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 JGVR20180131001Skin · corrodedCORROSION ON THE RT UPPER WING SKIN, BLENDED AND PERFORMED AN EDDY CURRENT AND ULTRASONIC THICKNESS INSPECTIONS, PREPPED AND TREATED AREAS IAW SRM 51-10-03, 51-70-08, AND MM 51-10-00.SDR DXTA2018012700514Oil System · leakingWHILE PERFORMING COCKPIT PREPARATION AND BEFORE ENGINE START WITH APU OPERATING, LIGHT GRAY SMOKE WITH AN ACRID ODOR THAT WAS DETECTED AND OBSERVED. CREW SHUTDOWN THE BLEED AIR FOR A FEW MOMENTS, THEN RETURNED TO LOW BLEED. A HEAVIER SMOKE WITH THE SAME ODSDR DXTA2018012600515Circuit Board · malfunctionedLEFT ENGINE COMPRESSOR STALLED PRIOR TO TAKEOFF ROLL, POWERING UP ENGINE, THREE POPS WERE HEARD FROM THE LEFT ENGINE FOLLOWED BY A BURNING OIL ODOR INSIDE THE CABIN. TROUBLESHOT THE ISSUE. REMOVED AND REPLACED THE NR 1 AND 2 INTERFACE PRINTED CIRCUIT BOARDS,SDR JGVR20180126003Trunnion · corrodedRIGHT MLG TRUNNION OTBD LUG HAS CORROSION AND MATERIAL LOSS AROUND TRAILING LINK TO TRUNNION PIN, BLENDED THE AREA. FOUND BLENDED AREA TO BE MORE THEN ALLOWABLE LIMITS. REMOVED AND REPLACED THE TRUNNION IAW CMM 32-10-01, AND MM 32-10-00.SDR JGVR20180126002Axle · corrodedLEFT MLG AXLE HAS CORROSION THAT IS BEYOND SRM LIMITS. REMOVED AND REPLACED THE AXLE.SDR JGVR20180126001Axle · corrodedRIGHT MLG AXLE HAS CORROSION THAT IS BEYOND SRM LIMITS. REMOVED AND REPLACED THE AXLE.SDR JGVR20180125002Axle · corrodedNLG AXLE TUBE IS CORRODED. FOUND DURING NJA TASK CARD TC-5XL-32-160207. REMOVED EXISTING CORRODED NLG AXLE TUBE AND INSTALLED NEW CUSTOMER SUPPLIED NEW AXLE TUBE IN THE SAME LOCATION IAW MM 32-41-01.SDR JGVR20180125001Spar · corrodedLEFT HORIZONTAL STAB AFT SPAR CORRODED. BLENDED THE CORROSION IAW SRM 51-70-08. REMOVED LH AND RH ELEVATORS FOR ACCESS TO HORIZONTAL STABILIZER AFT SPAR CORROSION AND REINSTALLED IAW CESSNA 560XL MM 27-31-01. PERFORMED AN EDDY CURRENT INSPECTION ON LH AND RHSDR 9JLA2018020215969Attach Bracket · crackedAFTER TAKE-OFF, THE AIRCRAFT RETURNED BACK TO THE AIRPORT DUE TO A LOUD NOISE HEARD AFTER GEAR RETRACTION. THE CREW FOLLOWED FLIGHT MANUAL INSTRUCTION AND LANDED WITH OUT INCIDENT. AFTER LANDING THE FLIGHT CREW DISCOVERED THAT THE RT NOSE LANDING GEAR DOOR CSDR DXTA2018011800487Switch · failedWHILE CLIMBING, THE RT THRUST REVERSER UNLOCK LIGHT CAME ON FOLLOWED BY THE ARM LIGHT. TURNED ON THE EMERGENCY STOW SWITCH PERFORMED MEMORY ITEMS FOLLOWED BY THE CHECKLIST. DECLARED THE EMERGENCY AND DIVERTED. