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 DXTA2013010705235Seal · leakingON CLIMBOUT , AFTER GEAR AND FLAPS UP, RECEIVED AN UNSAFE GEAR INDICATION, RED LIGHT ON, THREE GREENS OUT, FOLLOWED SHORTLY BY A HYD PRESSURE ANNUNCIATOR AND STAB MISCOMPARE ANNUNCIATOR. STAYED BELOW 200 KNOTS AT ALL TIMES. RAN CHECKLISTS, RETURNED TO LAND AJan 6, 2013 · N603QS · Cessna 560XL · Main Landing GearSDR DXTA2013010705234Bulb · burned outNO NOSE WHEEL DOWN/LOCK LIGHT INDICTAION AFTER GEAR EXTENSION. MANUAL EXTENSION AND BLOWDOWN PROCEDURE ACCOMPLISHED IAW CHECKLIST. SET UP ACFT ON JACKS. INSPECTED NOSE GEAR ACTUATOR AND SWITCH, FOUND SATISFACTORY. PERFORMED LANDING GEAR RETRACTION AND EXTEJan 6, 2013 · N629QS · Cessna 560XL · Landing Gear Position and WarningSDR DXTA2013010705230Ring · damagedON TAKEOFF, RETRACTED GEAR AND RECEIVED A RED GEAR UNSAFE LIGHT AND A FLASHING HYD LIGHT. THERE WAS A RUMBLE FROM THE NOSE SECTION. THE NOSE STRUT LOOKS TO BE LONGER THAN NORMAL. JACKED ACFT & CYCLED GEAR FIVE TIMES. NOTED GEAR "UNSAFE" LIGHT ILLUMINATED &Jan 4, 2013 · N672QS · Cessna 560XL · Nose/Tail Landing Gear Strut/AxleSDR CWQR20130131005Pressure Switch · out of toleranceDURING A SCHEDULED INSPECTION, PERFORMED TASK 35-01-00-710. FOUND THE INSTALLED PRESSURE SWITCH OUT OF TOLERANCE. A NEW SWITCH WAS INSTALLED, SWITCH OUT OF TOLERANCE. UNIT REJECTED AND RETURNED TO MFG.Dec 31, 2012 · N577QS · Cessna 560XL · Passenger Oxygen SystemSDR CWQR20130131004Pressure Switch · out of toleranceDURING A SCHEDULED INSPECTION, PERFORMED TASK 35-01-00-710. THIS TASK CHECKS THE ALITUDE IN WHICH THE PASSENGER MASKS WOULD DROP. FOUND THE INSTALLED PRESSURE SWITCH OUT OF TOLERANCE. A NEW SWITCH, SN 1512 WAS INSTALLED, THIS SWITCH WAS OUT OF TOLERANCE. Dec 31, 2012 · N577QS · Cessna 560XL · Passenger Oxygen SystemSDR CWQR20130131003Pressure Switch · out of toleranceDURING A SCHEDULED INSPECTION, PERFORMED TASK 35-01-00-710. FOUND THE INSTALLED PRESSURE SWITCH OUT OF TOLERANCE. A NEW SWITCH WAS INSTALLED, THIS SWITCH WAS OUT OF TOLERANCE. UNIT REJECTED AND RETURNED TO MFG.Dec 31, 2012 · N577QS · Cessna 560XL · Passenger Oxygen SystemSDR CWQR20130131002Pressure Switch · out of toleranceDURING A SCHEDULED INSPECTION, PERFORMED TASK 35-01-00-710. THIS TASK CHECKS THE ALITUDE IN WHICH THE PASSENGER MASKS WOULD DROP. FOUND THE INSTALLED PRESSURE SWITCH OUT OF TOLERANCE. A NEW SWITCH WAS INSTALLED, THIS SWITCH WAS OUT OF TOLERANCE. THIS UNIT Dec 31, 2012 · N577QS · Cessna 560XL · Passenger Oxygen SystemSDR DXTA2013010205224Control Valve · failedAFTER TAKEOFF, GEAR RAISED AND RED UNLOCK LIGHT STAYED ILLUMINATED AND WOULD NOT EXTINGUISH. R & R LANDING GEAR CONTROL VALVE IAW MM 32-30-02. LEAK AND OPS CHECKS GOOD.Dec 31, 2012 · N672QS · Cessna 560XL · Landing Gear Retraction/Extension SystemSDR CWQR20121221055Tube · crackedDURING AN APU CHANGE, FOUND A 2.5" CRACK IN THE BLEED AIR TUBE ATTACHMENT FLANGE. DISCOVERED VISUALLY AND THE CRACK DID NOT EXTEND INTO THE TUBE, NO BLEED AIR LEAK.Dec 21, 2012 · N600QS · Cessna 560XL · Pneumatic Distribution SystemSDR DXTA2012122105211Powerpack · failedON ROLLOUT ANTI-SKIP INOPERATIVE LIGHT ILLUMINATED. DURING TAXI IN LOW BRAKE PRESSURE LIGHT ILLUMINATED. FOLLOWED BY LOSS OF BRAKES. USED EMERGENCY BRAKING TO STOP ACFT. CIRCUIT BREAKER DID NOT TRIP. NO BREAK FLUID LEAKING NOTICED. REMOVED SUSPECTED FAULTDec 20, 2012 · N694QS · Cessna 560XL · Landing Gear Brake SystemSDR DXTA2012121905209Water Separator · dirtyWITH APU BLEED AIR RUNNING THERE IS A STRONG PUNGENT MILDEW ODOR. CLEANED ACM WATER SEPERATOR SOCK IAW MM 12-19-02. NO DEFECTS OR LEAKS NOTED.Dec 18, 2012 · N643QS · Cessna 560XL · Humidity Control SystemSDR 9JLA2012121904477Line · rupturedTHE CREW REPORTED WHEN LOWERING THE LANDING GEAR AND THE FLAPS IN PREPARATION FOR LANDING THEY NOTED THE LOW HYD LEVEL AND PRESSURE ANNUNCIATOR LIGHTS ILLUMINATE AND AFTER TOUCH DOWN THE CREW STATED THAT THE RT THRUST REVERSER DEPLOYED AND THE LT DID NOT. DURDec 16, 2012 · N309BT · Cessna 560XL · Hydraulic System, MainSDR DXTA2012121705206Apu · failedAFTER RUNNING APU TWO MINUTES, SMOKE STARTED TO FILL THE COCKPIT. REMOVED APU IAW AMM 49-10-00. INSTALLED SERVICEABLE APU IAW AMM 49-10-00. OPS CHECKED GOOD AND NO LEAKS DETECTED .Dec 15, 2012 · N665QS · Cessna 560XL · Airborne Auxiliary Power Unit (APU) SystemSDR 2013F00002Bolt · wornON PERFORMING AN INSPECTION-B, FOUND LT ENGINE FORWARD COWLING STRUT UPPER ATTACH BOLT SEVERELY WORN. SUSPECT VIBRATION CAUSING EXCESSIVE WEAR. THIS CONDITION HAS BEEN FOUND ON SEVERAL OF THIS MODEL ACFT.Dec 12, 2012 · N617QS · Cessna 560XL · Nacelle/Pylon Miscellaneous StructureSDR 9JLA2013010803563Throttle · out of adjustTHE CREW REPORTED THE RT ENGINE SHUTDOWN DURING TAXI, WHEN THE THROTTLE WAS ADVANCED, RETURNED BACK TO IDLE. THE MX TEAM RIGGED THROTTLE ADJUSTMENT IAW THE MM 76-11-00, PAR E AND FIG 502. POST MX ENGINE RUNS AND FUNTIONAL CHECKS SATISFACTORY.Dec 