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 CA150410011Warning System · activated(CAN) DURING CLIMB, THE RED MASTER WARNING LIGHT ILLUMINATED FLASHING WITH THE RT ENG LO OIL PRESS ANNUNCIATOR. THE OIL PRESS GAUGE READ BELOW THE RED LINE NEAR ZERO. THE INDICATION LASTED LESS THAN 10 SECONDS, AFTER 10 SECONDS ALL INDICATIONS REMAINED GREEN SDR DXTR2015041002Skin · looseVERTICAL L/E HAS MULTIPLE LOOSE, WORKING FASTENERS. COMPLIED WITH STRUCTURES REPORT NO: S-560XL-5360/04 PRD1 REPAIR DEFINITION.SDR O2GA2015042851001Cover · crackedDURING UNSCHEDULED ELEVATOR COUNTERWEIGHT MAINTENANCE, PLASTIC TRIM COVER WAS FOUND CRACKED INSIDE PEDESTAL COMPARTMENT. IAW ENGINEERING LETTER M150404DK DATED 04 02 2015 PANEL WAS DEFERRED & PLACED ON 04 19 2015. ACFT WAS RETURNED TO SERVICE.SDR DXTR2015041001Door Frame · crackedMCD FWD MAIN FRAME CRACKED AT COUNTERBALANCE. COMPLIED WITH THE ERO-720990 , AND SRM 53-20-01.SDR DXTR2015042304Stringer Clip · crackedVERTICAL SPAR PIVOT FITTING LOWER LT SIDE BOTTOM STRINGER CLIP CRACKED. R & R VERTICAL STABILIZER PIVOT CLIP IAW SRM 55-30-01.SDR DXTR2015041401Pivot · crackedVERTICAL SPAR PIVOT FITTING LOWER LT SIDE BOTTOM STRINGER CLIP CRACKED. R & R VERTICAL STABILIZER PIVOT CLIP REF SRM 55-30-01 AND REPAIR DEFINITION S-560XL-5240/05RD DATED 04/10/15.SDR CA150325017Indicator · inaccurate(CAN) THE RT ENGINE HAD BEEN RUNNING NEAR THE 720 DEGREES C REDLINE DURING THE FIRST 2 TAKEOFFS. DURING THE THIRD TAKEOFF AT 26 DEGREES C AT AT MAX GROSS WEIGHT, ITT WAS AT ABOUT 715 DEGREES C DURING TAKEOFF ROLL. AFTER ROTATION AND INITIAL CLIMB ITT WENT TOSDR DXTA2015031105992Pressure Switch · failedDURING LANDING, LOWERING THE LANDING GEAR THE LOW BRAKE PRESSURE & ANTI-SKID INOPERATIVE ANNUNCIATOR LIGHTS CAME ON. RAN THE CHECKLIST & USED THE EMERGENCY BRAKE AFTER LANDING. TROUBLESHOT TO A BAD PRESSURE SWITCH. REPLACED THE PRESSURE SWITCH WITH AN OVESDR CA150325007Engine · power loss(CAN) DURING TAKEOFF ROLL, THE F/O CALLED ABORT DUE TO THE RT ENGINE NOT INDICATING TAKEOFF POWER. THE LT CAME UP TO APPROXIMATELY 91 PERCENT WHILE THE RT ENGINE INDICATED APPROXIMATELY 83 PERCENT. UNABLE TO RECREATE EVENT DURING STATIC RUN UP AFTER EXITING SDR CWQR20150305008Bracket · crackedDURING A SCHEDULED INSPECTION WE FOUND THE LT ELEVATOR OTBD HINGE, INBD BRACKET ASSEMBLY PART 6634003-59 CRACKED. THE BRACKET WAS CRACKED 0.4 INCH ON THE UPPER RADIUS & 0.55 ON THE LOWER RADIUS OF THE BRACKET. WE HAVE SEEN THIS CONDITION ON OTHER ELEVATOR BRSDR CWQR2015022707Fitting · crackedDURING A SCHEDULED INSPECTION WE FOUND CLIP PAN 6622034-8 CRACKED ONE INCH IN LENGTH. IT IS LOCATED ON THE OTBD SIDE OF RT WING STATION 188.88 AT THE FLAP AILERON ISLAND SPAR. CLIP WAS REPLACED WITH NEW. SCR REPORT FILED UNDER 711505.SDR CWQR20150227006Fitting · crackedDURING A