Textron 560XL

Service difficulty reports · 3,810

Newest first. General aviation reporting is voluntary.

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 CA150817004Oil System · leaking(CAN) THE LEFT ENGINE OVER TEMPED CLIMBING OUT OF 400-500 FEET AFTER TAKEOFF. THE PILOT SAW 744 DEGREES BUT WAS NOT SURE IF THIS WAS THE MAX TEMP REACHED OR HOW LONG IT STAYED THERE. THE PILOT REDUCED POWER TO CRUISE AND TEMP WENT TO NORMAL RANGE. THE LEFT ENGAug 4, 2015 · Cessna 560XL · Turbine Engine Oil SystemSDR CA150730011Engine · overtemp(CAN) DURING FLIGHT FOLLOWING MOMENTARY REDLINE HIGH OIL PRESSURE ALONG WITH HIGH ITT AND OIL TEMPERATURE DURING TAKEOFF. INDICATIONS REMAINED IN GREEN BAND FOR REST OF FLIGHT TO DIVERSION AIRPORT. ENGINE WAS NOT SHUTDOWN. NO EMERGENCY WAS DECLARED.Jul 27, 2015 · Cessna 560XL · Engine (Turbine/Turboprop)SDR CA150730008Seal · leaking(CAN) DURING FLIGHT THE LOW OIL PRESSURE WARNING LIGHT CAME ON, OIL PRESSURE WENT DOWN TO 42 PSI. THE CREW ELECTED TO SHUT DOWN THE ENGINE AND DIVERTED THE FLIGHT WHERE AN UNEVENTFUL SINGLE ENGINE LANDING WAS MADE. TROUBLESHOOTING REVEALED AN OIL LEVEL BELOW TJul 26, 2015 · Cessna 560XL · Turbine Engine Oil SystemSDR CA150730005Engine · failed(CAN) AFTER TAKEOFF AT ABOUT 2500 FT, THE RIGHT ENGINE OIL PRESSURE DROPPED TO 0. RT LOW OIL PRESSURE WARNING ILLUMINATED. THE CREW REDUCED THE POWER ON THIS ENGINE TO IDLE AND RETURNED TO POINT OF DEPARTURE. THERE WAS A SMALL AMOUNT OF SMOKE THAT DID ENTER Jul 26, 2015 · Cessna 560XL · Engine (Turbine/Turboprop)SDR O2GA2015080550901Gearshaft · defectiveAT CRUISE ALTITUDE 40,000 RT ENG OIL PRESS WAS AT 102. TEN MINUTES LATER IT DROPPED TO 42, FOLLOWED BY MASTER CAUTION WARNING. DECLARED AN EMER & SHUTDOWN ENG ON ROLLOUT. R & R THE RT ENG HYD PUMP, GEAR SHAFT & GARLOCK SEAL. ENG RUNS WERE PERFORMED, LEAK &Jul 26, 2015 · N509UP · Cessna 560XL · Turbine Engine Accessory DriveSDR DXTA2015072706051Engine · failedAFTER DEPARTURE AT APPROX 2500' MSL RT LOW OIL PRESSURE WARNING ILLUMINATED, FOLLOWED IMMEDIATELY BY A ODOR OF SMOKE. RT OIL PRESSURE GAUGE INDICATION WAS ZERO. EMERGENCY RETURN WAS CONDUCTED WITH RT ENGINE AT IDLE POWER. REMOVED THE RT ENGINE DUE TO LOSS OJul 25, 2015 · N669QS · Cessna 560XL · Engine (Turbine/Turboprop)SDR DXTA2015072706048Pressure Switch · inoperativeWHILE TAXIING IN, AFTER LANDING THE, LO BRAKE PRESSURE & ANTI-SKID INOPERATIVE, ANNUNCIATION ILLUMINATED WITH THE MASTER CAUTION