wing, Rib/BulkheadSDR CWQR200705Closeout Panel · crackedDURING A PHASE 5 INSPECTION, FOUND LT WHEEL WELL AFT SPAR CLOSE OUT PANEL CRACKED. (3) CRACKS WERE FOUND BEGINING FROM THE LOWER SKIN ATTACH FLANGE AND GOES STRAIGHT UP THE PANEL. AN SCR HAS BEEN SUBMITTED TO MFG AIRCRAFT UNDER NR 303303.Jul 16, 2007 · N694QS · Cessna 560XL · Wing, Rib/BulkheadSDR DXTA200702338O-Ring · leakingBLUE GEAR FLUID LEAKING OUT OF NOSE GEAR AND A HALF CUP OF FLUID HAS POOLED IN LT AVIONICS BAY. STARTED SMOKING WITH BATTERY SWITCH ON. PULLED CIRCUIT BREAKERS. [07-23-07] FOUND BRAKE PUMP FILTER BOWL O-RING BLOWN & SMOKING WAS A SKYDROL MIST COMING FROM Jul 15, 2007 · N671QS · Cessna 560XL · Hydraulic System, MainSDR DXTA200702332Indicator · malfunctionedLT MAIN LANDING GEAR INDICATOR WOULD NOT EXTINGUISH AFTER GEAR WAS BROUGHT UP. CYCLED GEAR 3 TIMES, INDICATOR STAYED ON EACH TIME. [07-23-07] JACKED A/C IAW CESSNA AIRCRAFT TO MODEL 560 MAINTENANCE MANUAL 7-10-11. SWING LANDING GEAR THROUGH 5 CYCLES, COULJul 12, 2007 · N844QS · Cessna 560CESSNA · Landing Gear Position and WarningSDR DXTA200702323Actuator · inoperativeDURING LANDING GEAR EXTENSION THE RT MAIN GEAR WOULD NOT EXTEND AND THE (HYD PRESS) ANNUNCIATOR ILLUMINATED CONTINUOUSLY. THE LANDING GEAR EXTENDED AFTER COMPLETING THE LANDING GEAR WILL NOT EXTEND CHECKLIST. REMOVED AND REPLACED RT MAIN LANDING GEAR ACTUATORJul 7, 2007 · N641QS · Cessna 560XL · Landing Gear ActuatorSDR DXTA200702304Brake · stuckLT BRAKE IS STICKING CAUSING CONTROL ISSUES WHILE TAXIING. INSTALLED AN OVERHAULED BRAKE IN LT POSITION IAW MM CH 32-42. INSTALLED AN OVERHAULED METERING VALVE IN LT POSITION IAW THE MM CH 32-42.Jun 28, 2007 · N627QS · Cessna 560XL · Landing Gear Brake SystemSDR DXTA200702293Engine · unknownUPON ADDING TAKEOFF POWER, CREW HEARD VERY LOUD EXPLOSIVE SOUND. CREW ABORTED TAKEOFF AND AS WE TAXIIED OFF OF RUNWAY, CREW HEARD EXTREMELLY LOUD FLUTTER BANGS THAT WERE CONSTANT. CREW SHUTDOWN RIGHT ENGINE. [07-12-07] RAN ENGINE AND NOISE STOPPED. RAN BOTHJun 24, 2007 · N640QS · Cessna 560XL · Engine (Turbine/Turboprop)SDR DXTA200702279Landing Gear · malfunctionedWHEN GEAR SELECTED DOWN, LT MAIN GEAR DID NOT SHOW GREEN LIGHT. WENT TO GEAR WOULD NOT EXTEND CK LIST AND BLEW GEAR DOWN. UNEVENTFUL LANDING. [07-11-07] TROUBLESHOT TO A FAULTY DOWN & LOCK SWITCH ON LT MLG ACTUATOR. REMOVED LT MLG ACTUATOR, INSTALLED A REPAIJun 19, 2007 · N604QS · Cessna 560XL · Landing Gear Retraction/Extension SystemSDR DXTA200702280Unknown · smokeSMOKE WAS SEEN AND SMELLED IN THE COCKPIT. WITH APU RUNNING. [07-12-07] REMOVED AND REPLACED APU IAW 560XL M/M 49-10-00. APU LEAK CHECKS AND OPERATES NORMAL