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 DXTA2012090405118Sensor · malfunctionedACM OVERHEAT ANNUNCIATOR ILLUMINATED AFTER TAKEOFF. ABNORMAL CHECKLIST WAS FOLLOWED AND RETURNED TO AIRPORT. AFTER ILLUMINATION OF THE ACM OVERHEAT ANNUNCIATOR, A WARM RUSH OF AIR AND A BURNED ODOR DETECTED WITHIN CABIN. TROUBLESHOT SYS DOWN TO A RESISTIVE TSDR DXTA2012091005118Warning Light · illuminatedACM OVERHEAT ANNUNCIATOR ILLUMINATED AFTER TAKEOFF. ABNORMAL CHECKLIST WAS FOLLOWED AND WE RETURNED TO THE AIRPORT. AFTER OBSERVING ANNUNCIATOR, THERE WAS A WARM RUSH OF AIR AND A BURNED ODOR DETECTED WITHIN THE CABIN.SDR Z5FA2012090651101Bulb · burned outON FINAL APPROACH, CREW EXTENDED GEAR AND DID NOT GET LT MAIN GEAR DOWN INDICATION. FOLLOWING AFM CHECK LIST A ROTARY TEST FUNCTION FOR THE LANDING GEAR WAS PERFORMED AND THE RT GEAR DOWN DID NOT ILLUMINATE. CREW ABORTED APPROACH TO WORK GEAR CHECK LIST AND SDR CA120917006Eec · malfunctioned(CAN) DURING T/O, THE ENGINE ELECTRONIC ENGINE CONTROL REVERTED TO MANUAL. THE T/O WAS ABORTED AND THE ACFT RETURNED TO THE RAMP. TROUBLESHOOTING IS FOCUSING ON A POSSIBLE FAULTY BLEED VALVE TORQUE MOTOR.SDR DXTA2012090405113Servo Valve · inoperativeLEFT EEC REVERTED TO MANUAL DURING CLIMB. COMPLIED WITH CHECKLIST. THROTTLE RESPONSE WAS GREATER THAN EXPECTED A CHANGE OF 6 TO 8 PERCENT RATHER THAN 2 TO 3 PERCENT FOR SAME THROTTLE MOVEMENTS BETWEEN LT AND RT THROTTLES WITH BOTH IN MANUAL. ON POST FLIGHT FOUSDR DXTA2012083105010Gasket · leakingLEFT ENGINE ITT EXCEEDED LIMITS AFTER TAKEOFF. ITT REACHED 800 DEGREES FOR NO MORE THAN 30 SECONDS, AND RETURNED WITHIN LIMITS UPON THROTTLE RETRACTION. DOWNLOADED NR 1 ENGINE DCU, VERIFIED MAX ITT REACHED WAS 725. TURBINE TRACKER SHOWED MAX ITT REACHED 730.SDR DXTA2012083005109Coalescer Bag · contaminatedAFTER 10-15 MINUTES OF FLIGHT THERE IS AN ODOR (DIRTY DIAPER/OLD SOCKS) APPARENT IN THE CABIN THAT MOVES FORWARD TO THE COCKPIT. ODOR IS NOT NEAR THE FLOOR, ONLY MID CABIN AND HIGHER. CLEANED WATER SEPARATOR AND LT & RT OZONE CONVERTERS. LEAK AND OPS CHECK SDR 9JLA2012101804513Sensor · defectiveCREW REPORTED THAT THE RT PYLON PRE-COOLER DOOR STAYS OPEN ON GROUND. REMOVED THE RT TEMP SENSOR, PN 9914519-2, SN 6AY223. INSTALLED A NEW TEMP SENSOR OF THE SAME PN IAW THE MM 36-11-00. OPS CHECKS GOOD AT THIS TIME.SDR DXTA2012082305104Coalescer Bag · contaminatedDESCENDING THROUGH 34,000 FT, BOTH PILOTS OBSERVED AN EXHAUST FUME ODOR THAT DID NOT DISSIPATE UNTIL THE ENGINES WERE SHUTDOWN. R & R ECS WATER SEPARATOR CONDENSER IAW MM 21-51-00. OPS & LEAK CHECKED GOOD.SDR 9JLA2012082804512Control Valve · defectiveTHE CREW REPORTED THAT THE FLIGHTDECK TEMP COULD NOT BE CONTROLLED IN FLIGHT. TROUBLESHOOTING IDENTIFIED THE