Textron 560XL

Service difficulty reports · 3,810

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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 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 DXTA2009050403629Warning Light · illuminatedWHEN TAKEOFF POWER WAS APPLIED, RT WING OVERHEAT LIGHT ILLUMINATED. PERFORMED GROUND RUN AT TAKOFF POWER WITH ANTI-ICE WING/ENG IN OFF POSITION. DID NOT GET R WING OVHT ANNUNCIATOR. REMOVED RH INBOARD CUFF UPPER PANEL. NO DEFECTS FOUND INSIDE OF AREA. RAN ENGMay 4, 2009 · N610QS · Cessna 560XL · Central WarningSDR DXTA2009050403630Actuator · intermittentSTAB MISCOMPARE AND HYD PRESS LIGHT ILLUMINATED AFTER TAKEOFF. CHECKLISTS WERE RUN IAW SOP. STAB DID NOT MOVE TO CRUISE POSITION. AFTER LANDING STAB MISCOMPARE AND HYD PRESS LIGHTS ILLUMINATED AGAIN. REMOVED & REPLACED STAB ACTUATOR IAW MM 27-40-00. OPS & LEAMay 2, 2009 · N656QS · Cessna 560XL · Central WarningSDR DXTA2009043003624Pump · leakingRIGHT AFTER TOUCHDOWN, LT "LO HYD FLOW" LIGHT ILLUMINATED. ALSO RT "LO HYD FLOW" LIGHT ILLUMINATED, FOLLOWED BY "LO HYD LEVEL" & "STAB MISCOMPARE" LIGHT. ON POST FLT, FOUND HYD FLUID ON LT BACK THIRD OF ACFT. R&R LT HYD PUMP, FILTER & PRESS LINE. FLUSHED LIApr 30, 2009 · N594QS · Cessna 560XL · Hydraulic Pump (Electric/Engine), MainSDR DXTA2009042903623Tiller · activatedON THE TAKEOFF ROLL AT 70 KTS WE GOT A "NO TAKEOFF" ANNUNCIATOR WITH A MASTER CAUTION AND AURAL WARNING. FLAPS WERE AT TAKEOFF SETTING, AND THE TRIM WAS NEXT TO THE TEE. REPLACED TRIM WHEEL AND SHIMS INSTALLED ON WHEEL SPACER. SYS CK GOOD IAW MM 27-31-00.Apr 28, 2009 · N580QS · Cessna 560XL · Elevator Tab Control SystemSDR DXTA2009042703620Metering Valve · malfunctionedDURING TAXI THERE WAS A HEAVY VIBRATION HEARD AND FELT WHEN BRAKES WERE APPLIED. THE VIBRATION CAME FROM RT BRAKE ONLY. LT SIDE OK. REMOVED AND REPLACED BRAKE METERING VALVE WITH A REPAIRED UNIT. BLED BRAKES PERFORMED OPERATIONAL CHECKS, OPS CHECKS GOOD IAW MApr 24, 2009 · N686QS · Cessna 560XL · Landing Gear Brake SystemSDR DXTA2009042103611Apu · leakingAFTER APU START UP, COCKPIT AND CABIN FILLED WITH SMOKE. NOT SURE IF IT WAS ELECTRICAL OR ENVIRONMENTAL. APU BLEED AIR WAS ON. REMOVED & REPLACED APU IAW MM 49-10-00 & MM 49-10-00. OPERATION & LEAK CHECKS GOOD.Apr 20, 2009 · N670QS · Cessna 560XL · APU Core EngineSDR DXTA2009041303590Master Cylinder · malfunctionedON LANDING ROLLOUT, CAPTAINS LT BRAKE PEDAL WOULD GO ALL THE WAY TO THE FLOOR AND GRAB VERY LITTLE. REMOVED FAULTY PILOTS LEFT MASTER CYLINDER