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 DXTA2012073005062Apu · leakingON TAKEOFF AND WHILE AT TAKE OFF POWER AND APU RUNNING, LIGHT FOWL SMOKE FILLED COCKPIT AND AIR FROM A/C WAS BLOWING HOT AIR. WHILE AVOIDING WEATHER AND WAITING TO LAND, SMOKE DISSIPATED AND A/C STARTED BLOWING COLD AGAIN. NO ANNUNCIATORS ILLUMINATED AND ALL Jul 27, 2012 · N629QS · Cessna 560XL · APU Oil SystemSDR 9JLA2012073103552Indicator · defectiveCREW REPORTED THE NR 1 ENGINE N2 INDICATOR WAS INTERMITTENT. REMOVED THE N2, OIL TEMP/PRESSURE INDICATOR, INSTALLED AN O/H UNIT. FUNCTIONAL CHECKS SATISFACTORY.Jul 27, 2012 · N523KW · Cessna 560XL · Engine Integrated Instrument SystemSDR ZESA20120802Switch · intermittentPILOT WAS ON TAKEOFF AND APPROACHING V1 AND THE "NO TAKE OFF" WARNING ANNUNCIATED, PILOT ABORTED TAKEOFF. DETERMINED A SWITCH WITHIN THE RT WING SPEED BRAKE CAUSED THE ISSUE. BAD SWITCH AND CORROSION WITHIN THE CONNECTOR WERE REPAIRED. ACFT RETURNED TO SERVJul 26, 2012 · N228Y · Cessna 560XL · SpoilersSDR CA120802009Oil System · low pressure(CAN) DURING REVENUE FLIGHT, RT AFTER TAKEOFF, THE CREW EXPERIENCED A LOW OIL PRESSURE WITH SMOKE IN COCKPIT AND CABIN. THE CREW DECLARED AN EMERGENCY AND FLEW TO WHERE AN EMERGENCY LANDING WAS PERFORMED WITHOUT SHUTTING DOWN THE ENGINE.Jul 25, 2012 · Engine Oil PressureSDR DXTA2012072505057Valve · failedDURING TAKEOFF, AT ABOUT 300 FT AGL, THE ACM OVERHEAT LIGHT CAME ON FOLLOWED BY LT BLD AIR OVERHEAT. THERE WAS BLACK ACRID SMOKE IN THE COCKPIT AND CABIN. TURNED THE PRESS SOURCE TO OFF, DECLARED AN EMERGENCY AND LANDED. TURNING THE SOURCE TO OFF HELPED WITHJul 24, 2012 · N629QS · Cessna 560XL · Cabin Cooling SystemSDR CA121105013Engine · power loss(CAN) DURING THE ROLLING TAKE OFF, THE ENGINE NR 2 DID NOT PRODUCE THE TAKE OFF POWER REQUESTED BY THE CREW. THE CREW ABORTED TAKE OFF AND SUBSEQUENT GROUND TEST CONFIRMED THE ISSUE ON THE NR 2 ENGINE. BLEED VALVE AND ITS TORQUEMOTOR WAS SUSPECTED.Jul 19, 2012 · Cessna 560XL · Engine (Turbine/Turboprop)SDR CA120702003Indication Sys · malfunctioned(CAN) THE ACFT WAS ON A REPOSITIONING FLIGHT. SHORTLY AFTER TAKE OFF, DURING CLIMB, THE ICAS GAVE THE FOLLOWING MESSAGES: ENGINE FAULT RT OIL PRESSURE. FOLLOWING THE OIL PRESSURE LOSS CHECK LIST THE RT ENGINE WAS SHUTDOWN AND WE REQUESTED EMERGENCY TURN BACKJun 17, 2012 · Cessna 560XL · Engine Oil Indicating SystemSDR 9JLA2012071904455Control Valve · defectiveCREW REPORTED THAT THE APU BLEED AIR WAS INOPERATIVE. TROUBLESHOOTING INDICATED THAT THE APU BLEED AIR CONTROL VALVE WAS DEFECTIVE. AN OVERHAULED VALVE WAS INSTALLED, FUNCTIONAL CHECKED SATISFACTORY.Jun 7, 2012 · N309BT · Cessna 560XL · APU Bleed Air SystemSDR 17GR201205171001Engine · warning lightCREW RECEIVED A MASTER