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 DXTA2013032105327Apu · seizedAFTER LANDING AT DESTINATION, STARTED APU DURING TAXI IN. START NORMAL AND GENERATOR LOADED. AFTER 20 SECONDS, A HARD THUMP AND APU DROPPED OFF LINE. SMELLED ELECTRICAL FUMES IN IN MAIN CABIN. SECURED APU. APU WAS SEIZED. ATTEMPTED TO CONNECT WITH LAPTOPSDR DXTA2013032005325Apu · smokeWITH APU RUNNING ON ENGINE START, CABIN FILLED WITH SMOKE. SHUTDOWN ENGINES AND APU, LATER STARTED APU AND CABIN FILLED WITH SMOKE, APU SHUTDOWN BY ITSELF. STARTED RT ENGINE AND SMOKE CAME INTO CABIN AGAIN, SHUTDOWN RT ENGINE. CHECKED APU OIL AND BOTH LIGSDR DXTA2013031805318Relay · inoperativeBRAKE FAILURE AFTER LANDING WHILE TAXIING TO THE FBO. STOPPED ACFT USING EMERGENCY BRAKES. PERFORMED SATISFACTORY RINGOUT OF HIGH PRESSURE SWITCH FOR ANTI-SKID CONTROL MOTOR PUMP WITH PRESSURE AND WITHOUT PRESSURE ON THE SYSTEM. VERIFIED BRAKE CONTROL MOTORSDR Z5FA2013031557701Powerpack · defectiveDURING TAXI OUT, CREW OBSERVED POWER BRAKE-ANTI-SKID WARNING ANNUNCIATION CREW UTILZED PNUEMATIC EMERGENCY BRAKES TO STOP. ACFT TOWED TO LOCAL FBO FOR INSPECTION/REPAIRS. ACFT PERSONNEL TRAVELED TO LOCATION AND TROUBLESHOT TO DEFECTION BRAKE POWERPACK ASSY. SDR DXTA2013031505317Motor · failedAFTER ENGINE START LOW BRAKE PRESSURE ANNUNICATOR CAME ON. I RESET THE "PWR BRKS" CB IAW THE CHECKLIST. WE ATTEMPTED TO TAXI, BRAKE PEDALS WENT TO THE FLOOR. RED EMERGENCY HANDLE WAS PULLED TO STOP THE ACFT. . TROUBLESHOT TO AND REPLACED POWER BRAKE SYS HYDSDR DXTA2013031105316Tank · overheatedON PREFLIGHT THE WATER SYS CIRCUIT BREAKER WAS BLOWN. WHEN PUSHED BACK IN SMOKE BILLOWED FROM THE LAV SINK IMMEDIATELY. BREAKER WAS PULLED OUT WITHIN 5 SECONDS AFTER SMOKE STARTED. INSPECTED WATER TANK, SWITCH, CIRCUIT BREAKER AND SOLENOID. NO EVIDENCE OFSDR DXTA2013031105314Fire Loop · false indicationON FINAL APPROACH THE LT FIRE DETECT LIGHT ILLUMINATED ON AND OFF. THEN, THE LT ENGINE FIRE LIGHT ILLUMINATED, BUT THE FIRE DETECT LIGHT LIGHT WENT OUT. IAW FOLLOWING THE ENGINE FIRE CHECKLIST, THE LEFT ENGINE FIRE SWITCH WAS PUSHED AND BOTH WHITE BOTTLE LIGSDR DXTA2013031105313Motor · failedON SHORT FINAL, POWER BRAKES CIRCUIT BREAKER TRIPPED AND ANTI-SKID WARNING LIGHT ILLUMINATED. COMPLIED WITH QRH AND LANDED. R & R THE POWER BRAKE MOTOR. PERFORMED BLEED AND OPS CHECK OF BRAKE SYSTEM. OPS CHECK GOOD IAW MM 32-44-00 AND MM 32-44-20.SDR DXTA2013030605308Actuator · malfunctionedAILERON TRIM FROZE IN FLIGHT. UNABLE TO MOVE AIERLON TRIM ON CLIMB OUT. AFTER ON GROUND. REPORTED AILERON TRIM OK. REMOVED AILERON TRIM ACTUATOR AND INSTALLED NEW IAW MM 27-11-03. DUE RIGGED TRIM CABLES TO 20 LBS IAW MM 27-10-00. INSTALLED LT AILERON IAW SDR DXTA2013030505307Downlock Switch · inoperativeAFTER SELECTING MLG HANDLE