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 CWQD201408213Bellcrank · wornNOSE WHEEL SHIMMY FROM 60KTS DOWN TO TAXI STOPPED. AFTER REMOVAL OF THE CABLES, IT WAS NOTED THAT THE UPPER HOLE IN THE BELL CRANK WAS ELONGATED & THE BACK SIDE OF THE BELL CRANK WHERE THE WASHER UNDER THE BOLT HEAD SITS WAS WORN INTO THE MATERIAL OF THE BELLSDR CA140826019Engine · fire(CAN) DURING REVENUE FLIGHT WHILE TAXIING, PILOT NOTICED AN ERRATIC RISE IN ITT INDICATION. AS ITT STARTED TO RAPIDLY RISE THE PILOT ELECTED TO SHUTDOWN THE ENGINE. PILOT DRY MOTORED THE ENGINE IAW CHECKLIST. AT THIS POINT, THE AIRCRAFT BEHIND, NOTIFIED GROUNSDR 2014FA0000483Fitting · crackedFOUND A CRACKED HORIZONTAL STAB PIVOT BOLT FITTING ASSY. WHICH WAS POSSIBLY CAUSED BY IMPROPER INSTALLATION OF THE LOWER SUPPORT CLIP. UPON REMOVING THE LOWER SUPPORT TEE CLIP WE NOTICED THE HOLES WERE ELONGATED A LITTLE SO WE REQUESTED FROM MFG STRUCTURES ENSDR YCOA2014FA0000526Uplock Switch · out of alignmentDURING DEPARTURE AND RAISING GEAR HANDLE, CREW NOTED "HYD PRESS" ANNUNCIATOR LIGHT REMAINED ON, 3 GREEN GEAR LIGHTS EXTINGUISHED, "GEAR UNLOCK" RED LIGHT REMAINED ILLUMINATED. GEAR WAS RECYLED DOWN THEN BACK UP, PROBLEM PERSISTED. CREW ADVISED APPROACH CONTRSDR DXTA2014081805859Brake Sys · contaminatedWHEN LEFT BRAKE APPLIED FIRST IT GRABS MOMENTARILY. WHEN BOTH BRAKES APPLIED SIMULTANEOUSLY OR RT BRAKE APPLIED FIRST, LT BRAKE DOES NOT GRAB. VERIFIED DISCREPANCY WHILE TAXIING THE ACFT TO MX & FOUND THE ACFT PULLS TO THE LT WHILE APPLYING BRAKES. INSPECTESDR 9JLA2014091004549Control Valve · defectiveON TWO SEPARATE OCCASIONS THAT DURING THE TAKEOFF ROLL THAT THE ACM OVERHEAT ANNUNCIATOR ILLUMINATED. ABORTED TAKEOFF ON BOTH OCCASIONS. THE CREW COMPLETED TROUBLESHOOTING ACTIONS & COULD NOT DUPLICATE THE FAULT. THE SUBSEQUENT TAKEOFFS WERE NORMAL. TROUBLSDR DXTA2014081205855Engine · leakingAT TAKEOFF POWER JUST AFTER V1 HAD A STRONG OILY ODOR IN CABIN. THE ODOR APPEARED TO DISSIPATE AT REDUCED POWER. ALL ENG INDICATIONS WERE NORMAL, APU WAS OFF. GND RAN AC AT TAKEOFF POWER & ISOLATED ENGS. APU & THEIR BLEED SELECTIONS. TROUBLE SHOT TO BURNTSDR DXTA2014081105854Unknown · odorVERY STRONG SMELL, NOT BURNING, MORE OF AN OILY SMELL. THE ODOR STAYED FOR THE ENTIRE FLIGHT. INSPECTED LT & RT ENGS FOR EVIDENCE OF OIL LEAKS, NONE FOUND. RAN LT & RT ENGS INDEPENDENTLY FOR APPROXIMATELY 5 MINUTES, EACH AT DIFFERENT POWER SETTINGS UP TO 65SDR 2014FA0000477Wire · frayedFLAPS STOPPED MOVING AT 7 DEGREES AND STABILIZER DIDN'T NOT MOVE TO POSITION FROM CRUISE. THRUST REVERSORS DID NOT DEPLOY ON LANDING. LOAD VALVE WIRES FRAYED ADJACENT TO VALVE. SHORTED AND TRIPPED HYDRAULIC CONTROL CIRCUIT BREAKER.SDR XCGA201408070014Control Handle · intermittentPILOT REPORTED THAT THE MLG WOULD NOT RETRACT. MAINTENANCE