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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CWQR20160304010Attach Bracket · crackedDURING A SCHEDULED INSPECTION WE FOUND THIS AVIONICS SHELF ATTACH BRACKET PAT 9256023-16, CRACKED MORE THAN HALF ITS LENGTH. THIS ATTACH BRACKET IS FOR THE FWD NOSE AVIONICS SHELF OTBD BRACKET. SUBMITTED MFG SERVICE CONDITION REPORT 747902.SDR O2GA2016030350001Display · defectiveAPPROXIMATELY 1.5 HOURS INTO FLIGHT THE MULTI-FUNCTION DISPLAY WENT BLANK, FOLLOWED BY ELEC SMELL. CREW DONNED THEIR OXYGEN MASKS & DIVERTED. LANDING WAS UNEVENTFUL. REPLACED THE MULTI-FUNCTION DISPLAY. SYS OPERATIONAL CHECKS WERE PERFORMED. ACFT WAS RETUSDR CWQR20160224007Hinge Bracket · crackedTAIL BAGGAGE DOOR WAS UPGRADED TO SB560XL-52-13, TO PREVENT THE CRACKING OF ATTACH CHANNEL PN 6612069-11S. THIS NEW CRACK WAS FOUND IN HINGE BRACKET PN 6612072-2S, WHICH WAS ADDED IAW SB560XL-52-13 TO CORRECT THE ATTACH CHANNEL FROM CRACKING. SCR 746341 SUBMSDR CA160302002Oil System · low pressure(CAN) AFTER TAKEOFF ON CLIMB OUT, THE MASTER WARNING LIGHT ILLUMINATED AT 14,000` MSL ALONG WITH THE RIGHT ENGINE OIL PRESSURE ANNUNCIATOR. THE OIL PRESSURE INDICATED 22 PSI AT THAT POINT. AFTER TWO MINUTES, THE ANNUNCIATOR EXTINGUISHED AND THE OIL PRESSURE STSDR CA160301028Bleed Valve · malfunctioned(CAN) DURING LEVEL FLIGHT 10000FT, 265KTS, AND NO POWER CHANGE, THE LEFT EEC MANUAL ANNUNCIATOR ILLUMINATED. THE CHECKLIST WAS APPLIED WOULD NOT CLEAR ANNUNCIATOR. IT WAS NOTED THAT WITH POWER LEVERS IN THE SAME POSITION, ENGINE PERFORMANCES WERE DIFFERENT FROSDR CWQR20160217006Bracket · crackedDURING A SCHEDULED INSPECTION WE FOUND THE AVIONICS SHELF BRACKET, PN 9256023-16, CRACKED MORE THAN HALF ITS LENGTH. REPLACED BRACKET & SENT SCR 745616 TO MFG.SDR CWQR20160217005Bracket · crackedDURING A SCHEDULED INSPECTION WE FOUND THE AVIONICS SHELF BRACKET, PN 9256023-16, CRACKED MORE THAN HALF ITS LENGTH. REPLACED BRACKET & SENT SCR 745615 TO MFG.SDR CWQR20160216004Air Duct · crackedDURING AN INSPECTION WE FOUND THE APU AIR DUCT MOUNTING FLANGE CRACKED WHERE IT ATTACHES TO THE DUCT ASSEMBLY. REPLACED AIR DUCT WITH UPGRADED 6655600-49 ASSEMBLY & SENT A SERVICE CONDITION REPORT 745481 TO MFG.SDR CWQR20160216002Pulley Bracket · crackedDURING A SCHEDULED INSPECTION WE FOUND THE AUTOPILOT SERVO CABLE PULLEY BRACKET CRACKED. THE CRACK WAS THROUGH ONE ATTACH RIVET & WENT TO THE END OF THE BRACKET. REPLACED BRACKET & SENT SERVICE CONDITION REPORT 745468.SDR CA160224006Starter Gen · failed(CAN) DURING CRUISE FLIGHT, THE AIRCRAFT CREW EXPERIENCED MULTIPLE TIMES WHERE THE LT ENGINE STARTER GENERATOR WOULD COME OFFLINE, ILLUMINATING THE LT GEN OFF LIGHT. LT ENGINE GENERATOR WAS RESET, AND CAME BACK ONLINE EACH TIME. THE LT ENGINE LOWER COWL WAS OSDR 17GR201602080001Probe · departedPILOTS