Textron 560XL

Service difficulty reports · 3,810

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Query with SQL
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 = '560XL'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DXTA2011111404784Trim System · frozenELEVATOR TRIM STUCK. FROZE UP INFLIGHT. IT WOULD NOT OPERATE ELECTRICALLY OR MANUALLY. IT COULD NOT BE MOVED ANY AT ALL MANUALLY. IT CREATED POSITIVE FORWARD FORCE ON THE CONTROLLS INFLIGHT. ONCE ON THE GROUND IT STARTED TO WORK AGAIN. PERFORMED ELEVATORNov 11, 2011 · N630QS · Cessna 560XL · Elevator Control SystemSDR DXTA2011111104782Warning Light · intermittentDURING GEAR EXTENSION A FLICKERING GEAR UNLOCK INDICATION WAS NOTICED. ALL 3 GREEN LIGHTS WERE ON. APPROPRIATE CHECKLIST WAS COMPLIED WITH. AFTER PROCEDURE THE GEAR UNLOCK INDICATION EXTINGUISHED. CHECKED ALL WIRING AT SWITCHES, UPLOCK AND DOWN LOCK, NO FAULTNov 10, 2011 · N687QS · Cessna 560XL · Landing Gear Position and WarningSDR 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 DXTA2011110904779Actuator · bindingTHE AP PITCH MISTRIM ILLUMINATED AT FL410. AFTER THE AUTO PILOT WAS DISENGAGED, DISCOVERED THE ELEVATOR PITCH TRIM WAS JAMMED AND COULD NOT BE MOVED ELECTRICALLY OR MANUALLY IN THE NOSE UP DIRECTION BUT COULD SLIGHTLY BE TRIMMED MANUALLY BUT NOT ELECTRICALLY INov 8, 2011 · N677QS · Cessna 560XL · Elevator Control SystemSDR DXTA2011110504777Rudder Pedal · malfunctionedWHEN MAKING A TIGHT TURN USING RUDDER AND BRAKES, THE BRAKE PEDALS GO TO THE FLOOR WITHOUT BRAKING. THIS OCCURS BOTH IN RT AND LT TURNS AND IS FELT FROM BOTH PILOT & CO-PILOT PEDALS. BRAKING FEELS NORMAL WHEN MAKING SHALLOW TURNS OFF AND ON THE RUNWAY, BUT THNov 5, 2011 · N609QS · Cessna 560XL · Landing Gear Brake SystemSDR CA111113003Engine · smoke(CAN) AFTER COMPLETION OF THE FLIGHT AND ENGINE SHUTDOWN, WHITE SMOKE BEGAN EMANATING FROM THE RT ENGINE NACELLE. IN THE 2 MINUTES AFTER NOTICING THE SMOKE THE AMOUNT AND DENSITY COMING OUT INCREASED VERY RAPIDLY. THE ENGINE FIRE BOTTLES WERE DISCHARGED THEROct 31, 2011 · Cessna 560XL · Engine (Turbine/Turboprop)SDR DXTA2011103104772Wire Harness · damagedAFTER TAKEOFF, GEAR HANDLE WOULD NOT MOVE FROM THE EXTENDED POSITION. R & R LT MLG WIRING HARNESS IAW WM 20-10-01. ADJUSTED SQUAT SWITCH IAW MM 32-44-00. OPS CHECKED SATISFACTORY.Oct 30, 2011 · N609QS · Cessna 560XL · Landing Gear System WiringSDR DXTA2011103104769Engine · leakingAFTER FLIGHT AND ENGINE SHUTDOWN, WHITE SMOKE BEGAN EMANATING FROM THE RT ENGINE NACELLE. TROUBLESHOT RT ENGINE SMOKING AFTER SHUTDOWN