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 DXTA2011053104597Unknown · vaporAFTER LIFTOFF, THE COCKPIT FILLED WITH A NOXIOUS, VAPOR, THAT BURNED THE EYES. THE PRESSURIZATION SOURCE KNOB WAS SELECTED TO OFF AND THE CONDITION DID NOT WORSEN. IT WAS THEN SELECTED TO RIGHT AND THE CONDITION IMPROVED. INSPECTED PLUMBING ON LT SIDE. NOSDR CA110606002Oil System · low pressure(CAN) LOW OIL PRESSURE/IFSD DURING T/O, OIL PRESSURE WAS LOST, WENT TO ZERO. THE PILOTS COMPLETED THE TAKEOFF, THEN INITIATED THE ENGINE SHUTDOWN. THE ACFT RETURNED TO THE POINT OF DEPARTURE WHERE AN UNEVENTFUL SINGLE ENGINE LANDING WAS PERFORMED. TROUBLESHOOTSDR 9JLA3375Gauge · defectiveN1/ITT GAUGE (RT), N1 DIGITS DO NOT LIGHT, TAPE IS OK. REMOVED THE DEFECTIVE GAUGE P/N 9912497-8 S/N 02030781A INSTALLED OVERHAULED GAUGE. FUNCTIONAL CHECKS SATISFACTORY.SDR DXTA2011052504590Actuator · failedAFTER TAKEOFF, MLG & FLAPS RETRACTED. HYD PRESSURE, STAB MISCOMPARE & GEAR UNLOCK LIGHTS STAYED ON. ON RETURN FOR LANDING FLAPS & MLG LOWERED, ALL NORMAL. R & R THE LT MLG ACTUATOR IAW MM 32-30-04. PERFORMED MLG HYD SYS ADJUSTMENTMENT TEST IAW MM 32-01-00SDR DXTA2011051904584Actuator · malfunctionedAFTER TAKEOFF, GEAR SELECTED UP, NLG WHEEL INDICATOR LIGHT STAYED GREEN WITH SOUND INDICATION, GEAR DOORS WERE STILL OPEN. MLG SWITCH WAS SELECTED DOWN WITH 3 GREEN INDICATIONS OF DOORS OPEN. SELECTED GEAR UP AGAIN WITH SAME INDICATION. MLG SELECTED DOWN WITSDR DXTA2011051604582Rudder · bindingRUDDER PEDALS ARE BINDING ON TAKEOFF FROM RT SEAT AND BINDING FROM LT SEAT ON LANDING AFTER PASSING THROUGH NEUTRAL POSITION ON CROSSWIND LANDING. ALL RUDDER BIAS TESTS WERE GOOD PRIOR TO TAKEOFF. VISUALLY INSPECTED RUDDER CABLE RUNS. CHECKED PRIMARY, SECOSDR CA110516023Oil System · low pressure(CAN) LOW OIL PRESSURE/IFSD DURING CRUISE, THE LOW OIL PRESSURE WARNING CAME ON. THE ENGINE WAS SHUTDOWN AND AN UNEVENTFUL SINGLE ENGINE LANDING FOLLOWED. POST FLIGHT INSPECTION FOUND NO OIL ON THE SIGHT GLASS. TROUBLESHOOTING IS ON-GOING.SDR DXTA2011051204577Seal · failedLEFT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED DURING FLIGHT. LT OIL PRESSURE GAUGE READ 0. SHUT LT ENGINE DOWN IAW EMERGENCY CHECKLISTS. SUSPECT NR 4 BEARING SEAL FAILING. REMOVED AND REPLACED ENGINE.SDR CA110511002Ahrs · malfunctioned(CAN) ON TAKEOFF, CREW RECEIVED AN ATT FAIL ON LT EFFIS, CREW RETURNED TO LAND, AHARS UNIT REPLACED.SDR U5QA06035Landing Gear · malfunctionedNLG WOULD NOT RETRACT. CREW CYCLED LANDING GEAR RETRACT HANDLE SEVERAL TIMES AND NOSE GEAR REMAINED DOWN AND LOCKED. MAIN GEAR CYCLED NORMALLY.SDR DXTA2011050204571Knob · misinstalledFLAP HANDLE WOULD NOT MOVE FROM FLAP 15 DEGREE POSITION. FOUND KNOB INSTALLED TOO FAR DOWN ON FLAP SELECTOR HANDLE, ADJUSTED FLAP KNOB AND TIGHTEN SET SCREW IAW MM 24-53-01. OPS