AT THIS TIME. THIS CLEARS MEL 49-1 AREA.Jun 19, 2007 · N639QS · Cessna 560XL · Air Distribution SystemSDR DXTA200702268Unknown · smokeGROUND CONTROLLERS REPORTED SMOKE FROM RT SIDE OF AIRPLANE. UPON APU SHUTDOWN, SMOKE WAS OBSERVED COMING FROM APU INTAKE AND EXHAUST. BOTH RED AND YELLOW APU OIL LIGHTS ILLUMINATED. APU OIL LEVEL WAS VERIFIED NORMAL PRIOR TO THIS EVENT. [07-09-07] REMOVED AJun 16, 2007 · N677QS · Cessna 560XL · APU Cowling/ContainmentSDR DXTA200702263Eec · failedRT EEC FAILED DURING TAKE-OFF, ENGINE INDICATIONS WERE IN TRANSIENT LIMTS. [07-09-07] DOWNLOADED RIGHT EEC AND FOUND CODE F1-10 DISPLAYED FOR BLEED VALVE TORQUE MOTOR. CHECKED WIRING BETWEEN TORQUE MOTOR AND EED NO DEFECTS NOTED. REMOVED AND REPLACED TJun 14, 2007 · N643QS · Cessna 560XL · Engine (Turbine/Turboprop)SDR DXTA200702266Unknown · odorAFTER TAKEOFF RECEIVED ACM OVERHEAT INDICATION WITH RT BLEED AIR AND RT ITT (RED FLAG) INDICATION, ALSO HAD A ODOR OF SOMETHING BURNED COMING OUT OF THE VENTS ITT WAS APPROXIMATELY BETWEEN 750-760 DEG F FOR 4-5 SECONDS. [07-09-07] REMOVED AND REPLACED THE RJun 14, 2007 · N601QS · Cessna 560XL · Air Distribution SystemSDR DXTA200702260Unknown · smokeAFTER THE APU WAS STARTED AND THE BLEED AIR SELECTED ON THE CABIN IMMEDIATELY FILLED W/SMOKE. PERFORMED SPEED BRAKE OPERATIONAL CHECK IAW 400XP MM 27-60-00. OPS CHECKED GOOD. THE APU FAIL LIGHT CAME ON AND THE APU SHUT DOWN. REMOVED APU S/N P-403 AND INSTALLEJun 13, 2007 · N659QS · Cessna 560XL · Air Distribution SystemSDR DXTA200702257Servo · inoperativeRT ENGINE WILL NOT MAKE TAKEOFF POWER 88.1 N1 WAS NEEDED AND IT WOULD ONLY GO TO 80 PERCENT. R&R BOV TORQUE MOTOR IAW PRATT & WHITNEY 545A MAINT. MANUAL 75-30-01 & COMPLETED SECONDARY ORIFICE CALIBRATION I.A.W 560 EXCEL M.M. 71-00-04Jun 11, 2007 · N687QS · Cessna 560XL · Compressor Bleed ValveSDR DXTA200702237Engine · vibrationDURING TAKEOFF, THE NR 2 ENGINE HAD A HIGH PITCHED WHINE ACCOMPANIED BY A RT VIBE ADVISORY LIGHT, 101.1 PERCENT N2, AND AN OIL PRESSURE SPLIT OF APPROXIMATELY 30-35 PSI. T/O ABORTED. REMOVED NR 2 ENGINE AND INSTALLED SERVICEABLE UNIT. ALL OPS AND LEAK CHECKS Jun 2, 2007 · N612QS · Cessna 560XL · Engine (Turbine/Turboprop)SDR DXTA200702233Brake · weakRT BRAKE IS SPONGY, TRAVELS FURTHER THAN LT BEFORE GETTING PRESSURE, OCCURS ON BOTH PILOT & COPILOTS PEDALS. PERFORMED ANTI-SKID BRAKE SYSTEM BLEED AND OPERATIONAL TEST IAW AMM 32-42-00. NO DEFECTS NOTED.Jun 1, 2007 · N667QS · Cessna 560XL · Landing Gear Brake SystemSDR DXTA200702234Actuator · inoperativeSTAB MISCOMPARE LIGHT ILLUMINATES ON FLAP RETRACTION AFTER T/O. REMOVED HORIZONTAL STAB ACTUATOR AND INSTALLED AN