INSPECTED EXTERIOR OF ENGINE. INSPECTED THROTTLE RIGGING. REMOVED SPINNER, FOUND OIL UNDER SPINNER. R & R NR 2 ENGINE IAW Oct 30, 2011 · N580QS · Cessna 560XL · Turbine Engine Oil SystemSDR DXTA2011103104774Squat Switch · inoperativeGEAR WOULD NOT RETRACT AFTER TAKEOFF, GEAR HANDLE WOULD NOT MOVE INTO THE UP POSITION. REPLACED THE LT MLG SQUAT SWITCH WITH A NEW SWITCH IAW MM 32-61-00, OPS CHECKED GOOD. PERFORMED MLG HYD SYS ADJUSTMENT TEST WHICH INCLUDES ASSOCIATED SQUAT SWITCH SYS, FLAOct 28, 2011 · N609QS · Cessna 560XL · Landing Gear Retraction/Extension SystemSDR DXTA2011103104773Downlock Switch · failedUPON PLACING THE GEAR HANDLE IN THE GEAR DOWN POSITION, THE LT MAIN GEAR LIGHT WOULD NOT ILLUMINATE. TROUBLESHOT SYS TO FAULTY DOWNLOCK SWITCH ON LT MLG ACTUATOR. R & R NR 1 MLG ACTUATOR WITH REPAIRED UNIT IAW MM 32-30-04. PERFORMED CAMBER CHECK, BLED SYS, SOct 28, 2011 · N615QS · Cessna 560XL · Landing Gear Position and WarningSDR DXTA2011102604764Connector · unsecureINTERMITTENT FIRE LIGHT TEST ON LT ENGINE. FOUND LOCKING COLLAR ON LT FIRE DETECTION CONTROL UNIT CONNECTOR WAS UNLOCKED AND UNSECURE. RESECURED AND LOCKED CONNECTOR IAW MM 26-11-02. PERFORMED NUMEROUS OPS CHECKS OF FIRE DETECTION IAW MM 26-11-00, OPS CHECKEOct 25, 2011 · N611QS · Cessna 560XL · Fire Protection System WiringSDR DXTA2011102604763Trim System · frozenDURING CLIMB FROM FL390 TO FL400 AUTOPILOT PITCH MISTRIM ANNUNCIATOR ILLUMINATED. AFTER AUTOPILOT WAS DISCONNECTED, ATTEMPTED TO CHANGE TRIM USING ELECTRIC AND MANUAL ACTUATION AND FOUND IT TO BE JAMMED. DURING DESCENT THROUGH 10,000 FT, ELEVATOR TRIM BECAME Oct 25, 2011 · N615QS · Cessna 560XL · Elevator Control 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 Z5FA20111022001Roller Pin · bindingLT ENGINE THRUST REVERSER ARM LIGHT ILLUMINATED IN FLIGHT. EMERGENCY CHECKLIST WAS FOLLOWED, AN EMERGENCY WAS DECLARED AND THE ACFT DIVERTED, LANDING WAS UNEVENTFUL. SHIMMED ROLLER PIN ASSEMBLIES ON BOTH THRUST REVERSER THROTTLE LINKS AS REQUIRED IAW DWG 556Oct 22, 2011 · N546CS · Cessna 560XL · Engine Thrust ReverserSDR DXTA2011102404760Oil System · leakingCLIMBING THRU 3000 FT, RT RED OIL PRESSURE ANNUCIATOR ILLUMINATED WITH A MASTER WARNING. RT OIL PRESSURE GAUGE WENT TO ZERO. INITIALLY OIL TEMP GAUGE WAS IN NORMAL RANGE, THEN UNABLE TO CAPTURE OIL TEMP READING. BURNING ODOR IN CABIN WITH NO VISIBLE SMOKE. POct 22, 2011 · N601QS · Cessna 560XL · Turbine Engine Oil SystemSDR DXTA2011102104758Control Handle · malfunctionedAFTER TAKEOFF AND CALLING A POSITIVE RATE AND GEAR UP, THE