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED TSDR A8JA201801170001O-Ring · defectiveAT APPROXIMATELY 1315 HRS LOCAL, AIRCRAFT DEPARTED KAGC ENROUTE TO KHOU. AT TOP OF DESCENT, CREW NOTICED NR 2 ENGINE OIL PRESSURE FLUCTUATING, BUT REMAINING WITHIN OPERATIONAL RANGE. ALL OTHER ENGINE PARAMETERS (OIL TEMPERATURE, N1, N2, ITT) REMAINED STEADY.SDR O2GA2018020851501Connector · dirtyLEFT THRUST REVERSER UNLOCK LIGHT ILLUMINATED IN FLIGHT ON DESCENT COMING THROUGH 18,300 FT. MAINTENANCE COMPLIED WITH RESISTANCE CHECK OF T/R STOW LIMIT SWITCHES. CLEANED CONNECTORS. PERFORMED SYSTEM OPERATIONAL CHECK WITH NO DEFECTS NOTED. A SUCCESSFUL OPERASDR A59A201801090105Eec · malfunctionedPILOTS ATTEMPTED START AND START HUNG AT 16%. SAW ITT RISE HOWEVER ENGINE WOULD NOT ACCELERATE. REMOVED EEC AND INSTALLED ON LT ENGINE PROBLEM FOLLOWED.SDR DXTA2018010400435Brake Sys · contaminatedAFTER LANDING, AND DURING TAXI RECEIVED A LOW BRAKE PRESSURE AND ANTI-SKID INOPERATIVE ANNUNCIATORS WITH A MASTER CAUTION. ABLE TO STOP WITH NORMAL BRAKES, BUT THEN EMERGENCY BRAKES WERE NEEDED. ABOUT 30 SECONDS LATER, THE ANNUNCIATORS EXTINGUISHED AND NORMSDR CVGA20180105001Transmitter · malfunctionedMASTER WARNING INFLIGHT FOR LOW OIL PRESSURE ON RIGHT ENGINE. ZERO OIL PRESSURE NOTED ON PRESSURE GAUGE. OIL TEMP 60 DEG CELSIUS. PERFORMED ENGINE SHUTDOWN PER EMERGENCY CHECKLIST. FOLLOWING UNEVENTFUL LANDING, WIRING WAS CHECKED VISUALLY FOR SECURITY WITH NO SDR DXTA2018010400425Seal · leakingOIL ODOR IN THE COCKPIT AND CABIN. ODOR IS STRONGER WHEN THE APU IS RUNNING. INSPECTED THE APU AND FOUND STARTER GEN PAD SEAL LEAKING. REPLACED WATER COALESCER SOCK. RAN BOTH ENGINES AND NO ODOR NOTED. PULLED AND COLLARED APU MASTER C/B.SDR CVGA20180103001Thrust Reverser · partial deployAIRPLANE HAD SHALLOW VIBRATION INFLIGHT. VIBRATION INCREASED WITH AIRSPEED. AN EMERGENCY WAS DECLARED AS A PRECAUTION. LANDING WAS UNEVENTFUL. DURING POST FLIGHT, FOUND BOTTOM PORTION OF RIGHT THRUST REVERSER TO BE DEPLOYED APPROXIMATELY A 1/2 INCH.SDR DXTA2018010200001Seal · leakingOILY SMELL IN COCKPIT AND CABIN SMELL IS STRONGER WHEN THE APU IS RUNNING. INSPECTED APU AND FOUND STARTER/GEN PAD SEAL LEAKING. REPLACED WATER COALESCER SOCK. RAN BOTH ENGINES AND NO ODOR NOTED. APU DEFERRED IN ACCORDANCE WITH CE560XLS MEL. COMPLIED WITH MELSDR DXTA201712200635Warning Light · illuminatedWHEN LANDING GEAR WAS BROUGHT DOWN FOR LANDING, LOW BRAKE PRESSURE AND ANTISKD LIGHTS NEVER EXTINGUISHED. BRINGING THE MASTER CAUTION ON FLASHING. DEPARTED THE PATTERN AND RAN THE QRH. BRAKE CIRCUIT BREAKER WAS NOT TRIPPED. WHEN DESCENDING FOR LANDING, LOW BSDR 9JLA201801269721Control Switch · defectiveDURING