LIGHT. LOST ALL NORMAL BRAKING & STOPPED THE PLANE USING THE EMERGENCY BRAKING SYS. NO CIRCUIT BREAKERS HAD TRIPPED. TROUBLESHOTJul 24, 2015 · N664QS · Cessna 560XL · Landing Gear Brake SystemSDR ZESA2015072700003Switch · not seatedSHORTLY AFTER TAKEOFF, THE MAIN CABIN DOOR UNLOCK LIGHT CAME ON, CHECKLIST WAS FOLLOWED & THE PILOT ELECTED TO RETURN TO BLOCK. THEY LANDED WITHOUT INCIDENT. THE DOOR ALONG WITH LATCHING SYS WERE INSPECTED BY AN A & P. THE SYS WAS OPERATIONALLY CHECKED & THJul 23, 2015 · N504LV · Cessna 560XL · Door Warning SystemSDR DXTA2015072106045Unknown · smokeDURING TAXI OUT, HAD AN UNUSUAL WHINING NOISE FROM THE RT ENGINE. SHUTDOWN APU & NOISE CONTINUED. GROUND CONTROL REPORTED SMOKE COMING FROM THE RT ENGINE. SHUTDOWN ENGINES. FOUND OIL LEVELS ARE NORMAL. R & R RT GENERATOR, MOUNTING PAD & MAGNETIC GEARBOX Jul 20, 2015 · N659QS · Cessna 560XL · Engine (Turbine/Turboprop)SDR CVGA20150714003Fan · failedON ARRIVAL DESCENT TO 11,000 FT THERE WAS A NON-TYPICAL ELEC SMELL OF STRONG ODOR. SMELL WAS NEARLY GONE 15 MINUTES LATER AT TOUCHDOWN. NO VISUAL SMOKE WAS EVIDENT OR INDICATED. TROUBLESHOOTING REVEALED THE CABIN BLOWER FAN ASSEMBLY FAILED & A WIRE WAS BROKJul 14, 2015 · N926HL · Cessna 560XL · Air Distribution FanSDR W9BA20150710001Window · crackedTHE RT FORWARD SIDE WINDOW CRACKED ON THE INNER PANE DURING A FLIGHT AT 41,000 FT CAUSING THE CREW TO MAKE AN UNSCHEDULED LANDING. SPOKE WITH ACFT MFG AND THEY CONFIRMED THAT THAT THE INNER CRACKING IS UNCOMMON. UPON INSPECTION THERE WAS NO OVER VOLTAGE DAMAGJul 10, 2015 · N47HF · Cessna 560XL · Flight Compartment WindowsSDR CA150710018Engine · malfunctioned(CAN) WHILE PASSING 3000 FT, LT ENG OIL PRESS DECREASED RAPIDLY & SMOKE WAS OBSERVED IN THE COCKPIT. THE CREW USED OXYGEN MASKS & LANDED UNEVENTFULLY. NO INJURIES REPORTED. TROUBLESHOOTING IS ONGOING. MFG WILL INVESTIGATE TO ESTABLISH ROOT CAUSE & PROVIDE Jul 5, 2015 · Cessna 560XL · Engine (Turbine/Turboprop)SDR 2015FA0000309Control Cable · frayedDURING A SCHEDULED INSPECTION VISIT, THE PRIMARY FORWARD RUDDER CABLE WAS FOUND FRAYED MORE THAN 50 PERCENT THROUGH. NO STRUCTURE DAMAGE OR CHAFING INDICATION WAS FOUND AND THE ROUTING WAS CORRECT. THE CABLE DAMAGE WAS IN AN AREA THAT WAS OPEN AND CLEAR OF AJul 1, 2015 · N413SK · Cessna 560XL · Rudder Control SystemSDR DXTA2015070206038Unknown · malfunctionedWHILE USING BRAKES AT ANY TIME, BRAKES THUMP & MOMENTARILY LOCK UP. PIN