GEAR HANDLE COULD NOT BE MOVED. REPLACED LANDING GEAR CONTROL HANDLE ASSY IAW AMM CHP 32-30-00. PERFORMED GEAR SWING. OPS CK OF GEAR HANDLE GOOD.Oct 20, 2011 · N609QS · Cessna 560XL · Landing Gear SelectorSDR DXTA2011102004754Master Cylinder · reads lowBRAKES ARE VERY SOFT UPON LANDING. ANTI-SKID NEVER ENGAGED ON WET RUNWAY. UPON INSPECTION OF THE BRAKE PRESSURE CYLINDER, NOTICED IT READ LOW. AT 55 DEGREES, SHOULD HAVE BEEN 625-650 AND READ 425. TROUBLESHOT SYS, FOUND BRAKE ACCUMULATOR LOW. SERVICED BRAKEOct 19, 2011 · N566QS · Cessna 560XL · Master Cylinder/Brake ValveSDR CWQR2001101824Angle · crackedDURING A SCHEDULED MX CHECK, ANGLE WAS FOUND CRACKED THROUGH THE FREE FLOATING LEG INTO THE ANGLE RADIUS, THIS CRACK WAS 4.2 INCHES FROM THE END OF THE PART. THE ANGLE WAS REPLACED WITH A NEW PART.Oct 18, 2011 · N630QS · Cessna 560XL · APU Cowling/ContainmentSDR CWQR2011101823Angle · crackedDURING A SCHEDULED MX CHECK, ANGLE WAS FOUND CRACKED THROUGH THE FREE FLOATING LEG INTO THE ANGLE RADIUS, THIS CRACK WAS 4 INCHES FROM THE END OF THE PART. THE ANGLE WAS REPLACED WITH A NEW PART.Oct 18, 2011 · N665QS · Cessna 560XL · APU Cowling/ContainmentSDR Z5FA20111015001Cable · brokenON PREFLIGHT, CREW REPOTED ELEVATOR TRIM MOVED FREELY WITH NO MOTION ON TRIM TAB, ON SITE MX FOUND BROKEN ELEVATOR TRIM CABLE. R & R AFT RT ELEVATOR TRIM CABLE, TENSIONED CABLE RUN, CHECKED ALL PULLEYS AND PERFORMED "NO TAKEOFF" TEST. ALL TESTS WERE SATISFACOct 15, 2011 · N541CS · Cessna 560XL · Elevator Tab Control SystemSDR 9JLA201110153387Ahrs · failedTHE CREW REPORTED THE NR 1 AHRS FAILED IN FLIGHT. TROUBLESHOOTING FOUND THE NR 1 AHRS (S/N 2248) FAILED. INSTALLED A REPAIRED AHRS COMPUTER AND COMPLETED SATISFACTORY FUNCTIONAL CHECKS PER THE CESSNA 560XL MM 34-21-01.Oct 15, 2011 · N909LA · Cessna 560XL · Integrated Flight 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 9JLA20111093441Ahrs · failedTHE CREW REPORTED THAT THE NR 2 AHRS WOULD NOT COME ON LINE (ATT AND HEADING FAIL). TROUBLESHOT AND FOUND THAT THE AHRS UNIT S/N 1113 FAILED. INSTALLED A REPAIRED AHRS UNIT. FUNCTIONAL CHECKS SATISFACTORY. NOTE: AHRS UNIT S/N 1113 FAILED 2.9 HRS AFTER INSOct 7, 2011 · N309BT · Cessna 560XL · Integrated Flight SystemSDR CWQR20111006022Skin · damagedDURING A SCHEDULED INSPECTION, TECH NOTICED 2 RIVETS MISSING FROM THE LT DORSAL SKIN AFT OF THE NACA SCOOP. THE LOWER FASTENER HOLE ALSO APPEARED TO HAVE A CRACK ABOUT AN INCH LONG AND MOVING TOWARDS THE SECOND FASTNER HOLE. UPON DISASSEMBLE WE ALSO FOUND CRAOct 6, 2011 · N580QS · Cessna 560XL · Vertical Stabilizer, Plate/SkinSDR CA111019017O-Ring · leaking(CAN) OIL LEAK FROM OIL COLD START VALVE O-RING, AS3209-120 ON HSG 30J2350-01. REPLACED O-RING, PN AS3209-120 ON HOUSING AND O-RING, AS3209-120 ON CAP. RAN UP ENGINE AND OPERATION WAS SATISFACTORY WITH NO OIL LEAKS.Sep 30, 2011 · Cessna 560XL · Engine Start Valves/ControlsSDR 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 DXTA2011091904729Switch · out of adjustAFTER TAKEOFF FLAPS WOULD NOT RETRACT OUT OF 15 DEGREES. ADJUSTED FLAP UP SWITCH IN PEDESTAL SC012. CYCLED SEVERAL TIMES AND CHECKED FLAP DEFLECTION ANGLES. FOUND ALL OPS CHECKED NORMAL.Sep 18, 2011 · N664QS · Cessna 560XL · Trailing Edge Flap Control SystemSDR DXTA2011091904728Display · failedATTITUDE AND HEADING ON PFD NR 1 AND HEADING ON MFD FAILED ENROUTE. R & R NR 1 AHRU IAW AMM 34-21-01. OPS CHECKED GOOD.Sep 18, 2011 · N599QS · Cessna 560XL · Attitude and Direction Data SystemSDR DXTA2011091904730Bulb · inoperativeNOSE GEAR DID NOT INDICATE DOWN AND LOCKED WHEN ON APPROACH AND GEAR HANDLE DOWN. INSPECTED AND R & R ALL GREEN DOWN AND LOCKED INDICATOR LIGHT BULBS. RESET BLOWDOWN BOTTLE, JACKED AND PERFORMED GEAR SWINGS AS REQUIRED. SERVICED AND SAFETIED GEAR BLOW DOWNSep 16, 2011 · N644QS · Cessna 560XL · Landing Gear Position and WarningSDR CWQR20110915021Skin · damagedDURING A SCHEDULED INSPECTION, FOUND 2 FASTENERS MISSING FROM THE LT SIDE OF THE DORSAL FIN ASSY. UPON FURTHER INSPECTION, FOUND THE FRESH AIR DUCT ASSY TO BE CRACKED IN 2 PLACES. IT APPEARS THAT THE CRACKED DUCT ASSY ALLOWED AIR PRESSURE TO EXPAND THE DORSAL Sep 15, 2011 · N565QS · Cessna 560XL · Vertical Stabilizer, Plate/SkinSDR CWQR20110915020Support Bracket · crackedDURING A SCHEDULED MX CHECK, FOUND THIS SUPPORT BRACKET WITH A 2" CRACK IN THE CORNER RADIUS. HAVE SEEN SIMULAR CRACKED BRACKETS ON OTHER ACFT. THIS BRACKET SUPPORTS THE ECU.Sep 15, 2011 · N565QS · Cessna 560XL · Fuselage Main, Attach FittingsSDR DXTA2011091504727Motor · failedACFT WAS TAXIING TO THE RUNWAY, WHEN THE POWER BRAKES AND ANTI SKID SYSTEMS FAILED. THE CREW STOPPED THE ACFT ON THE TAXIWAY. REMOVED FAULTY MOTOR PN MP50B-1, SN 2728. FOUND COUPLER BETWEEN PUMP AND MOTOR WORN EXCESSIVELY. REPLACED COUPLER WITH NEW PN 6517Sep 15, 2011 · N617QS · Cessna 560XL · Landing Gear Brake SystemSDR DXTA2011091504715Metering Valve · malfunctionedEXCESSIVE GRABBING ON LT BRAKE. YOU CAN FEEL ON THE PEDALS AND IT IS AUDIBLE. R & R BRAKE METERING VALVE IAW MM 32-44-20, RIGGED BRAKE CABLES FROM BRAKE MIXER ASSY TO METERING VALVE IAW MM 32-44-10. OPS AND TAXI