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 DXTA2001082504710Brake · chatteringLT BRAKE CHATTERING WHEN ANY PRESSURE APPLIED. INSPECTED BRAKE SYS, CHECKED ACCUMULATOR PRESSURE AND FLUID LEVEL. SYS CHECKED GOOD. TAXIED ACFT AT 40 KTS, NO FAULTS NOTED. PERFORMED TAXI CHECK AT 70 KTS, NO FAULTS NOTED. DONE IAW MM 9-20-00.SDR DXTA2011082404709Bungee · bindingBINDING IN RUDDER PEDALS WHEN TURNING. MORE PROMINENT IN RIGHT HAND TURNS. FEELS LIKE SOMETHING BINDS MOMENTARILY THEN RELEASES. CAN HEAR "POP" AND FEEL IT IN BOTH PEDALS. PERFORMED TAXI CHECK. BINDING SOUND APPEARED TO BE LOUDER ON PILOT SIDE. INSPECTSDR DXTA2011082204705Landing Gear · malfunctionedNOSE GEAR DID NOT RETRACT AFTER TAKEOFF. MLG RETRACTED NORMAL & INDICATORS WENT OUT. NLG INDICATOR LIGHT REMAINED ILLUMINATED. HYDRAULIC LIGHT CYCLED NORMAL & WENT OUT AFTER FLAPS & MLG RETRACTED. LANDED NORMAL. POST FLIGHT INSPECTION SHOWED NO ABNORMAL INSDR CWQR2011081515Hinge Bracket · crackedDURING AN INSPECTION, FOUND INBD ELEVATOR HINGE BRACKET CRACKED. IT WAS CRACKED IN THE UPPER BRACKET RADIUS AREA THAT ATTACHES TO THE UPPER SKIN OF THE HORIZ STABILIZER. REPLACED CRACKED HINGE BRACKET WITH NEW AND SUBMITTED SERVICE CONDITION REPORT TO MFG UNSDR CWQR2011081514Hinge Bracket · crackedDURING AN INSPECTION, FOUND THE OTBD ELEVATOR HINGE BRACKET CRACKED. IT WAS CRACKED IN THE UPPER BRACKET RADIUS AREA THAT ATTACHES TO THE UPPER SKIN OF THE HORIZ STABLIZER. REPLACED CRACKED HINGE BRACKET WITH NEW AND SUBMITTED SERVICE CONDITION REPORT TO MFGSDR 9JL2011F00000Unknown · malfunctionedON 2 SEPARATE OCCASIONS UNS-1 MODEL FMS`S HAVE COMMANDED ERRONEOUS TURNS ON THE SAME APPROACH SEQUENCE. INITIAL INVESTIGATION SEEMS TO INDICATE A POSSIBLE SOFTWARE DEFECT.SDR DXTA2011081204703O-Ring · vibrationTHE RT BRAKE HAS A SHUDDER/ VIBRATION DURING BRAKE RELEASE. IT IS MOST NOTICEABLE AFTER LANDING WHEN THE BRAKES ARE HOT. FOUND RT BRAKE LEAKING FLUID AT FITTING ON SHUTTLE VALVE. REPLACED FITTING AND O-RING WITH NEW. PERFORMED BRAKE BLEEDING PROCEDURE IAWSDR Z5FA081211N523CS1Actuator · defectiveUPON LANDING GEAR EXTENSION FOR LANDING THE LT MAIN GEAR DID NOT HAVE A SAFE INDICATION (NO GREEN LIGHT & RED GEAR UNSAFE LIGHT). THE CREW EXECUTED A MISSED APPROACH AND COMPLIED WITH THE APPROPRIATED CHECK LIST. THE LANDING WAS UNEVENTFUL. THE LT MAIN LANDINSDR DXTA2011080904694Transducer · inoperativeDURING TAKEOFF ROLL, PRIOR TO 70KTS, MASTER CAUTION ILLUMINATED WITH ANTISKID INOPERATIVE CAUTION LIGHT. TAKEOFF WAS ABORTED. LIGHTS STAYED ON APROX 3 SECOND, WENT OUT, AND ILLUMINATED AGAIN DURING ROLLOUT FOR ANOTHER 3-4 SECONDS. R & R RT WHEEL SPEED TRANSDSDR 2011F00172Squat Switch · false indicationRT LANDING GEAR ACTUATOR GAVE A FALSE INDICATION, CONFLICTING WITH THE INDICATION OF THE SQUAT SWITCH GIVING A