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 DXTA2014020505639Brake Sys · contaminatedUPON LANDING BRAKES WERE EVENLY APPLIED BUT ASYMMETRICAL BRAKING WAS EXPERIENCED, ACFT PULLED TO THE LT, BRAKES WERE RELEASED & ACFT DIRECTION OF TRAVEL WAS CORRECTED & BRAKES WERE EVENLY APPLIED AGAIN & AGAIN THE ACFT PULLED TO THE LT, WE WERE ABLE TO CLEAR TSDR DXTA2014020305636Steering Sys · misalignedAFTER RETRACTING THE GEAR AFTER TAKEOFF THERE WAS A RED GEAR UNLOCK LIGHT ON. LG EXTENDED NORMALLY. AFTER LANDING WITH THE NOSE WHEEL STRAIGHT THE RUDDER PEDALS ARE OFFSET TO THE LT & THE RUDDER IS DEFLECTED TO THE LT. FOUND NOSE GEAR STEERING MISALIGNED. SDR 9JLA2014013103681Fan · noisyFLIGHT CREW REPORTED THAT THE PASSENGERS STATED THAT THE CABIN TEMP SENSOR FAN WAS VERY NOISY. THE TEMP FAN WAS SUSPECTED TO BE DEFECTIVE & IT WAS R & R WITH A NEW UNIT.SDR 9JLA2014013003586Hydraulic Line · failedAFTER ARRIVING AT THEIR DESTINATION & DURING THEIR POST FLIGHT INSPECTION THEY NOTED FLUID LEAKING FROM AN AFT FUSELAGE DRAIN & DETERMINED THAT IT WAS HYD FLUID. HYD RETURN LINE LOCATED IN THE HYD FILTER PANEL AREA FAILED CAUSING THE LEAK. THE FAILED HYD RETSDR XCGA20140129001Actuator · intermittentPILOT REPORTED THAT ON FIRST ATTEMPT TO LOWER GEAR ON APPROACH TO KAGC HE DID NOT GET A GREEN LIGHT ON THE LT MLG. HE RECYCLED THE GEAR & ALL GEAR EXTENDED NORMALLY. JACKED THE AIRPLANE & WAS ABLE TO DUPLICATE THE SQUAWK ON ONLY 1 RETRACTION OUT OF SEVERAL ASDR DXTA2014012005622Handle · malfunctionedAFTER TAKEOFF GEAR HANDLE WOULD NOT COME UP. R & R THE GEAR HANDLE ASSEMBLY IAW MM 32-30-01, OPERATIONS CHECKED GOOD.SDR 9JLA2014021203680Wire · brokenTHE FLIGHT CREW REPORTED THAT THE RT SIDE PITOT STATIC HEAT FAILED. TROUBLESHOOTING FOUND THE WIRE BROKE AT PIN 1 AT PITOT TUBE. REPAIRED WIRE AS REQUIRED & RETURNED THE ACFT TO SERVICE.SDR 9JLA2014013003583Uplock · stiffAFTER DEPARTURE & THE GEAR WAS RETRACTED THE RED GEAR UNSAFE LIGHT REMAINED ILLUMINATED, INDICATING THAT ONE OR MORE OF THE LG WERE NOT IN THE UP POSITION. THE LG WAS CYCLED SEVERAL TIMES & EACH TIME FAILED TO RETRACT PROPERLY. THE GEAR WAS EXTENDED & SINCE SDR 9JLA201401240659Switch · defectiveTHE FLIGHT CREW REPORTED THE RT ENG ANTI-ICE LIGHT TEST WAS OK WITH THE ROTARY SWITCH BUT WHEN THE SYS WAS ACTIVATED WITH ANTI-ICE SWITCH THE RT SIDE DOES NOT COME ON IN FLIGHT EVEN AFTER A 1 HOUR CRUISE. TROUBLESHOOTING FOUND THE RT TEMP SWITCH DEFECTIVE. NSDR DXTA2014010605614Relay · failedAPPROACHING PARKING AREA, LOW BRAKE PRESSURE & ANTI SKID INOPERATIVE ANNUNCIATORS ILLUMINATED. APPLIED BRAKES, PEDALS WENT TO THE FLOOR & THE BRAKES FAILED. COMPLIED WITH THE WHEEL BRAKE FAILURE MEMORY ITEMS & USED THE EMERGENCY BRAKE HANDLE TO STOP THE ACFSDR DXTA2014010605613Motor · overheatedDURING FINAL APPROACH, SELECTED LANDING GEAR DOWN, BOTH THE LOW BRAKE PRESSURE & ANTI-SKID INOPERATIVE CAUTION LIGHTS ILLUMINATED. COMPLETED THE EMERGENCY CHECKLIST FOR A POWER BRAKE SYS FAILURE. NO CIRCUIT BREAKERS TRIPPED. USED THE EMERGENCY BRAKE TO STOSDR CA140117006Warning Light · illuminated(CAN) THE OIL FILTER BYPASS LT ANNUNCIATOR ILLUMINATED DURING TAKEOFF ROLL. THE PILOT ELECTED TO ABORT TAKEOFF. NO DETAILS AVAILABLE ABOUT THE TROUBLESHOOTING AND THE ACFT WAS RETURN IN SERVICE.SDR DXTA2013123005608Landing Gear · inoperativeAFTER DEPARTURE, GEAR HANDLE WOULD NOT PULL OUT OF PANEL TO ALLOW GEAR RETRACTION. GEAR GREEN LIGHTS NEVER WENT OUT, RETURNED & LANDED UNEVENTFULLY. REMOVED AND RPLACED LT SQUAT SWITCH IAW AMM 32-61-00. REMOVED AND REPLACED GEAR CONTROL PCB IAW AMM 24-51-SDR DXTA2013122702609Flap System · malfunctionedAFTER TAKEOFF, WHEN FLAPS WERE SELECTED TO 0, FLAPS STUCK AT 7 DEGREES. ON GROUND FLAP HANDLE SELECTED TO 35 DEGREES & STUCK AT 35 DEGREES. REPLACED THE LT FLAP ACTUATOR ASSEMBLY, LT FLAP OUTBOARD BELLCRANK ASSEMBLY AND LT FLAP OUTBOARD BELLCRANK BOLT. SYSTSDR CA140117002Oil System · low pressure(CAN) THE PILOT INDUCE AN IFSD DUE TO A LOW OIL PRESSURE INDICATION. THE ON GROUND INVESTIGATION REVEALED PRESENCE OF OIL OUT OF THE FIRST STAGE COMPRESSOR, BEHIND NOSE CONE, INSIDE THE MAIN SHAFT AND THE TURBINE AND IN THE BYPASS DUCT. THE ENGINE WILL BE REMSDR DXTA2013122605607Reservoir · failedTHE RED GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF, LEADING TO A FLASHING HYD PRESSURE & STAB MISCOMPARE ANNUNCIATOR. AFTER ABOUT 45 SECONDS, GEAR UNSAFE LIGHT EXTINGUISHED WITH A HEAVIER THAN NORMAL THUD UNDER FLIGHT DECK FLOOR. A FEW SECONDS LASDR DXTA2013122005603Valve · defectiveON DEPARTURE, AFTER RAISING LG, WE GOT A RED UNLOCK LIGHT. FOLLOWED THE CHECKLIST, PULLED HYD PRESS CB, & HEARD A CLUNK IN THE NOSE OF THE PLANE, WE BELIEVED THE NOSE GEAR EXTENDED. BEFORE LANDING WE PUSHED THE CB BACK IN & EXTENDED THE LG. EXTENSION WAS NOSDR DXTA2013121805599Relay · unserviceableUPON SHUTDOWN OF THE APU WE NOTICED A STRONG ODOR WHICH SMELLED LIKE ELEC WIRES BURNING AS WE WALKED TOWARDS THE LAVATORY, OPENED THE ACCESSORY DOOR TO THE APU & NOTICED A VERY STRONG ELEC SMOKE ODOR. DISCONNECT THE BATTERY, INSPECTED AFT J BOX AREA & FOUND RSDR DXTA2013121605597Printed Ckt Board · defectiveLANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. RED LIGHT STAYED ILLUMINATED WITH NO GREEN LIGHT. THERE WAS NOTICEABLE DRAG AS IF THE AIRPLANE WAS NOT CLEAN. EXTENDED LANDING GEAR & BLEW THE BOTTLE FOR PRECAUTION. R & R A DEFECTIVE LANDING GEAR PCB NZ004 IAWSDR 9JLA20131217545Carbon Seal · defectiveDURING THE POST FLIGHT CHECKLIST ON DEC 10TH IT WAS DISCOVERED THAT THE OIL LEVEL FOR THE NR 1 