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 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 DXTA200702172Control Unit · inoperativeON TAKE OFF ROLL, THE RT WINDSHIELD FAULT ANNUNCIATOR ILLUMINATED. REMOVED AND REPLACED POWER CONTROL UNIT ON RT ENG, OPS CHECK GOOD IAW CE 560XL M/M CH 24-20-01.May 2, 2007 · N650QS · Cessna 560XL · Windshield/Door Rain/Ice RemovalSDR DXTA200702171Unknown · unknownAT FL190 AND 190KIAS, A SUDDEN LOUD, LOW 'THUD' WAS HEARD AND FELT. 3 SECONDS LATER IT WAS HEARD AGAIN. PASSENGER THOUGHT IT CAME FROM BENEATH HIM AT CABIN SEAT POSITION 5/6. NOISE/THUD WAS FELT AND HEARD THROUGH ENTIRE AIRFRAME. PERFORMED VISUAL INSPECTIOMay 2, 2007 · N625QS · Cessna 560XL · Aircraft StructuresSDR DXTA200702170Connector · corrodedDURING TAKEOFF ROLL, ABORTED TAKEOFF (BELOW 70KTS) DUE TO ILLUMINATION OF NO TAKEOFF ANNUNCIATOR AND NO TAKEOFF HORN. TROUBLESHOT SYSTEMS. FOUND EXCESSIVE MOISTURE AND CORROSION IN THE LT SPEEDBRAKE DISCONNECT PLUG PL001. REPLACED PINS, SOCKETS AND PLUG BACMay 2, 2007 · N681QS · Cessna 560XL · Flight Control System WiringSDR 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 DXTA200702161Unknown · malfunctionedDURING START BRAKE LOW PRESS AND ANTI SKID INOP LIGHT CAME ON. IT WENT OUT AS RPM INCREASED, CAME ON AGAIN AS TAXI STARTED. BRAKE PRESS REMAINED OK. EMER BRAKE NOT USED. [SUP 05-03-07] REMOVED BRAKE LOW PRESSURE SWITCH AND INSTALLED NEW UNIT IAW CESSNAApr 29, 2007 · N686QS · Cessna 560XL · Landing Gear Brake 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 DXTA200702154Unknown · malfunctionedPILOTS AUTO PILOT TRIM DISCONNECT BUTTON POPPED OUT OF YOKE IN FLIGHT. [SUP 05-03-07] SECURED PILOT A/P TRIM DISCONNECT SWITCH PER STANDARD PRACTICE.Apr 27, 2007 · N600QS · Cessna 560XL · Stabilizer Position IndicatingSDR DXTA200702147Indication Sys · malfunctionedGREEN LT GEAR POSITION INDICATOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION ON TAKEOFF. [SUP 05-02-07] INSTALLED MLG CONTROLLER (REPAIRED) AND INSPECTED ACTUATOR ON LT MAIN GEAR.CYCLED GEAR SEVERAL TIMES,NO FAULTS FOUND.SEE CJI W/O 026717 FOR DETAILS Apr 26, 2007 · N689QS · Cessna 560XL · Landing Gear Position and WarningSDR 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 DXTA200702126Access Panel · misinstalledIN FLIGHT ABOVE 200 KTS THERE IS A RUMBLING VIBRATION THAT VIBRATES THE WHOLE AIRPLANE. IT CHANGES PITCH OR SEVERITY WITH INCREASE IN SPEED, 250 KTS IS THE SPEED THAT IT IS MOST PRONOUNCED. FOUND ACCESS PANEL ON LOWER LT STUB WING NR 313AL TO BE OVERLAPPING Apr 21, 2007 · N693QS · Cessna 560XL · Wing, Plate/SkinSDR 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 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 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 DXTA200702105Indication Sys · malfunctionedNO (GREEN) LIGHT ON RT MAIN LANDING GEAR UPON EXTENSION. EMERGENCY PROCEDURES FOLLOWED AND BOTTLE WAS BLOWN, STILL NO GREEN LIGHT.Apr 12, 2007 · N634QS · Cessna 560XL · Landing Gear Position and WarningSDR 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 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 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 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 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 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 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 DXTA200702065Unknown · chatteringUPON RELEASING BRAKES FOR TAKEOFF AT SJC, (4) LOUD KNOCKS IN RAPID SUCCESSION WERE HEARD FROM REAR OF AIRCRAFT. ABORTED TAKEOFF AND RETURNEDTO RAMP. INSPECTED BRAKES & ENGINES & FOUND NO DEFECTS. TAXI CHECK & PERFORMED ENGINE RUN UP TO TAKE OFF POWER SEVERAL Apr 1, 2007 · N686QS · Cessna 560XL · Landing Gear Brake 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 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 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 