AND INSTALLED NEW MASTER CYL IAW MM 32-42-02. BLED BRAKES IAW 32-42-00. OPS CHECK GOOD. PEDALS FEEL NORMAL AT THIS TApr 12, 2009 · N639QS · Cessna 560XL · Master Cylinder/Brake ValveSDR DXTA2009041303589Strut · underservicedGEAR "UNLOCK" LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. PERFORMED INSPECTION OF GEAR. REMOVED ALL THREE NOSE GEAR DOORS. RESERVICED NOSE GEAR STRUT, AND RESAFTIED OIL FILL PLUG. LUBED UPLOCK ROLLERS. RECONNECTED NOSE GEAR DOORS. PERFORMED GEAR HYD SYApr 12, 2009 · N580QS · Cessna 560XL · Main Landing Gear Strut/Axle/TruckSDR DXTA2009041303592Windshield · crackedRT WINDSHIELD FAULT ANNUCIATOR ILLUMINATED IN FLIGHT. AFTER RESETTING WINDSHIELD HEAT SWITCH IAW CHECKLIST, THE ANNUNCIATOR CAME BACK ON AND AN APPROXIMATE 8 INCH CRACK APPEARED IN LWR CORNER OF WINDSHIELD. FOUND INNER PANE OF CO-PILOT'S WINDSHIELD SHORTED &Apr 11, 2009 · N608QS · Cessna 560XL · Flight Compartment WindowsSDR DXTA2009041303597Warning System · malfunctionedRT ENGINE ANTI-ICE ANNUNCIATOR AND MASTER CAUTION COMES ON WITH THE ENGINE/WING ANTI-ICE SWITCH IN THE OFF POSITION. REMOVED AND REPLACED R/H ENGINE STATOR VALVE. OP/LEAK CHECKS GOOD. IAW CE560XL MM CH 21-30-00Apr 9, 2009 · N626QS · Cessna 560XL · Air Intake Anti/De-Ice SystemSDR Z5FA040809N577CS1Pressure Switch · failedUPON LANDING, APPLIED BRAKES AND HAD A LOW BRAKE PRESS AND ANTI SKID INOP WITH REDUCED BRAKING CAPABILITY. CAUTION LIGHTS ILLUMINATE WITH EACH BRAKE APPLICATION. REMOVED FAILED BRAKE SYS LOW PRESSURE SWITCH, INSTALLED REPAIRED SWITCH. BLED THE BRAKE SYS, OPApr 8, 2009 · N577CS · Cessna 560XL · Brake Anti-Skid SectionSDR DXTA2009040603579Uplock Switch · illuminatedAFTER TAKEOFF, GEAR WAS RETRACTED AND UNLOCK LIGHT WOULD NOT GO OUT. CYCLED GEAR AND LIGHT REMAINED ON HYD PRESS LIGHT WAS NOT ON. HYD PRESS LIGHT WAS NOT ON. FOUND RT GEAR UPLOCK SWITCH OUT OF ADJUSTMENT. C/W RIGGING OF SWITCH IAW MM 32-61-00. OPS CHECKS GApr 4, 2009 · N626QS · Cessna 560XL · Landing Gear Position and WarningSDR DXTA2009040303576Downlock Switch · out of adjustDURING GEAR RETRACTION, RED GEAR "UNLOCK" LIGHT (ANNUNCIATOR) REMAINED ILLUMINATED ACCOMPANIED BY AMBER "HYD PRES" ANNUNCIATOR. NO GREEN GREEN GEAR ANNUNCIATION DURING RETRACTION. FOUND NOSE GEAR UPLOCK SWITCH OUT OF ADJUSTMENT. ADJUSTED UPLOCK SWITCH IAW MMApr 2, 2009 · N670QS · Cessna 560XL · Landing Gear Position and WarningSDR DXTA2009040803587Brake Sys · malfunctionedDURING BRAKE APPLICATION OF 20-40 PERCENT OF MAXIMUM, SYMMETRIC BRAKE APPLICATION CAUSES THE