CHECKED SATISFACTORY.SDR CWQR.2011.11Angle · crackedTHE CRACKED APU CONTAINMENT BOX ANGLES WERE FOUND DURING APU REPLACEMENT. BOTH ANGLES WERE FOUND CRACKED PAST THE LAST RIVET IN THE BEND RADIUS.SDR CWQR20110424001Angle · crackedTHE CRACKED APU CONTAINMENT BOX ANGLES WERE FOUND DURING APU REPLACEMENT. BOTH ANGLES WERE FOUND CRACKED PAST THE LAST RIVET IN THE BEND RADIUS.SDR DXTA2011042704567Warning Light · false activationDURING TAKEOFF "ACM OVERHEAT" LIGHT ILLUMINATED. ABORTED TAKEOFF. MAIN TIRES BLEW WHEN ACFT WAS ON TAXI WAY. RAN ACM FOR HALF AN HOUR, COULD NOT DUPLICATE DISCREPANCY. CLEANED COALESOR SOCK IAW THE MM 21-51-00. OPS AND LEAK CHECKED GOOD.SDR CVGA 11 120 2Warning System · activatedLT ENGINE BLEED AIR OVERHEAT LIGHT ILLUMINATES IN-FLIGHT.SDR DXTA2011042504557Brake Assy · malfunctionedWHILE TAXIING THE BRAKES WERE APPLIED ON THE RT (CO-PILOTS) SIDE, THEY GRABBED ABRUPTLY & PULLED TO ONE SIDE & WOULDN'T RELEASE RIGHT A SECOND TRY PRODUCED SIMILAR RESULTS PULLING TO THE OPPOSITE SIDE. PILOTS SIDE WORKED NORMALLY. INSPECTED TIRE PRESSURES, SDR DXTA2011042504560Unknown · unknownINTERMITTENTLY AFTER TAKEOFF AND GEAR RETRACTION, A VERY LOUD BANGING SOUND AND VIBRATION COMES FROM THE FWD RT SIDE OF ACFT. SLOW CYCLED GEAR. FOUND NOSE GEAR DOORS OUT OF ADJUSTED AND BINDING AGAINST EACH OTHER WHEN GEAR GOES UP IN WELL. NO DAMAGED TO DOORSSDR 9JLA3371Uplock Switch · defectiveAFTER TAKEOFF THE CREW ATTEMPTED TO RETRACT THE LANDING GEAR AND NOTED THE RED GEAR UNSAFE LIGHT ILLUMINATED. THE CREW CYCLED THE LANDING GEAR AND HAD THE SAME INDICATIONS. THEY SELECTED GEAR DOWN AND RETURNED TO STARTING POINT. MX TROUBLESHOT THE LANDING GSDR DXTA2011042004551Water Separator · odorDISTINCT EXHAUST ODOR IN COCKPIT AT TAKE OFF WITH APU ON AND APU BLEED AIR ON. WITH BLEED AIR OFF THE ODOR IS REDUCED. IN FLIGHT THERE IS AN EXHAUST ODOR (NOT AS DISTINCT). IT IS REDUCED WHEN EITHER PRESS SOURCE IS SELECTED. FOUND APU OIL OVERSERVICED. REMSDR CA110427004Fadec · malfunctioned(CAN) ABORTED T/O DURING T/O ROLL, THE RT ENGINE CONTROL FAULT LIGHT CAME ON. THE CREW ABORTED T/O AND THE ACFT RETURNED TO THE RAMP. TROUBLESHOOTING FOUND FAULT CODES INDICATING A FADEC CHANNEL LOSS. AN ENGINE CONTROL FAULT RESET WAS MADE AND THE FAULTS CLSDR CA110412003Line · misinstalled(CAN) RIGID FUEL LINE, WAS MAKING CONTACT WITH THE LOWER COWL ASSY AND SUBSEQENTLY WEARING THE SKIN. INVESTIGATION SHOWS THE FUEL LINE MAY NOT HAVE BEEN INSTALLED CORRECTLY. THE FUEL LINE HAS 1 SHORTER TUBE THAT SHOULD BE SECURED TO THE ENGINE DRIVEN FUEL PSDR DXTA2011041304545Tire · separatedRT MAIN TIRE SEPARATED ON LANDING. FOUND TIRE IN SHREADS AND LANDING GEAR WIRE BUNDLE BROKEN IN BOLT. R & R RT MAIN WHEEL ASSY WITH OH UNIT IAW MM CHAP 32-41-02. SERVICED TIRE TO 210 PSI ALSO R & R RT MAIN GEAR WIRE