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 DXTA2013070105424Acm · failedDURING PREFLIGHT WITH THE APU BLEED IN NORMAL, ACM FAN MADE A LOUD NOISE, NOTICED A BURNING ODOR IN CABIN, CABIN SUPPLY TEMP STARTED IN 130'S AND CLIMBED TO 180'S BEFORE BLEED TURNED OFF. IN MAX MODE, FAN NOISE NOT AS BAD BUT STILL HIGH SUPPLY TEMP AND ODOSDR DXTR2013062501Skin · crackedLEADING RT EDGE OF RUDDER HAS A CRACK AROUND RIVET HEAD LOWER SECTIONSDR CA130701014Oil System · low pressure(CAN) DURING APPROACH, THE CREW RECEIVED A MASTER WARNING FOR LOW OIL PRESSURE. THE ENGINE WAS SHUTDOWN AND THE FLIGHT DIVERTED, WHERE AN UNEVENTFUL SINGLE ENGINE LANDING WAS MADE. TROUBLESHOOTING IS ON-GOING.SDR DXTR2013062102Line · crushedLEFT BRAKE HARD LINE ON FWD BULKHEAD, FWD OF THE CO-PILOTS RT RUDDER PEDAL IS DAMAGED.SDR DXTA2013061405417Unknown · odorWHILE ON BATTERY POWER AND INTERIOR LIGHTS, DETECTED AN ACRID SMOKE ODOR, CENTERED NEAR COCKPIT INTERIOR LIGHTS FLICKERED BRIEFLY. ODOR EVENTUALLY DISSAPATED, 10 MINUTES.SDR CA130701003Eec · malfunctioned(CAN) DURING TAKEOFF ROLL, THE NR 2 ENGINE ELECTRONIC CONTROL, ELECTRONIC ENGINE CONTROL WARNING LIGHT CAME ON. THE TAKEOFF WAS ABORTED AND THE ACFT RETURNED TO THE RAMP WHERE IT WAS SHUTDOWN AND RESTARTED IN MANUAL MODE. RUN UPS SHOWED THAT THE NR 2 ENGINE SDR CA130701004Eec · malfunctioned(CAN) DURING T/O ROLL, THE NR 2 ENGINE, ELECTRONIC ENGINE CONTROL WARNING LIGHT CAME ON. THE TAKEOFF WAS ABORTED AND THE ACFT TAXIED BACK TO THE RAMP. TROUBLESHOOTING IS ON-GOING.SDR DXTA2013061105415Brake Sys · contaminatedTHE RIGHT TOE BRAKE PRESSURE SEEMS TO DIMINISH AS PRESSURE IS APPLIED, LEAVING AN ASYMETRICAL ALIGNMENT OF THE PEDALS THEMSELVES. BRAKES ARE GRABBING, BUT THE RT SIDE FEELS LIKE THERE IS VERY LITTLE PRESSURE IN THE LINE. BLED AIR FROM BRAKES AS REQUIRED IAWSDR DXTA2013060505411Oil System · overservicedDURING THE ATTEMPTED APU START, HEAVY SMOKE WAS OBSERVED BLOWING FORWARD (ACFT WAS PARKED WITH A TAIL WIND) AND AN OILY ODOR WAS PRESENT IN CABIN. OIL COULD ALSO BE OBSERVED ON THE APU EXAUST AND ON GROUND BELOW THE APU. INSPECTED APU INLET FOR EVIDENCE OF SDR DXTA2013053105407Switch · failedGEAR UNSAFE LIGHT STAYS ON WITH GEAR HANDLE IN UP POSITION. TROUBLESHOT TO A FAILED AIRSPEED SWITCH. REMOVED AND REPLACED AIRSPEED SWITCH IAW MM 27-40-00. OPS & LEAK CHECKED GOOD.SDR Z5FA2013060355001Cotter Pin · wornDURING CRUISE, A MODERATE VIBRATION WAS FELT IN THE CONTROLS. ACFT WAS AT FL220, APPROX 295 KNOTS INDICATED. VIBRATION BECAME MORE PRONOUNCED. CREW DIVERTED. VIBRATION WAS CONSTANT FROM FL220 DOWN TO ABOUT 8500 