INSPECTED ACTUATOR. OPS AND LEAK CHECKS GOOD. WORK DONE IAW CHAPTER 27-40-00 OF THE MM.Jun 1, 2007 · N686QS · Cessna 560XL · Stabilizer Control SystemSDR DXTA200702227Brake Assy · weakBRAKES ARE SPONGY, CAN BE FORCED TO THEIR STOPS RT SIDE MORE THAN LT. BLED BOTH LT AND RT BRAKES. ALSO CYCLED PARKING BRAKE SEVERAL TIMES DURING BLEEDING PROCEDURES. WORK DONE IAW AMM 32-42-00. SERVICED BRAKE RESERVOIR AS REQUIRED. WORK DONE IAW AMM 12-12-02.May 31, 2007 · N667QS · Cessna 560XL · Landing Gear Brake SystemSDR DXTA200702219Brake · weakLT BRAKE FADES NEAR END OF ROLLOUT DURING MEDIUM, CONTINUOUS BRAKING. ACCOMPLISHED BRAKE BLEEDING PROCEDURE IAW MM 32-42-00. OPS CHECKED NORMAL.May 27, 2007 · N670QS · Cessna 560XL · Landing Gear Brake SystemSDR DXT2007F00000Bolt · looseAIRCRAFT CAME INTO THE REPAIR STATION DUE TO THE ENGINE NR1 HIGH TT. DURING BORESCOPE INSPECTION OF THE HP COMPRESSOR AS PART OF THE TROUBLESHOOTING, THE TECHNICIAN OBSERVED 2 EACH LOOSE BOLTS (GAS GENERATOR CASE TO INTERMEDIATE CASE FLANGE, FLANGE C) THE ENMay 7, 2007 · N636QS · Cessna 560XL · Engine (Turbine/Turboprop)SDR DXTA200702166Unknown · smokeCABIN FILLED WITH SMOKE WHEN LT ENGINE WAS STARTED (APU WAS ON- ON THE GROUND. [SUP 05-16-07] REMOVED & REPLACED APU IAW 560XL M.M. CHAPTER 49-10-00. OPERATION AND LEAK CHECKS GOOD. REMOVED UNIT HRS. 140.3 CYL. 304. INSTALLED UNIT HOURS 2424.3 CYCLES 3905.May 1, 2007 · N606QS · Cessna 560XL · Air Distribution SystemSDR DXTA200702160Unknown · warning lightAFTER TAKE OFF THE RED GEAR UNLOCK LIGHT REMAINED ILLUMINATED. CYCLED THE GEAR DOWN, LIGHT EXTINGUISHED. [SUP 05-03-07] FOUND NOSE GEAR NOT SEATING IN UPLOCK. JACKED AIRCRAFT AND PERFORMED NOSE GEAR STRUT SERVICING PROCEDURE IAW CE560XL MM 12-14-00. PERFORMEApr 28, 2007 · N632QS · Cessna 560XL · Landing Gear Position and WarningSDR DXTA200702155Rudder Pedal · damagedAFTER ROTATION, THE YAW DAMPER WOULD NOT ENGAGE AND WHEN WE TURNED LT, THE LT RUDDER PEDAL WOULD NOT MOVE. AFTER ENGAGING AND DISENGAGING THE YAW DAMPER THE RUDDER OPERATED NORMALLY. ON THE GROUND WE COULD FEEL AND HEAR GRINDING SOUND IN THE RUDDER PEDALS WHApr 27, 2007 · N624QS · Cessna 560XL · Rudder Control SystemSDR DXTA200702133Brake · faultyLT BRAKE EXTREMELY SPONGY ON TAXI IN. [4-27-07] BLED BRAKE SYSTEM IAW CESSNA 560 XL M/M CHAPTER 32-42-00. OPS CHK SATISFACTORY.Apr 23, 2007 · N639QS · Cessna 560XL · BrakeSDR DXTA200702116Warning Light · illuminatedAFTER TAKEOFF GOT GEAR UNLOCK LIGHT / HYDRAULIC PRESSURE STEADY LIGHT AFTER GEAR RETRACTION. TROUBLESHOT TO THE NOSE GEAR UPLOCK SWITCH OUT OF RIG. MADE UPLOCK SWITCH ADJUSTMENT. OPS CHECK GOOD. IAW CE560 XL MM CH 32-30-05.Apr 