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 DXTA2018120301742Uplock · inoperativeALL LANDING GEAR RETRACTION DID NOT RETRACT - AFTER GEAR RETRACTION, THE GEAR UNLOCK LIGHT REMAINED ILLUMINATED. QRH CHECKLIST WAS ACCOMPLISHED. ADDITIONAL INFO...SQ 47339: JACKED AIRCRAFT. HOOKED HYDRAULIC MULE. PERFORMED GEAR SWINGS. NOTED NO DEFECTS WITH SDR DXTA2018113001738Strut · not extendedALL LANDING GEAR RETRACTION - GEAR WOULD NOT COME UP, GEAR UNSAFE WITH HYD PRESS LIGHT ILLUMINATED, RAN THE APPROPRIATE CHECKLIST CAME BACK AND LANDED WITHOUT EVENT. NOTE, IT WAS NOT AN OVERWEIGHT LANDING.//JACKED AIRCRAFT AND FOUND NOSE STRUT NOT FULLY EXTENDSDR DXTA2018112901730Coalescer Bag · odorCOCKPIT ODOR BURNING SMELL - THERE IS A STRONG SMELL OF FUMES IN THE COCKPIT AND CABIN. THERE IS A SMELL OF EXHAUST OR BURNT FUEL THAT COMES AND GOES IN THE AIRCRAFT, STRONG ENOUGH THAT IT MAKES YOUR EYES BURN. IT IS STRONGER WHEN THE THERMOSTAT KICKS THE HEATSDR O2GA201812035101Valve · intermittentDURING APPROACH SPEDD BRAKES WOULD NOT DEPLOY, FLAPS WOULD NOT MOVE AND LANDING GEAR WOULD NOT DEPLOY. NO WARNING ANNUNCIATORS ILLUMINATED AND CIRCUIT BREAKERS WERE NOT TRIPPED. CREW FOLLOWED THE NO FLAPS AND LANDING GEAR EXTENSION PROCEDURE PER CHECKLIST. EMESDR DXTA2018112601719Unknown · odorAT GEAR RETRACTION THE LO HYD LVL LIGHT ILLUMINATED. GEAR AND FLAPS RETRACTED NORMALLY WITH LIGHT ILLUMINATED.
LIGHT WENT OUT WHEN GEAR WAS EXTENDED. GEAR AND FLAPS EXTENDED NORMALLY. POST FLIGHT INSPECTION SHOWS LOW HYDRAULIC
FLUID LEVEL AND POSSIBLE BURNINSDR DXTA2018112601707Connector · looseRED GEAR ANNUNCIATOR REMAINED ON AFTER GEAR RETRACTION CAUSING THE HYD SYSTEM TO REMAIN PRESSURIZED. STAB MIS COMP ANNUNCIATION ILLUMINATED SHORTLY AFTER. AFTER PULLING THE HYD CONTROL CB "PER XLS QRH" THE NOSE AND LEFT MAIN GEAR EXTENDED. ALL HYDRAULIC SYSTEMSDR DXTA2018112601706Display · odorBURNING SMELL IN COCKPIT SECOND DAY IN A ROW. W/O T2PL6D006BYNF PERTAINS. THEN MFD WENT BLANK AT 1+50 OF 3.0 FLIGHT. BURNING SMELL CEASED WITH MFD FAILURE. SUPPLEMENTAL INFORMATION: REMOVED & REPLACED MFD..P/N OFF: 7023460-05001 / S/N OFF: 06022851 - P/N SDR 9JLA2019021210727Sensor · failedFLIGHT CREW REPORTED THAT THE LH ENGINE ANTI-ICE ANNUNCIATOR WAS SLOW TO EXTINGUISH AFTER SYSTEM WAS ACTIVATED.TROUBLESHOOTING DETERMINED THAT THE LH ENGINE INLET ANTI-ICE TEMP SENSOR WAS DEFECTIVE. THE SWITCH AS REPLACEDSDR CVGA20181116002Torque