WARNING AND A LOW OIL LIGHT FOR THE NR 2 ENGINE WHILE ON A CREW ONLY FLIGHT. ENTIRE FLIGHT WAS BELOW FL180.May 14, 2012 · N560ML · Cessna 560XL · Turbine Engine Oil SystemSDR CA120524006Oil System · low pressure(CAN) DURING CLIMB OIL PRESSURE DROPPED TO APPROXIMATELY 20 PSID AND THE MAIN OIL PRESSURE (MOP) LIGHT ILLUMINATED. THE CREW REDUCED POWER AND OIL PRESSURE DID NOT CHANGE. CREW ELECTED TO PERFORM AN IFSD AND CONTINUE TO DESTINATION WERE A UNEVENTFUL SINGLE ENGMay 14, 2012 · Cessna 560CESSNA · Engine Oil PressureSDR DXTA2012042504958Engine · bird ingestionAT FL390 IN CRUISE. RUBBER ODOR LIKE A BURNING TENNIS SHOE. AFTER 5 MINUTES EYES BEGAN TO BURN. NO SMOKE BUT THE BURNING ODOR WAS MODERATE TO STRONG. ADJUSTED COCKPIT TEMPERATURE CONTROLLER WITH NO NOTICEABLE CHANGE IN ODOR. THE ODOR DIDN'T APPEAR TO COMApr 24, 2012 · N604QS · Cessna 560XL · Engine (Turbine/Turboprop)SDR CA120507006Engine · smoke(CAN) IT`S REPORTED THAT A T/O WAS ABORTED DUE TO A SMOKE IN THE CABIN ISSUE. THE ENGINE FROM WHICH THE SMOKE ORIGINATED IS UNKNOWN. NO OTHER INFO IS AVAILABLE AT THIS TIME. TROUBLESHOOTING IS ON-GOING.Apr 24, 2012 · Cessna 560XL · Engine (Turbine/Turboprop)SDR CA120426010Switch · malfunctioned(CAN) DURING FLIGHT CREW WERE UNABLE TO CONTROL THE CABIN TEMPERATURE, ACM OVERTEMP WARNING RECEIVED AND AT 1 POINT THEY THOUGHT THEY COULD SMELL SOME FUMES, WITH FURTHER MANIPULATION OF CONTROLS CREW WAS ABLE TO GAIN SOME CONTROL OF TEMPERATURE. ECU TEMP SWITApr 23, 2012 · Cessna 560XL · Cabin Temperature Control SystemSDR CA120507005Engine · power loss(CAN) AT FL350 THE LT ENGINE N1 SPEED ROLLED BACK 5 PERCENT UNCOMMANDED AND BECAME UNRESPONSIVE TO THROTTLE LEVER INPUTS. THE ENGINE STARTED TO SURGE SLIGHTLY BUT EVENTUALLY STABILIZED AFTER SEVERAL MOMENTS. THE ACFT LANDED SAFELY AND POST FLIGHT TROUBLESHOOApr 21, 2012 · Engine (Turbine/Turboprop)SDR CA120411004Bleed Valve · faulty(CAN) DURING DEPARTURE TAKEOFF POWER WAS SET FOR 3-5 SECONDS, LT ELECTRONIC ENGINE CONTROL ANNUNCIATOR ILLUMINATED AND ENGINE REVERTED TO MANUAL MODE, TAKEOFF WAS ABORTED AT 50 KNOTS. ACFT WAS SENT TO MFG, TROUBLESHOOTING ONGOING. PERFORMED GROUND RUN AND CAApr 2, 2012 · Cessna 560XL · Compressor Bleed ValveSDR CA120312004Oil System · low pressure(CAN) PILOT REPORTED OIL PRESSURE GAUGE DROPPED INTO YELLOW AND THE RED LOW PRESSURE LIGHT POPPED ON AT 20 PSI. PILOT FOLLOWS REQUIRED ENGINE SHUTDOWN PROCEDURES. OVERWEIGHT LANDING RECORDED DUE TO MAX FUEL WEIGHT CONDITION.Feb 28, 2012 · Beech 200BEECH · Engine Oil Indicating SystemSDR CA120224007Pump · failed(CAN) AFTER CREW SELECTED GEAR DOWN, THEY HAD A LOW BRAKE PRESSURE WARNING, DECLARED EMERGENCY AND LANDED USING EMERGENCY PNEUMATIC BRAKE SYSTEM TO STOP. AFTER EVALUATION, SERVICE