BUNDLE ASSY WITH NEW UNIT IAW MM CHAP 32-4SDR Z5FA040811N547CS1Control Cable · failedDURING CLIMB, APPROACHING FL230, THE PITCH TRIM ANNUNCIATOR CAME ON. THE AUTO PILOT WAS MANUALLY DISCONNECTED AND THE ACFT IMMEDIATELY PITCHED UP WHICH WAS CONTROLLED WITH ABNORMAL CONTROL COLUMN PRESSURE. USE OF ELECTRIC OR MANUAL ELEVATOR TRIM WAS INEFFECTISDR DXTA2011040404538Water Separator · dirtyAFTER TAKEOFF AND REACHING 4000 FT NOTED SMOKE FILLING COCKPIT WITH APU ON. SHUT APU DOWN SMOKE DISSIPATED RETURNED TO FIELD. REMOVED WATER SEPARATOR, FOUND WATER SEPARATOR AND SOCK DIRTY, CLEANED WATER SEPARATOR AND SOCK. INSTALLED AND ASSEMBLED WATER SEPSDR DXTA2011040104537Actuator · inoperativeCLIMBING THROUGH 20,000 FT ACCELERATING TOWARD 270 KIAS THE LT GEAR DOWN LOCK LIGHT (GREEN) ILLUMINATED. THE ACFT WAS DECELERATED TO 200 KIAS AND THE LIGHT WENT OUT AFTER ABOUT 2 MINUTES TOTAL ILLUMINATION. AT NO TIME DID THE RED GEAR UNLOCK LIGHT ILLUMINATE, SDR DXTA2011040404537Warning Light · illuminatedCLIMBING THROUGH 20000FT ACCLERATING TOWARD 270KIAS THE LEFT GEAR DOWN LOCK LIGHT (GREEN) ILLUMINATED. THE AIRCRAFT WAS DECELERATED TO 200KIAS AND THE LIGHT WENT OUT AFTER ABOUT 2 MINUTES TOTAL ILLUMINATION. AT NO TIME DID THE RED GEAR UNLOCK LIGHT ILLUMINATE,SDR CA110413006Oil System · low pressure(CAN) LOW OIL PRESSURE/IFSD DURING CLIMB PASSING FL110, THE ENGINE LOW OIL PRESSURE WARNING SOUNDED. THE PILOT IMMEDIATELY REDUCED THE POWER TO IDLE, AND SHUT THE ENGINE DOWN BEFORE RETURNING TO THE POINT OF ORIGIN WHERE AN UNEVENTFUL SINGLE ENGINE LANDING WASDR 9JLA3430Uplock Switch · defectiveAFTER TAKEOFF THE CREW RETACTED THE LANDING GEAR AND NOTED A UNLOCK LIGHT FOR THE GEAR, THE CREW DECLARED AND EMERGENCY THEN FOLLOWED THE CHECKLIST AND RESOLVED THE PROBLEM. THEY RESENDED THE EMERGENCY AND LANDED SAFELY. MX TROUBLESHOT THE LANDING GEAR SYS ASDR 2011FA0000206Downlock Switch · leakingACTUATOR LEAKING FROM DOWNLOCK SWITCH. PART (MFG PN 9912537-4 (VENDOR PN 1550000-6B), SN 1197B)SENT TO MFG FOR REPAIR. SAME PART WAS REPAIRED/MODIFIED IAW CMM WITH IPL AND RETURNED (REF MFG ICT WO 2-80089). PART REINSTALLED BY MFG SERVICE CENTER, FUNCTIONAL SDR DXTA2011032804522Actuator · slowWHEN EXTENDING THE GEAR FOR LANDING, THE LEFT MAIN DOWN LIGHT DID NOT ILLUMINATE AND THE UNSAFE LIGHT DID NOT EXTINGUISH. RAN ROTARY TEST AND ASSURED THAT ALL GEAT INDICATORS WERE WORKING, AND EXTENDED FLAPS BEYOND 15 DEGREES AND RECEIVED WARNING HORN. AFTERSDR DXTA2011032904522Warning Light · false activationWHEN EXTENDING THE GEAR FOR LANDING, THE LEFT MAIN DOWN LIGHT DID NOT ILLUMINATE AND THE UNSAFE LIGHT DID NOT EXTINGUISH. AFTER ABOUT ONE MINUTE, THE GEAR DOWN INDICATOR LIGHTS ILLUMINATED AND THE THE GEAR UNSAFE LIGHTS EXTINGUISHED.SDR DXTA2011032804526Shimmy Dampener · malfunctionedNOSE WHEEL SHIMMY