ACFT TO YAW TO THE LT. CONDITION OCCURS FROM BOTH LT AND RT PILOT SEATS. INSPECTED BRAKES, NO DEFECTS NOTED. BLEED BRAKE SYSTEM AND PERFORMED TAXI CHECK. APPLIED BRAApr 1, 2009 · N576QS · Cessna 560XL · Landing Gear Brake SystemSDR DXTA2009032703573Shimmy Dampener · malfunctionedON TAKEOFF ROLL AT JUST PRIOR TO 40 KTS THE NOSE WHEEL STARTS A VERY EXCESSIVE VIBRATION. FOUND SHIMMY DAMPER LEAKING FLUID, NO FLUID LEFT. REMOVED AND REPLACED SHIMMY DAMPER WITH O/H UNIT IAW MM, CONFIRMED PROPER SERVICING OF INSTALLED SHIMMY DAMPER.Mar 31, 2009 · N689QS · Cessna 560XL · Wheel/Ski/FloatSDR DXTA2009033003571Indicator · unknownAT BEGINNING OF TAKEOFF ROLL THE RT FUEL QUANTITY INDICATOR DROPPED TO ZERO AND THE RT FUEL GAUGE ANNUNCIATOR AND MASTER CAUTION ILLUMINATED. STARTED APU AND WAITED 15 MIN. CHECKED SIGNAL CONDITIONER LED'S NO FAULTS DISPLAYED. STARTED ENGINES & TAXIED ACFT.Mar 29, 2009 · N627QS · Cessna 560XL · Fuel Indicating SystemSDR DXTA2009033003570Switch · inoperativeON CLIMBOUT AT ABOUT 20,000 FT, WE GOT AN ACM OVERHEAT ANNUNCIATOR FOLLOWED BY A RISE IN CABIN ALTITUDE. WE COMPLETED APPROPRIATE CHECKLISTS AND RETURNED TO DEPARTURE. REMOVED OLD OVER TEMP SWITCH, INSTALLED NEW SWITCH. LEAK AND OPS CHECK GOOD. WORK DONE Mar 27, 2009 · N658QS · Cessna 560XL · Cabin Cooling SystemSDR DXTA2009032703568Switch · looseUPON APPLYING T/O POWER THE LT ENGINE TR HAD AN UNCOMMANDED DEPLOYMENT, THIS HAPPEN MULTIPLE TIMES. EACH TIME WE USED EMER STOW. DID NOT BEGIN TAKEOFF ROLL. TROUBLESHOT SYS AND FOUND THE STOW AND DEPLOY SWITCHES LOOSE IN THE PEDESTAL. TIGHTENED AND ADJUSTED Mar 26, 2009 · N687QS · Cessna 560XL · Engine Thrust ReverserSDR DXTA2009032703565Angle · bentON TAKEOFF ROLL, THE RUDDER PEDALS FELT VERY STIFF. AFTER TAKEOFF WITH THE YAW DAMPER OFF, IT WAS VERY DIFFICULT TO DEPRESS THE RT RUDDER. ON FINAL APPROACH WITH THE YAW DAMPER OFF, THE RUDDER PEDALS FELT LIKE THEY WERE RUBBING SOMETHING WHEN DEPRESSED. FOUNDMar 26, 2009 · N600QS · Cessna 560XL · Rudder Control SystemSDR DXTA2009032503562Uplock Switch · out of adjustAFTER T/O, RECEIVED A GEAR UNSAFE LIGHT FOLLOWED BY STAB MISCOMPARE AND HYD PRESSURE LIGHT ILLUMINATED. INSPECTED UPLOCK SWITCHES AND FOUND THE NOSE SWITCH OUT OF ADJUSTMENT. ADJUSTED NOSE GEAR UPLOCK SWITCH IAW MM CHAP 32-30-05. PERFORMED GEAR SWING. OP CMar 24, 2009 · N671QS · Cessna 560XL · Landing Gear Position and WarningSDR CA090324003Fuel Control · leaking(CAN) DURING DAILY INSP OF ACFT, FUEL WAS NOTICED COMING OUT OF THE APU ENCLOSURE DRAIN MAST. APU