PERFORMED TROUBLESHOOTING. FAULT WAS DUPLICATED & FOUND TO BE INTERMITTENT. GEAR WOULD NOT GO UP & THE HYD DEMAND LIGHT WOULD NOT COME ON. FAULT WAS DETERMINED TO BE A DEFECTIVE MLG CONTROL HANDLE. SDR CWQD201408042Bellcrank · wornDURING TROUBLESHOOTING OF A STEERING KNOCKING SOUND, FOUND THE BOLT THAT ATTACHES THE CABLE TO THE STEERING BELLCRANK WAS ROCKING IN THE BELLCRANK. AFTER REMOVAL OF THE CABLES, IT WAS NOTED THAT THE UPPER HOLE IN THE BELLCRANK WAS ELONGATED & THE BACK SIDE OFSDR 9JLA2014091006971Solenoid · failedDURING PREFLIGHT OPERATIONS THE MAIN CABIN DOOR ANNUNCIATOR LIGHT WOULD NOT EXTINGUISH. THE SYS WAS TROUBLE SHOT & IT WAS FOUND THAT THE DOOR VENT SOLENOID HAD FAILED. THE SOLENOID PN 6711335-1 WAS REMOVED FROM SERVICE & A NEW UNIT WAS INSTALLED. OPERATION SDR DXTA2014072805834Apu · odorSMOKE WAS COMING INTO COCKPIT, WITH APU RUNNING, BLEED AIR ON OR OFF AND WITH ENGINE RUNNING. REMOVED AND REPLACED APU IAW MM 49-10-00. OPS AND LEAK CHECKED GOOD.SDR CA140804008Engine · failed(CAN) DURING REVENUE FLIGHT, CLIMBING OUT AT 5000 FT, A LOUD NOISE WAS HEARD ALONG WITH ITT AT RED LINE ON 1 OF THE ENGINES. AFTER A FEW SECONDS, THE POWER WAS REDUCED TO KEEP THE ITT IN NORMAL RANGE. THE FLIGHT WAS ABORTED AND THE ACFT RETURNED TO POINT OF SDR 9JLA2014072404547Washer · wornDURING MX TO CHANGE TO NLG WHEEL IT WAS DISCOVERED THAT THE AFT ATTACH POINT FOR THE NLG ACTUATOR HAD EXCESSIVE PLAY. INSPECTION FOUND THE AFT ATTACH POINT ELASTOMER WASHERS PN 6242217-1 BADLY WORN. NEW ELASTOMER WASHERS WERE INSTALLED. THIS SAME DISCREPANCSDR DXTA2014072205826Motor · failedDURING FLIGHT, ANTI-SKID INOPERATIVE ANNUNCIATOR LIGHT ILLUMINATED. LANDED AFTER RUNNING ABNORMAL CHECKLIST. LOST BRAKES AFTER LANDING, LOW BRAKE ANNUNCIATOR LIGHT ILLUMINATED & POWER BRAKES CIRCUIT BREAKER TRIPPED. USED THE EMERGENCY BRAKE HANDLE TO STSDR DXTA2014080605847Unknown · malfunctionedRETRACTED GEAR ON DEPARTURE & WE GOT A GEAR UNSAFE RED LIGHT & NOSE WHEEL DOWN & LOCKED GREEN LIGHT. MAIN GEAR RETRACTED NORMALLY. NO OTHER ABNORMAL INDICATIONS. BY THE SOUND & FEEL OF IT, NOSE WHEEL GEAR NEVER UNLOCKED. NORMAL LANDING WITH THREE GREEN & NSDR DXTA2014070805813Brake · malfunctionedWHEN PRESSING ON THE LT BRAKE AT 15 KTS OR ABOVE, THE AIRPLANE SHUTTERS. HAPPENS WHEN PUSHING ON BOTH BRAKES SIMULTANEOUSLY, BUT NOT ON THE RT BRAKE ONLY. TROUBLESHOT BRAKES, BLED RT & LT BRAKES, PER MM. TAXI AND LEAK CHECKED GOOD.SDR DXTA2014070705810Seal · failedDURING CLIMB OUT PASSING 18000 WITH ICE PROTECTION ON, RECEIVED A RT ENGINE FIRE LIGHT. LEVELED OFF PROCEEDED WITH CHECKLIST, WHEN THE POWER WAS PULLED BACK, AROUND HALF WAY, LIGHT EXTINGUISHED. NO SECONDARY INDICATIONS WERE SEEN. LIGHT OFF FOR REST OF FLISDR DXTA2014070705811Apu · malfunctionedAPU WAS STARTED NORMALLY FOR POST FLIGHT DUTIES, AFTER