REPORTED THAT AS FUEL WAS BURNED THE LEFT QUANTITY WOULD STOP SHOWING BURN AT AROUND 2300 AND THE RIGHT SIDE WOULD CONTINUE TO SHOW FUEL BURNED. AS THE RH SIDE SHOWED ABOUT 1100 THE LEFT WOULD DRIFT DOWN TO 1100. SYSTEM FUNCTIONED NORMAL ABOVE AND BELOWSDR DXTA2016022606190Engine · unserviceableCLIMBING THROUGH 11,000', THE MASTER WARNING LIGHT FLASHED & THE RT LOW OIL PRESS ANNUNCIATOR ILLUMINATED. THE RT OIL PRESS TAPE WAS AT ZERO, LESS THAN 5 SECONDS. CREW GOT OUT CHECKLIST, BUT RT OIL PRESS RETURNED TO NORMAL AFTER POWER WAS REDUCED. NO VISIBSDR O2GA2016020151401Control Unit · inoperativeAFTER TAKEOFF, THE GEARS WOULD NOT RETRACT. DIVERTED, GREEN INDICATION 3 THE WHOLE TIME. LANDING WAS UNEVENTFUL. ACFT WAS FERRIED FOR MX. REPLACED THE LG CONTROL, PERFORMED GEAR SWINGS & NO DEFECTS WERE NOTED. ACFT WAS RTS.SDR CA160203001Engine · overtemp(CAN) AT TAKEOFF POWER APPLICATION, THE RT ENGINE OIL PRESSURE SPIKES ABOVE RED AND THEN SLOWLY LOWERS TO NORMAL RANGE. THE RT ENGINE THRUST SPIKE WAS CAUSING YAW TO LEFT. BOTH THROTTLES WERE MOVED TOGETHER AND THE LT ENGINE ITT WENT SOLID RED BAR DURING CLISDR DXTA2016012406172Steering Sys · corrodedAFTER DEPARTURE THE LG UNLOCK LIGHT REMAINED ON. DURING CLIMB OUT THE HYD PRESS LIGHT REMAINED ILLUMINATED. COMPLETED THE LG WILL NOT RETRACT CHECKLIST. LG EXTENDED NORMALLY. JACKED ACFT & PERFORMED GEAR OPERATIONAL CHECKS, NO PROBLEMS FOUND. SLIGHTLY TURSDR DXTA2016012400171Actuator · corrodedNOSE GEAR WOULD NOT STAY RETRACTED. JACKED ACFT & CHECKED DIMENSION ON NOSE STRUT. SWING GEAR SEVERAL TIMES COULD NOT DUPLICATE AT THIS TIME. INSP NLG UPLOCK ASSY & FOUND TO BE BINDING. REMOVED UPLOCK ACTUATOR & FOUND ALL COMPONENTS ATTACHED TO ACTUATOR SHSDR CA160203012Engine · malfunctioned(CAN) DURING CRUISE AT FL430, A SUDDEN AND STRONG VIBRATION WAS FELT AND THE MASTER CAUTION CAME ON INDICATING LT ENGINE VIBRATION. THE WAS ACCOMPANIED BY A RAPID RISE IN OIL PRESSURE. THE ENGINE POWER WAS RETARDED, VIBRATIONS LEVEL REDUCED BY THE OIL PRESSUSDR O2GA2016012451502Switch · out of adjustFLAPS FAILED TO RETRACT AFTER LANDING. ADJUSTED THE 35 DEGREE FLAP SWITCH TO SPECIFICATIONS. A SUCCESSFUL OPERATIONAL CHECK FLIGHT WAS PERFORMED. ACFT WAS RTS.SDR O2GA2016012451401Actuator · defectiveVIBRATION FELT IN FLOOR & YOKE STARTING AT FL180, 250 KNOTS. AT CRUISE FL 410 & 410 LESS VIBRATION. R & R RUDDER TRIM TAB ACTUATOR & NLG SPADE DOOR HARDWARE. SUCCESSFUL OPERATIONAL CHECK FLIGHT WAS PERFORMED. ACFT WAS RTS.SDR DXTA2016012306168Fan · failedWHILE SITTING IN COCKPIT PRIOR TO ENGINE START, HEARD AN AUDIBLE POP WITH SIMULTANEOUS INDICATIONS OF THE RADOME FAN CAUTION LIGHT, FLASHING MASTER CAUTION, BOTH PFDS, MFD & FMS WENT BLANK BUT WERE BACK LIT. 45 SECONDS LATER A LOUD BUZZING NOISE CAME ACROSS SDR O2GA2016012051501Control Valve · inoperativeAFTER