COMPARTMENT WAS ACCESSED TO DETERMINE THE SOURCE OF THE FUEL AND IT WAS NOTED THAT THE ENCLOSURE WAS DAMP WITH FUEL. ENCLOSURE WAS CLEANED OF ALL FUEL AND COMPLETMar 23, 2009 · Cessna 560XL · APU Engine Fuel and ControlSDR DXTA2009032302558Brake Assy · wornREMOVED RT MAIN GEAR WHEEL BRAKES ASSY. INSTALLED O/H CUSTOMER SUPPLIED MAIN GEAR WHEEL BRAKE ASSY. PERFORMED EMERGENCY BRAKE SYS OPS CHECK AND BLED THE ANTISKID BRAKE SYS WITH NO DEFECTS NOTED. ALL WORK DONE IAW MM CHAP 32-42-01.Mar 22, 2009 · N673QS · Cessna 560XL · Landing Gear Brake SystemSDR DXTA2009032303558Brake · malfunctionedON LANDING, WHEN BRAKES ARE APPLIED THE AIRPLANE YAWS TOWARDS THE RT. REMOVED RT MAIN GEAR WHEEL BRAKES ASSY. INSTALLED O/H CUSTOMER SUPPLIED MAIN GEAR WHEEL BRAKE ASSY. PERFORMED EMERGENCY BRAKE SYS OPS CHECK AND BLED ANTI-SKID BRAKE SYS WITH NO DEFECTS NOMar 22, 2009 · N673QS · Cessna 560XL · Landing Gear Brake SystemSDR Z5FA030209N511CS1Transducer · failedAT CRUISE ALT FL4000, ENGINES AT REDUCED PWR FOR LANDING, BOTH ENGINE OIL PRESS INDICATIONS ENTERED THE RED WHEN ENGINES PULLED BACK. PRESSURE LOWERED THEN BACK INTO THE RED. REMOVED LT AND RT OIL PRESSURE TRANSDUCERS AND INSTALLED NEW. P/N ON AND OFF BOTH Mar 20, 2009 · N511CS · Cessna 560XL · Engine Oil PressureSDR Z5FA031909N515CS1Bleed Valve · malfunctionedAFTER DESCENT TO FL360 AND HOLDING FOR 15 MINUTES, EXPERIENCED CONTINUOUS COMPRESSOR STALLS ON RT ENGINE FOLLOWED BY EEC WARNING LIGHT. FOLLOWING AFM CHECKLIST, NOTED INCREASE IN STALLING WHEN THROTTLE ADVANCED, UNABLE TO MAINTAIN EFFECTIVE THROTTLE/ENGINE CONMar 19, 2009 · N515CS · Cessna 560XL · Compressor Bleed ValveSDR DXTA2009031603544Transducer · malfunctionedDURING TAKEOFF ROLL, THE MASTER CAUTION AND ANTI SKID LIGHT CAME ON. AFTER SHUTDOWN, NOTICED THE RT TRANSDUCER FLAG IN THE LT NOSE COMPARTMENT WAS SHOWING WHITE. R&R RT TRANSDUCER, OPS CHECK GOOD IAW MM 32-42-07.Mar 15, 2009 · N648QS · Cessna 560XL · Landing Gear Position and WarningSDR DXTA2009031603550Acm · smokeWHEN APU BLEED AIR IS SELECTED CABIN AND COCKPIT AREA BEGINS TO FILL WITH BLUE SMOKE. REMOVED ACM DUCTING & SEALS, R&R ACM. BEGAN INSTALLATION OF OVERHAULED ACM COMPLETED INSTALLED DUCTING, AND NEW SEALS. TORQUED AND/OR SAFETIED CLAMPS. INSTALLED APU ACCESSMar 13, 2009 · N630QS · Cessna 560XL · Cabin Cooling SystemSDR DXTA2009031603549Pcb · malfunctionedWHEN GEAR HANDLE WAS LOWERED RED GEAR UNLOCK ILLUMINATED; NO GREEN GEAR LIGHTS, NO HYD PRESS LIGHT. AFTER 20 SEC GEAR CAME DOWN NORMALLY. REMOVED AND REPLACED