FT. LANDING WAS UNEVENTFUL. MX FOUND THE LOWESDR DXTA2013052005398Bulb · burned outEXIT LIGHT OVER MAIN ENTRY DOOR WAS SEEN TO FLICKER ON AND OFF WHILE DECENDING FOR APPROACH. F/O NOTED A WISP OF SMOKE COMING FROM LIGHT. AFTER UNEVENTFUL LANDING AND DEPLANEING OF PASSENGERS, INSPECTED LIGHT AND FOUND ALL BULBS WERE OUT.SDR Z5FA2013052043201Lamp · inoperativeON FINAL APPROACH, THE LT MAIN GEAR DOWN INDICATOR DID NOT ILLUMINATE. A GO-AROUND WAS EXECUTED. THE LANDING GEAR WILL NOT EXTEND CHECKLIST WAS COMPLETED, INCLUDING AN EMERGENCY GEAR EXTENSION. LANDING WAS UNEVENTFUL. MX TROUBLESHOT THE DISCREPANCY TO FAULSDR CA130527001Engine · shutdown(CAN) DURING TAXIING, THE ENGINE HAD AN UNCOMMANDED SHUTDOWN. THE FLIGHT WAS CANCELLED AND THE ACFT RETURNED TO THE HANGAR FOR TROUBLESHOOTING WHICH IS ON-GOING.SDR CA130513006Oil System · low pressure(CAN) DURING REVENUE FLIGHT, THE OIL PRESSURE DROPPED BELOW THE YELLOW LINE AND OIL PRESSURE INDICATOR LIGHT TRIPPED. THE PILOT ELECTED TO SHUTDOWN THE ENGINE. AN UNEVENTFUL SINGLE ENGINE LANDING WAS PERFORMED. THE ENGINE ONLY HAD 33.1 HOURS AFTER BEING REPASDR DXTA2013050605376Bearing · failedNOSE WHEEL SHIMMY STARTING AT WALKING SPEED UP TO 60 KNOTS. MOST PRONOUNCED AT 40 KNOTS. REPLACED NOSE GEAR TORQUE LEAK BUSHING WITH NEW BUSHING IAW THE MM CHAPTER 32-20-01. OPS CHECKED NORMAL.SDR DXTA2013050605377Brake Sys · malfunctionedDURING TAXI INTO RAMP BRAKES STARTED GRABBING ABRUPTLY. COULD NOT TELL WHICH MAIN BRAKE.SDR DXTA2013050605373Apu · fodAFTER STARTING APU, A BURNING ODOR CAME FROM APU. WENT OUTSIDE AND FOUND FLAMES COMING FROM EXHAUST ALONG WITH DEBRIS FROM A BIRDS NEST. SOME OF THE STICKS AND GRASS WENT INTO THE INTAKE. SHUTDOWN APU AND DISCHARGED A PORTABLE FIRE EXTINGUISHER. CLEANED OSDR DXTA2013050205367Pointer · bentPITCH TRIM IS HARD TO MOVE AND BINDING AS IT IS MOVED NOSE UP THROUGH THE TAKEOFF RANGE. BINDING CAN BE FELT WHILE USING MANUAL TRIM. WHILE USING ELECTRIC TRIM YOU CAN SEE THE TRIM WHEEL SLOW AND ALMOST STOP AT THE SAME POSITIONS AS USING MANUAL TRIM. INSPECTSDR Z5FA2013050354701Radome · damagedACFT WAS STRUCK BY LIGHTNING, MIDFLIGHT AT 13,000 FT WHILE EN-ROUTE. IMMEDIATELY AFTER THE STRIKE COCKPIT BEGAN TO ODOR OF ELECTRICAL SMOKE. CREW DONNED 02 MASKS AND DECLARED AN EMERGENCY. LANDING WAS UNEVENTFUL. MX ACCOMPLISHED A LIGHTNING STRIKE INSPECTION SDR Z5FA201305030001Unknown · smokeAIRCRAFT WAS STRUCK BY LIGHTNING. IMMEDIATELY AFTER THE STRIKE COCKPIT BEGAN TO SMELL OF ELECTRICAL SMOKE. CREW DONNED 02 MASKS AND DECLARED AN EMERGENCY. LANDING WAS UNEVENTFUL. ACFT IS CURRENTLY IN