CENTER DETERMINED THAT THE ELECTRIC MOTOR PORTION OF PUMP WAS FUNTIONAL BUT THE Feb 23, 2012 · Cessna 560XL · Hydraulic Pump (Electric/Engine), MainSDR JEMA2012FA0000029Mount · damagedRT ENGINE AFT MOUNT ASSY FOUND TO BE DAMAGED. CENTER BOLT BENT. DEEP CHECK CUTS IN ENDS OF RUBBER INSERT MATERIAL. ATTACHING ARMS SIEZED TOGETHER AT CENTER BEARING, PN 6651602-4. PART REPLACEMENT RECOMMENDED AT SECOND ENGINE CHANGE (APPROX 10,000 HRS).Jan 16, 2012 · N108EK · Cessna 560XL · Engine Mount SectionSDR A59A2012F00020Engine · multiple failDURING A CLIMB, NOTICED RT ENGINE LOW OIL PRESSURE (RED) ANNUNCIATOR ILLUMINATE. ALSO NOTICED RT ENGINE MANUAL MODE WHITE ANNUNCIATOR ILLUMINATED AND THE OIL PRESSURE GAUGE TO ZERO. PILOTS NOTICED SMOKE IN THE COCKPIT, BOTH VISUALLY AND THROUGH ODOR. DECLANov 23, 2011 · N560ML · Cessna 560XL · Engine (Turbine/Turboprop)SDR 17GR2011231100001Oil System · overservicedDURING A CLIMB THROUGH 8,500' MSL TO 10,000' ON SBN APPROACH CONTROL, NOTICED RT ENGINE LOW OIL PRESSURE (RED) ANNUNCIATOR ILLUMINATE. ALSO NOTICED RT ENGINE MANUAL MODE WHITE ANNUNCIATOR ILLUMINATED & OIL PRESSURE GAUGE ZERO FOR RT ENGINE. WITHIN A FEW SECNov 23, 2011 · N560ML · Cessna 560CESSNA · Turbine Engine Oil SystemSDR CA111130007Oil System · low pressure(CAN) DURING REVENUE FLIGHT, ON CLIMBOUT THE CREW REPORTED THAT THE LOP LIGHT CAME ON, THE ENGINE OIL PRESSURE INDICATION WAS IN THE RED BAND AND THERE WAS OIL SMELL IN THE CABIN. THE CREW SHUTDOWN AND SECURED THE ENGINE THEN DIVERTED. POST-FLIGHT INSPECTIONNov 23, 2011 · Engine (Turbine/Turboprop)SDR DXTA2011111004780Oil System · overservicedWITH APU ON AND BLEED AIR ON, COCKPIT AND CABIN FILLED WITH THICK, PUNGENT AND ACRID SMOKE. TROUBLESHOT TO OIL LEVEL TO HIGH, ADJUSTED OIL LEVEL TO CORRECT LEVEL IAW MM 12-11-03. CLEANED WATER SEPERATOR CONDENSER IAW MM 12-19-02. OPS AND LEAK CHECKED GOOD.Nov 9, 2011 · N695QS · Cessna 560XL · Turbine Engine Oil SystemSDR CA111030003Carbon Seal · leaking(CAN) DURING CLIMB THROUGH FL30, THE RT OIL PRESSURE ANNUNCIATOR ILLUMINATED WITH A MASTER WARNING WHILE THE OIL PRESSURE FELL TO ZERO. A BURNING ODOR WAS DETECTED IN THE CABIN BUT WITH NO VISIBLE SMOKE. THE ENGINE WAS SHUTDOWN, AND THE CREW RETURNED TO THE Oct 22, 2011 · Cessna 560XL · Turbine Engine Oil SystemSDR CA111019012Line · leaking(CAN) DURING T/O CLIMB, THE LT ENGINE ROLLED BACK TO 40 PERCENT N2 AND COULD NOT BE ACCELERATED FURTHER. THE PILOT SHUT THE ENGINE DOWN AND A SUBSEQUENT RESTART SHOWED THE SAME PROBLEM. HE DIVERTED THE FLIGHT, PERFORMED AN UNEVENTFUL LANDING. POST FLIGHT INOct 13, 2011 · Cessna 560XL · Engine Fuel DistributionSDR CA110930018Mount · debonded(CAN) RT AFT ENGINE MOUNT, PN 9912480-2 (PN LM-451-SA2) BONDED RUBBER INSERTS DEBONDED