FALSE LOW BRAKE PRESSURE/ANTI SKID INOP WARNING.SDR Z5FA20110808001Switch · intermittentAFTER TAKEOFF, RT MAIN GEAR STILL INDICATED DOWN & LOCKED AFTER GEAR SELECTED UP. DURING APPROACH THE "LOW BRAKE PRESS" LIGHT AND THE "ANTI SKID" LIGHT ILLUMINATED. CREW FOLLOWED THE CHECKLIST AND AN EMERGENCY WAS DECLARED. "SUPPLEMENT INFORMATION" THE DISCSDR DXTA2011080804693Unknown · unknownAFTER TAKEOFF, WHILE CYCLING LANDING GEAR UP, A LOUD BANG AND THUD HEARD. FLAPS & ALL ENGINES OPS NORMAL. PERFORMED LANDING GEAR HYD FUNCTIONAL TEST. NO DEFECTS NOTED. OPS CHECKED NORMAL. WORK PERFORMED IAW MM 32-01-00.SDR Z5FA080611N546CS1Actuator · failedDURING OPS, CHECK FLIGHT FOR SAME PROBLEM, ENROUTE, THE LOW BRAKE PRESSURE & ANTI SKID INOPERATIVE LIGHT ILLUMINATED. AN EMERGENCY WAS DECLARED AND DIVERTED. LANDING WAS UNEVENTFUL. MX TROUBLESHOT ISSUE TO THE DOWNLOCK SWITCH INSIDE THE RT MAIN GEAR ACTUATOSDR DXTA2011080804690Circuit Breaker · trippedPOWER BRAKE CIRCUIT BREAKER TRIPPED OFF DURING TAKEOFF, GIVING A ANTI-SKID INOPERATIVE CAUTION. INSPECTED POWER BRAKE PUMP. ANTI SKID ROTARY TEST GOOD. NO FAULTS FOUND ON FAULT DISPLAY UNIT. TAXIED ACFT AND NO DEFECTS NOTED, REF MM 32-42-00.SDR DXTA2011080504686Ahrs · inoperativeDURING DECENT FL260 AT 300KIAS, NOTICED A BACK & FORTH FLUXUATION ON TRIANGLULAR RUDDER TRIM INDICATOR, FOLLOWED BY AUTOPILOT KICKING OFF WITH AUDIBLE ALARM. RESET AUTOPILOT & IT KICKED OFF 1 SECOND LATER. APPLIED SLIGHT PRESSURE TO RUDDER PEDALS & FELT A "THSDR Z5FA080306N564CS1Pressure Switch · intermittentENROUTE, THE LOW BRAKE PRESSURE AND ANTI-SKID INOP LIGHTS ILLUMINATED. CREW DECLARED AN EMERGENCY AND DIVERTED. LANDING WAS UNEVENTFUL USING THE EMERGENCY BRAKES. MX R & R THE ANTI SKID BRAKE PRESSURE SWITCH AND THE ANTI SKID LOW PRESSURE SWITCH. SYSTEM WASDR DXTA2011080404684Bearing · seizedIN FLIGHT WHEN LANDING GEAR EXTENDED, A LOUD CLUNKING NOISE HEARD IN COCKPIT. ON GROUND IF YOU WIGGLE THE RT NLG DOOR, SAME CLUNKING NOISE IN THE GEAR DOOR LINKAGE. FOUND RT NLG DOOR MIDDLE ROD END BEARING AND BOLT SEIZED. R & R ROD END BEARING & ATTACHING SDR 2011FA0000509Transducer · failedTHE RT ENGINE OIL PRESSURE TRANSDUCER FAILED IN-FLIGHT GIVING A FALSE INDICATION OF DECRESSING PRESSURE.SDR Z5FA080111N503CS1Bulb · failedAFTER LOWERING GEAR HANDLE, RECEIVED LT MAIN GEAR UNSAFE INDICATION. (NO LT MAIN GREEN LIGHTS). MANUALLY LOWERED GEAR WITH BLOWDOWN. ALL APPLICABLE EMERGENCY CHECKLISTS WERE FOLLOWED AND AN EMERGENCY WAS DECLARED. LANDING WAS UNEVENTFUL. MX R & R BOTH INOSDR DXTA2011080104675Ahrs · malfunctionedLEFT PFD: "HEADING FAILURE - SINGLE" AT ALTITUDE. R & R LT AHRS COMPUTER. OPS CHECKED GOOD. WORK DONE IAW MM 34-21-01.SDR Z5FA072511N549CS1Bearing · seizedUPON LANDING, THE NOSE WHEEL SEIZED UP. DUE TO THE INCIDENT FIRETRUCKS WERE