5, 2012 · N523KW · Cessna 560XL · Power LeverSDR DXTA2013010405230Unknown · smokeWITH THE APU ON, BLEED AIR OFF, DURING NR 2 ENGINE START, WHICH WAS FIRST TO BE STARTED, SMOKE STARTED TO COME INTO COCKPIT, PARTICULARLY THRU THE RT SIDE EYEBALL VENT BUT ALSO THRU BOTH WEMACS. IT CONTINUED DURING THE 2ND ENGINE START. SHUTDOWN BOTH APU AND Dec 3, 2012 · N651QS · Cessna 560XL · Air Distribution SystemSDR DXTA2012120405200Water Separator · odorWITH THE APU ON, BLEED AIR OFF, DURING THE NUMBER 2 ENGINE START (WHICH WAS FIRST TO BE STARTED) SMOKE STARTED TO COME INTO COCKPIT.PARTICULARLY THRU THE RT SIDE EYEBALL VENT BUT ALSO THRU BOTH WEMACS. IT CONTINUED DURING THE 2ND ENGINE START. WE SHUTDOWN BOTHDec 3, 2012 · N651QS · Cessna 560XL · Humidity Control SystemSDR DXTA2012112605192Actuator · inoperativeAFTER TAKEOFF THE RED GEAR UNLOCK LIGHT REMAINED ILLUMINATED. HYD PRESSURE ANNUNCIATOR CAME AND STAB MISCOMPARE ANNUNCIATOR. ADVISED TO SELECT GEAR DOWN AND RETURN TO DEPARTURE. RECEIVED NORMAL INDICATIONS AND RETURNED TO DEPARTURE. R & R THE NOSE GEAR UPLONov 25, 2012 · N670QS · Cessna 560XL · Landing Gear ActuatorSDR DXTA201211265192Landing Gear · malfunctionedAFTER TAKEOFF, THE RED GEAR UNLOCK LIGHT REMAINED ILLUMINATED. "HYD PRESS" ANNUNCIATOR THEN CAME ON AS WELL AS THE "STAB MISCOMPARE" ANNUNCIATOR. ADVISED TO SELECT GEAR DOWN AND RETURN AND GOT NORMAL INDICATIONS AND RETURNED TO DEPARTURE.Nov 25, 2012 · N670QS · Cessna 560XL · Central WarningSDR DXTA2012112605191Oil Fill Port · contaminatedAFTER BOTH ENGINES WERE STARTED, THE COCKPIT AND CABIN FILLED WITH SMOKE. APU WAS RUNNING AND BLEED VALVE OPEN. RT ENGINE WAS STARTED FIRST. UNABLE TO DETERMINE SOURCE. NOTHING ABNORMAL IN THE AFT TAILCONE. ENGINE OIL LEVELS WERE NORMAL AND NO LEAKS SEEN. FNov 24, 2012 · N670QS · Cessna 560XL · APU Oil SystemSDR DXTA2012111905184Gcu · failedON THE GROUND WITH THE APU RUNNING AND GENERATOR ONLINE, THE COCKPIT LIGHT STARTED GETTING BRIGHT AND THE AVIONICS FAN STARTED SPEEDING UP. I SAW THE VOLTS RAPIDLY CLIMB, AND THE GCU DID NOT KICK THE GENERATOR OFFLINE UNTIL APPROX 33 VOLTS. AN UNUSUAL SMELL WANov 16, 2012 · N635QS · Cessna 560XL · Battery Overheat Warning SystemSDR CWQR20121113052Hinge Bracket · crackedDURING A SCHEDULED INSPECTION, FOUND THE RT ELEVATOR OTBD HINDGE BRACKET CRACKED. PERFORMED AN EDDY CURRENT CHECK AND VERIFIED THE HINGE WAS CRACKED ON THE UPPER BRACKET EAR RADIUS. HINGE BRACKET REPLACED, CRACKED BRACKET SENT FOR