AND MIGRATED OUT PAST THE BOLTHEAD ON FRONT SIDE AND THE NUT ON THE AFT SIDE. THE REPLACEMENT SCHEDULE IS EVERY SECOND ENGINE CHANGE WHICH IN THIS CASE WOULD BE 10,000 HRS.Sep 29, 2011 · Cessna 560XL · Engine Mount SectionSDR CA110928003Compressor · malfunctioned(CAN) DURING CLIMB THROUGH FL300, A THUMPING NOISE WAS HEARD AND THE ACFT STARTED TO "FISHTAIL". THE CREW OBSERVED A HIGH TEMPERATURE ON THE RT ENGINE AND A "HOT" SMELL IN THE CABIN. THE POWER WAS REDUCED TO APPROX 50 PERCENT WHICH TOOK CARE OF THE TEMPERATUSep 13, 2011 · Cessna 560XL · Turbine Engine Compressor SectionSDR CA110928005Oil System · low pressure(CAN) 10 MINUTES INTO THE FLIGHT, A LOSS OF OIL PRESSURE OCCURRED AND THE ENGINE WAS SHUTDOWN. AN UNEVENTFUL EMERGENCY LANDING WAS PERFORMED. POST FLIGHT INSPECTION FOUND NO OIL ON THE SIGHT GLASS. OIL WAS ADDED AND A SUBSEQUENT GROUND RUN FOUND SOME NOISE ISep 13, 2011 · Cessna 560XL · Engine (Turbine/Turboprop)SDR CWQR20110901018Control Cable · frayedFRAYED ELEVATOR TRIM CABLE WAS FOUND DURING A SCHEDULED INSP CABLE WAS FRAYED A HALF OF THE CABLE'S DIAMETER. AND CABLE TENSION WAS WITHIN MM LIMITS.Sep 1, 2011 · N662QS · Cessna 560XL · Elevator Tab Control SystemSDR 9JL2011F00000Unknown · malfunctionedON 2 SEPARATE OCCASIONS UNS-1 MODEL FMS`S HAVE COMMANDED ERRONEOUS TURNS ON THE SAME APPROACH SEQUENCE. INITIAL INVESTIGATION SEEMS TO INDICATE A POSSIBLE SOFTWARE DEFECT.Aug 11, 2011 · N309BT · Cessna 560XL · Flight Management Computing Software SystemSDR 2011FA0000509Transducer · failedTHE RT ENGINE OIL PRESSURE TRANSDUCER FAILED IN-FLIGHT GIVING A FALSE INDICATION OF DECRESSING PRESSURE.Aug 2, 2011 · N268CM · Cessna 560XL · Engine Oil Indicating SystemSDR CA110803005Oil System · low pressure(CAN) AT 7000 FT CREW REPORTED LT ENGINE OIL PRESSURE HAD DROPPED TO ZERO. ENGINE WAS SHUTDOWN AND ACFT RETURNED TO POINT OF DEPARTURE AND LANDED UNEVENTFULLY. TROUBLESHOOTING IS ONGOING.Jul 20, 2011 · Cessna 560XL · Engine Oil PressureSDR CA110720001Pump · faultyLOW OIL PRESSURE/IFSD AFTER T/O, THE PILOT REPORTED A LOSS OF OIL PRESSURE INDICATION AND LOW OIL PRESSURE ON THE EICAS. THE ENGINE WAS SHUTDOWN AND THE ACFT RETURNED TO THE POINT OF DEPARTURE WHERE AN UNEVENTFUL SINGLE ENGINE LANDING WAS ACCOMPLISHED, POST FJul 15, 2011 · Turbine Engine Oil SystemSDR CA110713007Actuator · seizedPILOTS REPORTED "STAB MISCOMPARE" ILLUMINATES AND HYD ANNUNCIATOR FAILS TO EXTINGUISH WHEN FLAPS ARE SELECTED TO THE UP POSITION, IN THE JOURNEY LOG. THE PILOTS ALSO STATED THAT THEY HAD DIFFICULTY TRIMMING THE PITCH OF THE ACFT. MX TROUBLESHOOTING DETERMINEDJul 9, 2011 · Cessna 560XL · Stabilizer ActuatorSDR CA110711008Engine · unknown(CAN) INABILITY TO MODULATE THRUST DURING TROUBLESHOOTING ON GROUND, THRUST