TWO OR THREE MINUTES A STRONG ODOR WAS NOTED FROM THE ENVIRONMENTAL SYS & THE APU SHUT ITSELF DOWN. REMOVED AND REPLACED APU IAW MM 49-10-00. OPS AND LEAK CHECKED GOOD.SDR CWQR20140630004Hinge · crackedDURING A SCHEDULED INSPECTION, TECHNICIAN WAS INSPECTING THE RUDDER HINGES. ON THE UPPER RUDDER ATTACH HINGE, THE LOWER HINGE HALF HE FOUND A 0.21 INCH CRACK FROM THE BRACKET EDGE EXTENDING TOWARDS THE FIRST ATTACHMENT HOLE. RUDDER HINGE HALF WAS REMOVED & ASDR Z5FA2014070356801Warning System · false activationAT APPROX 80KTS ON TAKEOFF ROLL CREW OBSERVED A MASTER WARNING LIGHT & SAW A RED ANNUNCIATOR LIGHT, BATTERY OVERHEAT. ABORTED THE TAKEOFF & UNEVENTFULLY TAXIED CLEAR OF THE RUNWAY. THE APU HAD SHUT ITSELF DOWN & THE APU FIRE DETECTION CB HAD POPPED. NOT ABLSDR CA140701016Oil System · low pressure(CAN) DURING FLIGHT, THE PILOT ELECTED TO SHUTDOWN THE ENGINE NR 2 DUE TO OIL PRESSURE LOSS. THE PILOT PERFORMED AN UNEVENTFULLY SINGLE ENGINE LANDING. TROUBLESHOOTING ONGOING.SDR CA140711008Oil System · low pressure(CAN) DURING THE CRUISE, PORTION OF THE FLIGHT THE CREW NOTICE THE LT ENGINE OIL PX. A NOTICE 30 SEC DROP IN OIL PX. 50 PSI WHICH RETURN TO NORMAL WITH NO OTHER ABNORMAL INDICATION. AFTER 15 TO 20 MINUTES DURING CRUISE THE LT OIL PRESSURE BEGIN TO SLOWLY DROP,SDR CA140701007Warning Message · activated(CAN) DURING CRUISE, PILOT REPORTED LOSS OF OIL PRESSURE INDICATION AND ELECTED TO SECURE THE ENGINE. AN UNEVENTFUL SINGLE ENGINE LANDING PERFORMED.SDR CA140701006Engine · overtemp(CAN) THE PILOT ABORTED THE TAKEOFF DUE TO THE LT ENGINE ITT INDICATOR BAND MOVE TO RED ENGINE TEMPERATURE LIMIT AND THE WHITE INDICATOR BAND TURNED TO RED. ALL OTHER ENGINE INSTRUMENTS DISPLAYED NORMAL INDICATIONS PRIOR TO TAKING THE RUNWAY. TROUBLESHOOTISDR DXTA2014062605808Cylinder · leakingRIGHT BRAKE MAKES A LOUD SQUEAL DURING APPLICATION. EVEN APPLICATION OF BRAKE PEDALS RESULTS IN UNEVEN BRAKING. TAXIED AIRCRAFT AND DID NOT HEAR ANY SQUEAL FROM RIGHT OR LEFT BRAKES. JACKED AIRCRAFT AND REMOVED LEFT AND RIGHT WHEEL ASSEMBLIES, SET BRAKES ANDSDR CA140714007Tire · failed(CAN) CREW REPORTED JUST PRIOR TO ROTATION, FELT A SLIGHT PULL LEFT CAUSING PILOT FLYING TO APPLY SLIGHT RT RUDDER. DURING CLIMB-OUT, CENTER ADVISED CREW THAT THEY HAD FOUND RUBBER ON (DEPARTURE) RUNWAY. FLEW LOW OVER RUNWAY FOR INSPECTION, TOWER CONFIRMED ALLSDR 9JLA2014072106970Switch · defectiveTHE CREW REPORTED THE CABIN DOOR ANNUNCIATOR ILLUMINATED & WOULD NOT EXTINGUISH. TROUBLESHOOTING FOUND THE PAX DOOR LOWER AFT PIN SWITCH PN A4-18EM4111 DEFECTIVE. THE SWITCH WAS REPLACED WITH NEW, FUNCTIONAL CHECKS SATISFACTORY.SDR DXTA2014062505807Brake · malfunctionedDURING TAXI THE LT BRAKE IS VERY SENSITIVE & GRABBING. IT WAS OBSERVED DURING LANDING ROLLOUT & TAXI IN. BLED LT BRAKE SYSTEM, SERVICED