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 3EJA201612220001Uplock Switch · unserviceableAFTER T/O, WHILE CLIMBING TO 2000' THE THREE GREEN LIGHTS OF THE GEAR INDICATOR WENT OFF, BUT THE RED LIGHT "UNLOCK" TURNED ON. A THUMP SIMILAR TO A GEAR THAT IS FALLING FROM LOCK POSITION HAD BEEN FELT BY BOTH CREW MEMBERS. THE SPEED WAS KEPT AT OR BELOW 190KSDR DXTA2016121706343Unknown · odorTHE WINDSHIELD AIR OVERHEAT LIGHT ILLUMINATED DURING DESCENT IN ICING CONDITIONS. THE RAT WAS 5 DEGREES. COULD ALSO SMELL A BURNING ODOR. PERFORMED MULTIBLE OPS CHECKS TO WINDSHIELD ANTI-ICE. NO DEFECTS NOTED. PERFORMED RE RIGGING OF MANUAL CONTROL VALVES. SDR DXTA2016121606342Unknown · odorAFTER TAXI-OUT, A STRONG ELECTRICAL ODOR AND SMOKE WAS OBSERVED BY THE FLIGHT CREW. ELECTRICAL SMELL AND SMOKE APPEARED TO ORIGINATE ON THE LEFT SIDE OF THE COCKPIT.. FLIGHT CREW IMMEDIATELY SHUTDOWN THE AIRCRAFT ON THE TAXIWAY AND PROCEEDED TO EXIT THE AIRCSDR DXTA2016121506340Brake Sys · malfunctionedDURING LANDING ROLLOUT, ANTI-SKID ANNUNCIATOR ILLUMINATED. AFTER EXITING THE RUNWAY, LOW BREAK PRESSURE ILLUMINATED. PWR BRAKES CIRCUIT BREAKER TRIPPED. RESET THE CIRCUIT BREAKER, SERVICED BRAKE ACCUMULATOR TO FULL, CHECKED ACCUMULATOR FOUND PRESSURE NORMAL.SDR DXTA2016121406338Detector · malfunctionedRIGHT ENGINE FIRE LIGHT DIMLY FLICKERED ON AND OFF OVER TEN TIMES ON APPROACH AND LANDING. ANTI-ICE ON OVER OFF MADE NO DIFFERENCE NOT DID MODERATE POWER TO IDLE. TROUBLESHOT THE R ENGINE FIRE DETECTION SYSTEM AND INSPECTED RT ENGINE FIRE DETECTION SYSTEM IAWSDR 6EXR2016121511060Downlock · faultyOPERATOR REPORTED THAT UPON EXTENDING THE LANDING GEAR, THE NOSE GEAR GREEN LIGHT DID NOT COME ON. AN EMERGENCY EXTENSION WAS PERFORMED, AFTER APPROX. 30 SECONDS THE THE NOSE GEAR GREEN LIGHT ILLUMINATED. THE AIRCRAFT LANDED WITHOUT INCIDENT. TROUBLESHOT PROBLSDR O2GA2016120650101Brake Sys · contaminatedAIRCRAFT HAD TO BE REPOSITIONED POST MAINTENANCE FOR FUELING. WHEN CHOCKS WERE PULLED AIRCRAFT STARTED MOVING AND WOULD NOT STOP USING NORMAL BRAKING. EMERGENCY BRAKE APPLIED TO STOP AIRCRAFT WITHOUT ANY FURTHER INCIDENT. CIRCUIT BREAKERS FOR POWER BRAKES AND SDR O2GA2016120150101Control Valve · defectiveDURING PREFLIGHT INSPECTION, THE ACM OVERHEAT ANNUNCIATOR ILLUMINATED WHILE APU WAS RUNNING. E6/E5 FAULT CODE ON TEMPERATURE CONTROLLER. SMOKE IN COCKPIT OBSERVED. MAINTENANCE TROUBLESHOT THE DISCREPANCY TO A FAULTY RIGHT COCKPIT TEMPERATURE CONTROL VALVE. INSDR DXTA2016113006333Engine · failedAFTER TAKEOFF, A BANG WAS HEARD AND THE LEFT HAND ENGINE ITT SHOWED 800 DEGREES. THERE WAS VIBRATION FELT FOR ABOUT 30 SECONDS. AT THAT POINT THE LEFT OIL PRESSURE AND HYD FAIL LIGHTS ILLUMINATED. THE ENGINE FAILURE AND PRECAUTIONARY SHUTDOWN CHECKLIST WERE COSDR DXTA2016113006335Circuit Breaker · failed3 - 5 MINUTES AFTER TAKEOFF, POWER BRAKE CIRCUIT BREAKER TRIPPED & ANTISKID INOP ANNUNCIATOR ILLUMINATED. CIRCUIT BREAKER WOULD NOT RESET. AFTER 30 MINUTES, CIRCUIT BREAKER RESET. AT LANDING THE BRAKES WORKED, FELT SOFT. BRAKE FLUID LEVELS NORMAL. NO LEAKS NOSDR O2GA2016112250704Warning Light · illuminatedDURING CLIMB OUT THROUGH FL230 , MASTER WARNING ILLUMINATED WITH NO ASSOCIATED ANNUNCIATORS. LEFT AND RIGHT ENGINE OIL PRESSURES FLUCTUATED AND DROPPED THEN STABILIZED TWICE. ALL OTHER INDICATORS WERE GREEN. MAINTENANCE PERFORMED THE REQUIREMENTS OF SB72-3044SDR EBVR20161104001Skin · crackedCRACK IN LEADING EDGE RUDDER SKIN RT SIDE JUST BELOW TOP HINGE. REMOVED THE RUDDER UPPER LEADING EDGE SKIN AND INSTALLED NEW . ALL WORK WAS DONE IAW SRM 51-40-03 AND 51-40-06.SDR 9JLA2016110710774Computer · faultyWHILE IN THE CRUISE STAGE OF FLIGHT AT FL 410 THE FLIGHT CREW EXPERIENCED AN ENGINE FAILURE OF THE NR ENGINE. THIS OCCURRED AS THEY CAME OUT OF CROSS FEED GOING FROM THE LEFT TANK TO THE RIGHT ENGINE. THE ENGINE JUST FLAMED OUT, AND N2 ROLLED ITSELF BACK TO 11SDR O2GA2016110750703Oil System · low pressureDURING CLIMB, RIGHT ENGINE OIL PRESSURE WENT TO ZERO, TRIGGERED THE MASTER WARNING, THEN WENT BACK TO NORMAL RANGE FOLLOWED BY LEFT OIL PRESSURE GOING TO YELLOW RANGE (DID NOT TRIGGER MASTER WARNING) AND THEN BACK TO NORMAL RANGE. SYSTEM WAS NORMAL THE REST OFSDR EBVR20161101002Skin · chafedLARGE CHAFE AND GOUGES IN THE MAIN ENTRY DOOR SKIN AT THE FWD COUNTERBALANCE REEL LOCATION. COMPLIED WITH ERO-868632 IR. INSTALLING A REPAIR DOUBLER AT THE DAMAGED AREA OF THE MAIN ENTRY DOOR.SDR EBVR20161101001Skin · debondedRIGHT INBD FLAP LOWER SURFACE HAS AN AREA OF DE LAMINATION CAUSED BY IMPACT DAMAGE LOCATED DIRECTLY BEHIND THE MAIN TIRE. COMPLIED WITH ERO-868488 REV IR.SDR 2016FA0000577Transmitter · inoperativeFUEL FLOW STOPPED INDICATING. FOUND FUEL FLOW TRANSMITTER TO BE INOPERATIVE. REMOVED AND REPLACED WITH OVERHAULED UNIT.SDR DXTA2016102806326Apu · odorOIL BASED ODOR PRESENT IN THE CABIN WHEN THE APU BLEED AIR IS SELECTED ON. NO VISIBLE SMOKE BUT OIL PARTICLES ARE IRRITATING TO BOTH CREWMEMBERS EYES. INSTALLED A REPAIRED