MAINTENANCE.SDR CA130430010Oil System · leaking(CAN) AFTER TAKEOFF AT APPROXIMATELY 7000 FT, THE CREW REPORTED A MASTER WARNING ANNUNCIATION IN THE COCKPIT FOR LOW MOP ON ENGINE. THE CREW SECURED ENGINE, ACFT RETURNED TO DEPARTURE WHERE THEY PERFORMED AN UNEVENTFUL SINGLE ENGINE LANDING. TECH REPORTED HEASDR 9JLA201352203569Carbon Seal · leakingDURING CLIMB THROUGH APPROX 7,000 FT, CREW REPORTED A MASTER WARNING LIGHT AND A LOW OIL PRESSURE INDICATOR FOR LT ENGINE. AFTER COMPLETING THE ABNORMAL/EMERGENCY CHECKLIST THE ENGINE WAS SHUTDOWN. DECLARED AN EMERGENCY, RETURNED AND MADE AN UNEVENTFUL LANSDR DXTA2013050805385Lock Nut · missingDURING A BORESCOPE INSPECTION OF COMBUSTION CHAMBER LINER COOLING RING SEGMENT SELF LOCKING NUTS, IAW MFG SPECIAL INSTRUCTION 35-2013. LINER COOLING RING SELF LOCKING NUT ON NR 1 ENGINE HAD MISSING HARDWARE. ENGINE WAS DISASSEMBLED TO GAIN ACCESS TO CC LINERSDR DXTA2013050805383Ring Assembly · unserviceableDURING INSPECTION OF COMBUSTION CHAMBER LINER COOLING RING SEGMENT SELF LOCKING NUTS. FOUND TWO NUTS MISSING AT POSITION NR 15 AND NR 24. COMPLIED WITH A HOT SECTION REPAIR & 5.1. 36-2013.SDR DXTA2013050805390Lock Nut · unserviceableACCOMPLISH BORESCOPE INSPECTION OF COMBUSTION CHAMBER LINER COOLING RING SEGMENT SELF LOCKING NUTS. C/W BORESCOPE INSPECTION AND FOUND 1 MISSING BOLT AT POSITION NR 25. DISASSEMBLED ENGINE TO COMPLY WITH S.1 36-2013. REPAIRED COMBUSTION CHAMBER LINER BY INSTSDR CA130430006Oil System · low pressure(CAN) DURING REVENUE FLIGHT, THE PILOT NOTICED A LOSS OF OIL PRESSURE. THE ENGINE POWER WAS REDUCED TO IDLE. THE OIL PRESSURE RETURNED IN THE NORMAL RANGE AT IDLE. THE PILOT DECIDED TO KEEP THE ENGINE AT IDLE AND DIVERTED THE FLIGHT TO THE HOME STATION. THESDR DXTA2013050805384Ring Assembly · unserviceablePERFORMED BORESCOPE INSPECTION OF COMBUSTION CHAMBER LINER COOLING RING SEGMENT SELF LOCKING NUTS. FOUND ONE NUT MISSING AT POSITION NR 33. ACCOMPLISHED HOT SECTION REPAIR.SDR DXTR20130417001Attach Bracket · crackedRIGHT ELEVATOR OTBD ATTACH POINT BRACKET CRACKED. R & R RT ELEVATOR OTBD ATTACH POINT BRACKETS IAW SRM 51-40-03, 51-40-06, 51-40-09 & BALANCED IAW SRM 51-60-02.SDR 9JLA2013041706761Bowl · leakingDURING THE POST FLIGHT INSPECTION, SIGNIFICANT AMOUNT OF HYD FLUID WAS FOUND LEAKING FROM THE NOSE AREA. TROUBLESHOOTING FOUND THE BRAKE FILTER BOWL LEAKING. R & R THE DEFECTIVE FILTER BOWL AND O-RING. BLED BRAKE SYSTEM, LEAK CHECKS SATISFACTORY. REF: MM 32SDR DXTA201304170557Oil System · overservicedSWEET ODOR OF SMOKE IN CABIN ON GROUND, WITH APU SUPPLYING BLEED AIR FOR ACM. APU FAILED