BRAKE RESERVOIR. OPS AND LEAK CHECKED GOOD IAW 32-42-00.SDR DXTA2014062305805Landing Gear · malfunctionedDURING APPROACH, SELECTED GEAR DOWN. MAIN GEAR EXTENDED NORMAL BUT THE NOSE GEAR DID NOT EXTEND. WHILE RUNNING THE LANDING GEAR WILL NOT EXTEND CHECKLIST, NOTICED WHEN TEE HANDLE IS PULLED, THERE WAS NO RESISTANCE. FELT NOTHING WHEN PULLED DOUGHNUT TO BLOW SDR DXTA2014062305804Brake Assy · failedLEFT MAIN TIRE FAILED ON LANDING ROLL OUT. SUSPECT FAILURE OF ANTISKID. LT BRAKE APPEARS TO HAVE LOCKED UP. R & R LT BRAKE WITH OVERHAULED UNIT IAW MM 32-42-01. PERFORMED BLEED OF LT BRAKE IAW MM 32-42-00. OPS & LEAK CHECKED GOOD.SDR CA140630014Unknown · vibration(CAN) DURING REVENUE FLIGHT IN CRUISE, THE CREW FELT A HIGH VIBRATION IN THE CABIN AND ELECTED TO DIVERT. AN UNEVENTFUL LANDING WAS CARRIED OUT. TROUBLESHOOTING IN PROGRESS. BOROSCOPE OF THE ENGINE IS UNDERWAY.SDR Z5FA2014061954901Downlock Switch · defectiveCLIMBING THROUGH FL 240, THE LOW BRAKE PRESS & ANTI-SKID ANNUNCIATOR ILLUMINATED. CREW PERFORMED ABNORMAL CHECKLIST. NOTIFIED ATC OF SITUATION. DIVERTED DID NOT DECLARE AN EMER BUT REQUESTED EMER VEHICLES TO BE STANDING BY. THE TOWER DECLARED AN EMER ACFT SDR DXTR2014061702Check Valve · stuckONE HALF OF EMERGENCY PRESSURIZATION CHECK VALVE INOPERATIVE DUE TO USE OF RTV SEALANT INSTEAD OF GASKET. THE APPLIED RTV SEALANT OOZED INTO CHECK VALVE, DURING THE INSTALLATION PROCESS AND SEALED FLAPPER IN THE CLOSED POSITION. R & R EMERGENCY PRESSURIZATIOSDR DXTR2014061701Bracket · crackedRUDDER AUTOPILOT SERVO CABLE PULLEY BRACKET IS CRACKED. R & R RUDDER AUTO PILOT SERVO CABLE PULLEY BRACKET IAW SRM 51-40-03.SDR DXTA2014061605801Uplock Switch · failedAFTER GEAR RETRACTION ON TAKEOFF, RED GEAR UNSAFE LIGHT REMAINED ON. HYD PRESSURE LIGHT BEGAN FLASHING. PUT GEAR BACK DOWN USING THE NORMAL EXTENSION PROCEDURE. HYD PRESSURE & GEAR UNSAFE LIGHTS BOTH EXTINGUISHED. EXECUTED A NORMAL LANDING. HYD RESERVOIRSDR DXTA2014061205800Oil System · leakingDURING APU STARTUP, SMOKE ENTERED CABIN THROUGH WEMACS. SHUTDOWN APU. RAN APU, STILL HAD HEAVY SMOKE IN CABIN. FOUND APU INLET TO BE COATED WITH OIL. OIL FLUID LEVEL EXTREMELY BELOW MINIMUM LINE AFTER A FIVE MINUTE APU RUN. RAN BOTH ENGINES AT HIGH POWER WISDR CA140620004Engine · malfunctioned(CAN) AT 10,000 FT. WITH POWER IN CRUISE SETTING, THE MASTER WARNING ILLUMINATED WITH A FLASH OF "LOW OIL PRESSURE RT". THE CREW OBSERVED A LOW OIL PRESSURE FROM THE RIGHT HAND ENGINE AND THEY REDUCED POWER AND ANNUNCIATOR EXTINGUISHED. THE CREW CONTINUED NORMSDR Z5FA2014060854901Window · failedAT FL 280 DURING DESCENT, LEFT COCKPIT WINDOW FAILED. NO EMERGENCY WAS DECLARED & ACFT LANDED SAFELY. WINDOW REPLACED, LEAK & OPS CHECKED SATISFACTORILY, ACFT RETURNED TO SERVICE.SDR CA140620002Engine · power loss(CAN) ON TAKEOFF ROLL, THE RIGHT ENGINE WOULD NOT MAKE RATED POWER OF 90.1.