Tube · corrodedFOUND LH ELEVATOR TORQUE TUBE CORRODED. REMOVED AND REPLACED LH ELEVATOR TORQUE TUBE IAW CESSNA 560XL SRM 51-40-03.SDR CVGA20181116001Torque Tube · corrodedFOUND RH ELEVATOR TORQUE TUBE CORRODED. REMOVED AND REPLACED RH ELEVATOR TORQUE TUBE IAW CESSNA 560XL SRM 51-40-03.SDR CVGA20181108001Connector · looseFLIGHT CREW HEARD A POP THAT SOUNDED LIKE THE PRESSURIZATION WAS FAILING. CREW DECLARED AN EMERGENCY AND STARTED AN EMERGENCY DESCENT TO 11000 FEET. MAINTENANCE FOUND LINES TO SECONDARY OUTFLOW VALVE TO BE LOOSE. LINES COULD NOT BE TIGHTENED. INSTALLED 2 EACH SDR DXTA2018102901608Display · overheatedON ARRIVAL AT GXY, DESCENDING THRU 27000 THE RIGHT PFD WENT BLANK AND CAME BACK ON ABOUT 2 SECONDS LATER. THERE WAS A HOT ELECTRICAL ODOR BRIEFLY, NO SMOKE WAS DETECTED. I FELT AROUND AND UNDER INSTRUMENT PANEL AND NOTHING FELT HOT. CORRECTIVE ACTION: REMOVED SDR JGVR2018102901Service Door · crackedLEVEL 1 CORROSION ON TOILET SERVICE DOOR AROUND LATCHES AND FOUND A CRACK IN DOOR BELOW FWD LATCH.SDR JGVR20181027001Link · corrodedDURING THE REMOVAL OF THE LT MLG TRAILING LINK HINGE PIN FOUND THE ATTACHING CLEVIS POINTS TO BE CORRODED. REMOVED CORRODED LT MLG TRAILING LINK AND INSTALLED A NEW LINK.SDR JGVR20181026001Access Panel · crackedREMOVED CRACKED VERTICAL STABILIZER ACCESS PANEL 340ER AND INSTALLED NEW P/N 5531005-3.SDR CVGA20190125004Torque Tube · corrodedFOUND RT ELEVATOR TORQUE TUBE HAS CORROSION. REFERENCE AMM 27-31-01.SDR CVGA20190125003Torque Tube · corrodedFOUND LT ELEVATOR TORQUE TUBE HAS CORROSION. REFERENCE AMM 27-31-01.SDR DXTA2018101601559Motor · failedBRAKE PRESSURE LIGHT ILLUMINATED - UPON FINAL APPROACH FIX INBOUND ON THE GPS RWY 23 APPROACH, THE LOW BRAKE PRESSURE/ANTI SKID LIGHT ILLUMINATED AND STAYED ILLUMINATED TILL WE INITIATED THE MISSED APPROACH. AT WHICH TIME WE DECLARED AN EMERGENCY RAN THE CHECSDR 2018FA0000471Jam-Nut · looseAIRCRAFT DEPARTED RNY 33 AT KPNE FOR KLOM. UPON LIFTOFF, PILOT NOTED CONCERN AND SUSPECTED A FLAT MAIN TIRE OR DRAGGING BRAKES. DECLARED EMERGENCY AND RETURNED TO KPNE. DURING LANDING ROLL-OUT, AND WHILE APPROACHING TAXI SPEEDS, A/C VEERED RT AND CAME TO A FULSDR DXTA2018100801517Pump · faultyANTI-SKID LIGHT CAME ON 3 MILE FINAL 30L KSJC. RAN CHECKLIST. LANDED. ANTISKID CB POPPED OUT. ON TAXI IN LO BRK PRESS LIGHT CAME ON. USED AIR BRAKE TO PARK PLANE AS I HAD NO BRAKES LEFT TO STOP. SUPPLEMENTAL INFORMATION - REMOVED AND REPLACED BRAKE HYDRAULIC SDR JGVR20181004001Spar Cap · corrodedFOUND CORRODED FORWARD SPAR LT SPAR CAP OF THE VERTICAL STABILIZER. REPLACED THE FORWARD SPAR LT SPAR CAP WITH NEW P/N 6631216-1, REPLACED RIB WITH NEW P/N 5531030-14, REPLACED RIB WITH NEW P/N 6631221-6, AND REPLACED RIB WITH NEW P/N 6631228-7.SDR JGVR20181003001Door · corrodedBLENDED CORROSION ON THE MAIN ENTRY DOOR (MED) SPADE DOOR AND SUBMITTED FINDING. REPLACED MED SPADE DOOR WITH NEW P/N 6611333-41-1 REFERENCING MM 52-10-05 AND SRM 51-00-03, 51-40-03, 51-40-06, 51-40-08, AND 51-40-09.SDR DXTA2018093001484Apu · smokeAPU FILLED INTERIOR OF AIRCRAFT WITH SMOKE JUST WE TOOK THE RUNWAY FOR DEPARTURE.SDR 9JLA2018081005369Servo Valve · defectiveAN ABORTED TAKE-OFF WAS REPORTED AFTER THE RIGHT ENGINE ELECTRONIC FUEL CONTROL INDICATED A FAULT. ANOTHER TAKEOFF WAS ATTEMPTED, BUT IT ALSO WAS ABORTED DUE TO THE SAME ENGINE ECU FAULT. AFTER CONSULTING WITH XXX BASE MAINTENANCE, THE TRIP WAS ALLOWED TO CONTSDR DXTA2018092101444Brake Sys · contaminatedMLG BRAKE PRESSURE, BRAKING ON LANDING ROLLOUT IS WEAK AT SLOWING AIRCRAFT. ALSO EXCESSIVE FORCE IS NEEDED WHEN DOING BRAKE ASSISTED TURNS. BLED LT & RT BRAKE ASSEMBLIES IAW MM 32-32-00. TAXI CHKS GOOD AT THIS TIME.SDR 2019F00070Skin Panel · damagedREPAIR TO LT AND RT WING LOWER SKIN DAMAGE. REPAIR DEFINITION DQ15836M1 DATED SEPTEMBER 20, 2018.SDR 2019F00069Skin · damagedREPAIR OF RIGHT WING LEADING EDGE FASTENER PULLED THROUGH SKIN. REPAIR DEFINITION DQ15823M1 DATED SEPTEMBER 19, 2018.SDR JGVR20180920001Hinge · corrodedREMOVED MED AFT HINGE HALF, P/N UNKNOWN, FROM AIRCRAFT SIDE DUE TO LEVEL 2 CORROSION. INSTALLED NEW CUSTOMER SUPPLIED MED HINGE HALF P/N 6611037-1 PER SRM 51-40-03, 51-40-06, 51-40-08, 51-40-09, AND MM 20-32-00.SDR JGVR20180914001Spar Cap · corrodedREPAIRED CORRODED AREA ON THE LT FWD VERTICAL STABILIZER SPAR CAP, WHERE ACCESS PANEL 340ATC ATTACHES, BY BLENDING, TRIMMING SPAR WEB AND CHAMFERING THE SPAR CAP, TREATING AND PRIMING IAW FIELD REPAIR FR-560-5568-4523 REVISION (-) APPROVED BY FAA FORM 8100-9 DSDR DXTA2018091401427Converter · defectiveAFTER TAKEOFF CLIMBING THROUGH 10000' WE SHUT DOWN THE APU AND IMMEDIATELY SMELLED A VERY STRONG ODOR OF BURNING OIL OR SOME OTHER CHEMICAL. THE APU RAN FOR ABOUT 45 MINUTES PRIOR WITHOUT ANY ODOR. REMOVED & REPLACED LT & RT OZONE CONVERTERS IAW MM 27-71-00. OSDR CVGA20180918001Actuator · corrodedTHE