RT TEMP CONTROL VALVE AS DEFECTIVE, PN 27241287-14. THE DEFECTIVE VALVE WAS REMOVED AND AN OVERHAULED UNIT WAS INSTALLED.SDR CA120827004Oil System · failed(CAN) DURING REVENUE FLIGHT, ON TAKEOFF, THE OIL PRESSURE WENT TO ZERO ON VR, ROTATION OF THE ACFT. THE CREW COMPLETED THE CLIMBOUT, SHUTDOWN THE ENGINE AND RETURNED TO THE AIRPORT, WHERE AN UNEVENTFUL SINGLE-ENGINE LANDING WAS ACCOMPLISHED. POST-FLIGHT INSPSDR DXTA2012081505096Uplock Switch · unserviceableTROUBLESHOT LANDING GEAR SYS, FOUND UPLOCK ACTUATOR LINK/ SPRING ASSY STICKING IN THE RETRACTED POSITION. ALSO FOUND NLG UPLOCK SWITCH INTERMITTENT. R & R NOSE UPLOCK SWITCH AND NOSE UPLOCK LINK IAW THE MM 32-30-05. OPS CHECKED SATISFACTORY. LINK WAS REMOVED SDR 9JLA2012101804510Actuator · failedTHE CREW REPORTED THE AILERON TRIM FREEZES UP IN FLIGHT. TROUBLESHOOTING SUSPECTED MOISTURE IN THE AILERON TRIM ACTUATOR. THE AILERON TRIM ACTUATOR WAS DISASSEMBLED CLEANED AND REGREASED, THE ACTUATOR WAS ASSEMBLED AND OPS CHECKS WERE SATISFACTORY IAW THE MM 2SDR DXTA2012081305093Trim System · malfunctionedAFTER TAKEOFF, MORE THAN USUAL FORWARD PRESSURE ON YOKE WAS REQUIRED PRIOR TO FLAPS 0 DEGREES. AFTER LEVELING OFF AT FL190 (AUTO PILOT ON), AIRPLANE WAS USING MORE THAN USUAL NOSE DOWN TRIM. TRIM WAS ALMOST AT FULL NOSE DOWN STOPS (TOP OF WHITE ARC ON TRIM WHSDR CVGA20120904001Warning System · activatedSTAB MISCOMPARE ANNUNCIATOR ILLUMINATES AFTER FLAPS INDICATE RETRACTED.SDR DXTA2012081305088Switch · unserviceableAFTER TAKEOFF, PASSING 10,000' (WITH NO DEMAND ON ANY HYDRAULIC SYSTEMS) THE LOW HYD FLOW R ANNUNCIATOR ILLUMINATED. CONTINUED THE CLIMB TO FL250. 15 MINUTES LATER, DURING DESCENT THRU FL230 THE LIGHT EXTINGUISHED AND DID NOT REOCCUR. ALL HYDRAULIC SYTEMS WORKSDR DXTA2012081005083Brake Assy · chatteringBRAKES GRABBING AND CHATTERING DURING ALL TAXI PROCEDURES. BRAKES ALSO VERY GRABBY (PARTICULARLY TO THE RT) ON LANDING. AUDIBLE METAL ON METAL NOISE VERY DISTINCT IN CABIN, COCKPIT AND REPORTED BY GROUND CREW. PARTICULARLY WHEN APPLYING RT BRAKE. R & R RT BRSDR DXTA2012090605116Structure · corrodedCORROSION ON LT AND RT STRAKE ASSY. REPAIRED CORROSION ON LT AND RT VENTRAL STRAKE. MAJOR REPAIR.SDR DXTA2012090605115Attach Bracket · damagedRT WING INBD AILERON HINGE ATTACH BRACKET HAS 2.2500" BOLTS ON FWD SIDE INVESTIGATED RT WING INBD AILERON HINGE WITH .2500" BOLTS (AN4-7A, EXISTING) IN FWD HOLES. FOUND HOLES HAD BEEN PREVIOUSLY OVERSIZED. OVERSIZED HOLES ARE FOUND TO BE ACCEPTABLE IAW ENGINSDR DXTA2012080905082Brake · wornRIGHT WHEEL BRAKE BINDS AND DRAGS ON TAXI, WHEN BRAKE IS APPLIED A VIBRATION CAN ALSO BE FELT THROUGH THE AIRFRAME. PERFORMED TAXI CHECK, VERIFIED RT BRAKE VIBRATION. PERFORMED BRAKE BLEEDING IAW