EVALUATION.Nov 13, 2012 · N592QS · Cessna 560XL · Elevator StructureSDR DXTA2012111305181Brake Sys · malfunctionedWHEN BRAKES ARE APPLIED DURING TAXI THE ACFT VIBRATES AND SHAKES. BLED BRAKES, NOTICED AIR IN LT BRAKE, TAXI & LEAK CHECKED GOOD. WORK DONE IAW MM 32-44-00.Nov 12, 2012 · N633QS · Cessna 560XL · Landing Gear Brake SystemSDR CA121119003Oil System · high pressure(CAN) DURING CLIMB, THE ENGINE OIL PRESSURE WAS LOST. THE PILOT PULLED BACK ON THE THROTTLE AND THE PRESSURE CAME BACK TO NORMAL. ELECTED TO RETURN TO DEPARTURE WHERE AN UNEVENTFUL LANDING WAS MADE. DURING TAXI, BLACK SMOKE WAS SEEN COMING OUT OF THE ENGINENov 7, 2012 · Cessna 560XL · Turbine SectionSDR DXTA2012110705173Unknown · unknownSHORTLY AFTER A TAKEOFF A VERY PROMINENT GRINDING FEELING COULD BE FELT IN THE YOKE. THIS GRINDING COULD BE FELT DURING THE CLIMB AND AT INTERMEDIATE LEVEL OFF ALTITUDES. THE GRINDING DID NOT SEEM TO DISSIPATE UNTIL WE WERE ON FINAL APPROACH AND AT APPROACH SPNov 6, 2012 · N642QS · Cessna 560XL · Control Column SectionSDR DXTA2012110705172Apu · odorWITH THE APU RUNNING AND THE AVIONICS ON, COCKPIT AND THEN CABIN FILLED WITH SMOKE. SMOKE APPEARED TO BE COMING FROM THE GLARE SHIELD AREA AND FILLED THE COCKPIT FIRST. IT WAS A WHITE SMOKE WITH A PLASTIC LIKE ODOR. R & R THE APU IAW MM 49-10-00. OPS & LEAKNov 6, 2012 · N689QS · Cessna 560XL · Airborne Auxiliary Power Unit (APU) SystemSDR DXTA2012110705171Apu · odorABOUT 30 MINUTES AFTER COMPLETE SHUTDOWN, APU WAS RE-STARTED AND BLEEDS WERE PLACED TO LOW. AIRCRAFT CABIN AND FLIGHTDECK STARTED TO FILL WITH SMOKE. OPERATED APU FOR ABOUT 30 MINUTES, NO DISCREPANCIES NOTED. ACCESSED AND REMOVED AND CLEANED WATER SEPARATOR Nov 6, 2012 · N549QS · Cessna 560XL · Airborne Auxiliary Power Unit (APU) SystemSDR DXTA2012103105161Spring · brokenDURING TAXI BRAKE CHECK, LEFT BRAKE GRABS SEVERELY AND PULLS AIRCRAFT LEFT ON BOTH SIDES (PILOT AND COPILOT). NO LEAKS FOUND AROUND BRAKE ASSEMBLY. NO LEAKS FOUND AROUND BRAKE ASSY. REMOVED BROKEN LT BRAKE VALVE LEVER RETURN SPRING AND INSTALLED A NEW SPRIOct 30, 2012 · N643QS · Cessna 560XL · Landing Gear Brake SystemSDR 9JLA2012103004519Solenoid · defectiveCREW REPORTED THAT THE MAIN CABIN ENTRY DOOR ANNUNCIATOR LIGHT WOULD NOT EXTINGUISH. TROUBLESHOOTING IDENTIFIED THE DOOR VENT SOLENIOD DEFECTIVE. THE SOLENOID WAS REPLACED WITH NEW. FUNCTIONAL CHECKS SATISFACTORY. PART HAS BEEN REPLACED ON THIS AIRCRAFT 4 TIMOct 29, 2012 · N909LA · Cessna 