FOLLOWING INCIDENT HAPPENED IN FLIGHT, CREW WRITE UP“ NOSE WHEEL TRIM STUCK. WON’T MOVE FORWARD DID NOT MOVE BACK, COULD NOT MOVE WHEEL ANY FURTHER AND USED PHYSICAL FORCE TO LOWER NOSE. AN EMERGENCY WAS DECLARED AT THAT TIME AND THEY LANDED SAFELY. AFTER SDR DXTA2018090701390Apu · malfunctionedDURING PRE DEPARTURE CHECKS AND JUST PRIOR TO STARTING ENGINES, HARMONIC SOUND WAS COMING FROM APU. (WINDY COOL DAY AT KSFO). WHILE COMPLETING BEFORE 'ENGINE START CHECK' APU ABRUPTLY/INSTANTANEOUSLY SHUT DOWN. RPM WENT INSTANTLY TO 05 RPM NO EXCEEDANCE OR OTHSDR JGVR20180904001Stiffener · crackedREMOVED CRACKED STIFFENER FROM MED UPPER WEB ASSEMBLY AND INSTALLED NEW P/N 661039-2 USING MS20426AD4, MS20470AD4, MS20426AD5, AND MS20470AD5 RIVETS REFERENCING STRUCTURAL REPAIR MANUAL 51-40-03 AND 51-40-06.SDR DXTA2018090501385Manifold · leakingCOCKPIT ODOR, JET FUEL ODOR COMING FROM OVERHEAD VENTS. NOTICEABLE WITH APU RUNNING ON THE GROUND AND ALSO DURING FLIGHT WITHOUT APU. REMOVED & REPLACED LEAKING APU FUEL MANIFOLD & TEE FLOW DIVIDER IAW M/M 49-30-06. APU OPS & LEAK CHK GOOD.SDR DXTA2018090501382Manifold · leakingGAS SMELL COMING FROM GASPERS IN COCKPIT ENTIRE FLIGHT. FOUND FUEL MANIFOLD LEAKING. INSTALLED NEW FUEL MANIFOLD ASSY SECONDARY TUBE P/N: 3883899-1.SDR CVGA2018090500002Speed Switch · faultyDURING CRUISE FLIGHT AT FL430, HYD PRESS LITE ILLUMINATED ON ANNUNCIATOR PANEL, TWO OR THREE MINUTES LATER THE STAB MISCOMPARE LITE ALSO ILLUMINATED ON ANNUNCIATOR PANEL. COMPLIED WITH BOTH EMER/ABNORMAL CHECKLISTS. DIVERTED AND LANDED SAFELY. REMOVED AND REPLSDR CVGA20180905001Connector · corrodedDURING CRUISE FLIGHT AT FL430, ANTI-SKID INOP LIGHT APPEARS ON ANNUNCIATOR PANEL. COMPLIED WITH EMER/ABNORMAL CHECKLIST. DIVERTED AND LANDING SAFELY. CLEANED CORROSION FROM CONNECTOR ON RT MLG ACTUATOR AND PERFORMED OPERATIONAL CHECK OF ANTI SKID SYSTEM IAW AMSDR DXTA2018090401375Shutoff Valve · faultyDURING TAKE OFF 10KTS BEEFIER V1 AIRCRAFT PULLED HARD RIGHT, CORRECTED WITH FULL LEFT RUDDER MAINTAINED CONTROL, ROTATED MADE NORMAL CLIMB, CRUISE, DESCENT, LANDING OK. REMOVED AND REPLACED RUDDER BIAS ACTUATOR AND RUDDER BIAS CONTROL VALVE OPS AND LEAK CHECKSSDR O2GA2018090150901Actuator · failedIMMEDIATELY AFTER TAKEOFF EXCESSIVE FORWARD PRESSURE WAS REQUIRED TO PREVENT THE AIRCRAFT FROM PITCHING UP. THE POWER WAS PULLED BACK TO 60% AND TRIM ALMOST FULL FORWARD TO MAINTAIN CONTROLLED CLIMB. EMERGENCY