LENGTH IS GOOD & NO ANNUNCIATION WAS NOTICED. REMOVED LT & RT WHEEL ASSEMBLIES, INSPECTED RT BRAKES WITH NO DEFECTS NOTED. INSPECTED LT BRAKES WITH NO DEFECTS NOTED. CLEANED LT & RT BJul 1, 2015 · N686QS · Cessna 560XL · Landing Gear Brake SystemSDR DXTA2015062206035Light · intermittentRIGHT MLG GREEN DOWN & LOCKED LIGHT INTERMITTENT. RAN CHECKLISTS, GEAR WAS BLOWN DOWN HAD 3 GREEN LIGHTS ON LANDING.Jun 21, 2015 · N681QS · Cessna 560XL · Landing Gear Position and WarningSDR CA150701010Engine · unknown(CAN) DURING A TAKEOFF ROLL, AT 20 KNOT, THE ELEC ENG CONTROL ON THE LT ENG WAS ILLUMINATED & THERE WAS A SLIGHT THRUST DISSYMMETRY. THE CREW DECIDED TO ABORT THE TAKEOFF & RETURNED TO BASE UNEVENTFULLY. TROUBLESHOOTING ONGOING. MFG WILL INVESTIGATE TO ESTAJun 19, 2015 · Cessna 560XL · Engine (Turbine/Turboprop)SDR CA150701007Engine · malfunctioned(CAN) ON DECENT, NR 2 ENG CONTROL FAULT APPEARED FOLLOWED BY A VIBRATION & TLA REDUCTION BY THE PILOT. NO RESPONSE IN MANUAL MODE. THE ENG WAS SHUT DOWN BY CREW & THEY DIVERTED. AWAITING FEEDBACK FROM THE OPERATOR. MFG WILL INVESTIGATE TO ESTABLISH ROOT CAJun 18, 2015 · Cessna 560XL · Engine (Turbine/Turboprop)SDR 9JLA2015121114958Adapter · brokenDURING PREFLIGHT CHECKS THE CREW ATTEMPTED TO START THE APU, BUT THEY REPORTED THAT IT FAILED TO START. TROUBLESHOOTING DETERMINED THAT THE STARTER & GENERATOR DRIVE ADAPTER WAS BROKEN, PN 3861055-1. OPERATIONS CHECKED OK.Jun 6, 2015 · N868J · Cessna 560XL · Starter-GeneratorSDR DXTA2015060506024Apu · leakingDURING PREFLIGHT, WITH APU BLEED RUNNING, CABIN FILLED WITH BLUE SMOKE. FIRST OFFICER INDICATED CABIN WAS VERY HOT EVEN THOUGH TEMP SETTING WAS VERY LOW. REMOVED DEFECTIVE APU & REPLACED WITH REPAIRED APU. CLEANED APU CONTAINMENT BOX & FLUSHED DRAIN LINES. Jun 4, 2015 · N622QS · Cessna 560XL · APU Core EngineSDR DXTA2015052906023Transducer · failedDURING TAXIING IN, USING LEFT BRAKE PRESSURE TO TURN LEFT, PEDAL PRESSURE WAS FELT, BUT NO BRAKE ACTION OCCURRED. WITHOUT WARNING, FULL BRAKE ACTION OCCURRED & ACFT LEFT BRAKE WAS FULLY EFFECTIVE WITH SEVERE JERKING ACTION. LEFT BRAKE PEDAL PRESS WAS CONSTAMay 28, 2015 · N604QS · Cessna 560XL · Brake Anti-Skid SectionSDR 17GR2015FA0000232Striker · bindingINTERMITTENT DOOR UNLOCK LIGHT. OPENING AND CLOSING THE DOOR MULTIPLE TIMES WOULD RESULT IN A LOCKED INDICATION. UN-LOCK LIGHT ON PILOTS PANEL OFF. DISCOVERED THAT THE STRIKER PLATE FOR THE DOOR PROXIMITY LOCK