APU IAW MM 49-10-00, INSTALLED DRAIN LINES, SERVICED APU, OPS AND LEAK CHECK OF APU GOSDR EBVR20151026001Fairing · corrodedCORROSION FOUND ON AND UNDER FWD FUSELAGE CHIN FAIRING, ON CHIN FAIRING MINOR BLENDING . UNDER FUSELAGE FAIRING COMPLIED WITH AQRD ERO-867561 REPAIR.SDR DXTA2016102506323Control Unit · defectiveEXPERIENCED COMPLETE FAILURE OF NORMAL BRAKE SYSTEM WITH ILLUMINATION OF MASTER CAUTION AND ANTI-SKID INOP ANNUNCIATOR. THERE IS NO EVIDENCE OF FLUID LEAK. BRAKE ACCUMULATOR IS FULL WITH CORRECT PRESSURE. ANTI-SKID WIRING HARNESSES SEEM TO BE INTACT. THERSDR DXTA2016102406322Switch · failedDURING FLIGHT AT 25000, THE RIGHT ECC MANUAL LIGHT CYCLED ON AND OFF A FEW TIMES AND THE RIGHT ENGINE N1 FLUCTUATED BETWEEN 80 AND 89 PERCENT.NO CHANGES NOTICED WITH THE ANTI ICE ON/OFF. INSPECTED EEC CONNECTOR & PCBS IN AFT J BOX. NO DEFECTS NOTED. PERFORMESDR O2GA2016102650301Seal · leakingAFTER TAKEOFF THE LEFT ENGINE ITT INCREASED TO 723 DEGREES. TAPE TURNED RED. AFTER SELECTING CLIMB POWER ITT DECREASED BELOW 720 DEGREES. ENGINE ITT EXCEEDANCE WAS WITHIN ENGINE PERFORMANCE LIMITS PER THE EMM. DURING ENGINE RUNS SEVERAL BLEED AIR MANIFOLD COSDR O2GA2016102450702Transmitter · defectiveAFTER ENGINE SHUTDOWN AND ENGINE OIL PRESSURE TRANSMITTERS WERE SWAPPED DUE TO UNABLE TO DUPLICATE. AFTER TAKE OFF LEFT AT 6,000 FT, OIL PRESSURE ANNUNCIATOR ILLUMINATED, OIL PRESSURE WENT TO ZERO FOLLOWED BY MASTER CAUTION LIGHT. FOLLOWED ABNORMAL CHECKLIST. SDR WCEA20161024001Lamp · inoperativeDURING APPROACH, PILOT SELECTED GEAR DOWN AND DIDN'T RECEIVE A LT MAIN GEAR DOWN INDICATION. IAW CHECKLIST THE PILOT THEN BLEW THE GEAR DOWN AND DIVERTED AND DECLARED AN EMERGENCY. FOUND THE INDICATOR LIGHT INOPERATIVE. REMOVED AND REPLACED LAMPS.SDR JGVR2016101700001Flap Track · wornDISCOVERED NINE RIVETS PULLED THROUGH THE SKIN ON THE BOTTOM OF THE OUTBOARD FLAP TRACK OF THE RT WING.SDR ZESA20161013001Door · bindingAFTER TAKEOFF , THE CABIN DOOR ANNUNCIATOR ILLUMINATED AND THE CABIN ALTITUDE INDICATOR WAS INDICATING THAT THE AIRCRAFT WAS NOT PRESSURIZING. THE PILOTS CONTACTED THE TOWER AND RETURNED TO THE AIRPORT. UPON LANDING THE CABIN DOOR ANNUNCIATOR EXTINGUISHED. UPOSDR DXTA2016101206317Gasket · failedDURING TAKEOFF AT 1,500 FT, RIGHT ENGINE EXCEEDED ITT RED LINE PRIOR TO FLAP RETRACT ALTITUDE. COMPLIED WITH EXTENSIVE TROUBLESHOOTING. REF MESA WORK ORDER REV. 45358 FOR >FULL DETAILS. REPLACED BLEED AIR SEALS AS NEEDED. COMPLETED A COMPRESSOR WASH AND BLADESDR