CHECKED GOOD.Sep 15, 2011 · N576QS · Cessna 560XL · Landing Gear Brake SystemSDR 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 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 DXTA2011091204722Strut · dischargedRAISED LANDING GEAR AFTER TAKEOFF AND RED UNLOCK LIGHT STAYED ON. ALL GREEN INDICATORS WENT OUT. IN ADDITION THE HYD PRESSURE STAYED ON AND STAB MISCOMPARE LIGHT CAME ON. PERFORMED COMPLETE NOSE GEAR STRUT SERVICING IAW MM 12-14-00. GEAR AND STAB OPS CHECKESep 11, 2011 · N614QS · Cessna 560XL · Nose/Tail Landing Gear Strut/AxleSDR DXTA2011091204721Adc · failedCLIMBING THROUGH FL320 FOR FL340 RT SIDE IAS BEGAN CLIMBING RELATIVE TO LT SIDE AND STANDBY IAS. THIS GENERATED AN AMBER "IAS - MISCOMPARE" ANNUNCIATOR ON BOTH PFD'S. THE RT SIDE IAS CONTINUED TO CLIMB AND GENERATED AN OVERSPEED WARNING. R & R NR 2 ADC IAW Sep 11, 2011 · N603QS · Cessna 560XL · Air Data ComputerSDR DXTA2011091204719Actuator · bindingELEVATOR TRIM STUCK, BINDING AND DIFFICULT TO MOVE USING ELECTIRIC SWITCH AND MANUAL TRIM WHEEL. AT TIMES IT WAS IMPOSSIBLE TO MOVE. TROUBLESHOT & FOUND LT ELEVATOR TRIM ACTUATOR BINDING. REMOVED LT ELEVATOR ASSY & REPLACED LT ELEVATOR TRIM ACTUATOR ASSY, ASep 11, 2011 · N657QS · Cessna 560XL · Elevator Tab Control SystemSDR DXTA2011091204725Downlock Switch · inoperativeAFTER TAKEOFF, WITH THE LANDING GEAR HANDLE SELECTED UP, THE NOSE GEAR INDICATOR REMAINED ILLUMINATED (THE RED UNLOCK LIGHT WAS NOT ILLUMINATED). R & R NLG ACTUATOR DOWNLOCK SWITCH IAW MM 32-30-00. PERFORMED ACTUATOR LASH CHECK AND ACTUATOR LOCK/UNLOCK PRESSSep 9, 2011 · N668QS · Cessna 560XL · Landing Gear Position and WarningSDR DXTA2011091204726Brake Assy · malfunctionedWHEN APPLYING THE LEFT BRAKE, IT DOESN'T DO ANYTHING FOR A WHILE THEN GRABS SUDDENLY CAUSING ABRUPT TURN TO THE LEFT. PERFORMED TAXI CHECK OF BRAKES. NO DEFECTS FOUND OR NOTED. PERFORMED BRAKE BLEEDING PROCEDURE IAW AMM 32-42-00 LEAK CHECKED GOOD. SERVICED ASep 8, 2011 · N686QS · Cessna 560XL · Landing Gear Brake SystemSDR Z5FA020110905001Actuator · defectiveAT TOP OF DESCENT (FL300), AP PITCH MISTRIM ILLUMINATED FOR APPROX 5 SECONDS, THEN WENT OUT. APPROX 20 SECONDS LATER THE AUTOPILOT PITCHED ABRUPTLY NOSE DOWN, REQUIRING MANUAL CONTROL OF THE ACFT TO PREVENT A NOSE-DOWN PITCH UPSET. WITH THE AUTOPILOT DISENGAGSep 5, 2011 · N522CS · Cessna 560XL · Elevator Tab Control SystemSDR Z5FA20110902001Uplock Switch · inoperativeAFTER TAKEOFF, THE NOSE GEAR DID NOT RETRACT. RED GEAR UNSAFE ANNUNCIATOR ILLUMINATED AND WIND NOISE WAS HEARD FROM NOSE GEAR AREA. CREW