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 CA101122003Rib · damaged(CAN) DURING THE AIRCRAFT SERVICING AND WASHING, WE FOUND ON THE RT WING STATION 64, FIRST TRAILING EDGE RIB WAVED. GAP FROM STRAIGHT EDGE IS 0.140 INCH. THERE IS NO WAVINESS OR DAMAGE ON THE ATTACHING SKINS OR SURROUNDING AREA. A MAJOR STRUCTURAL DAMAGE RESDR DXTA2010112204315Metering Valve · malfunctionedAFTER LANDING AND DURING TAXI, THE RT BRAKE GRABS VIOLENTLY WHEN BRAKES APPLIED. AFTER SHUTDOWN SITTING IN CHOCKS, A LOUD NOISE COMES FROM RT WING WHEN RT BRAKE APPLIED. NORMAL OPERATION OF LT BRAKE. REMOVED BRAKE VALVE. INSTALLED OVERHAULED BRAKE METERING SDR DXTA2010111704308Transceiver · inoperativeDESCENDING THROUGH 11,500 FT WITH AN AIRSPEED OF 250 KTS. HAD GEAR WARNING AURAL INDICATION. IN CRUISE CONFIGURATION 11,000 AGL. HAD AN ADDITIONAL 4 AURAL WARNING LASTING FROM 3 SECONDS TO 25 SECONDS DURING THE REMAINDER OF FLIGHT. ALSO HAD AN EGPWS WARNINSDR CA101122008Engine · flamed out(CAN) FLAMEOUT DURING APPROACH AT FL40, THE LT ENGINE FLAMED OUT WITHOUT WARNING. NO ISSUES WERE OBSERVED PRIOR TO THIS. THE CREW DID NOT ATTEMPT A RE-START AND CONTINUED APPROACH, PERFORMING AN UNEVENTFUL SINGLE ENGINE LANDING AT DESTINATION. TROUBLESHOOTISDR DXTA2010111004302Inlet · contaminatedSMOKE IN CABIN. APU WAS RUNNING FOR APPROX 5 MINS WITH BLEED OFF. NOTICED NO SMOKE. TURNED BLEED ON AND AFTER APPROX 2 MINS HAD SMOKE IN THE CABIN. LATER WE RAN BOTH ENGINES WITH NO APU AND DID NOT NOTICE ANY SMOKE. FOUND OIL IN APU AIR INLET. REMOVED WATERSDR DXTA2010110804296Warning Horn · false activationGEAR WARNING HORN SOUNDED ON 3 SEPARATE OCCASIONS. FIRST, FOR 30 SECONDS AT IAS OF 210 KTS & FL220, FLAPS 0. INCREASE OR DECREASE OF THROTTLE SETTING WOULD NOT EXTINGUISH HORN. SECOND, HORN SOUNDED FOR ABOUT 10 SECONDS, AT 210 KIAS APPROACHING 8000 FT. THIRSDR DXTA2010102904281Handle · unknownAFTER PLACING LANDING GEAR HANDLE DOWN, LANDING GEAR ANNUNCIATOR LIGHTS DID NOT ILLUMINATE. ALSO NOTED NO SOUND OR VIBRATION NORMALLY ASSOCIATED WITH GEAR EXTENTION. CREW RAN LANDING GEAR WILL NOT EXTEND CHECKLIST AND ACHIEVED POSITIVE DOWNLOCK INDICATIONS. JSDR DXTA2010102804277Display · malfunctionedON CLIMB OUT, CO-PILOT'S PFD NR 2 WENT BLANK FOR 5 - 6 SECONDS, WITH CHECK PFD NR 2 ANNUNCIATOR ILLUMINATED & MASTER CAUTION. SCREEN CAME BACK ON WITH RED X FOR APROX 10 SECONDS, WITH CHECK PFD NR2 ANNUCIATOR ILLUMINATED WITH MASTER CAUTION. THEN SCREEN REBOOSDR CA101109003Bleed Valve · failed(CAN) ABORTED TAKEOFF DURING TAKEOFF ROLL, THE PILOT WAS NOT ABLE TO OBTAIN REQUIRED THRUST. TAKEOFF WAS ABORTED. TROUBLESHOOTING IDENTIFIED A FAULTY BLEED VALVE TORQUE MOTOR WHICH WILL BE REPLACED.SDR DXTA2010102704276Shutoff Valve · bindingON TAKEOFF, RUDDER PEDALS VERY STIFF. CONFIRMED YAW DAMPER OFF. RETURNED. RUDDER BIAS