18, 2007 · N663QS · Cessna 560XL · Landing Gear Position and WarningSDR DXTA200702114Warning Light · illuminatedAFTER TAKEOFF , THE RED GEAR UNLOCK LIGHT REMAINED ILLUMINATED. JACKED AIRCRAFT, INSPECTED AND CLEANED UPLOCK SWITCHES IN ALL THREE GEARS AND NO VISUAL DEFECTS WERE NOTED. PERFORMED SEVERAL OPERATIONAL CHECK OF LANDING GEAR FOR PROPER OPERATION AND ALSO NO DEApr 17, 2007 · N615QS · Cessna 560XL · Landing Gear Position and WarningSDR DXTA200702113Warning Light · illuminatedAFTER TAKEOFF RED GEAR UNLOCK LIGHT REMAINED ON. FLEW FOR APPROX 1 HOUR TO GET BELOW MAX LANDING WEIGHT AND IN THAT TIME THE HYDRAULIC PRESSURE ANNUNCIATOR CAME ON ONE TIME FOR APPROX 1 SECOND. JACKED AIRCRAFT, INSPECTED AND CLEANED UPLOCK SWITCHES IN ALL TApr 16, 2007 · N615QS · Cessna 560XL · Landing Gear Position and WarningSDR PAZR200700001Attach Fitting · crackedDURING A SCHEDULED INSPECTION, A 1.5 INCH CRACK WAS FOUND IN THE LOWER RADIUS OF THE HORIZONTAL STABILIZER AFT ATTACH FITTING.Apr 16, 2007 · N186XL · Cessna 560XL · Horizontal Stabilizer, Attach FittingsSDR DXTA200702098Bulb · inoperativeON GEAR EXTENSION , LT MAIN HAD NO LIGHTS , COMPLETED CHECKLIST Z3 STILL NO INDICATION, GEAR BLEW DOWN. [SUP 4-19-07] JACKED AIRCRAFT, RAN LANDING GEAR UP & DOWN SEVERAL TIME NOTED LEFT MAIN GEAR DOWN & LOCKED LIGHT NOT ILUMINATING CHECK BULBS. FOUND BAD. REApr 11, 2007 · N652QS · Cessna 560XL · Landing Gear Position and WarningSDR DXTA200702088Windshield · failedLT WINDSHIELD SHATTERED. RECEIVED LT FAULT, SELECTED OFF, LT O'HEAT WINDSHIELD, ARCED AND SHATTERED, DIVERTED. [SUP 4-19-07] REPLACED WINDOW IAW MM 56-11-00Apr 7, 2007 · N696QS · Cessna 560XL · Flight Compartment WindowsSDR DXTA200702085Brake Assy · malfunctionedIMMEDIATELY UPON, LANDING, PWR BRAKE AND ANTISKID ANNUNCIATOR CAME ON WITH MASTER, CAUTION, STILL HAD PRESSURE UPON EXITING RUNAWAY PWR BRAKE CIRCUIT BREAKER, POPPED RESET ONCE , STILL HAD SOME PRESSURE. THEN BREAKER POPPED AGAIN AND BRAKES FAILED, USED EMERGEApr 5, 2007 · N637QS · Cessna 560XL · Landing Gear Brake SystemSDR DXTA200702070Eec · failedLT EEC FAILED TO MANUAL ON TAKEOFF ROLL AT 40 KIAS. TWO TIMES. ABORTED TAKE OFF. REMOVED BLEED SERVO AND INSTALLED NEW SERVO SN TR2508 IAW PW MM CH 75-50-01. OPERATIONAL CHECKS GOOD ON TORQUE MOTOR INSTALLED NR 40 ORIFICE IN BOV IAW PW545A MM CH 71-00-00. OApr 3, 2007 · N690QS · Cessna 560XL · Fuel Control/Turbine EnginesSDR DXTA200702077Brake Assy · hotRT BRAKE EXCESSIVELY GRABS AND WHEN INSPECTED IS EXTREMELY HOT. PERFORMED TAXI CHECK. FOUND EVEN APPLICATION WHEN BRAKING. BRAKES USUALLY EXTREMELY HOT AFTER LANDING AND TAXING. BOTH BRAKES VERY WARM. FOUND RT