COULD NOT BE MODULATED. ELECTRONIC ENGINE CONTROL SWAP WAS PERFORMED AND A SIMILAR BEHAVIOR OCCURRED AGAIN. TROUBLESHOOTING IS ONGOING.Jun 28, 2011 · Cessna 560XL · Engine (Turbine/Turboprop)SDR 2011FA0000382Throttle Switch · defectiveLT AND RT ENGINE THROTTLES HAVE A BANK OF 6 SWITCHES CONNECTED TO EACH THROTTLE LEVER. CUSTOMER`S SQUAWK WAS THAT THE DETENT INDICATOR LIGHTS (MOUNTED ON THE INSTRUEMENT PANEL) FOR THE INDIVIDUAL THROTTLE WERE INOPERATIVE. TROUBLESHOT SYS AND FOUND 2 OUT OF Jun 9, 2011 · N868J · Cessna 560XL · Power LeverSDR DJFA2011026Inlet · crackedDURING INSP OF RT ENGINE INLET, CRACKS, SCRATCHES, AND MISSING RIVETS WERE FOUND ON BOTH ENGINE INLETS. THE AIRCRAFT MANUFACTURER HAS DETERMINED THAT THE DAMAGE IS ACCEPTABLE AND HAS ALLOWED THE INLET TO CONTINUE IN SERVICE WITH ADDITIONAL PERIODIC INSPECTIONJun 6, 2011 · N306FL · Emb EMB505 · Engine Air Intake SystemSDR DXTA2011060104600Uplock Switch · failedNLG MAKES LOUD MECHANICAL BUMPING NOISES WHEN RAISED WHICH DOES NOT STOP. SOUNDED LIKE UPLOCK WOULDN'T HOLD & GEAR CONTINUOUSLY CYCLED UP. RED UNLOCK LIGHT DIMLY FLICKERED AS WELL. LOWERED HANDLE AND MLG PROPERLY LOCKED DOWN WITH 3 GREEN INDICATION. UNABLE May 31, 2011 · N606QS · Cessna 560XL · Landing Gear Position and WarningSDR CA110613002Oil System · pressure loss(CAN) IFSD DURING REVENUE FLIGHT PILOTS NOTED OIL PRESSURE DROPPED TO 25 PSI IN CLIMB. OIL PRESSURE RECOVERED TO NORMAL RANGE AFTER A FEW SECONDS. SUBSEQUENTLY, DURING CRUISE, A SIGNIFICANT DROP OF OIL PRESSURE OCCURRED. PILOTS REDUCED ENGINE POWER TO FLIGHTMay 30, 2011 · Cessna 560XL · Engine (Turbine/Turboprop)SDR DXTA2011051204577Seal · failedLEFT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED DURING FLIGHT. LT OIL PRESSURE GAUGE READ 0. SHUT LT ENGINE DOWN IAW EMERGENCY CHECKLISTS. SUSPECT NR 4 BEARING SEAL FAILING. REMOVED AND REPLACED ENGINE.May 12, 2011 · N699QS · Cessna 560XL · Turbine Engine Oil SystemSDR CA110516023Oil System · low pressure(CAN) LOW OIL PRESSURE/IFSD DURING CRUISE, THE LOW OIL PRESSURE WARNING CAME ON. THE ENGINE WAS SHUTDOWN AND AN UNEVENTFUL SINGLE ENGINE LANDING FOLLOWED. POST FLIGHT INSPECTION FOUND NO OIL ON THE SIGHT GLASS. TROUBLESHOOTING IS ON-GOING.May 12, 2011 · Cessna 560XL · Engine (Turbine/Turboprop)SDR CA110511002Ahrs · malfunctioned(CAN) ON TAKEOFF, CREW RECEIVED AN ATT FAIL ON LT EFFIS, CREW RETURNED TO LAND, AHARS UNIT REPLACED.May 10, 2011 · Cessna 560XL · Attitude and Direction Data SystemSDR CA110427004Fadec · malfunctioned(CAN) ABORTED T/O DURING T/O ROLL, THE RT ENGINE CONTROL FAULT LIGHT CAME ON. THE CREW ABORTED T/O AND THE ACFT RETURNED TO THE RAMP. TROUBLESHOOTING FOUND FAULT CODES INDICATING A FADEC CHANNEL LOSS. AN ENGINE CONTROL FAULT RESET WAS MADE AND