CHECKED NORMAL ON TAXI. AFTER LANDING, ON TAXI IN, CHECKED RUDDER STIFFNESS AND FOUND NORMAL AT IDLE POWER BUT RUDDER BECAME PROGRESSIVELY STIFFER AS POWER ADVANCED. COULSDR DXTA2010102704275Oil System · overservicedWITH APU RUNNING & APU BLEED AIR ON, A STRONG BURNING RUBBER LIKE ODOR ENTERED CABIN ON TAXI OUT. APU BLEED AIR SELECTED OFF & ODOR WENT AWAY. INSPECTED WATER SEPARATOR IAW MM 21-51-00. LEAK CHECKED APU & BLEED AIR PLUMBING. CHECKED GOOD. FOUND APU OIL OVSDR DXTA2010102604273Actuator · contaminatedDURING CRUISE THE PITCH TRIM JAMMED/FROZE IN THE CRUISE POSITION. REMOVED OLD GREASE AND MOISTURE FROM TRIM ACTUATORS AND APPLIED NEW GREASE. OPS CHECKS GOOD. WORK PERFORMED IAW CH 12-21-01 OF MM. ACCESSED TRIM CABLES IN TAILCONE, NO DISCREPANCIES NOTED. OPSDR DXTA2010102604271Computer · failedDURING CLIMB OUT OF 28,000 FT, WITH RT SEAT PILOT FLYING, THE ATTITUDE AND HEADING FAILURE MESSAGE ILLUMINATED IN THE LT SIDE PFD AND THE MFD. THE AUTO-PILOT ALSO FAILED. PUSHED THE LT SIDE ATTITUDE AND HEADING REVERSIONARY BUTTONS AND THE RT SIDE INFORMATIONSDR DXTA2010102004268Tire · failedNOSE TIRE BLEW OUT DURING LANDING. R & R NOSE WHEEL/TIRE ASSY IAW MM 32-41-01.SDR CA101019002Oil System · low pressureABORTED T/O THE LOW OIL PRESSURE LIGHT ILLUMINATED DURING T/O. THE T/O WAS ABORTED AND WHEN THROTTLES WERE RETARDED THE LIGHT EXTINGUISHED AND THE OIL PRESSURE RETURNED TO NORMAL. SUBSEQUENT INSP REVEALED NO VISIBLE OIL ON THE SIGHT GLASS. TROUBLESHOOTING IS SDR DXTA2010101204259Transmitter · out of adjustDURING TAKEOFF CLIMB, THE WIND SHEAR WARNING CAME ON IN CALM WINDS. AT 170 KNOTS INDICATED AND FLAPS UP THE ANGLE OF ATTACK TAPE ON THE AIR SPEED INDICATOR SHOWED APPROX 145 KNOTS AT THE TOP OF THE WHITE ARCH. ADJUSTED FLAP POSITION TRANSMITTER IAW MM 34-14SDR DXTA2010101204258Autopilot Sys · unknownCLIMBING THROUGH FLIGHT LEVEL 380 WITH THE AUTO PILOT ON AND FLIGHT LEVEL CHANGE SET TO .65, THE ACFT PITCHED UP TO APPROX 10 DEGREES. THE VERTICAL SPEED INDICATED A CLIMB OF OVER 3000 FT PER MINUTE. ACFT LOST 18 KNOTS INDICATED AND STARTED TO EXPERIENCE BUFFSDR CA101007011Heat Shield · crackedDURING TROUBLESHOOTING OF A RT WING OVERHEAT IN CLIMB, WE FOUND DURING ACCESS THAT THE RT INBD L/E HEAT SHIELD WAS CRACKED ON THE LOWER SECTION APPROX 42 INCHES LONG. REMAINING RT WING HEAT SHIELD WERE INSPECTED, NO DEFECT FOUND. WE ALSO INSPECTED THE LT WINGSDR Z5FA100610N523CS1Bulb · inoperativeON FINAL APPROACH, CREW EXTENDED GEAR AND DID NOT GET RT 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 ELECTED TO DECLARE AN EMERGENCY AND DIVERTED, SDR DXTA2010100604257Brake Assy · malfunctionedBRAKES NOT FUNCTIONING PROPERLY. GRINDING AND GRABBING. TAXIED ACFT & VERIFIED PROBLEM, BUT WENT AWAY DURING TAXI. LET BRAKES COOL DOWN & RETAXIED & BRAKE FUNCTIONED NORMALLY. BLED LT & RT BRAKES IAW MM 32-44-00 & NEW BLEEDING PROCEDURE. TAXI CHECKED ACFT SDR DXTA2010100104254Display · illuminatedABORTED THE TAKEOFF BETWEEN 50 AND 60KTS DUE TO THE ILLUMINATION OF THE IAS COMPARISON MONITOR ON BOTH PFD'S. PURGED THE NR 1 AND NR 2 STATIC PRESSURE SYS REMOVING EXCESSIVE MOISTURE IN THE STATIC LINES AND R & R GASKET PN M25988-1-010 ON THE PILOTS LT STATICSDR DXTA2010092404252Brake Assy · weakLT BRAKE PEDAL MUSHY AND DEPRESSES TO THE STOP. WHILE TAXING IN, MAKING A LT TURN, FELT LITTLE TO NO BRAKING ACTION REMAINING. RT SIDE, LT BRAKE PEDAL NOMINAL. INSPECTED BRAKE, BRAKE COMPONENTS AND LINES FOR LEAK. NONE FOUND. CHECKED OPERATION AND FOUND AIRSDR DXTA2010092204250Actuator · inoperativeAFTER TAKEOFF, FLAPS WERE SELECTED TO ZERO POSITION RESULTING IN A STAB MISCOMP, A HYD PRESS, AND A MC LIGHT. UPON LANDING, STAB CONFIRMED NOT TO MOVE FULL UP OR DOWN. TROUBLESHOT TO INOPERATIVE STAB ACTUATOR. REPLACED ACTUATOR WITH MODIFIED UNIT IAW MM. OPSSDR CA100928001Engine · shutdownIFSD LT ENGINE SHUTDOWN UN-COMMANDED AND ACFT LANDED SAFELY AT DESTINATION. POST FLIGHT INSP REVEALED HEAT DISTRESS CONSISTENT WITH A FUEL MANIFOLD LEAK. INVESTIGATION IS ONGOING.SDR DXTA2010092104248Reservoir · lowRIGHT HYD FLOW LOW DURING TAKEOFF ROLL. ABORTED TAKEOFF, LIGHT EXTINGUISHED AT IDLE POWER. FOUND HYD RESERVOIR LEVEL LOW. SERVICED HYD RESERVOIR TO FULL IAW MM 12-12-01. PERFORMED ENGINE RUN ON BOTH ENGINES TO TAKEOFF POWER SEVERAL TIMES WITH FLAPS AT ALL SDR DXTA2010092004246Actuator · wornUNSAFE GEAR ANNUNCIATOR ILLUMINATED AFTER GEAR RETRACTION. TROUBLESHOT TO NOSE STRUT EXTENSION GREATER THAN 9.10 INCHES, IT IS 9.25 INCHES. WHEN RETRACTED UPLOCK ROLLERS ON NLG NOT FULLY SEATED IN UPLOCK HOOK. UPLOCK SWITCH IS AT FULL EXTENSION FOR ADJUSTMENTSDR DXTA2010092004245Ahrs · failedDURING FTL LT PFD AND MFD DISPLAYED ATTITUDE AND HEADING FAILED. TROUBLESHOT AND FOUND NR 1 AHRS TO BE INOPERATIVE. R & R NR1 AHRS UNIT REPAIRED IAW MM 34-21-01. OPS CHECKED GOOD.SDR DXTA2010091304234Actuator · failedGEAR WOULD NOT RETRACT. TROUBLESHOT TO BAD NLG ACTUATOR. R & R NLG ACTUATOR AND BLED HYD SYS. OPS CHECKED GOOD IAW MM 32-30-03.SDR DXTA2010090804226Servo Valve · surgesLEFT EEC ANNUNCIATOR ILLUMINATED DURING FLIGHT. LT ENGINE RESPONDED TO THROTTLE INPUT. COMPLETED ABNORMAL CHECKLIST. LT N1 & N2 WOULD NOT REMAIN CONSTANT, FLUCTUATED UP TO 1.5 PERCENT FOR REMAINDER OF FLIGHT. FELT OCCASIONAL SLIGHT SURGING FROM THE ENGINE. SDR DXTA2010090704218Tire · failedRT TIRE BLEW AND SEPARATED UPON BRAKE APPLICATION DURING LANDING. R & R WHEEL AND TIRE ASSY IAW MM 32-41-02. OPS CHECKED GOOD.SDR DXTA2010090204217Pulley · damagedIN FLT, GEAR UP, & FLAPS RETRACTED, A PRONOUNCED GRINDING/BINDING OF ELEVATOR WHEN YOKE IS MOVED FORE & AFT. NOTICABLE WHEN HAND FLYING BETWEEN 160KIAS & 220 KIAS. THERE