DXTA2016101106316Control Unit · failedON DEPARTURE, LANDING GEAR HANDLE WOULD NOT MOVE TO UP POSITION. UNABLE TO RETRACT GEAR. UNABLE TO RETRACT GEAR. WITH A MULTI METER CHECK FOR 28VDC AND GROUND AT THE GEAR CONTROL ASSY WITH AIRCRAFT IN AIR MODE POWER AND GROUND PRESENT, BUT SOLENOID WON'T PUSDR O2GA2016101150701Transducer · malfunctionedAFTER TAKE OFF AND DURING CLIMB, THE RED MASTER CAUTION LIGHT AND RIGHT ENGINE OIL PRESSURE LIGHT ILLUMINATED. RIGHT ENGINE OIL PRESSURE DROPPED TO ZERO. COMPLIED WITH CHECKLIST PROCEDURE WHICH LED TO THE SHUTDOWN OF THE RIGHT ENGINE. EMERGENCY WAS DECLARED SDR DXTA2016092606309Brake · malfunctionedRIGHT BRAKE SHUDDERS REPEATEDLY UPON LANDING AND APPLICATION OF BRAKES AT HIGH SPEED. BRAKES RESPONDED NORMALLY DURING TAXI. DURING TROUBLESHOOTING, IT WAS DISCOVERED THAT INTERNALLY THE NR 2 MLG BRAKE WAS MALFUNCTIONING. ALSO, DURING INSPECTION IT WAS NOTEDSDR EBVR20160926001Torque Tube · corrodedDURING INSPECTION, FOUND LEFT AND RIGHT ELEVATOR TORQUE TUBES CORRODED. REMOVED ELEVATORS AND REPLACED TORQUE TUBES. PAINTED AND BALANCE ELEVATORS. REINSTALLED ELEVATORS ON AIRCRAFT.SDR DXTA2016091906303Fastener · looseRIGHT ENGINE FWD LOWER ENGINE MOUNT HAS TWO LOOSE LOCK FASTENERS. REMOVED AND REPLACED IAW ERO-858851.SDR DXTA2016091506302Motor · inoperativeON TAXI OUT, POWER BRAKE CIRCUIT BREAKER TRIPPED. RESET ONCE AND IT TRIPPED AGAIN. R & R POWER BRAKE MOTOR. REMOVED PN: MP50B-1, SN:4642, INSTALLED MP50B-1, SN:2658. OPS CHECKED GOOD.SDR DXTR2016091402Skin · corrodedMAIN CABIN DOOR EXTERIOR SKIN CORRODED BS 194 WL 100, 2 INCHES LONG AND WL 167, 3 INCHES LONG, 1 INCH WIDE. REPAIRED IAW AQRD ERO-859860.SDR DXTR2016091401Skin · corrodedMAIN CABIN DOOR EXTERIOR SKIN CORRODED AT BS 194 WL 100, 2 INCHES LONG AND WL 167, 3 INCHES LONG AND 1 INCH WIDE. REPAIRED IAW ERO-859860.SDR 9JLA2016112210769Pcb · defectiveFLIGHT CREW REPORTED THAT DURING FLIGHT THEY RECEIVED A STAB MISCOMPARE ANNUNCIATOR ILLUMINATED AND WOULD NOT EXTINGUISH AFTER SEVERAL CYCLES OF THE FLAPS. TROUBLESHOOTING IDENTIFIED THE TWO-POSITION HORIZONTAL STAB PCB N2017 DEFECTIVE. THE PCB WAS REPLACED WISDR IGXR20160921004Trim Tab · crackedTHE LOWER AFT CORNER OF THE RUDDER TRIM HAS A CRACK MEASURING 0.76 INCHES LONG. PERFORMED PERMANENT REPAIR USING APPROVED ENGINEERING ORDER ERO-859505.SDR DXTA2016090600177Spar · corrodedLEFT HORIZONTAL STABILIZER REAR SPAR CORRODED.SDR JGVR2016090600002Frame · corrodedFRAME 0 IN NOSE WHEEL WELL AROUND NOSE COOLING