A PORTION OF INITIAL PREFLIGHT CHECK, WITH "READY TO LOAD LIGHT" FAILING TO ILLUMINATE UNTIL APU MASTER HAD BEEN CYCLED PRIOR TO SUCCESSFUL FULL TEST. FOUND APU OIL LEVSDR DXTA201304150555Actuator · seizedON LANDING GEAR EXTENTION LT MLG DID NOT LOCK DOWN AND HAD UNLOCK LIGHT ON TESTED LIGHT AND LIGHT WORKED DID CHECK LIST AND STILL NO LT MLG ON LANDING AND AT TOUCH DOWN LT MLG LOCKED AND HAD THREE GREEN. REMOVED LT MLG ACTUATOR, REMOVED SEIZED UPPER BOLT FROMSDR Z5FA2013041557701Motor · intermittentWHILE TAXING AFTER LANDING, BRAKE PRESSURE WAS LOST, MASTER CAUTION WITH LOW BRAKE PRESSURE AND ANT-SKID ANNUNCIATOR ILLUMINATED. THE ACFT WAS TOWED TO THE FBO. MX TROUBLESHOT THE DISCREPANCY TO A BAD ANTI-SKID POWER PACK MOTOR ASSY. LEAK AND OPS CHECKS WESDR DXTA2013041105352Actuator · bindingTRIM WHEEL VERY DIFFICULT TO TRIM MANUALLY. WHEN TRIMMING WITH ELECTRIC TRIM IT STOPS/BINDS FOR A MOMENT APPROX EVERY INCH OF ROTATION. WHEN IN AUTOPILOT IT DID NOT KICK OFF THE AUTOPILOT. TRIM BINDING WAS THE SAME AT ALL ALTITUDES, AIRSPEEDS, AND FLAP CONFSDR DXTA2013050805386Ring Assembly · unserviceablePERFORMED BORESCOPE INSPECTION OF COMBUSTION CHAMBER LINER COOLING RING SEGMENT SELF LOCKING NUTS. FOUND TWO NUTS MISSING AT THIS TIME AT POSITION NR 1 & NR 18. COMPLIED WITH A HOT SECTION REPAIR SI 36-2013.SDR 9JLA2013040504486Solenoid · defectiveTHE CREW REPORTED THAT THE CABIN DOOR MONITOR CIRCUIT BREAKER POPPED DURING FLIGHT. TROUBLESHOOTING IDENTIFIED THE CABIN DOOR VENT SOLENIOD, PN 6711335-1 AS DEFECTIVE. WE HAVE HAD SEVERAL OF THESE SOLENIODS FAIL IN THE LAST YEAR. THIS IS THE FIRST TO FAIL ISDR DXTA2013040505349Actuator · failedDURING DESCENT, AT APPROX FL290, AN AP PITCH MISTRIM ANNUNCIATION. AFTER DISCONNECTING AUTOPILOT, FOUND TRIM WOULD NOT MOVE FORWARD ELECTRICALLY OR MANUALLY. WITH ENOUGH FORCE IT DID BREAK LOOSE CAUSING A SUDDEN PITCH DOWN WITH THE ADDED TRIM FORCE. IT WASSDR CA130416008Oil System · low pressure(CAN) ON TAKEOFF, THE PILOT REPORTED A LOSS OF OIL PRESSURE INDICATION. HE SECURED THE ENGINE, RETURNED TO THE DEPARTURE AIRPORT WHERE UNEVENTFUL SINGLE ENGINE LANDING WAS PERFORMED. TROUBLESHOOTING IS ONGOING.SDR 9JLA2013040904523Solenoid · defectiveCREW REPORTED THAT THE CABIN DOOR VENT SOLENIOD WAS INOPERATIVE. THIS IS THE 3RD SOLENIOD THIS YEAR, AND 5 TOTAL SINCE MAR/2011. THE SOLENIOD WAS REPLACED WITH NEW AND RIGGED IAW AMM. FUNCTIONAL SATISFACTORY.SDR CA130416003Oil System · low pressure(CAN) AIRCRAFT BEING DIVERTED DUE TO LOSS OF OIL PRESSURE AND LOW OIL LEVEL INDICATION IN COCKPIT. TROUBLESHOOTING.SDR DXTA2013050805388Blades · damagedACCOMPLISH BORESCOPE INSPECTION OF COMBUSTION CHAMBER LINER COOLING RING SEGMENT SELF LOCKING NUTS. ACCOMPLISHED PREINDUCTION GROUND PERFORMANCE RUN AND TRANSIENT VIBRATION SURVEY. ACCOMPLISHED A BORESCOPE INSPECTION OF THE COMBUSTION LINER NUTS. ACCOMPLISHESDR CA130416004Engine · malfunctioned(CAN) DURING DESCENT THROUGH FL170, N1 = 50 PERCENT, 1 ENGINE ACCELERATED TO MAX POWER TRIGGERING THE N2 OVERSPEED RED WARNING. THE IDLE POWER WAS SELECTED BUT THE ENGINE STAYED AT FULL POWER. AFTER APPROXIMATELY 2 SECONDS THE ENGINE RETURNED TO IDLE AND NORSDR Z5FA2013032900001Control Box · intermittentDURING TAXI OUT, CREW OBSERVED "ANTI-SKID INOP" ANNUNCIATION. EXPERIENCED LOSS OF NORMAL BRAKING. MANAGED TO STOP ACFT USING PNEUMATIC EMERGENCY BRAKE. MX PERSONNEL TRAVELED TO LOCATION AND AFTER TROUBLESHOOTING FOUND FAULT WITH ANTI-SKID DIGITAL CONTROL BSDR DXTA2013050805389Lock Nut · unserviceableACCOMPLISH BORESCOPE INSPECTION OF COMBUSTION CHAMBER LINER COOLING RING SEGMENT SELF LOCKING NUTS. COMPLIED WITH TASK CARD TC-5XL-72-100504R1 IAW TASK CARD INSTRUCTIONS AND SB30335R1 INSTRUCTIONS. FOUND 2 BOLTS CONDITION "D" (MISSING) AND ALL REMAINING BOLTS SDR DXTA2013032505338Skin · dentedDENT DAMAGE SKIN ASSY.SDR DXTA2013032505337Structure · dentedVERTICAL STAB LEADING EDGE HAS SEVERAL DENTS. COLD WORKED DENTS IAW SRM 51-40-03. MINOR REPAIR.SDR DXTA2013032505336Door Frame · gougedEMERGENCY EXIT OPENING HAS TWO GOUGES IN LOWER AFT RADIUS OF AIRFRAME. PERFORMED ULTRASONIC THICKNESS CHECK ON GOUGED AREAS ON THE EMERGENCY EXIT AFT LOWER RADIUS NDT UT 01. FOUND NOMINAL THICKNESS TO BE 0.050" THICK AND 0.035" THICK IN THE THINNEST AREA. PERFSDR DXTA2013032505335Frame · chafedFRAME IN MX BAY ABOVE HYD RESERVOIR IS CHAFED BY LP BLEED AIR VALVE. REMOVED LP BLEED AIR VALVE FOR ACCESS TO FRAME. CUT OUT CHAFED SECTION OF FRAME AT BS 479.5. FABRICATED DOUBLER FROM NEW FRAME SECTION AND INSTALLED. IAW MM 21-11-00.SDR DXTA2013050805387Ring Assembly · unserviceablePERFORMED BORESCOPE INSPECTION OF COMBUSTION CHAMBER LINER COOLING RING SEGMENT SELF LOCKING NUTS. DISASSEMBLED CLEANED AND VISUALLY INSPECTED HT DISC ASSEMBLY. REPLACED 70 BLADES WITH NEW DUE TO IMIPACT DAMAGE. SKIM CUT TO 11.5685 BALANCE AND B25 TRIM ADDEDSDR DXTA2013032105328Pump · failedDURING TAXI, ANTI-SKID INOPERATIVE ANNUCIATOR ILLUMINATED. RETURNED TO RAMP. WHILE TURNING TO PARK THE BRAKE FAILED AS THE BRAKE LOW PRESSURE LIGHT ILLUMINATED. TROUBLESHOT TO BRAKE HYDRAULIC PACK. HYDRAULIC MOTOR WOULD ONLY BUILD PRESSURE UP TO 1300 PSI AN
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