LANDING GEAR CONTROL PCB PER MAINT. CONTROL REQUEST IAW MM 24-51-02. ACCOMPLISHED GEAR SWINGS, OPERAMar 13, 2009 · N673QS · Cessna 560XL · Landing Gear Retraction/Extension SystemSDR DXTA2009031603547Pcb · inoperativeON TAKEOFF ROLL JUST PRIOR TO 70 KTS, NO TAKEOFF ANNUNCIATOR, WARNING HORN, AND MASTER CAUTION. EVERYTHING AS FAR AS FLAPS, SPEED BRAKES & TRIM WAS IN CORRECT POSITION FOR TAKEOFF. AFTER SHUTTING DOOR, RESTARTED ACFT & CHECKED TO MAKE SURE ANNUNCIATOR LIGHT, Mar 13, 2009 · N695QS · Cessna 560XL · Central WarningSDR Z5FA031209N512CS1Warning Light · illuminatedON CLIMB OUT CREW RECEIVED MASTER CAUTION WARNING WITH NO OTHER ANNUNCIATORS. CREW RESET MASTER WARNING AND TWO MINUTES AFTER FIRST WARNING ANOTHER MASTER WARNING INDICATION WITH LOW OIL PRESS RT INDICATION. CREW BROUGHT RT ENGINE BACK TO IDLE AND DECLARED EMMar 12, 2009 · N512CS · Cessna 560XL · Central WarningSDR DXTA2009031303543Uplock Switch · out of positionAFTER TAKEOFF, GEAR UNLOCK LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION FOLLOWED BY STAB MISCOMPARE, GEAR, HYD PRESSURE CAUTION LIGHTS. ADJUSTED BOTH MLG UPLOCK SWITCHES IAW MM 32-30-05. REPOSITIONED ADEL CLAMPS FOR ANTI SKID WIRING HARNESS ON BOTH MLG TMar 12, 2009 · N671QS · Cessna 560XL · Landing Gear Position and WarningSDR DXTA2009031303542Monopole · failedSHORTLY AFTER TAKEOFF, LT EEC FAILED WITH BOTH EEC'S IN MANUAL. LT ENGINE WOULD COMPRESSOR STALL WHEN N1 REDUCED BELOW 70 PERCENT AND N2 BELOW 85 PERCENT. NO NOTICEABLE RISE IN ITT WAS OBSERVED WITH POWER INCREASES. A SPLIT OF APPROX 2 INCHES IN POWER LEVERS TMar 12, 2009 · N566QS · Cessna 560XL · Turbine Engine Compressor SectionSDR CWQR200902Stiffener · misinstalledDURING A SCHEDULED INSP, FOUND THE LANDING ACTUATOR CHAFING STIFFENER P/N 6621211-25 LOCATED IN RT MAIN GEAR WELL. CONTACTED MFG FIELD ENGINEERS, DISCOVERED THE THE LT SIDE STIFFENER WAS INSTALLED ON THE RT SIDE FROM THE FACTORY. INSTALLED CORRECT STIFFENER ANMar 10, 2009 · N623QS · Cessna 560XL · Wing, Plate/SkinSDR CWQR200901Stiffener · misinstalledDURING A SCHEDULED INSPECTION, FOUND THE LANDING ACTUATOR CHAFING STIFFENER P/N 6621211-26 LOCATED IN LT MAIN GEAR WELL. CONTACTED MFG FIELD ENGINEERS, DISCOVERED THE THE RT SIDE STIFFENER WAS INSTALLED ON THE LT SIDE FROM THE FACTORY. INSTALLED CORRECT STIFFEMar 10, 2009 · N693QS · Cessna 560XL · Wing, Plate/SkinSDR DXTA2009030903534Coalescer Bag · dirtyWITH THE APU RUNNING AND THE BLEED AIR OFF. THERE WAS A STRONG ODOR OF ELECTRICAL WIRES MELTING. ODOR WAS COMING FROM