ON T/O AND LANDING ROLL. TROUBLSHOT NOSE WHEEL SHIMMY INSPECTED NW STEARING, GOOD, INSPECTED NG TORQUE LINKS, GOOD INSPECTED NOSE WHELL ASSY GOOD. FOUND SHIMMY DAMPER HEADS SERVICED, SERVICED SHIMMY DAMPER IAW MM 12-14-01, LEAK CHECKED GOODSDR DXTA2011032804525Warning Light · illuminatedCLIMBING THROUGH FL280, THE RIGHT ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. THE EMERGENCY STOW SWITCH WAS SELECTED AND THE UNLOCK LIGHT EXTINGUISHED. A MINUTE LATER THE UNLOCK LIGHT REILLUMINATED AND REMAINED ON THROUGHOUT DESCENT AND LANDING. IT WAS STSDR 2011FA0000196Support Bracket · damagedDURING MX (PERFORMING MSG3 TASK 27-90-20-721 RUDDER AND RUDDER TRIM CONTROL SYSTEM FUNCTIONAL CHECK) IT WAS NOTED THAT THE FAIRLEAD TUBE PN 6661051-20 FOR THE RUDDER CABLES, WHICH PASSES THROUGH THE EXTERNAL FRAMES ON THE BOTTOM OF THE FUSELAGE AT LBL4.00 WAS SDR DXTA2011032104520Actuator · bindingELEVATOR TRIM TAB JAMMED AND COULD NOT BE MOVED ELECTRICALLY OR MANUALLY. FLIGHT WAS AT 41000' AND THE PITCH TRIM ANNUNCIATOR ILLUMINATED DESCENDING THROUGH 34000'. THE TRIM TAB REMAINED LOCKED IN POSITION UNTIL 19000' WERE ABLE TO MANUALLY BREAK IT LOOSE. RESDR DXTA2011031704512Uplock Switch · out of adjustNORMAL TAKEOFF ROLL, UPON POSITIVE RATE, GEAR LEVER WAS SELECTED UP, IT APPEARED GEAR CYCLED UP HOWEVER RED "UNLOCK" LIGHT REMAINED ILLUMINATED. FOUND HYD FLUID LEVEL FULL AND NO LEAKS NOTED. PERFORMED GEAR SWINGS MULTIPLE TIMES IAW MM 32-01-00 AND COULD NOTSDR DXTA2011031504508Warning Light · illuminatedDURING FIRST ENGINE START WITH PARKING BRAKE SET "LOW BREAK PRESSURE/ANTISKD INOP" CAUTION ANNUNCIATOR ILLUMINATED WITH CORRESPONDING MASTER CAUTION ANNOUNCIATOR ILLUMINATED. DURING POST-FLIGHT, ELECTRICAL ODOR NOTICED IN THE LT FORWARD COMPARTMENT AROUND THE SDR DXTA2011031004502Drain · obstructedON CLIMB OUT, PASSING FL 220, RUDDER EFFECTIVENESS LOST. RUDDER FELT FROZEN. FREEZING LEVEL FL160. ON DESCENT REGAINED RUDDER EFFECTIVENESS AT FL140, JUST BELOW FREEZING LEVEL. RUDDER WAS NORMAL FOR APPROACH AND LANDING. REMOVED ACCESS PANEL AND FOUND ICE.SDR DXTA2011030704493Relay · erodedAT POWER UP PRIOR TO TAKE OFF ANTISKID LIGHT ILLUMINATED. THE POWER BRAKE CB POPPED. RETURNED TO RAMP. POWER BRAKE HAD BLED DOWN SUFFICIENTLY AND PNUEMATIC BRAKES WERE USED TWICE TO STOP AND PARK AIRCRAFT. OPS CHECKED BRAKES REPEATEDLY & NO PROBLEM NOTED (INISDR DXTA2011030704491Warning Light · false indicationON DEPARTURE AFTER LANDING GEAR RETRACTION RED UNLOCK LIGHT REMAINED ILLUMINATED. ALL THREE GREEN LIGHTS WERE EXTINGUISHED. COMPLIED WITH GEAR EXTENSION & RETRACTION TEST IAW MM 32-30-00 R20. OPS CHECKED GOOD AT THIS TIME. INSPECTED UPLOCK SWITCHES. NO DEFESDR DXTA2011030704490Drain · icedUPON LANDING, THE RUDDER PEDDELS WERE JAMMED AND WE HAD NO STEERING. AFTER INSPECTING NOSE