IS SOUND ASSOCIATED WITH THE GRINDING AS WELL AS BEING ABLE TO FEEL IT IN THE FLOORBOARDSSDR DXTA2010090204216Control Handle · failedUNABLE TO RETRACT LANDING GEAR AFTER TAKEOFF. GEAR HANDLE STUCK IN THE DOWN POSITION. APPEARS TO BE A SQUAT SWITCH ISSUE. JACKED ACFT AND SWUNG GEAR. NO DEFECTS NOTED. SPOKE WITH MX WHO REQUESTED LANDING GEAR CONTROL HANDLE BE REPLACED. REPLACED LANDING GESDR DXTA2010083004209Oil System · emptyDURING CLIMB, HAD A MASTER WARNING ANNUNCIATOR & LT OIL PRESS ILLUMINATE. NOTED A LT ENGINE OIL PRESSURE READING 45 PSI. RT ENGINE INDICATED 75 PSI. DURING NEXT 90 SECS, LT ENGINE OIL PRESSURE VARIED BETWEEN 45 & 55 PSI. RT ENGINE REMAINED STEADY AT 75-80 PSSDR CA100903005Engine · failedABORTED TAKEOFF DURING A REPOSITIONING FLIGHT, ON TAKEOFF THE PILOTS PUSHED THE TLA`S FWD AND ITT INCREASED RAPIDLY INTO THE RED. PILOT IMMEDIATELY RETARDED THE THROTTLES AND TAKEOFF WAS ABORTED. TROUBLESHOOTING IS ONGOING.SDR Z5FA082210N546CS1Blower Motor · burned outENROUTE, CREW SMELLED A BURNING ODOR AND ATTEMPTED TO LOCATE SOURCE. AS ODOR INTENSIFIED AND SMOKE WAS OBSERVED IN THE DROPPED ISLE AFT OF COPILOT, THE CREW DECLARED AN EMERGENCY AND DIVERTED. AS ACFT DESCENDED, THE CREW DROPPED O2 MASKS FOR PASSENGER CONVENIESDR DXTA2010082304201Yoke · bindingFROM THE RT YOKE, IN FLIGHT WITH THE AUTOPILOT ON THERE IS A VIBRATION IN THE RT YOKE AND YOU CAN FEEL A VIBRATION IN THE FLOORBOARDS AT THE BASE OF THE YOKE. YOU CAN ALSO FEEL A GRINDING WITH FORE/AFT MOVEMENT OF THE RT YOKE.SDR DXTA2010082304205Bracket · bentMAIN CABIN DOOR WILL NOT OPEN. TRIED BOTH INSIDE AND OUTSIDE HANDLES. BOTH HANDLES BIND AND REQUIRE A SIGNIFICANT AMOUNT OF FORCE TO TAKE TO FULL TRAVEL. MULTIPLE PINS REMAIN ENGAGED IN THEIR FUSELAGE HOLES. BOTH LOWER PINS AND UPPER LT PINS REMAIN ENGAGED. TSDR DXTA2010082304204Anti-Skid Valve · malfunctionedBRAKES APPEAR TO LEAK FLUID. RES FULL AT UPPER SIGHT GAUGE. NO AIR BUBBLE VISIBLE. 15 MINS AFTER DEPLANING UPPER SIGHT GAUGE ONLY 1/3 FULL. BRAKE PUMP CYCLES EVERY 26 SECS. BRAKE PRESS GOES TO 1400 PSI & BLED DOWN TO 1200 PSI IN 26 SECONDS, PUMP ACTIVATES. BRSDR DXTA2010082004198Knob · looseAFTER TAKEOFF, FLAP LEVER WOULD NOT MOVE OUT OF TAKEOFF FLAP POSITION. RETURNED FOR LANDING. FOUND KNOB LOOSE UPON ARRIVAL TO ACFT. RESECURED FLAP LEVER KNOB AS REQ'D IAW 20-00-00, OPS TEST GOOD.SDR 2010FA0000926Garlock Seal · failedOIL LOSS BOTH ENGINES: ACFT HAD BEEN IN AN "INACTIVE FLT STATUS" FOR APPROX 18 MONTHS. ACFT HAD BEEN FULLY MAINTAINED & ENGINE/ APU RUN UPS & ACFT TAXI CHECKS COMPLETED EVERY 30 DAYS. APPROVED OIL HAD BEEN USED SINCE DELIVERY. ACFT HAD BEEN PREPPED FOR A MX SDR DXTA2010081704195Relay · malfunctionedON FINAL AFTER GEAR EXTENSION, LOW BRAKE PRESSURE ANNUNCIATOR AND ANTI-SKID INOP ANNUNCIATOR BOTH CAME ON AND STAYED ILLUMINATED. EMERGENCY