SCHEDULED INSPECTION WE FOUND CLIP PN 6622034-6 CRACKED ONE INCH IN LENGTH. IT IS LOCATED ON THE INBD SIDE OF RT WING STATION 188.88 AT THE FLAP AILERON ISLAND SPAR. CLIP WAS REPLACED WITH NEW. SCR REPORT FILED UNDER 711502.SDR DXTA2015022705987Actuator · malfunctionedTRIED TO MOVE THE RUDDER TRIM BOTH LT & RT. THE RUDDER TRIM WOULD NOT MOVE EITHER WAY. ON TAXI IN AFTER LANDING THE RUDDER PEDALS WERE STIFF TO STEER THE AIRPLANE. NO MECHANICAL DEFECTS WERE NOTED, HOWEVER THE RUDDER TRIM ACTUATOR DID NOT APPEAR TO HAVE MUCSDR CNQR2015FA006034Actuator · intermittentAIRCRAFT WAS OUT ON AN OPS CHECK AND DECLARED AN IN-FLIGHT EMERGENCY DUE TO GEAR INDICATION ISSUE. THEY PERFORMED A FLYBY AND IT WAS CONFIRMED THE GEAR WAS DOWN AND MADE AN UNEVENTFUL LANDING. PILOT SQUAWK: AFTER COLD SOAK, LT MLG WOULD NOT FREEFALL TO DOWNLSDR DXTR2015022401Support Angle · crackedCRACK AT FWD DOOR SPRING ON FWD FRAME, PERFORMED EDDY CURRENT INSPECTION OF THE MAIN CABIN DOOR STRUCTURE IAW NDI MANUAL PN 6 20-00-02. VERIFIED EXISTENCE OF CRACK. NDI SERVICES PROVIDED ON W/O B180183. PERFORMED CUTOUT OF DAMADGED AREA. FABRICATED AND MATSDR DXTA2015022005984Display · failedAPU WAS STARTED & ELECTRICAL POWER WAS APPLIED TO ALL SYSTEMS. AFTER ABOUT 15 MINUTES AN ELECTRICAL BURNING ODOR WAS NOTED FOLLOWED BY SMOKE, A BLANK PFD 2 & ILLUMINATION OF THE PFD 2 FAIL LIGHT. REMOVED NR 2 PFD & VERIFIED BURNING ODOR IS COMING FROM UNIT. SDR 9JLA201502268404Adapter · brokenTHE FLIGHT CREW REPORTED THAT THE APU FAILED TO START AFTER LANDING, INDICATING A FAULT ON THE CONTROL PANEL. TROUBLESHOOTING IDENTIFIED THAT THE STARTER GEN DRIVE ADAPTER PN 3861055-1 FAILED. THE BROKEN DRIVE ADAPTER WAS REMOVED & A NEW ADAPTER INSTALLED.SDR DXTR2015022402Pulley Bracket · crackedRUDDER AUTOPILOT SERVO PULLEY BRACKET CRACKED. R & R BRACKET REF SRM 51-40-03. INSTALLED, PN 6661154-2.SDR DXTA2015021705979Switch · out of adjustLOW HYDRAULIC FLUID LEVEL LIGHT CAME ON & WOULDN'T GO OFF ALONG WITH THE CAUTION LIGHT. NO EMERGENCY EXTENSION WAS NECESSARY, DECLARED AN EMERGENCY. DID NOT OBSERVE ANY LEAKS, THE HYD RESERVOIR FULL. INSPECTED HYDRAULIC QTY SYS & FOUND LOW HYD LEVEL SWITCSDR DXTA2015021705978Unknown · unknownDURING LANDING ROLL OUT AT SPEEDS ABOVE NORMAL TAXI SPEED, THE LT BRAKE GRABS EXCESSIVELY & PULLS THE ACFT TO THE LEFT. THE RT BRAKE APPEARED TO RELEASE & REAPPLY THE BRAKE 5 OR 6 TIMES DURING THE ROLL OUT. NO ANTI-SKID RELEASE MARKERS WERE NOTED AFTER LANDISDR CWQR20150129005Fitting · crackedDURING A SCHEDULED INSPECTION, FOUND THE HORIZONTAL STABILIZER ATTACH FITTING CLIP CRACKED IN TWO PLACES. THE CRACKS WERE IN THE CUT OUT RADIUS ABOUT .12 INCH LONG. CLIP WAS SENT TO FOR EVALUATION. A REPORT WAS FILED UNDER SCR 708902.SDR DXTR2015020501Hinge Fitting · corrodedMCD FORWARD, LOWER HINGE HALF ASSY CORRODED. R & R MCD LOWER HINGE IAW SRM 51-40-03 AND DWG 6611071, DWG 0003.2. CORROSION DAMAGED WAS CONTAINED TO LOWER HINGE ONLY; NO DAMAGE TO UPPER HINGE OR SURROUNDING FUSELAGE.SDR DXTA2015012605969Unknown · odorAFTER ROTATION & TAKEOFF THERE WAS A STRONG PLASTIC SMELL THAT SEEMED TO BE COMING FROM WEMACS. APU WAS SHUT OFF PRIOR TO TAKEOFF. AT 2000' MSL RE-ENTERED THE PATTERN & LANDED UNEVENTFULLY. SMELLED SEEMED TO DISSIPATE WHEN WEIGHT WAS ON WHEELS. RAN APU WITSDR W9BR2015031900099Cable · failedUPON PERFORMING INSPECTION DOCUMENT 9 TASK RUDDER AND TRIM CONTROL SYSTEM FUNCTIONAL CHECKS, THE RUDDER AUTO PILOT SERVO CABLE WAS FOUND COMPLETELY BROKEN WITH NO EVIDENCE OF COMING IN CONTACT OF ANY PART OF THE AIRCRAFT AIRFRAME. THE RUDDER SERVO ASSY, PN 40SDR DXTA2015012005964Transmitter · failedSHORTLY AFTER LEVEL OFF AT FL350, LT ENGINE OIL PRESSURE DROPPED RAPIDLY TO THE 25 - 30 PSI RANGE. INDICATOR BAR TURNED AMBER. OIL PRESSURE REMAINED IN THIS RANGE FOR THE REST OF THE FLIGHT TO LANDING. OIL PRESSURE INDICATOR BAR TURNED WHITE WHEN THROTTLE RSDR CWQR20150119004Tube · leakingDURING A SCHEDULED INSPECTION FOUND SLIGHT DISCOLORATION ON COWLING ASSEMBLY. INSPECTED & FOUND THE TWO FLEX JOINTS ON THE ENG INLET ANTI-ICE TUBE ASSEMBLY WERE LEAKING. THE FLEX JOINTS ARE NOT REPAIRABLE, SO THE ENTIRE TUBE ASSEMBLY WILL BE REPLACED. SERVISDR CWQR20150119003Frame · crackedDURING A SCHEDULED INSPECTION WE FOUND A HYD LINE STAND OFF BRACKET BROKEN & THE LINE CHAFING THE STRUCTURE. UPON FURTHER INSPECTION WE FOUND THE HYD LINE STAND OFF BRACKET ATTACH RIVET HOLES IN THE FRAME WERE CRACKED. TWO CRACKS WERE MEASURED AT 1.65 & .65 ISDR CWQR20150119002Pan · crackedDURING A SCHEDULED INSPECTION WE FOUND THE FLEX PAN CRACKED ON THE CAPTAIN’S SEAT ASSEMBLY. THE FLEX PAN HOLD THE CREW SEATS LOWER SEAT CUSHION. SEAT MODEL 1423 IN THE COMPONENT MM ITEM 100. SERVICE CONDITION REPORT SENT TO UNDER REPORT 707939.SDR CWQR20150119001Tube · crackedDURING A SCHEDULED INSPECTION WE FOUND THE BLEED AIR, AIR TUBE MOUNTING FLANGE CRACKED 1/3 THE WAY AROUND THE BLEED AIR TUBE ASSEMBLY. ABOUT 2.5 INCHES LONG. THIS CRACKED FLANGE ATTACHES TO THE APU CONTAINMENT BOX & IS THE PASS THROUGH FOR THE BLEED AIR TUBISDR DXTR2015020401Bracket · crackedLOWER CLIP ON VERTICAL STABILIZER HAS 2 SMOKED HI-LOCKS ON OTBD EDGES ON FWD SIDE. FOUND A CRACK PROTRUDING FROM THE LT OTBD LOWER PIVOT FITTING FLANGE TRAVELING UP & OTBD APPROX .5" FOUND 2 CRACKS TRAVELING FROM THE RT OTBD HOLE, ONE TRAVELING UP & OTBD APPRSDR DXTA2015010805958Unknown · odorAT FLIGHT LEVEL 410, ODOR DEVELOPED, SHORTLY FOLLOWED BY AIR DUCT OVERHEAT, COCKPIT LIGHT ILLUMINATED. RAN APU WITH BLEED AIR ON & OPERATED TEMP CONTROLLER AT FULL HOT IN AUTO MODE LONG ENOUGH FOR DUCT TEMPERATURES TO CLIMB, DESCEND & STABILIZE. CYCLED TEMSDR