SWITCH WAS CONTACTING THE COVER HOLDING THE SWITMay 26, 2015 · N851AC · Cessna 560XL · Door Warning SystemSDR DXTA2015051906020Coalescer Bag · odorMILDEW SMELL AT FLIGHT LEVEL 410. R & R WATER SEPARATOR CONDENSER SOCK IAW AMM 21-51-00. OPS & LEAK CHECKED GOOD.May 18, 2015 · N696QS · Cessna 560XL · Humidity Control SystemSDR DXTA2015051806019Trim System · jammedDESCENDING THROUGH APPROXIMATELY FL 340 GOT PITCH TRIM ANNUNCIATOR. DISENGAGED AUTOPILOT & REALIZED IT WAS A JAMMED ELEVATOR TRIM. RAN CHECKLIST WHILE MAKING DECENT TO LOWER & WARMER ALTITUDE. AFTER LEVEL AT 4000 FEET FOR APPROX FIVE MINUTES ELEVATOR TRIM UMay 15, 2015 · N642QS · Cessna 560XL · Elevator Tab Control SystemSDR DXTA2015051506018Brake Sys · contaminatedWHEN DOING STATIC TAKEOFF AROUND 88% N1 WITH FULL APPLICATION OF BRAKES, ACFT MOVES FWD. PERFORMED BRAKE SYS BLEED IAW MM 32-44-00. PERFORMED ACFT POWER RUN, OBSERVER OUTSIDE OF ACFT. NOTED THAT TIRES WERE NOT ROLLING BUT SLIDING.May 14, 2015 · N619QS · Cessna 560XL · Landing Gear Brake SystemSDR DXTA2015051306016Control Cable · out of adjustIN STRAIGHT & LEVEL FLIGHT RUDDER TRIM REQUIRES 1/2 DEFLECTION TRIM TO LT. WITH FLAPS 35 & APPROACH AIRSPEED 3/4 DEFLECTION TO LT IS REQUIRED, REMOVED THE STINGER & INSTALLED BOTH THE RUDDER PEDAL BLOCKS & THE AFT SECTOR RIG PIN, WITH BOTH INSTALLED THE RUDDMay 12, 2015 · N681QS · Cessna 560XL · Rudder Control SystemSDR DXTA2015051306017Unknown · unknownIN STRAIGHT & LEVEL FLIGHT RUDDER TRIM REQUIRES 1/2 DEFLECTION TRIM TO LT. WITH FLAPS 35 & APPROACH AIRSPEED 3/4 DEFLECTION TO LT IS REQUIRED.May 12, 2015 · N681QS · Cessna 560XL · Rudder Control SystemSDR CA150525006Engine · overtemp(CAN) DURING TAKEOFF ROLL, ENGINE TEMPERATURE WENT TO RED AREA INDICATION, APPROX. 720 DEGREES C. THIS LASTED FOR 5-8 SECONDS UNTIL CREW REDUCED POWER AT 400 FT CREW ELECTED TO DIVERT TO ALTERNATE AIRPORT AND PERFORMED AND UNEVENTFUL LANDING.May 7, 2015 · Cessna 560XL · Engine (Turbine/Turboprop)SDR CA150603001Oil System · low pressure(CAN) REPORTED LOSS OF OIL PRESSURE INDICATION AT TAKEOFF POWER SETTING FOR ABOUT 1 MINUTE. WHEN THE PILOT MOVED THE TLA TO TAKE OFF POWER SETTING, THE OIL PRESSURE INDICATION CAME BACK. PILOT ELECTED TO PERFORM A TURN AROUND AND LANDED AT POINT OF ORIGIN WIMay 6, 2015 · Cessna 560XL · Engine Oil Indicating SystemSDR DXTA2015050806015Yoke · vibrationAFTER TAKEOFF, FIRST OFFICER FELT BINDING IN THE CONTROL YOKE & COULD FEEL IT