THE REAR OF THE CABIN. THE APU GEN WAS ON. CONFIRMED DISCREPANCY, FOUND SMELL COMING FROM A/C COOLING VENTS NOT FLOOR HEAT VENTS. CHECKED ALL Mar 7, 2009 · N691QS · Cessna 560XL · Humidity Control SystemSDR DXTA2009030503530Actuator · inoperativeREPLACED ACTUATOR WITH INSPECTED RENTAL UNIT. OPS LEAK AND AMBER CHECKS. SERVICED BLOW DOWN BRIDLE AND BLED HYD SYS IAW MM 32-30-04.Mar 5, 2009 · N580QS · Cessna 560XL · Landing Gear ActuatorSDR DXTA2009030503529Oil System · leakingBORESCOPED EXHAUST AND INLET OF APU. FOUND OIL IN INLET. REMOVED AND REPLACED APU AND ECU IAW MM CH 49-10-00 LEAK AND FUNCTIONAL CHECKED GOOD.Mar 5, 2009 · N630QS · Cessna 560XL · APU Oil SystemSDR DXTA2009030603530Actuator · inoperativeAFTER SELECTING GEAR DOWN, THE LT MAIN GREEN GEAR LIGHT DID NOT ILLUMINATE AND THE RED GEAR UNSAFE LIGHT REMAINED ILLUMINATED. T/S TO BAD LT MAIN GEAR ACTUATOR DOWN LOCK SWITCH. REPLACED ACTUATOR WITH INSPECTED RENTAL UNIT. OPS, LEAK AND AMBER CHECKS. SERVICMar 5, 2009 · N580QS · Cessna 560XL · Landing Gear ActuatorSDR DXTA2009030603529Ecu · leakingAFTER TURNING ON APU BLEED AIR, EXCESSIVE FUMES AND ODOR ENTERED THE CABIN. REMOVED AND REPLACED APU AND ECU IAW MM CH 49-10-00 LEAK AND FUNCTIONAL CHECKED GOOD.Mar 5, 2009 · N630QS · Cessna 560XL · APU Oil SystemSDR DXTA2009030503528Master Cylinder · inoperativeNO RESISTANCE ON CAPTAINS SIDE LEFT BRAKE PEDAL. REMOVED AND REPLACED PILOTS LT MASTER CYL WITH O/H UNIT. BLED BRAKE SYSTEM LEAK CHECK GOOD, TAXI CHECK BRAKE OPS CHECK GOOD, ALL 4 BRAKE PEDALS ARE FIRM. WORK IAW MM 32-42-00 AND CH 32-42-02Mar 5, 2009 · N639QS · Cessna 560XL · Master Cylinder/Brake ValveSDR DXTA2009030403528Master Cylinder · inoperativeREMOVED AND REPLACED PILOTS LT MASTER CYL WITH O/H UNIT. BLED BRAKE SYSTEM LEAK CHECK GOOD, TAXI CHECK BRAKE OPS, CHECK GOOD, ALL 4 BRAKE PEDALS ARE FIRM. WORK IAW MM CH 32-42-00 AND CH 32-42-02.Mar 4, 2009 · N639QS · Cessna 560XL · Master Cylinder/Brake ValveSDR CA090305010Strut · low(CAN) RT MLG OLEO FAILED TO EXTEND FULLY WHEN THE CREW RETRACTED THE GEAR. THE RT MAIN TIRE STRUCK THE AFT OTBD EDGE OF THE WHEEL CAUSING DAMAGE TO THE STRUCTURE WITHIN THE RT WHEEL WELL. CREW DID NOT HAVE ANY INDICATION OF A PROBLEM OR FEEL THE WHEEL STRIKE TMar 2, 2009 · Cessna 560XL · Main Landing Gear Strut/Axle/TruckSDR DXTA2009022803526Apu · leakingREMOVED APU ACCESS PANNEL, AND FOUND OIL PRESENT AROUND THE STARTER GENERATOR. REMOVED APU BLEED AIR SUPPLY TUBE, AND FOUND OIL PRESENT INSIDE OF TUBE. REMOVED THE APU IAW MM 49-10-00, REV