THE IAW MM 32-42-00. PERFORMED TAXI CHECK, VIBRATION STILL FOSDR DXTR20120808002Drum · crackedCABIN DOOR FWD COUNTERBALANCE CABLE DRUM CRACKED AT HUB.SDR DXTR20120808001Pulley Bracket · crackedRUDDER AUTOPILOT CABLE BRACKET, AT AFT CANTED BULKHEAD IS CRACKED ON INBD RIVET LINE. R & R RUDDER AUTOPILOT CABLE BRACKET IAW SRM 51-40-03 AND MM 22-11-01.SDR DXTA2012080605078Exhaust Duct · damagedHAD APU RUNNING, ACM OVERHEAT ILLUMINATED FOR A SECOND AND WENT OUT, AFTER 15 TO 25 SECONDS SMOKE FILLED THE CABIN AND COCKPIT FROM THE OVERHEAD VENTS. FOUND ACM EXHAUST DUCT ASSY MATERIAL COMING APART AND BLOCKING EXHAUST AIR FLOW. R & R EXHAUST DUCT ASSYSDR DXTA2012080305076Actuator · failedAFTER TAKEOFF, MLG HANDLE SELECTED UP, RED "UNLOCK" GEAR LIGHT ILLUMINATED. STAB MISCOMPAIR AND HYD PRESSURE LIGHT ALSO ILLUMINATED. MLG LOWERED NORMALLY FOR LANDING. TROUBLESHOOTING FOUND NOSE ACTUATOR ALLOWING THE GEAR TO LOCK BUT NOT FULLY SEAT TO DEPRESDR GB72012F00000Hose · deterioratedEN ROUTE, AT APPROX 41000 FT AGL, THE CABIN DOOR SEAL ANNUNCIATOR LIGHT ILLUMINATED. FLIGHT CREW FOLLOWED ACFT FLIGHT MANUAL AND DESCENDED BELOW 41000 FT AT WHICH POINT THE ANNUNCIATOR EXTINGUISHED. A NORMAL DESCENT, APPROACH AND LANDING WAS MADE. WHILE EXASDR DXTA2012080205072Wire · chafedSHORTLY AFTER TAKEOFF AN ODOR OF SMOKE APPEARED IN THE CABIN. ONE OF THE PASSENGERS ADVISED THAT THE FORWARD ENTRY LIGHT AT THE TOP OF THE STAIRS WAS ARCING. UPON LANDING WE FOUND THAT THE PLASTIC LENS WAS MELTED. FOUND FWD ENTRY LIGHT HAD CHAFED WIRE ARCING SDR DXTA2012073005069Wire Harness · chafedON TAXI, ANTI SKID LIGHT ILLUMINATED FOR ABOUT 1-2 SECONDS AND WENT OUT. SLOWED ACFT AND BRAKES SEEMED FINE. CONTINUED TO DECELERATE THE ANTI-SKID LIGHT ILLUMINATED AGAIN ALONG WITH THE MASTER CAUTION CAME ON. APPLIED THE BRAKES AND THE PEDALS WENT TO THE SDR DXTA2012073005068Cable · chafedAT APPROXIMATELY 9000 FT, AFTER TAKEOFF RECEIVED A LEFT ENGINE FIRE MASTER LIGHT, NO MASTER WARNING, PERFORMED MEMORY ITEMS AND LIGHT WENT OUT WHEN LEFT THROTTLE WAS BROUGHT TO IDLE. NO OTHER INDICATIONS. INSPECTED LT ENGINE AND FOUND FIRE DETECTOR CABLE CHSDR DGCA201207270002Garlock Seal · leakingOIL PRESSURE WARNING ANNUNCIATION, LOSS OF OIL PRESSURE. FOUND BREATHER TUBE GARLOCK SEAL TO BE ALLOWING OIL TO BE BLOWN OUT OF THE ENGINE.SDR 9JLA2012073103552Indicator · defectiveCREW REPORTED THE NR 1 ENGINE N2 INDICATOR WAS INTERMITTENT. REMOVED THE N2, OIL TEMP/PRESSURE INDICATOR, INSTALLED AN O/H UNIT. FUNCTIONAL CHECKS SATISFACTORY.SDR DXTA2012073005062Apu · leakingON TAKEOFF AND WHILE AT TAKE OFF POWER AND APU RUNNING, LIGHT FOWL SMOKE FILLED COCKPIT AND AIR FROM A/C WAS BLOWING HOT AIR. WHILE AVOIDING WEATHER AND WAITING TO LAND, SMOKE DISSIPATED