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 SystemSDR 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 DXTA200701978Panel · departedACCESS PANEL JUST AFT OF LT LANDING LIGHT IN JUST IN FRONT OF WING CAME OFF DURING FLIGHT. INSTALLED ACCESS PANEL UNDER LT WING IAW CE560XL MM CHP 53-30-00Feb 28, 2007 · N639QS · Cessna 560XL · Fuselage Main, Plate/SkinSDR DXTA200701971Cable · out of adjustGEAR 'UNLOCK' LIGHT ILLUMINATED AFTER GEAR RETRACTION. CYCLED GEAR TWICE WITH SAME RESULT. HYD SYSTEM REMAINED PRESSURIZED UNTIL GEAR SELECTED DOWN. ADJUSTED & CHECKED FREE FALL CABLE IAW CESSNA 560XL M/M CHPT 32-30-08Feb 27, 2007 · N694QS · Cessna 560XL · Landing Gear Position and WarningSDR DXTA200701969Master Cylinder · bypassingCAPTAINS LT BRAKE IS VERY SPONGY BUT WILL CATCH AFTER ALMOST FULL DEPRESSION. REMOVED AND REPLACED PILOT'S LT AND RT BRAKE MASTER CYLINDERS AND BLED SYSTEM IAW MM 32-42, OPS AND LEAK CHECK GOOD. PERFORMED TAXI CHECK, NO DEFECTS FOUND.Feb 27, 2007 · N639QS · Cessna 560XL · Master Cylinder/Brake ValveSDR DXTA200701972Master Cylinder · malfunctionedLT SEAT RT BRAKE PEDAL IS SOFT REALITIVE TO LT BRAKE PRESSURE WHEN BRAKES ARE APPLIED. REMOVED AND REPLACED CAPTAINS RT MASTER CYLINDER IAW MM 32-42. BLEED OPS AND LEAK CHECK GOOD.Feb 26, 2007 · N628QS · Cessna 560XL · Master Cylinder/Brake ValveSDR DXTA200701959Anti-Skid Sys · malfunctionedDURING TAXI CAPTAINS RIGHT BRAKE PEDAL BECOMES VERY "SPONGY". PERFORMED ANTI-SKID BRAKE BLEEDING PROCEDURE IAW CESSNA 560XL MM 32-42-00. OPS AND LEAK CHECK GOOD.Feb 20, 2007 · N628QS · Cessna 560XL · Brake Anti-Skid SectionSDR DXTA200701953Windshield · failedCAPT`S WINDSHIELD SHATTERED.Feb 17, 2007 · N624QS · Cessna 560XL · Flight Compartment WindowsSDR 021607N511CS1Switch · failedON APPROACH INTO BTV THE RT MLG LIGHT DID NOT ILLUMINATE FOLLOWED BY THE RED GEAR UNSAFE INDICATION. THE CREW FOLLOWED THEIR CHECKLIST THE EMERGENCY GEAR/BRAKE BOTTLE WAS USED AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE TROUBLEFeb 16, 2007 · N511CS · Cessna 560XL · Landing Gear ActuatorSDR DXTA200701929Indicator · out of adjustRECEIVED A NO TAKEOFF MESSAGE AROUND 40KTS, ABORTED TAKEOFF. FOUND ELEVATOR TRIM INDICATOR STRIP AND PROX SWITCH FOR NO TAKEOFF SYSTEM OUT OF ADJUSTMENT. ADJUSTED ELEVATOR TRIM STRIP INDICATOR AND PROX SWITCH IAW CH 27-31-00 OF THE CE 560 XL M.M. OPS CHECKSFeb 12, 2007 · N632QS · Cessna 560XL · Elevator Tab Control SystemSDR DXTA200701943Control Module · inoperativeRT WINDSCREEN FAULT ANNUNCIATOR ILLUMINATED, WHILE COMPLETING CHECKLIST, THE RIGHT WINDSHIELD SHATTERED. REMOVED CRACKED RT WINDSHIELD INSTALLED NEW WINDSHIELD. INSTALLED REPAIRED WINDSHIELD CONTROL RT PN ON 856-1-1 SN ON 205080073 RT WINDSHIELD TEMP CONTROLFeb 11, 2007 · N651QS · Cessna 560XL · Windshield/Door Rain/Ice RemovalSDR DXTA200701941Annunciator · faultyWITH GEAR SELECTED DOWN AND LOCKED (3 GREEN, NO RED) SELECTED FLAP SWITCH TO 15 AND 'HYD' PRESSURE LIGHT CAME ON FLASING WITH MASTER CAUTION FLASHING INSTANTLY WITH NO DELAY.TROUBLESHOT TO FAULTY ANNUNCIATOR PANEL. REPLACED WITH SERVICEABLE UNIT. OPERATIONAL CFeb 11, 2007 · N694QS · Cessna 560XL · Hydraulic Indicating SystemSDR DXTA200701940Engine · malfunctionedDURING ENGINE START, LT ENGINE OIL PRESSURE WOULD NOT COME OUT OF THE RED . AFTER APPROX 15 SEC ITT CLIMBED TO 680 DEG C AND THEN SHOT UP TO 800 DEG C FOR 2-3 SECS . AS SOON AS ITT WENT PAST 720 DEG START WAS ABORTED . ITT WAS NOT AT 800 DEG C FOR MORE THANFeb 11, 2007 · N601QS · Cessna 560XL · Engine (Turbine/Turboprop)SDR DXTA200701939Valve · intermittentAFTER CROSSFEEDING FROM LEFT OT RIGHT TANK , WHEN CROSSFEED SWITCH IS TURNED OFF ( CENTER ) THE RIGHT LO FUEL PRESS ANNUNCIATOR ILLUMINATES MOMENTARILY, FOLLOWED BY A STEADY R FUEL BOOST ON ANNUNCIATOR. SWITCHING THE RT BOOST PUMP SWITCH TO ON AND BACK TO NORFeb 11, 2007 · N642QS · Cessna 560XL · Aircraft Fuel Distribution System
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