560XL · Door Warning SystemSDR DXTA2012102305160Squat Switch · out of adjustAFTER TAKEOFF, GEAR HANDLE WOULD NOT COME UP. HANDLE STAYED IN DOWN LOCKED POSITION. FOUND LT SQUAT SWITCH ON EDGE OF ADJUSTMENT. ADJUSTED SQUAT SWITCH TO SPECS IAW MM 32-61-02, LANDING GEAR CONTROL OPS CHECKED GOOD IAW MM 32-61-00.Oct 22, 2012 · N633QS · Cessna 560XL · Landing Gear Retraction/Extension SystemSDR DXTA2012102205156Brake Sys · malfunctionedRIGHT BRAKE MAKING A LOUD MOANING AND CHATTERING NOISE. ALSO GRABS WHEN APPLYING BRAKES. COMPLIED WITH VISUAL INSPECTION OF RT BRAKE. NO FAULTS FOUND. FOUND WEAR INDICATOR MEASURING 0.20", FOUND PRESSURE AT BOTH BRAKES NORMAL. COMPLIED WITH TAXI CHECK FOUOct 20, 2012 · N671QS · Cessna 560XL · Landing Gear Brake SystemSDR DXTA2012102205155Trunnion · damagedON ROTATION, LOST APPROX. 180 GALLONS OF FUEL IN THE 10 MIN FLIGHT. FUEL WAS STREAMING FROM THE LT WHEEL WELL AT TAXI IN. REMOVED LT MLG ASSY. INSTALLED LT MLG WITH NEW TRUNNION AND AN INSPECTED TRAILING LINK. PERFORMED GEAR SWINGS AND HYD SYS BLEEDING.Oct 19, 2012 · N576QS · Cessna 560XL · Wing, Landing Gear Attach FittingsSDR CA121015012Lock Ring · cracked(CAN) WHILE CARRYING OUT REQUIRED NDT INSPECTION OF WHEEL ASSY, CRACKING WAS NOTED IN LOCKING RING WHERE CLIP LOCKING RING, PN 53-387, CLIPS, PN 245-627 TOGETHER. THE NDT FACILITY ADVISED US THAT THIS IS THE 3RD SUCH INCIDENT OF CRACKING IN THIS AREA SO FAR FOct 15, 2012 · Cessna 560XL · Wheel/Ski/FloatSDR DXTA2012101605149Apu · odorWITH APU RUNNING AND BLEED AIR ON, CABIN AND COCKPIT BEGAN FILLING WITH SMOKE. COMPLIED WITH BOROSCOPE INSPECTION OF THE APU INLET AND FOUND THE INSIDE FAN SEAL LEAKING. REMOVED AND INSTALLED APU IAW MM 49-10-00. AFTER REPLACEMENT OF APU REMOVED WATER SEPERAOct 15, 2012 · N574QS · Cessna 560XL · Airborne Auxiliary Power Unit (APU) SystemSDR DXTR20121015002Axle · corrodedRIGHT MLG AXLE CORRODED UNDER BRAKE ASSY. R & R AXLE ASSY BY REPLACING TRAILING LINK ASSY IAW COMPONENT MM 32-10-01. TRAILING LINK ASSY, NR 6641648-14, SN 3911.Oct 15, 2012 · N678QS · Cessna 560XL · Main Landing Gear Strut/Axle/TruckSDR DXTR 20121015001Bracket · crackedDURING A ROUTINE A/B INSPECTION, DISCOVERED THE AUTOPILOT RUDDER CABLE BRACKET LOCATED AFT OF THE CANTED BULKHEAD IS CRACKED IN 2 PLACES. REPLACED RUDDER AUTO PILOT CABLE PULLEY BRACKET, REF SRM 51-40-03, PN 6661154-2.Oct 15, 2012 · N678QS · Cessna 560XL · Rudder StructureSDR 2012FA0000710Control Cable · frayedWHILE