IN HIS FEET. PASSING 230 KTS, BOTH YOKES VIBRATED & FELT IN THE COCKPIT. MOVED FLT CONTROLS, ELEVATOR & RUDDER CONTROL CABLE DAMPENER PULLEYS , RUN BLOCK WORN & GROOVED. INSPECTEDMay 6, 2015 · N606QS · Cessna 560XL · Control Column SectionSDR CA150519013Wire Harness · defective(CAN) AT FL410, IN CRUISE FLIGHT, THE CREW REPORTED AN ENG TEMP OSCILLATION. THE CREW ELECTED TO DIVERT & PERFORMED AN UNEVENTFUL LANDING. THE TROUBLESHOOTING REVEALED A DEFECTIVE T1 HARNESS. THE PART WAS ORDERED. MFG WILL INVESTIGATE TO ESTABLISH ROOT CAUMay 3, 2015 · Cessna 560XL · Engine Indicating System WiringSDR CA150519004Engine · leaking(CAN) THE CREW REPORTED A LOSS OF OIL PRESS WITH ACFT ALARM & OIL SMELL IN COCKPIT. THEY SHUT DOWN THE ENG. AFTER LANDING THEY ADDED ONE CAN & A HALF OF ENG OIL. FLEW FOR 40 MINUTES WITHOUT ANY ISSUE. AN ENG OIL CONSUMPTION CHECK WILL BE PERFORMED. MFG WIApr 28, 2015 · Cessna 560XL · Turbine Engine Oil SystemSDR DXTA2015042906013Acm · seizedWHILE SITTING ON THE RAMP WAITING FOR A PAX WITH THE APU RUNNING & BLEED AIR ON, SMOKE BEGAN FILLING THE CABIN. REMOVED THE ACM FROM THE AIRCRAFT. PERFORMED A TORQUE CHECK OF THE TURBINE. FOUND THE TURBINE SEIZED IN PLACE, FAILING THE TORQUE CHECK. REMOVED AApr 28, 2015 · N607QS · Cessna 560XL · Cabin Cooling SystemSDR DXTA2015042906012Engine · contaminatedAFTER ENGINE SHUTDOWN FOLLOWING A SHORT REPOSITION TAXI, THE LT ENGINE HAD THICK WHITE SMOKE BILLOWING FROM THE EXHAUST AREA. SMOKE CONTINUED FOR 10 MINUTES FOLLOWING SHUTDOWN. SMOKE HAD ODOR OF BURNING OIL OR HYD FLUID. A FRESH ACCUMULATION OF LEAKED FLUIDApr 28, 2015 · N579QS · Cessna 560XL · Engine (Turbine/Turboprop)SDR DXTA2015042706011Bulb · inoperativeWHEN LANDING, LEFT MAIN GEAR DIDN'T HAVE GREEN LIGHT. PERFORMED EMERGENCY GEAR EXTENSION. FOUND THE LT GEAR DOWN & LOCK LIGHT BULBS INOPERATIVE. REMOVED THE FAILED INDICATOR BULBS & INSTALLED NEW BULBS. JACKED ACFT & CYCLED THE GEAR SEVERAL TIMES WITH NO FApr 26, 2015 · N587QS · Cessna 560XL · Landing Gear Position and WarningSDR JGVR201504022001Structure · corrodedDURING A INSPECTION OF THE TUBE ASSOCIATED WITH THE AILERON SECTOR. THE SECTOR WAS REMOVED TO FACILITATE CLEANING THE MINOR SURFACE CORROSION. IT WAS THEN DISCOVERED THAT THE UPPER SECTOR PORTION WAS SEVERELY CORRODED TO THE EXTENT OF STARTING TO SEPARATE. Apr 22, 2015 · N770CK · Cessna 560XL · AileronsSDR CA150518010Engine · power loss(CAN) EEC REVERSION, TWO EVENTS