BRAKE WAS USED TO STOP THE AIRPLANE ON THE RUNWAY CIRCUIT BREAKERS PULLED FOR SAFETY. ANTI-SKID PUMP MOTOR DOES NOT RUNSDR DXTA2010081604194Brake Sys · malfunctionedRT MAIN BRAKE GRABBING DURING TAXI, LOUD POPPING SOUNDS, SHUDDERING OF ACFT. HAD UNCOMMANDED APPLICATION AT SEVERAL POINTS. BRAKE DID NOT SEEM OVERLY WARM 10 MIN AFTER LANDING. JACKED ACFT , RT MAIN WHEEL ROTATED WHEEL & DID NOT HEAR BRAKES BINDING OR DRAGGISDR DXTA2010081604190Engine · smokeABOUT 3 MINUTES AFTER DEPARTING AND CLIMBING TO 10,000 FT WE GOT A MASTER WARNING LIGHT AND A R OIL PRESSURE ANNUNCIATOR. ALSO, OBSERVED THAT THE OIL PRESSURE TAPE ON THE RT SIDE WAS AT THE BOTTOM IN THE RED. SECONDS AFTER WE SMELLED SMOKE AND THE PASSENGER SDR CA100831004Engine · shutdownIFSD DURING REVENUE FLIGHT, A FEW MINUTES AFTER TAKEOFF, A LOW OIL PRESSURE WARNING CAME ON WITH SMOKE IN THE CABIN. THE RT ENGINE SHUTDOWN BY ITSELF AND AN EMERGENCY DECLARED. UNEVENTFUL LANDING BACK TO POINT OF ORIGIN WAS PERFORMED (FAA SDR 2010091100220/DXSDR DXTA2010080904187Unknown · smokeHAD VISIBLE SMOKE IN COCKPIT ON TAKEOFF, THRU ABOUT 2K FT, WITH APU RUNNING. SMOKE SEEMED TO BE ISOLATED TO COCKPIT AREA. SMOKE DISSIPATED ON ITS OWN IN A VERY SHORT TIME. COULD NOT DUPLICATE, ENGINES AND APU BLEED AIR SYS CHECKS OK.SDR CA101027004Transponder · failedATC TRANSPONDER FAILED IN NR 2 COM UNIT. INTEGRATED COM UNIT RC2833K, PN 7510700-665, SN 0707B537. REPLACED WITH SN 10014843 COM OPS TEST AND ATC TRANSPONDER TEST PERFORMED ON MEL 23-01-1 THE ACFT REMAINED RVSM COMPLIANT.SDR DXTA2010080204182Pressure Switch · failedRESIDUAL BRAKE FLUID WAS FOUND ON LT BRAKE LINE AND THREADS. WHEN DEPRESSING BRAKE PEDALS, PEDALS FEEL SOFT AND BOTTOM OUT TO THE STOPS, THEN MASTER CAUTION WITH LOW BRAKE PRESSURE ANTISKID INOP ANNUNCIATOR ILLUMINATES. BRAKE FLUID RESERVOIR LEVEL IS GOOD ANDSDR DXTA2010072804180Garlock Seal · failedRT ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED INFLIGHT AT 25,000'. OIL PRESSURE ON GUAGE AT CRUISE POWER SETTING WAS APPROX 28PSI. RETARDED THROTTLE TO IDLE AND OIL PRESSURE ROSE TO APPROX 68 PSI. ENG DATA BUTTON PRESSED DURING DESCENT. PASSING 6,000' ON DSDR Z5FA07252010N568CInsert · detachedDURING LANDING ROLL OUT, THE RT BRAKE FAILED. EMERGENCY BRAKES WERE USED TO STOP THE ACFT. INVESTIGATION REVEALED THE WHEEL DRIVE INSERT SEPARATED FROM THE WHEEL AND BECAME LODGED BETWEEN THE WHEEL AND BRAKE, SHEARING (2) BRAKE FITTINGS CAUSING LOSS OF HYD FLUSDR DXTA2010072604178Control Cable · failedDURING PREFLT, HEARD A GRINDING NOISE WHEN DEPRESSING RUDDER PEDALS. ATTEMPTED 1 DEFLECTION OF RUDDER PEDALS IN EACH DIRECTION TO INVESTIGATE. UPON DEPRESSING RT RUDDER PEDAL, A SUDDEN RELEASE OF PRESSURE FELT ALONG WITH A LOUD "BANG". THERE IS NOW ZERO RESIS
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