DISPATCHED TO THE ACFT ON THE RUNWAY. ACFT WAS TOWED OFF OF THE RUNWAY. NLG WHEEL BEARINGS WERE FOUND SEIZED. REPLACED THE NOSE LANDING GEAR FORK ASSY AND NOSE WHEEL/TIRE ASSY. ACSDR DXTA2011072504669Display · failedSTANDBY ATTITUDE INDICATOR BLINKED OFF. SECONDS LATER SMELLED AN ELECTRICAL BURNING ODOR IN COCKPIT WITH LIGHT SMOKE. R & R SECONDARY FLIGHT DISPLAY, OPS CHECKED GOOD IAW MM 34-22-01.SDR DXTA2011072204664Wheel · malfunctionedON DEPARTURE, AUTOPILOT DISENGAGED AND SIGNIFICANT FORWARD PRESSURE REQUIRED ON CONTROL WHEEL. AUTOPILOT WAS REENGAGED AND DISENGAGED 2 MORE TIMES UNTIL ACFT WAS SLOWED TO BELOW 160 KNOTS. INSPECTED SYS, FOUND ELEVATOR TRIM WHEEL POINT HAD JUMPED OFF TRACK. SDR CA110803005Oil System · low pressure(CAN) AT 7000 FT CREW REPORTED LT ENGINE OIL PRESSURE HAD DROPPED TO ZERO. ENGINE WAS SHUTDOWN AND ACFT RETURNED TO POINT OF DEPARTURE AND LANDED UNEVENTFULLY. TROUBLESHOOTING IS ONGOING.SDR CA110715002Wire Harness · faulted"APU RELAY ENGAGED" LIGHT CAME ON AND STAYED ON ANYTIME THE APU MASTER SWITCH WAS SELECTED ON. THIS LIGHT IS SUPPOSED TO INDICATE TO THE CREW ANY TIME EITHER THE APU STARTER OR GENERATOR RELAYS HAVE BEEN ACTIVATED. WITH THIS FAILURE, IT WAS NOT POSSIBLE TO VSDR DXTA2011071104655Unknown · vibrationON APPROACH, AT 122 KNOTS, EXPERIENCED A VIBRATION AND ASSOCIATED LOW PITCH RUMBLE NOISE, SEEMED TO CHANGE WITH THROTTLE CHANGES. NOISE LASTED UNTIL TOUCHDOWN. RUMBLE COULD NOT BE HEARD ON TAXI IN. INSPECTED AIRFRAME AND BOTH ENGINES, RAN ENGINES AT ALL PSDR CA110713007Actuator · seizedPILOTS REPORTED "STAB MISCOMPARE" ILLUMINATES AND HYD ANNUNCIATOR FAILS TO EXTINGUISH WHEN FLAPS ARE SELECTED TO THE UP POSITION, IN THE JOURNEY LOG. THE PILOTS ALSO STATED THAT THEY HAD DIFFICULTY TRIMMING THE PITCH OF THE ACFT. MX TROUBLESHOOTING DETERMINEDSDR Z5FA070511N540CS1Windshield · failedDURING CRUISE AT FL 390, THE F/O WINDSHIELD SHATTERED. CREW DECLARED AN EMERGENCY, DESCENDED TO 13,000 FT., COMPLIED WITH ABNORMAL PROCEDURES AND DIVERTED. ACFT LANDING WAS UNEVENTFUL. WINDSHIELD WAS DEFERRED BY THE CREW UNDER CDL 56-1. LOCAL MX INSPECTED TSDR DXTA2011070504646Bearing · wornCLIMBING THROUGH 10,000 FT & ACCELERATING PAST 200, A NOTICABLE VIBRATION FELT IN YOLK, MOST NOTICABLE AFTER AILERON TRIM WAS PUT INTO LEVEL WITH WINGS. AFTER LEVEL OFF AT FL230 IAW INSTRUCTIONS, RETARDED EACH THOTTLE ONE AT A TIME & NO CHANGE IN VIBRATION.SDR DXTA2011070504645Brake Sys · malfunctionedUPON LANDING, NOTICED THAT THE LT BRAKE PEDAL REQUIRED VERY LITTLE MOVEMENT BEFORE IT WOULD GRAB, THE RT BREAK PEDAL REQUIRED A NORMAL AMOUNT OF MOVEMENT. THIS WAS ON BOTH LT AND RT SIDES AND BOTH HIGH SPEED AND LOW SPEED. TAXIED ACFT AND CONFIRMED SQ LT BRASDR DXTA2011070504641Flap System · malfunctionedDURING TAKEOFF, FLAP 15 IMMEDIATELY AFTER