BRAKE WEAR INDICATOR AT .15" WHICH GIVES OUT TO 1Apr 3, 2007 · N668QS · Cessna 560XL · Landing Gear Brake SystemSDR DXTA200702076Unknown · unknownAFTER LOWERING LANDING GEAR (MASTER CAUTION) ALONG WITH (LOW BRAKE PRESS) AND (ANTISKID INOP) ILLUMINATED FLASHING FOR APPROX 30 SECONDS. LIGHTS EXTINGUISHED PRIOR TO LANDING AND NORMAL BRAKING WAS NOTED. T/S FOUND SYSTEM OPS CHECKS NORMAL. ITEM IS A COLD SOApr 3, 2007 · N631QS · Cessna 560XL · Central WarningSDR DXTA200702068Connector · contaminated(P) SMOLDERING ELECTRICAL ODOR COMING FROM SEAT NR 4 VIDEO SCREEN RECEPTICLE WHEN SCREEN IS INSERTED. NO DIVERTION. FOUND DEBRIS ACROSS CONTACTS INSIDE SCREEN RECEPTACLE AT SEAT NR 4. REMOVED DEBRIS AND CLEANED CONTACTS AS REQUIRED. VIDEO MONITOR OPS CHECKApr 2, 2007 · N616QS · Cessna 560XL · Communications System WiringSDR DXTA200702067Trim System · stuck(P) ON TAKEOFF TRIM STUCK JUST BETWEEN THE TOP LINE AND THE TOP OF THE (T) IN THE TAKEOFF RANGE. WE MANUALLY FORCED IT FREE AND IT BEGAN TO WORK AGAIN. DURING THE RETURN TO THE AIRPORT, THE ELECTRIC TRIM SEEMED TO DRAG IN THE TAKEOFF RANGE. PERIODICALLY MOVINGApr 2, 2007 · N603QS · Cessna 560XL · Elevator Tab Control SystemSDR DXTA200702066Hook · stickingGEAR UNLOCK LIGHT REMAINED ILLUMIATED AND HYDRALIC PRESSURE LIGHT REMAINED ON, RAN CHECKLIST AND LIGHTS EXTINGUISH WHEN HYDRAULIC CONTROL CIRCIUT BRAKER RESET IAW CHECKLIST. REMOVED AND REPLACED NOSE GEAR UPLOCK SWITCH WITH NEW. NOSE GEAR UPLOCK HOOK WAS STICApr 1, 2007 · N651QS · Cessna 560XL · Landing Gear Retraction/Extension SystemSDR DXTA200702058Control Cable · out of adjustAIRCRAFT WILL NOT FLY LEVEL IN FLIGHT AFTER AILERON RIGGING WITH CONTROLS CENTERED. ADJUSTED AILERON WING AND FAIRING CABLE TENSION AND RIG IAW 560XL MM 27-10-00. OPS CHECK OK.Mar 31, 2007 · N604QS · Cessna 560XL · Aileron Control SystemSDR DXTA200702056Unknown · unknown(NO TAKEOFF) LIGHT ILLUMINATED ON TAKEOFF ROLL-ABORTED-CYCLED STAB, FLAPS AND SPEED BRAKE MANY TIMES, NO CHANGE. PULLED SPEED BRAKE BREAKER AND LIGHT WENT OUT. TROUBLE SHOT SPEED BRAKE SYSTEM. FOUND EXCESSIVE MOISTURE LET SPEED BRAKE DOWN SWITCH CONNECTOR. Mar 31, 2007 · N603QS · Cessna 560XL · Drag Control SystemSDR DXTA200702038Warning Light · inoperativeNO TAKEOFF LIGHT ILLUMINATED ON TAKEOFF ROLL. FLAPS, TRIM AND SPEEDBRAKES WERE ALL VERIFIED IN CORRECT POSITION, ABORTED TAKEOFF. (SUPPLEMENTAL 23 MARCH 07) FOUND DURING OP'S CHECK NO TAKEOFF LIGHT WOULD ILLUMINATE BY JUST BUMPING ELEVATOR TRIM WHEEL, REMOVEMar 20, 2007 · N603QS · Cessna 560XL · Central WarningSDR CA070514021Engine · low pressure(CAN) THE ENGINE EXPERIENCED AN INCREASE IN OIL PRESSURE AND TEMPERATURE