WHEEL ON RAMP WE WERE ABLE TO MOVE THE NOSE WHEEL BY HAND FREELY IN EITHER DIRECTON BUT COULD NOT MOVE IT W/ THE RUDDER PEDDELS AS THEY WERE STILL JAMMED. FOUND ICE ACCSDR 9JLA201103033369Solenoid · defectiveCREW REPORTED CABIN DOOR ANNUNCIATOR REMAINED ILLUMINATED AFTER THE CABIN DOOR WAS CLOSED. TROUBLESHOOTING IDENTIFIED THE DOOR VENT SOLENOID AS DEFECTIVE. THE SOLENOID WAS REPLACED, FUNCTIONAL CHECKS WERE SATISFACTORY.SDR DXTA2011030304489Bearing · wornVIBRATION IN AIRFRAME. MOST NOTABLE AT HIGHER SPEEDS-290K. NOT NOTICEABLE AT SPEEDS LESS THAN 240K. NO CHANGES WITH CONFIGURATION CHANGE. VIBRATION FELT THROUGHOUT AIRFRAME, AUTOPILOT ON AND OFF. R & R ELEVATOR, LT TRIM TAB HORN BEARINGS AND REPLACED RUDDSDR DXTA2011022304476Uplock Switch · out of adjustGEAR UNLOCK LIGHT REMAINED ON AFTER GEAR RETRACTION.( HYD PRESS LIGHT NEVER EXTINGUSHIED , AND THEN THE STAB MIS-COMPARE LIGHT CAME ON , UNABLE TO DETERMINE WHICH DID NOT LOCK. ADJUSTED LT & RT MLG UPLOCK SWITCHES IAW MM 32-30-05, OPS CHECKED GOOD.SDR DXTA2011022104472Pitot Tube · obstructedBOTH PILOTS PFD'S DISPLAYED AN AMBER IAS MESSAGE AFTER PASSING THROUGH 160 KTS. AT MINIMUM LT PILOTS IAS INDICATING 160, RT PILOTS INDICATING 166 & STANDBY INDICATING 167. ACCELERATED TO 200 KTS, SPLIT INCREASED TO ABOUT 9 KTS BETWEEN PRIMARY IAS INDICATORS SDR DXTA2011022104471Gyro · inoperativeAT FL 430, WITH PFD 2 SELECTED (RT SEAT FLYING) LT PFD COMMAND BAR TURNED BLUE ALONG WITH ALL TREND BARS AND COURSE INDICATORS. THE RED AIRSPEED TAPE DISSAPEARED AND THE ATTITUDE GYRO TURNED TO GRAY, VICA, BLUE AND BROWN. REPOSITIONED THE NR 1 PFD TO THE MFSDR CA110228016Oil System · low pressure(CAN) LOW OIL PRESSURE FOLLOWING T/O AT FL130, THE LOW OIL PRESSURE WARNING LIGHT CAME ON. THE PILOT REDUCED POWER TO IDLE AND THE OIL PRESSURE CAME BACK NORMAL, HOWEVER UPON RE-ADVANCING THE THROTTLE, THE WARNING CAME BACK ON. POWER WAS REDUCED, EMERGENCY WSDR Z5FA021711N521CS1Windshield · crackedDURING CRUISE ALTITUDE AT FL40, F/O INNER WINDSHIELD CRACKED. CREW DECLARED AN EMERGENCY AND DIVERTED. LANDING WAS UNEVENTFUL. THE RT WINDSHIELD WAS REPLACED BY MX. LEAK AND OPS CHECK WAS GOOD. ACFT RETURNED TO SERVICE.SDR Z5FA021711N508CS1Actuator · inoperativeON APPROACH, THE NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE, FOLLOWED BY THE RED UNSAFE LITE DURING NORMAL GEAR EXTENSION. CREW EXECUTED A MISSED APPROACH, FOLLOWED BY THE "LANDING GEAR FAILED TO EXTEND" CHECK LIST PROCEDURE AND DECLARED AN EMERGENCY. AFTER EMSDR CA110228009Engine · failed(CAN) ABORTED TAKEOFF, DURING TAKEOFF ATTEMPT, NR 2 ENGINE ELECTRONIC ENGINE CONTROL MANUAL LIGHT ILLUMINATED. THE T/O WAS ABORTED AND THE ACFT SHUTDOWN. THE ACFT WAS CYCLED, ENGINES STARTED IN MANUAL MODE AND A SECOND TAKEOFF WAS PERFORMED, DURING CLIMBOUT,
Back to Textron 560XL