ROTATION, A GRINDING/RUBBING FELT IN THE YOKE WITH FORE AND AFT YOKE MOVEMENTS. AFTER RETACTION OF FLAPS AND LEVEL OFF, GRINDING WAS STILL PRESENT. AFTER LANDING, UNABLE TO REPRODUCE GRINDING. INSPECTED ELEVATOR CASDR DXTA2011070504642Brake Sys · malfunctionedRT BRAKE GRABS HARD ON HIGH SPEED LANDING ROLLOUT AND TAXIING. RT BRAKE GRABS HARD ON HIGH SPEED LANDING ROLLOUT AND TAXIING. , BLED BRAKES AND CHECK SYS IAW MM 32-44-00. COMPLETED HIGH SPEED TAXI CHECK, NO FAULTS NOTED. OPS AND LEAK CHECKS COMPLETED.SDR 2011FA0000462Pushrod · looseOPERATOR FOUND ELEVATOR TRIM PUSHROD ASSY LOOSE BETWEEN FORWARD TUBE AND FORWARD JAM NUT. ALL SAFETY WIRE WAS IN PLACE BETWEEN FORWARD AND AFT JAM NUT. ALSO NOTICED SLIGHT BOW IN TUBE NEAR FORWARD CLEVIS. CAUSE UNDETERMINED. OPERATOR REPLACED ASSY.SDR DXTA2011070504640Control Unit · malfunctionedRIGHT ENGINE FIRE LIGHT. EXECUTED CHECKLIST, BOTH BOTTLES EXPENDED. FIRE LIGHT REMAINED ON FROM 41000 TO LANDING. TROUBLESHOT PROBLEM TO CONTROL UNIT. REMOVED CONTROL UNIT. INSTALLED NEW CONTROL UNIT. RAN ENGINE, OPS CHECKED GOOD IAW MM 26-11-00 AND MMSDR CA110711008Engine · unknown(CAN) INABILITY TO MODULATE THRUST DURING TROUBLESHOOTING ON GROUND, THRUST COULD NOT BE MODULATED. ELECTRONIC ENGINE CONTROL SWAP WAS PERFORMED AND A SIMILAR BEHAVIOR OCCURRED AGAIN. TROUBLESHOOTING IS ONGOING.SDR 9JLA3378Bearing · looseTHE CREW REPORTED THE LANDING GEAR UNLOCK ANNUNCATOR REMAINED ON AFTER GEAR RETRACTION AND THE HYD LIGHT STAYED ON. THIS HAS BEEN A REOCCURRING DISCREPANCY WITH THIS AIRCRAFT. EVERYTHING FROM THE ADJUSTMENT OF THE NOSE LANDING GEAR UPLOCK AND UPLOCK SWITCH TSDR DXTA2011061504617Control Valve · malfunctionedAIR DUCT OVER HEAT CABIN (ENVIRONMENTAL DUCT OVERTEMP) REACHED A TEMP OF 325C AND WAS INCREASING AND SMOKE IN THE CABIN IN-FLIGHT. FOLLOWED CHECKLIST Q4 AND TEMP DECREASED TO 208C. TROUBLESHOT "AIR DUCT O' HEAT CABIN" LIGHT, CABIN SUPPLY AIR UNCONTROLLABLE ISDR DXTA2011061604617Environ Sys · overheatedAIR DUCT OVER HEAT CABIN (ENVIRONMENTAL DUCT OVERTEMP) REACHED A TEMP OF 325C AND WAS INCREASING AND SMOKE IN THE CABIN IN-FLIGHT. FOLLOWED CHECKLIST Q4 AND TEMP DECREASED TO 208C.SDR 2011FA0000397Bolt · wornTWO PUSH/PULL TUBES THAT ATTACH TO THE AFT ELEVATOR BELLCRANK, WHEN TORQUING ATTACHING HARDWARE, THE NUT SHANKS OUT ON THE BOLT, ALLOWING THE BOLT TO BE ROTATED BY AND AND CAUSING WEAR IN THE BELLCRANK ATTAHCH HOLE. THIS WEAR CAUSES EXCESSIVE PLAY AT THE ATTSDR 2011FA0000396Shaft · wornFOUND GROOVES WORN INTO SHAFT OF THE 2 SCREWS THAT ENTER INTO THE RUDDER ACTUATOR ASSEMBLY. ACFT IS SET FOR CRUISE CONFIGURATION: DURING FLIGHT, TAIL VIBRATES CAUSING GROOVES TO WEAR INTO SHAFT OF SCREWS AT POINT WHERE SCREWS ENTER INTO ACTUATOR.SDR DXTA2011061404611Windshield · failedRIGHT WINDSHIELD FAULT LIGHT