AND A/C STARTED BLOWING COLD AGAIN. NO ANNUNCIATORS ILLUMINATED AND ALL SDR ZESA20120802Switch · intermittentPILOT WAS ON TAKEOFF AND APPROACHING V1 AND THE "NO TAKE OFF" WARNING ANNUNCIATED, PILOT ABORTED TAKEOFF. DETERMINED A SWITCH WITHIN THE RT WING SPEED BRAKE CAUSED THE ISSUE. BAD SWITCH AND CORROSION WITHIN THE CONNECTOR WERE REPAIRED. ACFT RETURNED TO SERVSDR DXTA2012072505057Valve · failedDURING TAKEOFF, AT ABOUT 300 FT AGL, THE ACM OVERHEAT LIGHT CAME ON FOLLOWED BY LT BLD AIR OVERHEAT. THERE WAS BLACK ACRID SMOKE IN THE COCKPIT AND CABIN. TURNED THE PRESS SOURCE TO OFF, DECLARED AN EMERGENCY AND LANDED. TURNING THE SOURCE TO OFF HELPED WITHSDR CVGA20120724002Lamp · burned outDID NOT GET A GREEN DOWN AND LOCKED INDICATION FOR THE NOSE WHEEL DURING APPROACH.SDR DXTA2012072305055Duct · contaminatedCREW ENCOUNTERED STRONG COCKPIT ODOR ALL PHASES OF FLIGHT, SMELLS LIKE BURNING RUBBER AND BURNED TOAST IN THE COCKPIT. COULD NOT IDENTIFY THE PROBLEM. REMOVED & CLEANED OZONE CONVERTER. OPS AND LEAK CHECKS GOOD. BORESCOPED INSIDE DUCT, FOUND B1/2 SEALANT ONSDR CA121105013Engine · power loss(CAN) DURING THE ROLLING TAKE OFF, THE ENGINE NR 2 DID NOT PRODUCE THE TAKE OFF POWER REQUESTED BY THE CREW. THE CREW ABORTED TAKE OFF AND SUBSEQUENT GROUND TEST CONFIRMED THE ISSUE ON THE NR 2 ENGINE. BLEED VALVE AND ITS TORQUEMOTOR WAS SUSPECTED.SDR DXTA2012071605052Sensor · inoperativeAFTER TAKEOFF, CLIMBING TO 3000 FT AT 160 KTS, THE GEAR RETRACTED, BUT THE RED GEAR UNSAFE LIGHT WAS ILLUMINATED. HYD PRESSURE AND STAB MISCOMPARE ILLUMINATED ALSO. CHECKLIST WAS CONSULTED FOR ALL ANNUNCIATIONS. SELECTED GEAR DOWN AND 3 GREEN AND NO RED UNSSDR DXTA2012071605051Speed Brake · dentedTHERE IS A LARGE DENT ALONG THE CENTERLINE OF BOTH THE TOP AND BOTTOM SPEEDBRAKES ON THE RT WING. THE SPEEDBRAKES OPERATE NORMALLY AND NO ISSUES WERE NOTED WHILE IN FLIGHT. REMOVED RIGHT WING LOWER SPEED BRAKE DUE TO DAMAGE (PN 6525101-4) AND INSTALLED A NEW SDR DXTA2012071305048Elevator System · frozenAFTER PLANE SAT IN HEAVY RAIN, DEPARTED AND STARTED CLIMB TO ALTITUDE. CLIMBING THROUGH MID 20000, NOTICED ELEVATOR STARTING TO BECOME STIFF. ADJUSTED TRIM AND TRIM WHEEL MOVED FINE. DECIDED TO LEVEL OFF AT FL360 AND ASSESS SITUATION. ACCELERATED ELEVATORSDR DXTA2012071205046Brake Assy · malfunctionedDURING SLOW SPEED TAXI AFTER CLEARING RUNWAY, ACFT SHUDDERED VIOLENTLY ABOUT 4 TIMES AS IF THE BRAKES WERE GRABBING. AFTER SOME DISCUSSION ABOUT POSSIBLE FLAT TIRES WE SLOWLY CONTINUED TO THE RAMP. FELT ONE MORE SLIGHT VIBRATION THROUGHT LT RUDDER PEDAL DURISDR DXTA2012070905042Unknown · odorDURING EARLY PART OF CLIMB AFTER SHUTTING OFF THE APU THERE WAS A FOUL ODOR IN THE COCKPIT THAT SMELLED ELECTRICAL IN ORIGIN. ODOR