THE FAULTS CLApr 14, 2011 · Cessna 560XL · Fuel Controlling SystemSDR CA110413005Oil System · low pressure(CAN) OIL PRESSURE LOSS/IFSD DURING FLIGHT AT FL100, THE PILOT NOTED LOSS OF MAIN OIL PRESSURE, "0" READING ON THE GAGE. THE ENGINE WAS SHUTDOWN AND AN UNEVENTFUL SINGLE ENGINE LANDING FOLLOWED. TROUBLESHOOTING IS ON-GOING.Mar 30, 2011 · Engine Oil PressureSDR CA110413006Oil System · low pressure(CAN) LOW OIL PRESSURE/IFSD DURING CLIMB PASSING FL110, THE ENGINE LOW OIL PRESSURE WARNING SOUNDED. THE PILOT IMMEDIATELY REDUCED THE POWER TO IDLE, AND SHUT THE ENGINE DOWN BEFORE RETURNING TO THE POINT OF ORIGIN WHERE AN UNEVENTFUL SINGLE ENGINE LANDING WAMar 30, 2011 · Cessna 560XL · Engine (Turbine/Turboprop)SDR CA110228009Engine · failed(CAN) ABORTED TAKEOFF, DURING TAKEOFF ATTEMPT, NR 2 ENGINE ELECTRONIC ENGINE CONTROL MANUAL LIGHT ILLUMINATED. THE T/O WAS ABORTED AND THE ACFT SHUTDOWN. THE ACFT WAS CYCLED, ENGINES STARTED IN MANUAL MODE AND A SECOND TAKEOFF WAS PERFORMED, DURING CLIMBOUT,Feb 16, 2011 · Cessna 560XL · Engine (Turbine/Turboprop)SDR CA110214005Hmu · failedFLAMEOUT IT WAS REPORTED THAT THE LEFT ENGINE FLAMED OUT ON APPROACH FOR LANDING. TROUBLESHOOTING IS ONGOING WITH MFG ASSISTANCE. TROUBLESHOOTING LEADS TO TLA UNIT AND HMU REPLACED.Feb 4, 2011 · Cessna 560XL · Fuel Control/Turbine EnginesSDR CA110209002Engine · flamed out(CAN) IFSD DURING A FERRY FLIGHT ENGINE FLAMED OUT DURING APPROACH. THE AIRCRAFT PERFORMED AN UNEVENTFUL SINGLE ENGINE EMERGENCY LANDING. TROUBLESHOOTING IS ONGOING WITH MANUFACTURER ASSISTANCE. MANUFACTURER WILL INVESTIGATE TO ESTABLISH ROOT CAUSE AND SUPPLEMFeb 3, 2011 · Cessna 560XL · Engine (Turbine/Turboprop)SDR CA110315010Oil System · low pressure(CAN) OIL PRESSURE LOSS/IFSD DURING CRUISE, THE OIL PRESSURE AND OIL TEMPERATURE STARTED TO FLUCTUATE. THE PILOT ELECTED TO RETARD THE POWER TO FLIGHT IDLE APPROXIMATELY 50 MILES OUT OF GRAND JUNCTION. OIL PRESSURE FLUCTUATIONS WERE FOLLOWED BY LOW OIL PRESSURJan 28, 2011 · Cessna 560XL · Engine Oil Indicating SystemSDR Z5FA010711N506CS1Servo Valve · inoperativeDURING CLIMB OUT AT FL330 THE LT ENGINE EEC FAIL LIGHT ILLUMINATED. THE LT EEC CIRCUIT BREAKER WAS RESET IAW THE EMERGENCY CHECKLIST AND THE EEC FAIL ANNUNCIATOR RETURNED. LT ENGINE WAS PRODUCING 10 PERCENT-15 PERCENT LESS POWER AT MAX LIMIT. ACFT DIVERTED ANDJan 7, 2011 · N506CS · Cessna 560XL · Fuel Controlling SystemSDR DXTA2011010304388Brake Assy · weakAFTER TOUCHDOWN BRAKES FELT SPONGY AND THEN BECAME EXCESSIVELY GRABBY WHEN SLOWING. CONDUCTED BRAKE BLEED PROCEDURE AND TAXI CHECK. BRAKES FUNCTION NORMAL AT THIS TIME IAW MM 32-42-00.Jan 1, 2011 · N695QS · Cessna 560XL · Landing Gear Brake System
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