ILLUMINATED. NO OVERHEAT LIGHT. SHORTLY AFTER RT WINDSHIELD SHATTERED. WINDSHIELD SEAL LOOKS BUCKLED ON TOP CENTER PORTION. MELTED, STREAKING UP FROM BOTTOM OF WINDSHIELD. LT WINDSHIELD FAULT LIGHT ILLUMINATED. NO OVERHEAT LIGSDR DXTA2011061304610Seal · leakingDURING CRUISE BOTH ENGINE FIRE SWITCHLIGHTS ILLUMINATED. EXECUTED EMERGENCY CHECKLIST ITEMS. ALL ENGINE INSTRUMENTS INDICATED NORMAL. DESCENDING THROUGH 5000 FT AT 180 KTS, BOTH FIRE LIGHTS EXTINGUISHED. AFTER VISUAL INSPECTION OF BOTH ENGINES, THERE WAS NOSDR 2011FA0000382Throttle Switch · defectiveLT AND RT ENGINE THROTTLES HAVE A BANK OF 6 SWITCHES CONNECTED TO EACH THROTTLE LEVER. CUSTOMER`S SQUAWK WAS THAT THE DETENT INDICATOR LIGHTS (MOUNTED ON THE INSTRUEMENT PANEL) FOR THE INDIVIDUAL THROTTLE WERE INOPERATIVE. TROUBLESHOT SYS AND FOUND 2 OUT OF SDR CA110614003Oil System · pressure loss(CAN) OIL PRESSURE LOSS/IFSD DURING FLIGHT, THE PILOT NOTICED A LOSS OF OIL PRESSURE. SHUT THE ENGINE DOWN AND HAD AN UNEVENTFUL SINGLE ENGINE LANDING. POST FLIGHT INSPECTION FOUND NO OIL INDICATION ON THE SIGHT GLASSES AND NO EVIDENCE OF EXTERNAL OIL LEAK. SDR DXTA2011060704609Trunnion · corrodedCORROSION FOUND ON RT LANDING GEAR RETRACT ACTUATOR TRUNNION ATTACH POINT. INSTALLED RT MLG TRUNNION ASSY REF MM 32-10-00.SDR DXTA2011060704608Actuator · leakingWITH HIGH POWER SETTING, BOTH PEDALS ARE VERY DIFFICULT TO MOVE FROM BOTH COPILOT AND PILOT SIDE. SUSPECT RUDDER BIAS IS PRESSURIZING BOTH SIDES SIMULTANEOUSLY. RUDDER BIAS CHECKED OK ON GROUND. REMOVED RUDDER BIAS ACTUATOR AND ACTUATOR MOUNT. INSTALLED ACTUSDR Z5FA060311N523CS1Cable Assy · brokenDURING POST MX PRE-FLIGHT, CREW DETECTED A BROKEN ELEVATOR TRIM CABLE. CABLE WAS REPLACED IAW MM PROCEDURES, RIGGED AND OPS CHECKED SATISFACTORY. CREW PERFORMED OPS CHECK FLIGHT SATISFACTORILY AND ACFT WAS RETURNED TO SERVICE.SDR DXTA2011060104600Uplock Switch · failedNLG MAKES LOUD MECHANICAL BUMPING NOISES WHEN RAISED WHICH DOES NOT STOP. SOUNDED LIKE UPLOCK WOULDN'T HOLD & GEAR CONTINUOUSLY CYCLED UP. RED UNLOCK LIGHT DIMLY FLICKERED AS WELL. LOWERED HANDLE AND MLG PROPERLY LOCKED DOWN WITH 3 GREEN INDICATION. UNABLE SDR DXTA2011053104598Motor · bindingAT 4000 FT, 180KTS, 10 SECONDS AFTER SELECTING FLAPS 7, AUTOPILOT KICKED OFF & ACFT PITCHED 20 DEGREES NOSE UP. AFTER STABILIZING ACFT AT 180 KTS, NO NOSE DOWN TRIM REMAINING, & TRIM WAS ALL THE WAY TO STOP. ACFT LANDED, FLAPS 7 & FLAPS WERE LEFT SELECTED AT SDR CA110613002Oil System · pressure loss(CAN) IFSD DURING REVENUE FLIGHT PILOTS NOTED OIL PRESSURE DROPPED TO 25 PSI IN CLIMB. OIL PRESSURE RECOVERED TO NORMAL RANGE AFTER A FEW SECONDS. SUBSEQUENTLY, DURING CRUISE, A SIGNIFICANT DROP OF OIL PRESSURE OCCURRED. PILOTS REDUCED ENGINE POWER TO FLIGHT
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