FOLLOWED CHECKLIST PROCEDURES, AN EMERGENCY WAS DECLARED AND THE ACFT DIVERTED. LANDING WAS UNEVENTFUL. MX TROUBLESHOT TSep 2, 2011 · N599CS · Cessna 560XL · Landing Gear Position and WarningSDR CWQR20110901019Control Cable · frayedFRAYED ELEVATOR TRIM CABLE WAS FOUND DURING A SCHEDULED INSP. CABLE WAS FRAYED ONE THIRD OF THE CABLE'S DIAMETER. AND CABLE TENSION WAS WITHIN MM LIMITS.Sep 1, 2011 · N588QS · Cessna 560XL · Elevator Tab Control SystemSDR 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 CWQR20110901017Control Cable · frayedFRAYED ELEVATOR TRIM CABLE WAS FOUND DURING A SCHEDULED INSPECTION. CABLE WAS FRAYED A QUARTER OF THE CABLE'S DIAMETER AND TENTION WAS 2 POUNDS BELOW MM LIMITS.Sep 1, 2011 · N678QS · Cessna 560XL · Elevator Tab Control SystemSDR CWQR20110831016Control Cable · frayedDURING A SCHEDULED INSPECTION FOUND ELEVATOR TRIM CABLE FRAYED AT LEAST HALF WAY THROUGH. THIS CABLE IS A PART OF A LARGER CABLE ASSY, PN 6660003-1. THIS CABLE HAS BEEN A SUBJET OF SL, BUT THESE CABLES HAVE IN THE PAST AND CONTINUE TO FRAY PREMATURELY. A SERAug 31, 2011 · N622QS · Cessna 560XL · Elevator Tab Control SystemSDR DXTA2011082904712Apu · leaking5 MINUTES AFTER ENGINE START, GRAY SMOKE BEGAN FILLING CABIN. APU HAD BEEN RUNNING FLAWLESSLY FOR 40 MINUTES. PERFORMED VISUAL INSP OF THE APU INLET, FOUND OIL RESIDUE IN THE APU INTAKE. REMOVE EXCHANGE NOZZLE, INLET AIR DUCT, CONNECTORS, FUEL AND DRAIN LINEAug 26, 2011 · N681QS · Cessna 560XL · APU Core EngineSDR CA110830002Oil System · low pressure(CAN) DURING REPOSITIONING FLIGHT, DURING CLIMB, PILOT NOTICED LOSS OF OIL PRESSURE FOLLOWED BY ELECTRONIC ENGINE CONTROL CAUTION LIGHT, CREW REDUCED POWER TO IDLE, DECLARED AN EMERGENCY AND DIVERTED THE FLIGHT WHERE AN UNEVENFUL EMERGENCY LANDING WAS PERFORMEAug 24, 2011 · Cessna 560XL · Engine (Turbine/Turboprop)SDR Z5FA20110824001Oil System · leakingRT ENGINE LOW OIL PRESSURE LIGHT ON DURING CRUISE. DIVERTED AFTER DECLARING EMERGENCY. CREW FOLLOWED EMERGENCY CHECK LIST AND LANDED WITHOUT INCIDENT. RT ENGINE IS BEING REPLACED. ENGINE WAS REPLACED DUE TO OIL FOUND BEHIND FAN SPINNER AND IN ENGINE COMPRAug 24, 2011 · N546CS · Cessna 560XL · Turbine Engine Oil SystemSDR Z5FA082411N546CS1Oil System · low pressureRT ENGINE LOW OIL PRESSURE LIGHT ON DURING CRUISE. DIVERTED AFTER DECLARING EMERGENCY. CREW FOLLOWED EMERGENCY CHECK LIST AND LANDED WITHOUT INCIDENT. RIGHT ENGINE IS BEING REPLACED. OPENAug 24, 2011 · N546CS · Cessna 560XL · Engine Oil Indicating System
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