TO DOWN POSITION. RECEIVED A RT MLG UNSAFE INDICATION. RAN CHECKLIST, UNSAFE INDICATION REMAINED. (RED UNSAFE LIGHT) A GREEN NOSE AND LT MAIN LIGHTS ON WITH NO RT MAIN LIGHT. LIGHT TESTED GOOD. WHEN FLAPS WERE SELECTED PAST 15, SDR DXTA2013030405304Uplock Switch · inoperativeNOSE GEAR DID NOT RETRACT AFTER TAKEOFF. GREEN NOSE GEAR LIGHT ON AND RED GEAR UNLOCK LIGHT ON. NO OTHER INDICATIONS. SELECTED GEAR DOWN GOT ALL 3 GREEN DOWN AND LOCKED AND NO RED AND LANDED. JACKED ACFT. RETRACTED GEAR, FOUND NLG WOULD PARTIALLY RETRASDR DXTA2013030405303Bearing · worn230 KNOTS IN A CLEAN CONFIGURATION THE PLANE STARTING TO VIBRATE THROUGH THE YOKE AND RUDDER PEDALS. R & R RUDDER AND ELEVATOR TRIM TAB CONTROL HORN BEARING AND BOLTS IAW MM 20-10-08. PERFORMED FREE PLAY CHECKS IAW MM 27-90-30. OPS CHECKED GOOD.SDR DXTA2013030105301Starter Gen · failedDURING PREFLIGHT THE APU WAS STARTED AND THE THE BLEED AIR WAS SELCTED ON. AFTER ABOUT 1MIN THE CABIN BEGAN TO FILL FULL OF SMOKE. BLEED AIR WAS SELECTED OFF AND APU WAS SHUTDOWN. RAN BOTH ENGINES WITH PRESSURE SOURCE SELECTOR IN BOTH, LT, RT AND OFF AND COUSDR DXTA2013022505296Unknown · odorIMMEDIATELY AFTER TAKEOFF, NOTICED A VERY STRONG ODOR IN THE COCKPIT ACCOMPANIED BY A SLIGHT HAZE. THE ODOR SMELLED MORE LIKE AN OIL THAN ELECTRICAL. RETURNED TO AIRPORT. ODOR DID NOT DISSAPATE, BUT DID NOT GET WORSE THAN INITIALLY NOTICED. INSPECTED APU INLSDR DXTA2013022505295Actuator · damagedAPPROXIMATELY ONE MINUTE AFTER TAKEOFF THE TRIM WHEEL FROZE. NEITHER THE ELECTRIC TRIM OR MANUAL PRESSURE WOULD MOVE THE WHEEL. PUT MORE FORCE INTO MOVING THE WHEEL MANUALLY THAN NORMAL AND THE WHEEL BROKE LOOSE AND ALL TRIM FUNCTIONS RETURNED TO NORMAL. TRSDR DXTA2013022505292Trim System · frozenAPPROXIMATELY ONE MINUTE AFTER TAKEOFF THE TRIM WHEEL FROZE. NEITHER THE ELECTRIC TRIM OR MANUAL PRESSURE WOULD MOVE THE WHEEL. PUT MORE FORCE INTO MOVING THE WHEEL MANUALLY THAN NORMAL AND THE WHEEL "BROKE LOOSE" AND ALL TRIM FUNCTIONS RETURNED TO NORMAL. SDR DXTA2013021805291Uplock Switch · out of adjustAFTER TAKEOFF LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AS WELL AS THE HYD PRESS ON LIGHT AND THE STAB MISCOMPARE LIGHT. RESETTING THE HYD PRESS CIRCUIT BREAKER CAUSED A THUMP SOUND AS THE GEAR COMPLETED RETRACTING AND ALL THE WARNING LIGHTS EXTINGUISHEDSDR DXTA2013021405285Actuator · stuckDURING DESCENT, ELEVATOR TRIM STUCK IN THE NOSE DOWN POSITION. COULD NOT MOVE THE ELEVATOR EITHER MANUALLY OR ELECTRICALLY. REMOVED LT AND RT ELEVATOR TRIM TAB ACTUATORS AND INSTALLED NEW ACTUATORS. C/W RIGGING, TENSION, SAFTEY, AND TRAVEL CHECKS. ALL CHECKSDR Z5FA2013021351401Rmu · defectiveWHILE ENROUTE, NR 2 RADIO DISPLAY UNIT FROZE AND CREW WAS UNABLE TO CHANGE COMM 1 OR COMM 2 FREQUENCIES USING RDU 1 OR RDU 2 AND