LANDING FLAPS WOULD NOT RETRACT. REPLACED THE FLAP CONTROL VLV. A SUCCESSFUL OPERATIONAL CHECK FLIGHT WAS PERFORMED. ACFT WAS RTS.SDR CA160121008Oil System · erratic(CAN) DURING CRUISE THE LT OIL PRESSURE GAUGE STARTED ACTING ERRATICALLY AND SPIKING UP TO THE RED LINE BEFORE FALLING ALTOGETHER. THE CREW RAN THE APPROPRIATE CHECKLIST AND DECIDED TO MAKE A PRECAUTIONARY LANDING.SDR DXTR2016012002Cable · frayedTOP ELEVATOR TRIM FORWARD CABLE UNDER CENTER PEDESTAL IS FRAYED. R & R FWD ELEVATOR TRIM CABLES IAW MM 27-32-02. CABLE ASSEMBLY CONSISTS OF CABLE, PN: 6660002-33, CABLE PN: 6660002-34, AND CHAIN, PN: S2295P25-249.SDR O2GA2016011450702Actuator · defectiveCLIMBING THROUGH FL370, PITCH TRIM ANNUNCIATOR ILLUMINATED. DISCONNECTED AUTOPILOT & MANUAL TRIM WAS INOPERATIVE. EMER CHECKLIST FOLLOWED, DIVERTED. ON DESCENT 10,000 FT, TRIM WORKED NORMAL. LANDING WAS UNEVENTFUL. REPLACED THE LT & RT ELEVATOR TRIM ACTUASDR O2GA2016011350101Hinge Pin · backed outAIRCRAFT HAS BAD VIBRATION THROUGH YOKE & RUDDER PEDALS. VIBRATION GETS MUCH WORSE WITH INCREASE IN AIRSPEED. POWER SETTINGS MODE MADE NO DIFFERENCE. TROUBLE SHOT THE DISCREPANCY TO A DEFECTIVE RUDDER LOWER TRIM TAB HINGE PIN THAT BACKED OUT CAUSING THE VIBSDR O2GA2016011350701Actuator · lack of lubeDESCENDING OUT OF FL390, PITCH TRIM ANNUNCIATOR ILLUMINATED. FOLLOWED CHECKLIST, TURNED OFF AUTOPILOT. UNABLE TO TRIM ACFT USING MANUAL & ELEC PITCH TRIM. WENT TO LOWER ALTITUDE 12,000 FEET & MANUAL & ELEC PITCH TRIM & AUTOPILOT OPERATED NORMAL. LANDING WASDR DXTA2016011106160Unknown · odorAT FL300 STRONG SMELL OF KEROSENE WITH EYEBALL VENTS OPEN IN COCKPIT. CREW HAD TO DON OXYGEN MASKS. TROUBLESHOT, RAN APU & BOTH ENGS WITH BLEEDS ON INDEPENDENTLY, COULD NOT DUPLICATE DISCREPANCY. R & R CONDENSER SOCK, INSPECTED, CLEANED & DRIED AT DUCTS. RSDR DXTR2016012001Cable · frayedFOUND FORWARD ELEVATOR TRIM CABLES FRAYED. R & R FWD ELEVATOR TRIM CABLES IAW MM 27-32-02. CABLE ASSEMBLY CONSISTS OF CABLE, PN: 6660002-33, CABLE, PN: 6660002-34 AND CHAIN, PN: S2295P25-249.SDR YRJR20160128001Wheel · crackedPILOT REPORTED THAT THE PITCH TRIM WHEEL WAS OUT OF RIG WITH THE TRIM INDICATOR. INSPECTED TRIM WHEEL AND FOUND THAT IT WOULD NOT MOVE FULL TRAVEL. REMOVED TRIM WHEEL AND FOUND THE GROOVE FOR THE INDICATOR HAD A BROKEN OUT AREA.SDR 2016FA0000020Track · brokenAIRCRAFT PITCH TRIM WHEEL HAS SPIRAL GROOVE THAT INDICATOR RIDES IN TO DISPLAY PITCH TRIM POSITION. WHEEL TRACK BROKE AND ALLOWED FOD TO INHIBIT WHEEL MOVEMENT DUE TO BEING JAMMED WITH INDICATOR. INDICATOR JUMPED TRACKS AND GAVE ERRONEOUS INDICATION TO CREW RSDR DXTA2016010806158Light · inoperativeBURNING SMELL COMING FROM INSIDE PAX DOOR. STRONG ENOUGH TO BE SMELLED IN THE COCKPIT. SUSPECT BURNING SMELL IN PASSENGER DOOR WAS LOWER AFT STEP LIGHT HAVING BURNT OUT. BULB WAS REPLACED. RAN