ENG WAS BELOW THE INSPECTION SIGHT GLASS WITH OIL STREAKING PRESENT IN THE BYPASS DUCT. THE TROUBLESHOOTING FOR THE DEC 10TH OIL LEAK EVENT FOUND THAT THE OIL LEAK WSDR DXTA2013121105598Unknown · odorIN FLIGHT ON TWO SEPARATE OCCASIONS AFTER GND DE ICE WITH TYPE 1 FLUID. ONCE 45 MIN INTO FLIGHT THE 2ND TIME 5 MIN INTO FLIGHT. WING ENG ANTI-ICE WAS SELECTED & A VERY STRONG ACRID SMELL FILLED COCKPIT & WENT AWAY AFTER A FEW MINUTES. THE SMELL WAS VERY DIFSDR DXTA2013120905595Actuator · faultyIN FLIGHT AFTER TAKEOFF, GEAR THEN FLAP RETRACTION HYD PRESS ANNUNCIATOR REMAINED ON. CYCLED FLAPS & GEAR LIGHT REMAINED ON. ON LANDING PREP AFTER GEAR EXTENSION HYD PRESS LIGHT WENT OUT AT 170 KTS. AFTER LANDING & FLAP RETRACTION HYD PRESS LIGHT STAYED ON.SDR DXTA2013120905594Door · out of adjustAFTER TAKEOFF & GEAR SELECTED UP, ALL THREE GEAR LIGHTS EXTINGUISHED BUT RED, GEAR UNLOCKED, LIGHT REMAINED ILLUMINATED. THE STAB MISS COMPARE & HYD PRESS LIGHTS ILLUMINATED AS EXPECTED. AFTER PULLING THE HYD CONTROL CB IAW HYDRAULIC PRESS CHECKLIST, THE RT SDR DXTA2013120505592Actuator · faultyAT FL400 PITCH MISTRIM ANNUNCIATED IN OUR PFDS. UPON DISCONNECTING THE AUTOPILOT, THE ACFT PITCHED DOWN. NEEDED SIGNIFICANT BACK PRESS TO HOLD ALTITUDE. NOTICED THAT THE TRIM WAS JAMMED IN POSITION, WOULD NOT MOVE ELECTRICALLY NOR BY HAND. UPON DESCENDING SDR DXTA2013120505590Apu · malfunctionedAFTER APU WAS STARTED & GEN SWITCH WAS ON, WE TURNED THE BLEED AIR ON. ALMOST IMMEDIATELY SMOKE STARTED FILLING THE COCKPIT. THE SMOKE DID NOT APPEAR TO BE COMING FROM WEMACS. IT SMELLED LIKE DIRTY SOCKS, APU WAS SHUTDOWN & SMOKE EVENTUALLY DISSIPATED. NO SDR DXTA2013120205586Controller · faultyDURING DECENT TO LANDING, THE RT ENG FIRE LIGHT WAS DIMLY FLICKERING ON & OFF, 1 SECOND ON THEN ABOUT 3 SECONDS OFF, UNTIL LANDING. PLACING THE RT THROTTLE TO IDLE TO DETERMINE IF THERE WAS A BLEED AIR LEAK, THE LIGHT STILL CONTINUED TO FLICKER. ON THE GND TSDR CA131215004Carbon Seal · failed(CAN) THE PILOT REPORTED UNUSUAL ODOR OF POSSIBLE FUMES OR OIL-BASED FLUID DURING TAKEOFF. THE ON GROUND TROUBLESHOOTING FOUND PRESENCE OF CARBON IN THE NOSE CONE. REPLACED THE NR 1 BEARING CARBON SEAL.SDR DXTA2013112705582Tube · damagedDURING CLIMB OUT WING O HEAT R CAME ON & STAYED ON FOR ABOUT 10 SECONDS. WE REDUCED POWER TO APPROXIMATELY 70% N1. LIGHT CAME ON AGAIN AT SHORT FINAL FOR ABOUT 3 SECONDS WITH POWER AT ABOUT 50% N1. REPLACED HEAT SHIELD & BLANKET PN 6621281-30, NSN, PN F7802SDR DXTA2013112705581Actuator · faultyIN CRUISE FL410 PITCH MIS TRIM LIGHT ILLUMINATED, DISENGAGE A/P IAW CHECK LIST. CONFIRMED BOTH LT & RT ELEC TRIM FROZEN & MANUAL TRIM ALSO FROZEN IN PLACE. ON TAXI IN ATTEMPTED MANUAL TRIM & IT WORKED NORMAL. REMOVED LT & RT ELEVATOR TRIM ACTUATORS