STANDBY OR FMS TUNE BUTTON. CREW WAS ABLE TO STAY IN CONTACT WITH ATC USING 121.5. CREW ELECTED TO DIVERT. ACFT LANDED UNEVENTFULSDR DXTA2013021205282Threshold · crackedMAIN ENTRY DOOR THRESHOLD IS CRACKED. REPLACED CRACKED THRESHOLD WITH NEW INNER THREASHOLD. WORK ACCOMPLISHED PER SRM 51-30-03, 51-30-06, 51-40-09.SDR DXTA2013020705277Control Valve · inoperativeBOTH RUDDER PEDALS ARE IMMOVABLE DURING FLIGHT. DURING FLIGHT IN ALL PHASES, IN ALL POWER SETTINGS, NEITHER PILOT IS ABLE TO MOVE THE RUDDER PEDALS AT ALL. AUTO PILOT AND YAW DAMP WAS CONFIRMED OFF. RUDDER BOOST CHECK ON GROUND CHECKED OK. PEDALS WORK CORRESDR DXTR20130207001Rib · crackedRT WING INBD FLAP, INBD T/E RIB IS CRACKED AT WS 64.073. COMPLIED WITH WING T/E RIB CRACK REPAIR IAW SRM 57-60-00 FOR RT INBD FLAP WELL RIB T/E.SDR DXTR20130206002Rib · crackedLT INBD FLAP INBD RIB CRACKED AT WS 64.073. COMPLETED REPAIR OF WING T/E RIB CRACKS IAW SRM 57-60-00 FOR LT INBD FLAP WELL RIB T/E.SDR DXTR20130206001Web · crackedMAIN CABIN DOOR STRUCTURE CRACKED UNDER INTERIOR DOOR HANDLE. REMOVED IDENTIFIED DAMAGED AREA AND COMPLETED WEB REPAIR IAW SRM 52-10-00.SDR CA130212012Oil System · low pressure(CAN) DURING REVENUE FLIGHT, ON CLIMBOUT, THE CREW OBSERVED THE LOW OIL PRESSURE WARNING LIGHT AND THE OIL PRESSURE INDICATION DROPPED TO ZERO. THE PRESSURE RECOVERED, DROPPED TO ZERO AGAIN AND ONCE AGAIN RECOVERED WITH NO FURTHER ISSUES. THE CREW ELECTED TO SDR DXTA2013020405268Actuator · failedLANDING GEAR WOULD NOT RETRACT. UPON SELECTING THE GEAR HANDLE TO UP GEAR RETRACTION COMMENCED BUT PILOTS DID NOT HEAR THE NORMAL SOUND OF THE GEAR HITTING AND LOCKING ON THE UPLOCKS. THE RED UNLOCK LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED NOSE LANDISDR CWQR20130131001Pressure 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. THIS CONDITION HAS BEEN REPORTED TO MFG UNDER SDR 647960.SDR 9JLA2013020504482Solenoid · defectiveCREW REPORTED THAT THE CABIN DOOR ANNUNCIATOR REMAINS ILLUMINATED, AGAIN. AIRCRAFT HAS HAD 5 DOOR SOLENOIDS INSTALLED IN THE PAST 12 MONTHS. DEFECTIVE SOLENIOD, NEW SOLENIOD INSTALLED IAW THE MM 52-10-00.SDR DGCA2012013113038Tire · separatedRIGHT MLG TIRE TREAD SEPARATED, BUT DID NOT GO FLAT. TREAD WHIPPED AROUND AND PUNCTURED THE FLAP, DAMAGED THE FAIRING BETWEEN THE REAR SPAR AND FLAP LEADING EDGE, BENT THE MAIN GEAR DOOR ATTACH ROD, BROKE A BONDING BRAID, DAMAGED THE WIRE BUNDLE PROTECTIVE COSDR DXTA2013013005266Connector · dirtyFLAPS WOULD NOT EXTEND WHEN FLAP LEVER MOVED TO ANY FLAPS DOWN POSITION. HYD PRESS LIGHT REMAINED ILLUMINATED UNTIL FLAP LEVER PLACED BACK TO THE FLAPS UP POSITION. VERIFIED PROPER RIGGING OF FLAP UP AND DOWN CONTROL SWITCHES AND FOLLOW-UP CABLE. CLEANED FLSDR DXTA201301305266Unknown · smokeCOCKPIT PAC TEMPERATURE WAS