APU AND ENGINES WITH NO SMELL IN COCKPIT OR CABIN. POWER WAS OSDR DXTA2016010806156Vent · obstructedDURING POST FLIGHT, ALL EXTERNAL LIGHTS WERE SHUT DOWN WHILE WALKING AROUND THE ACFT DOING THE LIGHT CHECK. WHEN WALKING INTO THE AIRPLANE, THERE WAS A NOTICEABLE ELEC BURNING SMELL IN THE CABIN WITH THE BURNING SMELL GETTING WORSE TOWARDS THE COCKPIT. AN EMSDR CWQR20160106001Attach Bracket · crackedDURING SCHEDULED INSPECTION, FOUND THE RT FWD AVIONICS SHELF ATTACHED BRACKET CRACKED. REPLACED WITH NEW.SDR CA160119015Oil System · pressure loss(CAN) CLIMBING OUT THROUGH 14,000 FT, THE RT ENGINE OIL PRESSURE ANNUNCIATOR ILLUMINATED AND THE OIL PRESSURE INDICATION WENT TO ZERO. THE PILOT RETARDED THE THROTTLE AND PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN. THE ACFT LANDED UNEVENTFULLY. DURING TROUBLESDR DXTA2016010406154Engine · failedCLIMBING OUT THROUGH 14000 FT, RT OIL PRESS ANNUNCIATOR ILLUMINATED & THE OIL PRESS INDICATION WENT TO ZERO. RETARDED THE THROTTLE & PERFORMED A PRECAUTIONARY ENG SHUTDOWN. LANDED UNEVENTFULLY. ON POST FLIGHT OIL DRIPPING FROM COWLING. SOME OIL STILL IN SISDR DXTA2016010406151Probe · faultyDURING CLIMB AROUND 8,000 FT, THE MASTER WARNING LIGHT ILLUMINATED WITH NO INDICATION WHY. IT WAS RESET & IT ILLUMINATED AGAIN WITH A BATTERY OVER TEMP ABOVE 160 FLASHING ANNUNCIATOR LIGHT. THE MASTER WARNING LIGHT REPEATEDLY ILLUMINATED AFTER BEING RESET. SDR ZESA20160104001Ahrs · failedTHE ACFT TOOK OFF & WHILE IN CRUISE THE COPILOTS AHRS FAILED, CAUSING THE LOSS OF HEADING & ATTITUDE, THE REVERSIONARY SYS WAS USED. THE PILOTS MADE THE DECISION TO DIVERT & A TECHNICIAN WAS DISPATCHED TO THE ACFT & IT WAS DETERMINED TO BE A FAULTY AHRS UNIT.SDR ZESA20160102001Squat Switch · frozenAFTER TAKEOFF THE ACFT DID NOT PRESSURIZE PROPERLY, THE PILOTS ATTEMPTED TO RESET THE PRESSURIZATION CONTROL SEVERAL TIMES THEN THE DECISION WAS MADE TO DIVERT FOR MAINTENANCE. A TECHNICIAN WAS DISPATCHED TO THE ACFT & ICY SLUSH WAS FOUND ON THE LG SQUAT SWITSDR DXTA2016010406149Brake Cable · brokenLEFT BRAKE PEDAL ON LT SEAT HAS NO PRESSURE. LT WEAR PIN WILL MOVE WHEN LT BRAKE ON THE RT SEAT IS PRESSED. FOUND PILOT'S LT MIDDLE BRAKE CABLE BROKEN. R & R CABLE WITH NEW IAW MM 32-44-10. RIGGED & SAFETIED CABLE, TAXI CHECKED GOOD AT THIS TIME.SDR DXTA2015122306143Rheostat · failedIN FLIGHT CREW NOTICED RT SIDE MAP LIGHT WOULD NOT EXTINGUISH. ON APPROACH TO DESTINATION CREW SMELLED AN ELEC SMOKE ODOR. CB RT PANEL, LT SIDE LIGHTS, POPPED & ODOR WENT AWAY. DID NOT RESET CIRCUIT BREAKER. REMOVED RT CB PANEL & FOUND CHART LIGHT RHEOSTATSDR DXTA2015122306142Horn · failedON TAKEOFF EXPERIENCED VIBRATION THAT WAS PRESENT IN BOTH YOKE & PEDALS. SEEMED TO INTENSIFY WITH INCREASED POWER & PITCH. CONTINUED THRU FL 230 BEFORE DECIDING TO DIVERT. DID NOT SEEM TO BE AS PRONOUNCED