FAN ATTACHMENT WAS CORRODED AND OUT OF LIMITS.SDR DXTA2016090600412Spar · corrodedLEFT WING AFT SPAR SPLICE CORROSIONSDR JGVR201609060001Threshold · crackedCRACKED MAIN ENTRY DOOR LOWER INNER THRESHOLD AND OUTER THRESHOLD. INSTALLED NEW INNER THRESHOLD, AND NEW OUTER THRESHOLD IAW SRM AND MM.SDR DXTA2016082906294Display · malfunctionedDURING FERRY FLIGHT WITH INOPERATIVE PRESSURIZATION, ACM, AND TEMPERATURE CONTROL AT FL100 NR 1 PFD STARTED TO DEVELOP A HOT SPOT IN CENTER OF SCREEN AS IF OVERHEATING AND RAPIDLY EXPANDED. DUE TO EXTREME HEAT IN PLANE OF 105 DEGREES F AND CONCERN OF POSSIBLESDR 9JLA2016093010655Speed Switch · defectiveTHE FLIGHT CREW REPORTED THAT ON APPROACH TO LANDING THEY RECEIVED A STAB MISCOMPARE INDICATION. LANDING WAS WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND IDENTIFIED THAT THE TWO POSITION HORIZONTAL STABILIZER AIRSPEED SWITCH WAS DEFECTIVE. THE SWITCH WAS RSDR DXTA2016082606292Engine · malfunctionedRIGHT ENGINE HAD A LOUD BANG AND RED LINED ITT AT ABOUT 500' AFTER TAKEOFF. REDUCED POWER TO IDLE. ENGINE CONTINUED TO RUN AT IDLE WITH AN ITT ABOUT 600 AND A LOUD WHINE. CONTINUED WITH IN FLIGHT PRECAUTIONARY SHUTDOWN. ENGINE VIBRATION ANNUNCIATOR WAS ALSSDR DXTA2016082106289Oil System · overservicedEARLY IN THE FLIGHT AIR SMELLS NORMAL. AFTER SOME TIME, ENROUTE AND AFTER ADJUSTING BLEED AIR TO A WARMER TEMPERATURE THERE IS AN ACRID OIL BURNING ODOR COMING FROM THE COCKPIT AND CABIN WARM AIR VENTS. COMPLIED WITH APU MEL MAINTENANCE PROCEDURES. RAN APU,SDR O2GA2016082650201Switch · failedAT FL390 ACM OVER HEAT ANNUNCIATOR ILLUMINATED AND CABIN STARTED TO CLIMB. EMERGENCY CHECKLIST WAS FOLLOWED. EMERGENCY WAS DECLARED AND AIRCRAFT DIVERTED. LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE ACM OVER HEAT SWITCH. A SUCCESSFUL OPERATIONAL CHECSDR ZESA201608221Vhf Comm · failedRIGHT VHF COMMS FAILEDSDR O2GA2016082250601Switch · intermittentDURING TAXI, LOW BRAKE PRESSURE ANNUNCIATOR LIGHT ILLUMINATED FOLLOWED BY LOSS OF BRAKES. THRUST REVERSERS DEPLOYED AND EMERGENCY BRAKES USED TO SUCCESSFULLY STOP THE AIRCRAFT. CREW REPORTED POWER BRAKE CIRCUIT BREAKER WAS EXTENDED. MAINTENANCE REPLACED THESDR DXTA2016F00184Spar · corrodedLEFT HORIZONTAL STABILIZER REAR SPAR CORROSION BETWEEN SS 9.3 TO SS 19.00.SDR DXTR2016081701Door Frame · crackedFRONT FRAME CRACKED ON MAIN CABIN DOOR. REPAIRED IAW AQRD-ENG-014, REV B ERO-853215. NO DEFECTS NOTED AT THIS TIME.
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