%N1. THE ENGINE ONLY RAISED ABOUT 80% N1. THE TAKEOFF WAS ABORTED.SDR DXTA2014060505791Relay · failedON TAXI OUT RECEIVED FLASHING LOW BRAKE PRESSURE & ANTI SKID INOPERATIVE ANNUNCIATORS. ABOUT 20 SECONDS LATER, LOST NORMAL BRAKES, BRAKE PEDALS LOST PRESSURE & WENT TO THE FLOOR. HAD TO USE EMERGENCY BRAKE SYS TO STOP ACFT. SHUT DOWN ACFT & HAD TO BE TOWED SDR DXTA2014052805783Display · odorAFTER TAKEOFF AROUND 200 FT AGL, A STRONG ODOR OF BURNING ELECTRIAL WAS NOTICED BY CREW MEMBERS. THE MFD WHICH HAD JUST BEEN ON MEL & HAD A BLACK SCREEN, STARTED FLASHING OFF & ON. CREW CONTINUED WITH NORMAL DEPARTURE UNTIL THROUGH APPROXIMATELY 5000 FT. FISDR DXTA2014052705782Wire Harness · damagedRIGHT ENGINE VIBRATION ANNUNCIATOR ILLUMINATED IMMEDIATELY AFTER TAKEOFF. NOTICEABLE ACFT TREMOR WAS FELT IN THE CONTROLS. TROUBLESHOT AND COMPLIED WITH ENGINE VIBRATION SURVEY IAW MCC AND MANUFACTURER. REMOVED AND REPLACED RTH ENGINE. COMPLIED WITH OPS CHESDR 2014FA0000357Support Tube · bindingTWO OF THE IGNITOR SUPPORT TUBES WERE IN A BIND AND COULD NOT BE REMOVED, ONE PER ENGINE. WERE ABLE TO REMOVE ONE SUPPORT TUBE ON EACH ENGINE. WITH THE TUBES REMOVED, IT APPEARS THAT THE COMBUSTION CHAMBER HAS SHIFTED, AND MIS-ALIGNED ITSELF WITH THE GAS GENSDR DXTA2014052005777Brake Sys · unknownAFTER LANDING AND DURING TAXING ONTO RAMP, THE RT BRAKE ON MAIN GEAR WAS HANGING UP WHEN THE BRAKE PEDAL WAS PUSHED. ACFT WOULD SHAKE & SHUTTER. HAPPENED 5 TO 6 TIMES. VISUAL INSPECTION PERFORMED ON ANTI-SKID BRAKE SYS, NO DEFECTS NOTED. BRAKES BLEED PROCSDR DXTA2014052005774Spring · failedWITH EQUAL PRESSURE APPLIED TO BOTH BRAKE PEDALS, ACFT PULLS HARD TO THE LEFT. FOUND THAT BRAKES HAD A BROKEN RETURN SPRING AT LT POWER BRAKE METERING VALVE ACTUATION ARM. R & R SPRING, OPS CHECKED GOOD IAW MM 32-44-10.SDR DXTA2014051505773Door · unsecureON TAKEOFF & CLIMB THROUGH 1000 FEET, THERE WAS A PRESS BUMP, FOLLOWED BY WIND NOISE & THE DOOR SEAL & CABIN DOOR ANNUNCIATORS COMING ON. WE DID NOT CLIMB ABOVE 1500 FEET. ON DESCENT FOR LANDING, THE DOOR OPENED FULLY & IT MADE CONTACT WITH THE RUNWAY DURINGSDR CA140602010Engine · overheated(CAN) JUST AFTER TAKEOFF, THE PILOT OBSERVED A HIGH ITT. THE HIGH ITT CAME BACK EVERY TIME PILOT RETARDED AND SLOWLY INCREASED THE THROTTLE. THE PILOT ELECTED TO DIVERT. DURING THE REST OF THE FLIGHT HE KEPT THE THROTTLE AT A REDUCED THRUST TO KEEP THE ITT LSDR 9JLA201405210389Actuator · failedWHILE CROSS FEEDING FUEL FROM THE LT WING TANK TO THE RT ENG THE RT ENG FUEL BOOST LIGHT BEGAN FLASHING THEN REMAINED ON. AFTER TURNING CROSS FEED OFF, BOTH BOOST PUMPS REMAINED ON. TROUBLESHOOTING FOUND THE CROSS FEED VLV ACTUATOR ASSEMBLY DEFECTIVE PN 9914
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