UNCONTROLLABLE WHILE ON THE GROUND. COCKPIT FILLED WITH BLUEISH WHITE SMOKE BEFORE COCKPIT PAC WAS SECURED. COCKPIT SUPPLY TEMP INDICATED 234 BEFORE PAC WAS SECURED. INSPECTION OF PAC OIL SIGHT CUP INDICATES BLACK OIL.SDR CA130212003Engine · failed(CAN) DURING CLIMBING THRU 18000`, THE ANTI-ICE TURNED OFF. THE CREW HEARD A LOUD NOISE FOLLOWED BY MULTIPLE NOISES WITH VIBRATION AND A MOMENTARY ODOR OF SMOKE THRU THE ENVIRONMENTAL SYS. THE CREW NOTICED THE LT ENGINE ITT WAS IN THE RED. THE CREW DECLARED SDR DXTA2013012905264Apu · smokeDURING "BEFORE START" CHECKLIST AND WHILE STARTING THE APU, SMOKE WAS NOTICED IN THE CABIN. THE APU HAD COMPLETED IT'S START SEQUENCE AND THE APU GENERATOR WAS "ON". THE "BLEED AIR" SWITCH WAS NOT ON. SHUT OF THE APU AND SHUT OFF THE THE REST OF THE EQUIPMENTSDR DXTA2013012805263Engine · shutdownCLIMBING THRU 18,000' AND JUST TURNED ANTI-ICE OFF, WE HEARD A LOUD BANG FOLLOWED BY MULTIPLE BANGS, WITH VIBRATION AND A MOMENTARY SMELL OF SMOKE THRU THE ENVIROMENTAL SYS. LEFT ENG ITT WAS IN THE RED WITH NO OTHER ENG PARAMETERS NOTED TO BE IN THE RED. WE SSDR DXTA2013012305258Uplock Switch · failedAFTER TAKEOFF, BROUGHT GEAR UP AND NOTICED A THUMPING SOUND LIKE A TIRE HITTING SOMETHING SPINNING DOWN, SAW THE HYDRAULIC ANNUNCIATOR FLASHING ON AND OFF, WITH THE RED GEAR UNLOCK LIGHT ALSO FLASHING ON AND OFF. ALL THREE GREEN GEAR LIGHTS WERE OUT. EXTENDEDSDR DXTA2013012305257Bolt · shearedNOSE WHEEL WOBBLING AFTER ONLY 100 YARDS OF TAXIING FROM THE BLOCKS. 3 BOLTS HOLDING THE SHIMMY DAMPENER TO THE STEERING ARE SHEARED OFF. INSPECTED NOSE GEAR AND FOUND STEERING GEAR BOLTS SHEARED OFF. INSPECTED OTHER COMPONENTS, NO OTHER DEFECTS NOTED. REMOSDR DXTA2013012305256Actuator · malfunctionedAFTER TAKEOFF AND COMPLETING GEAR UP AND FLAPS CALL, WARNING LIGHT ILLUMINATED DUE TO STAB MISCOMPARE, AND HYD PRESSURE LIGHT ILLUMINATED. RED GEAR UNSAFE LIGHT ILLUMINATED. CREW RAN CHECKLISTS FOR STAB MISCOMPARE AND THEN GEAR. LEFT MAIN DROPPED WHEN HYD CSDR 2013FA0000152Drain · leakingWHILE PERFORMING DOCUMENT 45, TASK 34-90-10-210, FOUND STANDBY STATIC SYS LEAKING AT A RATE OF 211 FT/MIN. INSPECTED SURROUNDING CONNECTIONS WITH NO NOTICEABLE DEFECTS NOTED. CONNECTED ADC TESTER AND CONFIRMED LEAK RATE OF 200-250 FT/MIN. FOUND ELBOW FITTSDR 2013FA0000151Bolt · seizedAFT APU MOUNT LINK, BOTTOM ROD END AND BOLT SHOWING SIGNS OF CORROSION. FOUND BOLT SEIZED WITH ROD END BEARING, USE KROIL, AND HEAT GUN TRIED TO REMOVE BOLT SEVERAL TIMES WITH NO SUCCESS. CONTINUED USING KROIL AND USED C-CLAMP TO LOOSEN BOLT, BROKE C CLAMP. SDR 9JLA2013020504481Solenoid · defectiveCREW REPORTED THAT THE CABIN DOOR ANNUNCIATOR REMAINS ILLUMINATED, AGAIN. ACFT HAS HAD FOUR DOOR SOLENIODS INSTALLED IN THE PAST TWELVE MONTHS. DEFECTIVE SOLENOID, PN 