PN 66601SDR CA131202003Oil System · low pressure(CAN) THE RT ENGINE WAS SHUTDOWN IN FLIGHT DUE TO LOSS OF OIL PRESSURE. THE ACFT WAS FLOWN WITH THE ENGINE SHUTDOWN FOR ABOUT AN HOUR AND 15 MINUTES. TROUBLESHOOTING ON GOING.SDR DXTA2013112205579Fire Loop · chafedDURING DECENT WE ENCOUNTERED MODERATE TURBULENCE & PRECIP. BOTH RED FIRE LIGHT SWITCHES FLICKERED ON IN CONJUNCTION WITH TURBULENT BUMPS AT THE SAME TIME IN SYNC. THEY DID NOT REMAIN ILLUMINATED ONLY A FAINT FLICKER. PERFORMED ROTARY TEST, ENG FIRE LIGHTS CHSDR DXTA2013112105576Sign · defectiveAFT DIVIDER EMERGENCY EXIT SIGN WILL NOT LIGHT & HEARD SPARKING NOISE COMING FROM SIGN. R & R AFT DIVIDER EMERGENCY EXIT SIGN IAW 560XL MM 33-50-02. OPERATIONAL CHECKS GOOD.SDR CA131120012Hinge Bracket · cracked(CAN) RT ELEVATOR, OTBD HINGE-OTBD BRACKET CRACKED, SIMILAR TO 2 OTHER ACFT WE HAVE FOUND THIS ON.SDR 9JLA2014021204531Wire · damagedTHE CREW REPORTED THAT THE LT PITOT HEAT WARNING LIGHT WAS ON. TROUBLESHOOTING IDENTIFIED AN ELEC PIN INSIDE THE PROBE HEAT CONNECTOR AT THE PROBE TO HAVE A BROKEN WIRE SOLDER JOINT. REPAIRED THE WIRE AT CONNECTOR AS REQUIRED.SDR DXTA2013111805570Servo · damagedIMMEDIATELY AFTER TAKEOFF, A GRINDING COULD BE FELT IN THE YOKE WHILE APPLYING FORWARD OR AFT MOVEMENT. VIBRATION WAS FELT IN FLOOR AT THE SAME TIME. NO GRINDING DURING FLIGHT CONTROL CHECK ON GROUND. GRINDING IS EXCESSIVE. REMOVED AND REPLACED THE ELEVATSDR DXTA2013111205563Brake Assy · malfunctionedLT BRAKE GRABS. R & R LT BRAKE ASSY IAW MM 32-42-01. BLED SYS AND PERFORMED OPS CHECKS. OPS CHECKS SATISFACTORY AT THIS TIME. TAXI, OPS, & LEAK CHECKED GOOD.SDR DXTA2013111105561Apu · failedACFT ON GROUND, APU RUNNING, COCKPIT & CABIN SUDDENLY FILLED WITH ELECTRICAL SMOKE ODOR. NO INDICATIONS OF FIRE, RAN SMOKE CHECKLIST. APU SHUTDOWN ON ITS OWN. CHECKED APU BAY, , COMPARTMENT WAS ALSO FILLED WITH ELECTRICAL SMOKE ODOR. REMOVED AND RPLACED FASDR FUEA2013000011Window · crackedAPPROXIMATELY 10 MINUTES AFTER REACHING FL 410 A LOUD BANG OCCURRED IN THE COCKPIT AREA OF THE AIRCRAFT. A VISUAL INSPECTION REVEALED A CRACK, COMPLETE SPIDER WEBBING, THROUGHOUT THE FWD RT HAND SIDE HEATED WINDOW. WE INITIATED A DESCENT TO 10,000' MSL. REQSDR DXTA2013103105553Unknown · odorDURING CRUISE FLIGHT, A LOUD CLICK OR POP WAS HEARD. CREW NOTICED A STRONG ELECTRICAL BURNING ODOR IN THE COCKPIT THAT QUICKLY WENT AWAY. NO SMOKE WAS NOTED. NO CIRCUIT BREAKERS WERE TRIPPED. PERFORMED COCKPIT LIGHTING CHECK IAW MM 33-10-00, NO DEFECTS NOTSDR DXTA2013103005552Display · failedON ARRIVAL, CREW NOTICED AN ELECTRICAL BURNING ODOR, FOLLOWED QUICKLY BY THE MFD GOING BLANK. PULLED THE MFD CIRCUIT BREAKER AND FLT CONTINUED UNEVENTFULLY. ALL OTHER AVIONICS OPERATED NORMALLY. REMOVED INOPERATIVE MFD AND