REPORTED, THE FIRST EVENT WAS ON APRIL 21 & SECOND EVENT ON APR 25. THE SAME CRM CASE WAS USED. ON A COMMERCIAL FLIGHT WITH 2 CREW ON BOARD & PAXS, DURING CLIMB AT FL115, PILOT NOTICED ENG CONTROL FAULTS LIGHT & ENG ROLLED BACApr 21, 2015 · Cessna 560XL · Engine (Turbine/Turboprop)SDR 2015F00052Window · failedDURING CRUISE AT FL260 THE LT FWD SIDE WINDOW OUTER PANE SHATTERED. THE CREW DESCENDED TO A LOWER ALTITUDE AND BEGAN THEIR DECENT. THEY DID NOT DECLARE AN EMERGENCY AND LANDED WITH OUT INCIDENT. THE AIRCRAFT IS CURRENTLY OUT OF SERVICE WHERE THE WINDOW IS BEIApr 19, 2015 · N227MC · Cessna 560XL · Flight Compartment WindowsSDR CA150511006Oil System · low pressure(CAN) DURING DEPARTURE THE RT ENG OIL PRESS DROPPED TO 0 PSI. THE LOW OIL PRESS RT ANNUNCIATOR & THE MASTER WARNING ILLUMINATED. THE CREW SHUTDOWN THE ENG, DECLARED AN EMER, & RETURNED TO POINT OF DEPARTURE. AN UNEVENTFUL LANDING WAS MADE.Apr 18, 2015 · Cessna 560XL · Engine Oil Indicating SystemSDR DXTA2015042006010Apu · smokeSMOKE IN THE COCKPIT. APU WAS STARTED ABOUT FIVE MINUTES PRIOR TO LANDING & WAS OPERATING NORMALLY. UPON LANDING & TAXI IN APU QUIT DURING ENG SHUTDOWN. WE THOUGHT WE HAD BUMPED A SWITCH. AFTER THE PAXS DEPARTED ABOUT FIVE MINUTES WE TESTED, GOOD TEST & REApr 18, 2015 · N662QS · Cessna 560XL · Airborne Auxiliary Power Unit (APU) SystemSDR DXTA2015042006009Engine · unserviceableAFTER A NORMAL TAKEOFF LEVELED OFF AT 8000 FT AND THE RT ENGINE OIL PRESS LIGHT ILLUMINATED WITH A MASTER WARNING. THE RT ENGINE OIL PRESS GAUGE SHOWED ZERO. ACCOMPLISHED THE ENGINE SECURING CHECKLIST. DECLARED AN EMERGENCY AND RETURNED TO THE DEPARTURE AIRPORApr 17, 2015 · N633QS · Cessna 560XL · Engine (Turbine/Turboprop)SDR DXTR2015042302Flex Hose · damagedCOPILOTS LT BRAKE MASTER CYLINDER HOSE DAMAGED FROM RUDDER TORQUE TUBE BRIDGE CONTACT. INSTALLED NEW BRAKE LINE IAW MM 32-42-02.Apr 16, 2015 · N640QS · Cessna 560XL · Hydraulic System, MainSDR DXTR2015042301Line · chafedLEFT BRAKE LINE IN COCKPIT ON FWD PRESSURE BULKHEAD FWD OF COPILOT'S RT RUDDER PEDAL CHAFED. INSTALLED NEW BRAKE LINE, PN 6617118-1 AT ORIGINAL LOCATION IN CONJUNCTION WITH SB560XL-27-33, SQ. 274 AND IAW MM CHAP. 20-00-00.Apr 16, 2015 · N640QS · Cessna 560XL · Hydraulic System, MainSDR IGXR201504150001Static System · leakingDURING RVSM RE-CERTIFICATION TESTS ON MULTIPLE MFG AIRFRAMES, EXCESSIVE INSTRUMENT STATIC SYSTEM LEAKAGE HAS BEEN TRACED TO LOOSE 90 DEGREE FITTINGS