6711335-1, NEW SOLENOID INSTALLED IAW THE MM 52-10-00.SDR DXTA2013012205253Seal · failedBOTH ENGINE FIRE WARNING LIGHTS ILLUMINATED WHEN THROTTLES WERE MOVED FROM CRIUSE DETENT TOWARDS A LOWER POWER SETTING. THE LIGHTS ILLUMINATED FROM TOP OF DECENT UNTIL 3,000 FT WHEN THE THROTTLES WERE MOVED OUT OF THE IDLE POSITION. LIGHTS REMAINED OUT FOR RSDR DXTA2013012105250Uplock Hook · failedAFTER TAKEOFF AND SELECTING GEAR UP, RED "UNSAFE" AND AMBER "HYD PRESS" LIGHT REMAINED ILLUMINATED. AFTER APPROX 1-2 MINUTES A LOUD THUMP WAS HEARD FROM THE LT MAIN GEAR. THE "HYD CONTROL" CIRCUIT BREAKER WAS PULLED IAW ABNORMAL CHECKLIST PROCUDURE. WHEN CISDR DXTA2013011805249Pulley · damagedDURING CLIMB OUT, ACFT SUDDENLY PITCHED NOSE DOWN. ON DETECTING THE PITCH CHANGE, AUTOPILOT WAS DISENGAGED. CONTROLS WERE DIFFICULT TO MOVE ALONG VERTICAL AXIS AND EACH CONTROL INPUT REQUIRED EXCESSIVE FORCE TO PITCH THE ACFT IN A CLIMB OR DESCENT. CONTROL SDR DXTR20130118003Bracket · crackedRUDDER AUTO/PILOT SERVO CABLE BRACKET IS CRACKED. R & R RUDDER AUTO/PILOT SERVO CABLE BRACKET IAW SRM 51-40-03.SDR DXTA2013011405244Pump · failedON LANDING, LEFT SKID WAS CYCLING ON A DRY RUNWAY WITH NORMAL APPLICATION. BRAKES SEEMED TO GRAB A LITTLE. UPON EXITING THE RUNWAY THE BRAKES FAILED. THE LOW BRAKE PRES AND SKID ANNUNICATOR ILLUMINATED. WE APPLIED THE EMERGENCY BRAKES CLEARED THE RUNWAY ANSDR DXTA2013020605273Uplock Switch · faultedON CLIMB OUT, AFTER LANDING GEAR AND FLAPS WERE UP, RECEIVED AN UNSAFE GEAR INDICATION FOLLOWED SHORTLY BY A FLASHING HYD PRESSURE AND STAB MISCOMPARE ANNUNCIATOR. RAN CHECKLISTS, PUT GEAR AND FLAPS DOWN NORMALLY AND RETURNED TO LAND. CONTROL PRESSURES INDICSDR DXTR20130118004Support · crackedRT WING TO FUSELAGE FAIRING ANGLE SUPPORT CRACKED IN SEVERAL SPOTS. R & R RT AFT STRAP (PN 6610146-20-1) IAW SRM 51-40-03.SDR DXTA2013011005241Apu · failedWITH APU ON AND BLEED AIR FOR APROX 10 MINUTES, COCKPIT FILLED WITH SMOKE, SMOKE STARTED IN THE COCKPIT AND MOVED BACK INTO THE CABIN. ALL THIS HAPPENED ON THE GROUND WITH MAIN CABIN DOOR OPEN. R & R THE APU IAW MM 49-10-00. OPS AND LEAK CHECKS GOOD.SDR DXTA2013010805239Valve · inoperativeAT HIGH POWER SETTINGS THE RUDDER COULD NOT BE USED. LEFT RUDDER PEDAL WAS STIFF AND COULD NOT BE PRESSED. R & R RUDDER BIAS CONTROL VALVE, REMOVED PN 5307-1, SN 1763C. WOULD NOT PASS OPS CHECK, ANNUNCIATOR WOULD NOT COME ON WHEN BREAKER PULLED BUT WOULD COSDR DXTA2013010805237Actuator · intermittentSELECTED GEAR DOWN FOR LANDING. TWO MAINS IMMEDIATELY DROPPED BUT THE NOSE DID NOT COME DOWN. RECEIVED A RED UNLOCK LIGHT, AND NO INDICATION ON THE NOSE WHEEL. 180 KTS WITH FLAPS 15 AND STAB ALREADY IN POSITION. ALL HYD INDICATIONS WERE NORMAL. NOSE WHEEL
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