IN DESCENT. REMOVED RUDDER HORN ASSEMBLY. INSPECTSDR CA151229010Engine · malfunctioned(CAN) WHILE CLIMBING OUT AT APPROXIMATELY 4000 FT WITH THRUST SET IN THE CLIMB DETENT, THE LT ENGINE EXPERIENCED A REDUCTION IN THRUST IN CONJUNCTION WITH LT ELECTRONIC ENGINE CONTROL ANNUNCIATION. THE PILOT ELECTED TO DO A DIVERSION AND LANDING AT HOME BASE.SDR CA151228005Oil System · low pressure(CAN) DURING CLIMB, THROUGH FL100, THE NR 2 ENGINE OIL PRESSURE DROPPED TO ZERO WITH ACCOMPANYING INDICATOR, WARNING LIGHTS. THE PILOT RETARDED THE POWER TO IDLE AND RECEIVED NO SECONDARY WARNINGS. RETURNED ACFT TO THE DEPARTURE AIRPORT WHERE AN UNEVENTFUL LSDR CA151228004Lever · out of adjust(CAN) DURING PRE-FLIGHT CHECKS WHILE ON THE TAXIWAY, THE PILOT DEPLOYED THE THRUST REVERSERS FOR TESTING, THE RT ENGINE SHUTDOWN. TROUBLESHOOTING ONGOING AND WILL INCLUDE CHECKING THE ENGINE RIGGING SINCE THE DATA DOWNLOAD SHOWED A VERY LOW THROTTLE LEVER ANGSDR CA151228002Oil System · pressure loss(CAN) DURING CLIMB, THE LT ENGINE LOW OIL PRESSURE WARNING LIGHT CAME ON. THE CREW RETARDED THE THROTTLE AND THE LIGHT WENT OUT, 30 SECONDS LATER THE RT ENGINE LOW OIL PRESSURE LIGHT CAME ON, THROTTLE WAS RETARDED AND LIGHT WENT OUT. ALL INDICATIONS LOOKED NOSDR DXTA2015120306135Warning Light · false activationFIRE BOTTLE LOW INDICATOR CAME ON INFLIGHT AT FL380, STAYED ON THROUGH FL240. REMOVED BOTTLES, WEIGHED BOTTLES, FWD BOTTLE WEIGHED 7.05 POUNDS, LAST CHARGED IN 10 2015 & WEIGHED 7.06 POUNDS. AFT BOTTLE WEIGHED 7.00 POUNDS, LAST CHARGED 3 2014 & WEIGHED 7.06SDR O2GA2015121050101Unknown · malfunctionedAFTER TAKEOFF THE FLAPS WOULD NOT RETRACT TO 0*. DURING FLIGHT ALL OTHER HYD SYS WORKED. ACFT DIVERTED BACK & AFTER LANDING THE FLAPS WOULD NOT RETRACT TO 0*. ON POST FLIGHT NOTICED FLAP STUCK IN 7* POSITION. ACFT WAS INSPECTED & FERRIED WITH THE FLAPS AT SDR DXTA2015111306132Uplock Switch · out of adjustNOSE GEAR DID NOT COME UP. RED UNLOCK LIGHT ILLUMINATED. GEAR HANDLE WAS PLACED DOWN PRODUCING 3 GREEN LIGHTS. INSPECTED LG SYS FOR VISIBLE DEFECT, NONE NOTED. JACKED ACFT & PERFORMED SEVERAL GEAR SWINGS AT VARIOUS PRESS SETTINGS & SLOW RATES, NO DEFECTS NSDR DXTA2015111306131Control Wheel · out of adjustELEVATOR TRIM WHEEL IS LOOSE, ELEVATOR TRIM IS JAMMED & WILL NOT MOVE AFT OF MID TAKEOFF RANGE ELECTRICALLY OR MANUALLY. INSPECTED ELEVATOR TRIM AFT CABLE RUN, NO DEFECTS NOTED IAW AMM 27-32-02. INSPECTED TRIM HAND WHEEL & FOUND THE TRIM POINTER OUT OF ADJUSDR O2GA2015112350701Lock Tab · brokenDEPARTED WE EXPERIENCED A STAB MISS COMPARE, HYD PRESS, & GEAR UNLOCK LIGHT. FOLLOWED EMER CHECKLIST. GEAR EXTENDED & STAB MISS COMPARE LIGHT REMAINED ILLUMINATED. A DIVERSION WAS MADE FOLLOWED BY AN UNEVENTFUL LANDING. EMER SERVICES ESCORTED ACFT SERVICE C
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