ATTACHED TO THE LOWER FUSELAGE STATIC SYSTEM MOISTURE DRAINS. TESTING HAS SHOWN THAT THE O-RING ON THE DRAIN BOApr 15, 2015 · Cessna 560XL · Pitot/Static SystemSDR 2015FA0000146Bulb · failedLT LANDING LIGHT, RECOGNITION LIGHT LENS CRACKING IN FRONT OF 150 WATT TAXI BULB. WE HAD A LENS CRACK AND REPLACED IT LEAVING THE BULBS IN PLACE AS THEY WERE WORKING. REPLACED THE LENS AGAIN AFTER 10 HOURS. CONTACTED MFG`S AND NEITHER WERE AWARE OF ANY PROBLApr 15, 2015 · N851AC · Cessna 560XL · Exterior LightingSDR 2015F00058Apu · smokeCOCKPIT FILLED WITH SMOKE ON UPWIND CLIMB - NOTED THAT THE APU OIL QUANTITY WAS LOW. SERVICED APU OIL TO FULL, PERFORMED GROUND POWER RUNS WITH ACM (PACK)- ON, INSPECT WATER SEPARATOR SOCK FOR OIL CONTAMINATION. PERFORMED APU / ENGINE GROUND RUNS UTILIZING DIApr 14, 2015 · N47HF · Cessna 560XL · APU Oil SystemSDR CA150507001Oil System · low pressure(CAN ON DEPARTURE THE RT ENGINE OIL PRESSURE DROPPED TO ZERO & LOW OIL PRESS ANNUNCIATOR ILLUMINATED. THIS WAS FOLLOWED BY SMOKE IN THE CABIN SO THE CREW DONNED O2 MASKS & DROPPED THE PAXS MASKS. AN EMER WAS DECLARED & THE CREW MADE AN IMMEDIATE RETURN TO THApr 12, 2015 · Cessna 560XL · Engine Oil Indicating SystemSDR DXTA2015041306004Engine · failedRIGHT ENGINE LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED WITH THE MASTER WARNING LIGHT CLIMBING THROUGH ABOUT 3000 FT. THE OIL PRESSURE GAUGE INDICATED BELOW 20 PSI & WAS RED. FELT A SUDDEN CHANGE IN THRUST ON THE RT ENGINE. POWER WAS REDUCED ON BOTH ENGINES TApr 11, 2015 · N568QS · Cessna 560XL · Engine (Turbine/Turboprop)SDR DXTA2015041306005Unknown · smokeSMOKE WAS NOTICED IN THE CABIN & COCKPIT. ONCE THE POWER WAS REDUCED THE SMOKE SEEMED TO DISSIPATE.Apr 11, 2015 · N568QS · Cessna 560XL · Air Distribution SystemSDR DXTR2015041402Spar Web · chafedLIGHT CHAFING FOUND ON FWD SIDE OF VERTICAL STAB SPAR UNDER PIVOT FITTING CLIP. REPAIRED IAW REPAIR DEFINITION S-560XL-5240/05RD AND SRM 51-70-08.Apr 10, 2015 · N640QS · Cessna 560XL · Vertical Stabilizer, Spar/RibSDR DXTA201504136003Brake Sys · failedTHE LT BRAKE FAILED ON TAXI OUT. BRAKE PEDAL WAS FIRM BUT BRAKE WAS STILL INOPERATIVE. BRAKE RESERVOIR IS FULL & ALL BRAKE ACCUMULATORS ARE IN LIMITS. ALSO THERE WERE NO BRAKE SYS BITE INDICATORS SHOWING FLAGGED. INSPECTED LT BRAKE ASSEMBLY & BRAKE WEAR PApr 10, 2015 · N604QS · Cessna 560XL · Landing Gear Brake System
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