TROUBLESHOOTING, AN AUTO PILOT PORPOISE DISCREPANCY, THE TECH PULLED ON A PRIMARY RUDDER CABLE IN THE TAIL CONE AND IT SNAPPED. THE CABLE HAS BEEN BROKEN EXCEPT FOR A FEW STRANDS. IT APPEARS THE CABLE WAS NOT RIDING IN A PULLEY AND WAS CHAFING ON THE UOct 10, 2012 · N627QS · Cessna 560XL · Aerodynamic FairingsSDR DXTA2012101105143Uplock Switch · failedNOSE GEAR WILL NOT RETRACT. AFTER TAKEOFF, WHEN THE GEAR HANDLE WAS SELECTED TO THE UP POSITION, THE MAIN GEAR LIGHTS EXTINGUISHED, BUT THE NOSE GEAR LIGHT REMAINED ILLUMINATED. THE SOUND INDICATIONS WERE ALSO THAT THE NOSE GEAR REMAINED DOWN. THE GEAR HANDLOct 10, 2012 · N580QS · Cessna 560XL · Landing Gear Position and WarningSDR DXTA2012101105141Lead · burnedTHE APU WAS OPERATING AND BLEED AIR WAS ENGAGED, PRESSED THE ENGINE START BUTTON FOR NR 2 ENGINE, AFTER FUEL WAS INTRODUCED DURING THE START, THE APU DROPPED OFFLINE AND OUR ENGINE AVIONICS SCREENS MOMENTARILY WENT BLANK. DETECTED A FAINT ODOR OF SMOKE. AFOct 10, 2012 · N655QS · Cessna 560XL · APU System WiringSDR ZDVA201210100802Windshield · failedWINDSHIELD FAULT LIGHT ILLUMINATED APPROX 30 SECONDS PRIOR TO PILOTS SEEING CRACK IN LOWER RT COPILOTS WINDSHIELD, DECLARED EMERGENCY AND DECENDED TO A SAFE DEPRESSURIZED ALTITUDE IAW ACFT PROCEDURES, PROBABLE CAUSE BROUGHT ON BY FAILED ELECTRICAL HEATING ELEOct 8, 2012 · N531RQ · Cessna 560XL · Flight Compartment WindowsSDR CA121017011Oil System · low pressure(CAN) DURING TAKEOFF ROLL, THE CREW OBSERVED A LOSS OF OIL PRESSURE ON NR 2 ENGINE. THE TAKEOFF WAS ABORTED AND THE ACFT RETURNED TO THE GATE. DURING EVENT INSPECTION FOUND THE OIL LEVEL TO BE BELOW MINIMUM. THE SYS WAS REPLENISHED, ENGINE GROUND RUNPERFORMEDOct 2, 2012 · Cessna 560XL · Engine Oil Indicating SystemSDR CA121003010Oil System · low pressure(CAN) DURING CLIMB, THE ENGINE LOW OIL PRESSURE WARNING ILLUMINATED AS THE PRESSURE DROPPED BELOW 20 PSI. THE PILOT THROTTLED BACK AND THEN SMOKE CAME INTO THE CABIN. THE ENGINE WAS SHUTDOWN AND THE FLIGHT DIVERTED BEFORE AN UNEVENTFUL SINGLE ENGINE LANDING WSep 28, 2012 · Cessna 560XL · Engine Oil Indicating SystemSDR DXTA2012092805134Uplock Switch · failedLANDING GEAR RED UNLOCK ANNUNCIATOR REMAINED ILLUMINATED AFTER TAKEOFF. ACFT WAS LANDED NORMALLY (BELOW MAX LANDING WEIGHT) AFTER POSITIVE GEAR DOWN INDICATION WAS CONFIRMED. R & R RT MLG UPLOCK SWITCH IAW MM 32-30-05. OPS CHECKED GOOD.Sep 27, 2012 · N667QS · Cessna 560XL · Landing Gear Position and WarningSDR