CA150120009Oil System · malfunctioned(CAN) DURING REVENUE FLIGHT, AFTER TAKEOFF WHILE LEVELING AT 11,000FT ALTITUDE, THE RIGHT ENGINE LOW OIL PRESSURE WARNING AND MASTER WARNING LIGHT CAME ON. THE RIGHT OIL PRESSURE STRIP INDICATOR MOMENTARILY WENT TO ZERO (0) PSI, THEN IMMEDIATELY ROSE TO 40 PSISDR EBVR201501070001Isolator · debondedTHE RUBBER ISOLATORS ON BOTH THE FORWARD AND AFT END OF THE MOUNT HAS DISBONDED ALLOWING THE MOUNT BOLT, RUBBER ISOLATORS AND THE MOUNT STRUTS TO MOVE AXIALLY 0.1155".SDR CA150120004Engine · malfunctioned(CAN) UPON SETTING "T/O" POWER FOR DEPARTURE, OBSERVED LEFT ENGINE AT BOTTOM OF YELLOW ITT BAND, WHERE IT REMAINED FOR T/O ROLL. JUST AFTER ROTATION, LEFT ENGINE ITT ROSE AND SPIKED AT 744, WHERE IT REMAINED ONCE THE THRUST LEVER HAD BEEN REDUCED TO THE CLIMB SDR DXTA2014122305953Unknown · odorDURING TAXI OUT CABIN DOOR MONITOR CIRCUIT BREAKER TRIPPED. DID NOT ATTEMPT RESET. RETURNED TO RAMP. HEAVY ELEC FIRE SMOKE FILLED COCKPIT. R & R AN INOPERATIVE CABIN DOOR PCB, IAW AMM 24-51-02. OPS CHECKED GOOD IAW MM 52-70-00-710. R & R THE VENT DOOR SSDR 9JLA2015022614512Uplock Switch · defectiveAFTER TAKEOFF THE CREW REPORTED THAT AFTER GEAR RETRACTION THE GEAR UNSAFE ANNUNCIATOR REMAINED ILLUMINATED, THE HYD PRESS ANNUNCIATOR REMAINED ILLUMINATED FOLLOWED BY A STAB MIS COMPARE WARNING ANNUNCIATOR. THE LG WAS RECYCLED & THE FAULT CLEARED. TROUBLESHSDR DXTA2014121905950Trim System · frozenTRIED ELECTRICAL & MANUAL TRIM, FOUND TO BE FROZEN. THE ELEVATOR WAS SHAKING. BOTH HAD TO PUSH FULL FWD ON THE YOKE TO ARREST THE CLIMB. IT FELT AS IF THE ELEVATOR WAS ALSO FROZEN. DECLARED AN EMERGENCY & REDUCED THROTTLES AS MUCH AS POSSIBLE TO DESCEND. SDR O2GA2014121950701Uplock Switch · failedDURING CLIMB, THE GEAR HANDLE WAS SELECTED UP & THE LT GEAR INDICATION REMAINED ILLUMINATED. SELECTED THE GEAR HANDLE DOWN & ALL THREE LG INDICATIONS WERE GREEN. DECLARED AN EMERGENCY, PERFORMED A FLY BY THE TOWER TO CONFIRM LG WAS DOWN & DIVERTED BACK. LANSDR DXTA2014121605949Motor · failedMAIN BRAKE SYS FAILED WITH LOW BRAKE PRESSURE & ANTI-SKID INOPERATIVE LIGHTS ON LANDING. POWERED ACFT UP, AND RAN THE BRAKE SYSTEM SEVERAL TIMES AND COULD NOT FIND ANY DISCREPANCIES. INSPECTED THE WIRING FROM THE MOTOR, PRESSURE SWITCHES, AND THE RELAY COULDSDR DXTA2014121505945Line · chafedLOW HYD LEVEL LIGHT CAME ON SHORTLY AFTER TAKEOFF. RAISED THE GEAR & THEN THE FLAPS. THE LIGHT CAME ON IMMEDIATELY AFTER THE FLAPS WERE RAISED. THERE WERE NO OTHER INDICATIONS. WENT TO THE ABBREVIATED CHECKLIST WHICH STATED IN PART TO LAND AS SOON AS PRACTSDR DXTA2014120805943Apu · contaminatedSMOKE FILLED COCKPIT & CABIN AFTER ACTIVATION OF BLEED AIR ON APU. BORESCOPED APU INLET AREA AND IMPELLER. HEAVY AMOUNTS OF OIL THROUGHOUT THE AREA. REMOVED APU IAW MM 498-10-00 AND DRAINED