DECLARED AND DIVERTED BACK TO KMCO. LANDING WAS UNSDR DXTA2018082701349Unknown · odorODOR DETECTED, WAS SIMILAR TO A NEW CAR MOTOR BURNING WHEN IT'S BEEN RUN FOR THE FIRST TIME AND GETS HOT. APU HAD BEEN RUNNING PRIOR TO TAKE OFF, BUT DIDN'T NOTICE ANYTHING BEFORE SHUTTING IT DOWN. CLEANED THE OZONE FILTER, NO ODOR.SDR CVGA20180920002Torque Tube · corrodedFOUND RT ELEVATOR TORQUE TUBE CORRODED. REMOVED AND REPLACED ELEVATOR TORQUE TUBE IAW AMM 27-31-01 AND SRM 55-20-01.SDR CVGA20180920001Torque Tube · corrodedFOUND LT ELEVATOR TORQUE TUBE CORRODED. REMOVED AND REPLACED ELEVATOR TORQUE TUBE IAW AMM 27-31-01 AND SRM 55-20-01.SDR DXTA2018081701311Coalescer Bag · dirtyWHILE RUNNING APU WITH THE BLEED AIR OFF, DURING HEAVY RAIN THE CABIN FILLED WITH SMOKE WITH THE ODOR OF OIL. FOUND THE COALESCER SOCK DIRTY. REMOVED AND REPLACED THE COALESCER SOCK.SDR CVGA20180809001Skin · crackedLOWER LEFT OF RUDDER LEADING EDGE WAS FOUND TO BE SCRATCHED. REMOVED PAINT AND FOUND A CRACK IN LEADING EDGE SKIN. CRACK WAS BEYOND LIMITS AND THE LOWER LEADING EDGE SKIN WAS REPLACED.SDR DXTA2018072501228Engine · malfunctionedCABIN ODOR BURNING SMELL, COPILOT COMPLAINED ABOUT SOMETHING BOTHERING HIS EYES WHILE CLIMBING OUT WITH APU OFF AND I DIDN'T NOTICE ANYTHING AT THAT TIME. WHILE SITTING ON THE GROUND IN LAS APU ON WITH BLEED AIR ON WE BOTH COULD DETECT WHAT SMELLED LIKE A BURNSDR DXTA2018072302013Converter · dirtyCOCKPIT ODOR BURNING SMELL - AFTER TAXI OUT, WE SMELLED A SMOKY ODOR COMING FROM OVERHEAD GASPER VENTS. OPENED COCKPIT WINDOW TO VERIFY IT WAS NOT AN OUTSIDE SOURCE. WHEN WE WENT INTO CABIN TO CHECK, THE FRONT OVERHEAD VENTS HAD THE ODOR EVEN STRONGER. CLEANEDSDR CVGA20181005002Torque Tube · corrodedFOUND RT ELEVATOR TORQUE TUBE CORRODED. REMOVED AND REPLACED RT ELEVATOR TORQUE TUBE IAW SRM 51-40-03.SDR CVGA20181005001Torque Tube · corrodedFOUND LT ELEVATOR TORQUE TUBE CORRODED. REMOVED AND REPLACED LT ELEVATOR TORQUE TUBE IAW SRM 51-40-03.SDR JGVR20180718001Fitting · corrodedMECHANICALLY BLENDED 8 AREAS CORROSION ON LT AND RT HORIZONTAL STAB PIVOT FITTINGS 6631102-29 AND -30, PERFORMED ULTRASONIC AND EDDY CURRENT INSPECTIONS AND REPORTED TO ENGINEERING FOR DISPOSITION. CLEANED TREATED, PRIMED AND TOP COATED AREAS PER REPAIR MEMO.SDR DXTA2018071601192Engine · flamed outON CLIMB OUTAGE LEFT ENGINE FAILED AT 24,000 FT. R&R ENGINE
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