WAS LIMITED TO COCKPIT INITIALLY. RAN ENGINES FOR 45 MINS, WHILE RUNNING ENGINES HAD APU BLEED AIR ON AND NO SMELL NOTED. TURNSDR DXTA2012070905041Motor · inoperativePOWER BRAKE CIRCUIT BREAKER TRIPPED ON TAXI OUT. RESET AND SHORTLY THEREAFTER TRIPPED AGAIN. AFTER TURNING AROUND AND TAXING BACK TOWARD FBO, LOST ALL BRAKE PRESSURE. EMERGENCY BREAKS WERE UTILIZED WITH ONE APPLICATION. FOUND ANTI-SKID PUMP MOTOR FAULTY. SDR DXTA2012070905040Switch · inoperativeACM OVERHEAT WITH MASTER CAUTION ABOVE V1 ON TAKEOFF WITH EMERGENCY PRESSURE ACTIVATION DURING CLIMB. TAKOFF CONTINUED, RAN CHECKLIST AND LANDED NORMALLY. R & R ACM OVERTEMP SWITCH IAW MM 21-51-00. PERFORMED OPS, GOOD IAW MM 21-51-00.SDR CWQR20120705043Hinge Bracket · crackedDURING SCHEDULED MX, FOUND RT ELEVATOR OTBD HINGE BRACKET CRACKED. CRACK WAS FOUND USING EDDY CURRENT NDT METHOD, CRACK FROM THE EDGE OF THE PART INBD TO THE FIRST ATTACH HOLE IN THE LEG RADIUS.SDR DXTA2012070605033Control Handle · inoperativeSHORTLY AFTER GEAR RETRACTION, THE ANTI-SKID FAULT ANNUNCIATOR FLASHED AND THEN EXTINGUISHED, ENROUTE FLASHED AND EXSTINGUISHED AGAIN. DURING POST FLIGHT INSPECTION, CREW NOTICED ANTI SKID FAULT INDICATOR HAD TRIPPED. INDICATOR RT TRANSDUCER. FOUND LANDSDR DXTA2012070505029Actuator · failedON TAKEOFF GEAR WAS RETRACTED AND MAIN GEAR CAME UP ON SCHEDULE BUT NOSE GEAR REMAINED DOWN FOR APPROX 10 SECONDS. NO OTHER HYD SYS WAS IN USE (FLAPS REMAINED DOWN) UNTIL NOSE GEAR RETRACTED. THIS WAS NOT AN INDICATION PROBLEM VERIFIED BY WIND NOISE FROM NOSE SDR DXTA2012070505028Motor · inoperativeDURING TAXI OUT THE "ANTISKID INOP" LIGHT ILLUMINATED FOLLOWED SHORTLY THEREAFTER BY THE "PWR BRKS" CIRCUIT BREAKER POPPING. R & R THE HYD PUMP MOTOR IAW MM 32-44-20. OPS & LEAK CHECKED GOOD. TAXI CHECKED GOOD.SDR DXTA2012070505027Motor · burnedAFTER TAKEOFF, CLIMBING THROUGH 10000 FT, COCKPIT RECIRC FAN WAS SWITCHED ON HI. A STRONG ODOR OF BURNING AND MELTED PLASTIC WAS NOTED. FAN WAS TURNED OFF, BUT ODOR CONTINUED AND SEEMED TO GET STRONGER. NO SMOKE WAS NOTED. CO-PILOT NOTED A RATTLING SOUND CSDR CWQR20120627042Stiffener · crackedDURING A SCHEDULED INSPECTION, FOUND WEB ASSY CRACKED WHERE THE CABIN DOOR HANDLE ASSY ATTACHES TO IT WITH NUT PLATES. AFTER REVIEW OF IPC, DISCOVERED STIFFENER SHOULD HAVE BEEN INSTALLED ON THIS ACFT DURING PRODUCTION. INSTALLATION OF STIFFENER AND OTHER MSDR CA120628012Wheel Half · cracked(CAN) ON A BASE INSPECTION, MAINTENANCE FOUND THE RT MAIN WHEEL PRESSURE WAS LOW AT 40 PSI. THEY REPLACED WHEEL ASSY WITH REPAIRED UNIT. IT WAS INFLATED IT TO RATED PRESSURE AND THE ACFT WAS RELEASED FOR SERVICE. ON DISASSEMBLY BY PERSONS IN THE COMPONENT SHOP
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