CA120926005Heat Shield · contaminated(CAN) AFTER LANDING & TAXIING TO THE FBO, THE CREW NOTICED WHITE SMOKE EMANATING FROM INSIDE THE OTBD SIDE OF THE RT MAIN WHEEL. THE CREW WATCHED THE SMOKE FOR A FEW MINUTES BEFORE THE WHEEL STOPPED SMOKING. THE CREW, AFTER CONSULTATION WITH AN AME, TEST TAXISep 24, 2012 · Cessna 560XL · Wheel/Ski/FloatSDR DXTA2012092005128Unknown · odorDURING ENGINE START UP, ENCOUNTERED SMOKE IN CABIN. THE APU WAS RUNNING ALONG WITH THE BLEED AIR. INITIALLY SHUT THE BLEED AIR OFF TO THE APU FOR THE PASSENGER BRIEFING. TURNED THE BLEED AIR BACK ON, HEARD SUBTLE SQUEALING NOISES. ON ENGINE START UP, ALL THSep 19, 2012 · N638QS · Cessna 560XL · Air Distribution SystemSDR 9JLA2013020504464Solenoid · defectiveCREW REPORTED THAT THE CABIN DOOR ANNUNCIATOR REMAINS ILLUMINATED, THIS ACFT HAS HAD THREE DOOR SOLENOIDS INSTALLED IN THE PAST 9 MONTHS. DEFECTIVE SOLENIOD, PN 6711335-1, NEW SOLENOID INSTALLED IAW THE MM 52-10-00.Sep 16, 2012 · N309BT · Cessna 560XL · Door Warning SystemSDR 9JLA2012101804464Solenoid · defectiveCREW REPORTED THAT THE CABIN DOOR WARINING LIGHT WILL NOT GO OUT WITHOUT MULTIPLE CLOSINGS OF THE CABIN DOOR. THE SYSTEM WAS TROUBLESHOT AND THE CABIN DOOR VENT SOLENOID WAS FOUND TO BE DEFECTIVE. A NEW SOLENOID WAS INSTALLED. OPS CHECKS SATISFACTORY IAW MM 52Sep 16, 2012 · N309BT · Cessna 560XL · Door Warning SystemSDR 9JLA201101804465Bearing · defectiveCREW REPORTED THAT DURING THE TAKEOFF AND LANDING ROLL UNUSUAL NOISE FROM THE NOSE GEAR. THE ACFT NOSE WHEEL BEARINGS WERE REPLACED ALONG WITH THE WHEEL RACES AND BEARING SEALS. CMM 32-47-42, MM 32-41-01 AND 32-41-02.Sep 16, 2012 · N309BT · Cessna 560XL · Nose/Tail Landing Gear Strut/AxleSDR DXTA2012091705125Bungee · damagedDURING LANDING ROLLOUT UNEVEN PRESSURE ON BRAKE APPLICATION. THE LT BRAKE PEDAL TRAVELED SIGNIFICANTLY FURTHER THAN THE RT PEDAL CAUSING A JERKING MOTION. AFTER EXITING THE RUNWAY (TRANSFER CONTROLS), PIC TAXIED IN AND NOTICED UNEVEN BRAKE PRESSURE AND A SIGSep 16, 2012 · N566QS · Cessna 560XL · Landing Gear Brake SystemSDR DXTA2012091305120Unknown · smokeHEAVY SMOKE ENTERED AFT CABIN TO THE COCKPIT WHEN THE APU BLEED WAS TURNED ON. THE CABIN GOT HOT AND A RUMBLING NOISE WAS HEARD. THE ACFT WAS SHUTDOWN. PERFORMED APU RUNS. PERFORMED ECU OPS CHECKS WITH NO DEFEFCTS NOTED. RAN APU BLEED AIR TO FULL HOT AND FULSep 12, 2012 · N655QS · Cessna 560XL · Air Distribution System
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