AND WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED METALLIC DEBRIS IN THE ENGINE OIL. MFG WILL INVESTIGATE THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 200705Mar 18, 2007 · Cessna 560XL · Engine Oil PressureSDR DXTA200702033Control Column · vibrationNOTICEABLE VIBRATION OF CONTROL COLUMN DURING TAKEOFF,CLIMB,REDUCED DURING. CRUISE AND BEGINS TO BE MORE NOTICEABLE DURING DECENT AND LANDING. TROUBLESHOT ELEVATOR SYSTEM. FOUND LEFT AND RIGHT ELEV. TRIM TAB BEARINGS TO HAVE EXCESSIVE PLAY. REMOVED AND REPLACMar 17, 2007 · N643QS · Cessna 560XL · Control Column SectionSDR DXTA200702017Transmitter · malfunctionedDURING POWER REDUCTION TO IDLE AT 10.000 FT, LT ENGINE OIL PRESSURE DROPPED TO BELOW 20 PSI AND JUMPED BACK AND FORTH TO 40 PSI. ON POWER INCREASE, PRESSURE STAYED AROUND 30 PSI. ENGINE WAS LEFT AT IDLE UNTIL COMPLETION OF FLIGHT. LOWERED NR 1 ENGINE COWLING.Mar 13, 2007 · N696QS · Cessna 560XL · Engine Oil PressureSDR CA070514013Engine · low pressure(CAN) THE ENGINE EXPERIENCED AN LOSS OF OIL PRESSURE DURING CRUISE AND WAS REMOVED FROM SERVICE FOR FURTHER INVESTIGATION. MFG WILL INVESTIGATE AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514013)Mar 9, 2007 · Cessna 560XL · Engine Oil PressureSDR CA070614005Bolt · loose(CAN) DURING SCHEDULED MAINTENANCE ACTIVITIES, 3 OF THE MS9556-08 BOLTS LOCATED AT THE ENGINE GAS GENERATOR TO INTERMEDIATE CASE FLANGE WERE DETERMINED TO BE LOOSE. AN ADDITIONAL BOLT WAS FOUND TO BE COMPLETELY MISSING. MFG WILL INVESTIGATE AND ADVISE ON ROOTMar 7, 2007 · Cessna 560XL · Turbine SectionSDR DXTA200701993Motor · failedNR 2 ENGINE EEC FAILED AFTER DEPARTURE PASSING THROUGH 10,000 FEET. AFTER CHECKLIST ITEMS WERE COMPLETE ENGINE COMPRESSOR STALLS CONTINUED. VERIFIED DISCREPANCY. INSPECTED AND FOUND DEBRIS INSIDE BOV TORQUE MOTOR AND SECONDARY ORIFICE. REMOVED AND REPLACED WMar 3, 2007 · N690QS · Cessna 560XL · Fuel Control/Turbine EnginesSDR DXTA200701983Unknown · unknownSTAB MISCOMPARE AND HYD PRESS LIGHT CAME ON OUT OF APPROX 3000 FT WITH THE GEAR UP AND FLAPS UP SPEED APPROX 220 KTS. RAN CHECKLIST . PULLED HYD CONTROL CB. HYD CONTROL CB. HYD PRESS WENT OUT. CONFIGURED FOR LANDING . WITH FLAPS 15 STAB MISCOMP WENT OUT. PMar 1, 2007 · N664QS · Cessna 560XL · Flight Control SystemSDR CA070514003Seal · leaking(CAN) ENGINE OIL PRESSURE WAS SEEN TO FLUCTUATE IN CLIMB AND DURING CRUISE THE LOW OIL PRESSURE WARNING ACTIVATED. THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED A LEAKING ACCESSORY GEARBOX LIP SEAL. (TC NR 20070514003)Mar 1, 2007 · Cessna 560XL · Turbine Engine Oil System
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