INSTALLED A REPAIRED UNIT IAW AMM SDR EBVR20131024001Bearing · frozenDURING ELEVATOR REMOVAL, NOTICED THAT A NUMBER OF ELEVATOR ATTACHMENT BEARINGS ARE FROZEN AND REQUIRE REPLACEMENT.SDR 9JLA2013120403577Display · inoperativeTHE CREW REPORTED THAT THE MULTI-FUNCTION DISPLAY WAS INOPERATIVE. THE MFD WAS REMOVED PN 7014300-901 SN 96031332 & A REPAIRED UNIT WAS INSTALLED. FUNCTIONAL CHECKS WERE SATISFACTORY IAW CITATION 560XL AMM 34-26-00.SDR CA131117003Engine · malfunctioned(CAN) THE ACFT WAS PARKED FOR THE PAST 4 YEARS AND CLAIMED TO HAVE HAD MONTHLY GROUND RUNS PERFORMED TO PREVENT LONG TERM STORAGE/PRESERVATION. THE OIL LEVEL WAS CHECKED GOOD ON THE 2 ENGINES ON OCTOBER 21ST JUST BEFORE A REPOSITIONING FLIGHT AS THE CUSTOMER SDR CA131023003Oil System · leaking(CAN) DURING FERRY FLIGHT IN CLIMB THE NR 2 ENGINE LOST OIL PRESSURE THE CREW BROUGHT THE THROTTLE BACK TO IDLE AND THE PRESSURE DROPPED TO 15 PSI AND THE RED PRESSURE ANNUNCIATOR CAME ON. ON THE WAY BACK THE NR 1 ENGINE STARTED TO SHOW SIGNS OF LOW OIL PRESSSDR DXTA2013101405540Unknown · odorDURING DESCENT, A STRONG ODOR OF OIL THROUGHOUT CABIN. REMOVED AND REPLACED WATER SEPARATOR SOCK. PERFORMED OPS CHECK WITH NO DEFECTS NOTED AT THIS TIME. REF AMM 21-51-00.SDR CWQR20131016044Hinge · crackedDURING A SCHEDULED MAINTENANCE, FOUND THE AFT MAIN CABIN DOOR HINGE HALF VERTICAL ATTACH FLANGE CRACKED FROM THE EDGE OF THE PART 0.60" INWARD. NDT INSPECTION VERIFIED CRACK. R & R HINGE HALF ASSY. SUBMITTED SERVICE CONDITON REPORT TO MFG REF NR 672273.SDR DXTA2013102905550Actuator · frozenAFTER BEING AT ALTITUDE FOR APPROXIMATELY 45 MINS THE ELECTRIC AND MANUAL PITCH TRIM FROZE UP, IT BROKE FREE WHILE DESCENDING THROUGH THE LOW 20'S. SUP: R &R LT AND RT ELEVATOR TRIM TAB ACTUATORS WITH O/H UNITS IAW THE MM CH 27-32-04 RIG, TRAVEL AND OPS CHECKSSDR CA131010002Hinge Bracket · cracked(CAN) DURING CAMPAIGN INSPECTION AS A RESULT OF ANOTHER ACFT FINDING OF ALL ELEVATOR BRACKETS IN OUR FLEET THE SAME BRACKET WAS DISCOVERED CRACKED. THIS CRACK WAS ALMOST UNDETECTABLE BY THE NAKED EYE BUT USING 10X IT COULD BE DETERMINED IT WAS CRACKED.SDR DXTA2013101105536Circuit Breaker · trippedAFTER TAKEOFF, LANDING GEAR FAILED TO RETRACT. THREE GREEN LANDING GEAR LIGHTS ALONG WITH THE RED UNLOCK LIGHT. PUT THE GEAR HANDLE BACK DOWN AND HAD THREE GREEN AND NO RED. NOTICED AFTER LEVELING OFF THE GEAR CONTROL CIRCUIT BREAKER OUT. LEFT IT OUT AND MSDR DXTA2013100905532Seal · failedAFTER TAKEOFF, RED GEAR UNSAFE LIGHT REMAINED ON, CAUSING THE HYD LIGHT TO REMAIN ON AND THE STAB MISCOMPARE LIGHT TO COME ON. VISUAL INSPECTION OF NLG STRUT FOR LEAKAGE, NONE FOUND. JACKED ACFT. WRANG OUT WIRING TO NOSE, LEFT AND RIGHT UPLOCK SWITCHES:
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