OIL. CLEANED OUT APU CONTAINMENT BOX AS REQUIRED. INSTALLED THE APUSDR CA141204007Oil System · low pressure(CAN) DURING CLIMB, OIL PRESSURE IN THE RIGHT ENGINE SUDDENLY DROPPED TO 0 TOGETHER WITH THE MASTER WARNING AND R ENG OIL ANNUNCIATION ILLUMINATED FOR ABOUT 3 SECONDS. THE FLIGHT CREW REPORTED THAT THE OIL PRESSURE RECOVERED ONCE THEY PULLED THE THROTTLE BACK SDR DXTA2014120105939Master Cylinder · failedDURING TAXI ONTO RUNWAY WITH LT RUDDER DEFLECTION, HEARD & FELT A POP IN THE RUDDER PEDALS & THEN SMELLED A NOXIOUS ODOR. THE LT BRAKE PEDAL HAD NO EFFECT, HAD TO USE EMERGENCY BRAKING TO STOP THE ACFT. AFTER STOPPING THERE WAS A LARGE PUDDLE IN THE FIRST OFSDR BKER2014120100680Monitor · false indicationRIGHT ENGINE VIBRATION LIGHT ILLUMINATED ON CLIMB OUT. PILOTS RETURNED TO DEPARTURE. T/S TO ENGINE VIBRATION MONITORING UNIT. UNIT WAS REMOVED AND A NEW UNIT INSTALLED. OPS CHECK GOOD. THIS WAS INDICATION PROBLEM , NO VIBRATION OF THE ENGINE WAS EVER FELT.SDR CA141204001Engine · warning light(CAN) IN THE CLIMB AT APPROXIMATELY 9,000 FT, THE CREW RECEIVED A MASTER WARNING LIGHT WITH RIGHT ENGINE LOW OIL PRESSURE ANNUNCIATION AND 0 INDICATION ON THE RIGHT OIL PRESSURE TAPE. RIGHT THROTTLE WAS PULLED TO IDLE WITH NO CHANGE IN OIL PRESSURE INDICATION.SDR DXTA2014112405936Valve · failedBLEED AIR OVERHEAT LIGHT CAME ON AFTER TAKEOFF WITH A STRONG BURNING ODOR. PERFORMED HIGH POWER RUNS WITH NO DEFECTS NOTED IAW AMM 21-21-00. FOUND LEFT ENGINE SUPPLYING INSUFFICIENT AIR AT HIGH POWER. SELECTED THE BLEED AIR SOURCE FROM LT TO RT MULTIPLE TIMSDR DXTA2014112405934Valve · failedDURING PERFORMANCE A STATIC TAKE OFF, THE LT SEAT BRAKES WOULD NOT HOLD THE AIRPLANE. PERFORMED ENGINE RUNS AND VERIFIED DISCREPANCY. CHECKED FOR CORRECT BRAKE PRESSURE WITH BRAKES APPLIED, NO DEFECTS NOTED. CHECKED LEFT AND RIGHT SEAT BRAKE CABLE TENSIONS, SDR DXTA2014112405935Coalescer Bag · odorSMOKE ENTERED CABIN, APU AND BOTH ENGINES RUNNING WITH BLEED AIR ON. HEAVY MIST BLOWING OUT OF ALL VENTS, FILLED THE CABIN. HAD A DIRTY SOCK ODOR, NO BURNING OR ENGINGE EXHAUST. REMOVED & CLEANED WATER SEPARATOR IAW MM 21-51-00. OPS CHECKED GOOD, NO OIL INSDR CA141202024Oil System · low pressure(CAN) DURING CLIMB, ENGINE LOW OIL PRESSURE LIGHT CAME ON FOLLOWED BY RED MASTER WARNING LIGHT WITH NO OIL PRESSURE INDICATION. PILOT SHUT DOWN ENGINE AND RETURNED BACK TO ORIGIN UNEVENTFULLY.CUSTOMER REPORTED AIRCRAFT BACK IN SERVICE BEING UNABLE TO DUPLICATESDR DXTA2014112105930Computer · failedENROUTE PICS MFD, PFD, FAILED WITH RED X & ANNUNCIATOR, FMS FAILED AS WELL AS YAW DAMPER, AUTOPILOT, TCAS, GND PROX & FLIGHT DIRECTOR. TROUBLESHOOT SYS TO AN INOPERATIVE NR 1 INTEGRATED AVIONICS COMPUTER. REMOVED NR 1 INTEGRATED AVIONICS COMPUTER, REPAIRED,
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