APU CYCLES , APU HOBBS 4069.4 BEFORE REMOVAL OF APU. BUILT UP APU FOFeb 28, 2009 · N608QS · Cessna 560XL · Airborne Auxiliary Power Unit (APU) SystemSDR DXTA2009030203526Unknown · smokeWHEN EITHER THE BLEED AIR FROM THE APU IS TURNED ON OR AN ENGINE IS STARTED WITH THE APU BLEED AIR OFF, SMOKE BEGINS TO EMIT FROM THE WEMACS IN BOTH THE COCKPIT AND THE CABIN. DOES NOT ODOR ELECTRICAL.Feb 28, 2009 · N608QS · Cessna 560XL · Air Distribution SystemSDR CA090227006Uplock Switch · stuck(CAN) WHEN CARRYING OUT THE GEAR SWINGS AS CALLED UP IN SB 560XL-32-40, MX OBSERVED THAT THE RT MAIN GEAR UPLOCK SWITCH S3 WAS JAMMED IN THE CLOSED POSITION. THERE IS NO INDICATION TO SAY THAT THIS SWITCH WAS NOT WORKING CORRECTLY. THE GEAR SWINGS THAT WERE CAFeb 25, 2009 · Cessna 560XL · Landing Gear Position and WarningSDR DXTA2009021703508Actuator · out of adjustAFTER TAKEOFF, WHEN LANDING GEAR HANDLE SELECTED UP, ALL THREE GREEN LIGHTS WENT OUT, RED UNLOCK LIGHT REMAINED ON. FOUND THE LT MAIN SIDE BRACE ACTUATOR OUT OF ADJUSTMENT. ADJUSTED LT MAIN CAMBER TO SPEC IAW MM 32-10-00. SYS OPS CHECK GOOD IAW SAME.Feb 16, 2009 · N611QS · Cessna 560XL · Landing Gear ActuatorSDR DXTA2009021603507Rod End · out of adjustGEAR UNLOCK LIGHT REMAINED ON AFTER GEAR RETRACTION. RT DOOR WOULD BND UP WITH LT DOOR. ADJUSTED FWD NOSE GEAR DOOR ROD ENDS AS REQUIRED. (IAW MM 32-20-00) SWUNG GEAR AND PERFORMED SEVERAL CLEARANCE CHECKS ALL CHECKS GOOD.Feb 15, 2009 · N574QS · Cessna 560XL · Landing Gear Door Retract SectionSDR DXTA2009021303503Brake Sys · weakBRAKE PEDALS FEEL SPONGY. BLED ANTI-SKID BRAKE SYS IAW CH 32-44-00 OF AMM. LEAK CHECK OF BLEEDER PLUGS GOOD. TAXI CHECK OF BRAKES GOOD. ALL WORK IAW MM 32-44-00.Feb 12, 2009 · N686QS · Cessna 560XL · Landing Gear Brake SystemSDR DXTA2009020903495Actuator · failedON CLIMB OUT THE RED GEAR UNLOCK LIGHT CAME ON. WHEN WE PULLED THE HYD PRESS CB THE NOSE GEAR WENT DOWN AND LOCKED EVEN THOUGH THE HANDLE WAS UP. M2B - R&R NOSE GEAR ACTUATOR WITH NEW HARDWARE. PERFORMED OPS CHECK OF LANDING GEAR SYSTEM. SYSTEM CHECKED GOOFeb 6, 2009 · N574QS · Cessna 560XL · Landing Gear ActuatorSDR DXTA2009020103486Actuator · inoperativeREMOVED AND REPLACED LT MLG ACUATOR WITH REPAIRED UNIT. PERFORMED ALL OPS CHECKS AND LEAK CHECKS. OPS AND LEAK CHECKS GOOD. ALL ACTUATOR HARDWARE REPLACED WITH NEW. SERVICED EMERGENCY BLOWDOWN BOTTLE TO FULL AND SAFETIED WORK DONE IAW MM 32-30-04.Feb 1, 2009 · N686QS · Cessna 560XL · Landing Gear Actuator
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