THE PRE-FLIGHT CHECKLIST THE TRAILING EDGE FLAPS WERE FOUND TO BE DROOPING. THE FLAPS WERE EXTENDED AND RETRACTED AND IT WAS NOTED THAT THE FLAPS CONTINUED TO DROOP. TROUBLESHOOTING REVEALED THAT THE FLAP UP CONTROL SWITCH WAS DEFECTIVE. THE CONTROL SWISDR DXTA20171129612Trunnion · gougedLT MLG TRUNNION GOUGED INSIDE BUSHING WHERE ACTUATOR IS MOUNTED. REPAIRED PER REPAIR DEFINITION S-560XL-5334/09RD DATED: 20NOV2017.SDR DXTAT2PL6D005K07HUnknown · malfunctionedON TAKE OFF, AFTER GEAR HANDLE WAS RAISED, THE NOSE WHEEL BANGED 4-5 TIMES ATTEMPTING TO STOW. EACH BANG FELT IN AIRFRAME AND HEARD. WITH EACH BANG, THE RED NOSE WHEEL UNSAFE INDICATOR FLASHED. GEAR SUBSEQUENTLY STOWED PROPERLY. JACKED AIRCRAFT. PERFORMED GSDR EBVR20171120001Skin · corrodedCORROSION ON THE LT WING SKIN. REPAIRED IAW REPAIR REPORT NO 5650/07RD.SDR JGVR20171121001Skin · crackedFOUND A FOUR INCH CRACK IN THE LT LOWER WING SKIN, JUST INBOARD OF WHEEL WELL OPENING. REPAIRED THE SKIN IAW ERO-911328, REV IR.SDR DXTA2017111700032Indicator · malfunctionedLANDING GEAR WOULD NOT RETRACT, GEAR HANDLE UP, 3 GREEN, NO RED. NO CIRCUIT BREAKER TRIP. CYCLED LANDING GEAR 15 TIMES WITH NO FAILURE NOTED. ALL EXTENSION, RETRACTION, AND GEAR INDICATORS OPS CHECKED GOOD. REMOVED LANDING GEAR CONTROL HANDLE AND INSPECTESDR JGVR20171115001Rib · wornEXCESSIVE FREE-PLAY FOUND IN RUDDER TRIM TAB HINGE. REPLACED RUDDER TRIM TAB HINGES WITH NEW HINGE PINS. FOUND RUDDER RIB, BELOW THE TRIM TAB, WORN/DAMAGED BY FROM OLD TRIM TAB HINGE PIN, REPLACED RIB WITH NEW.SDR 2018F00039Skin · corrodedLEFT AND RIGHT WING UPPER SKIN CORRODED.SDR 2018F00038Channel · damagedMAIN CABIN DOOR PRIMARY SEAL CHANNEL DAMAGED.SDR JGVR20171117001Cotter Pin · missingRUDDER TRIM TAB HINGE PIN, RETAINING COTTER PIN WAS MISSING WHICH CAUSED THE HINGE PIN TO MIGRATE AND CHAFE A HOLE INTO LOWER RUDDER RIB BENEATH RUDDER TRIM TAB. REMOVED AND REPLACED THE RIB IAW 51-40-03, 51-40-04, 51-40-06, AND MM 20-32-00.SDR JGVR20171114001Bracket · corrodedUPPER BRACKET OF THE CENTER RUDDER HINGE FOUND CORRODED OUT OF LIMITS. REPLACED THE BRACKET.SDR JGVR20171113001Axle · damagedFOUNDS PLATING MISSING ON THE NOSE WHEEL AXLE TUBE DURING NOSE WHEEL R&R. REPLACED AXLE TUBE WITH NEW ONE P/N 7142022-21.SDR DXTA201711125HUEDLimit Switch · unserviceableDURING TAKE OFF WITH BOTH ENGINES IN THE TAKEOFF DETENT, THE RIGHT ENGINE ONLY PRODUCED 82 PERCENT N1. THE CORRECT NUMBER FOR TEMPERATURE AND ALTITUDE SHOULD HAVE BEEN 88.3 PERCENT N1. RESOLUTION: REMOVED DEFECTIVE RH T/R INBOARD DEPLOY SWITCH DUE TO HIGH RESISDR DXTA201711105HQ2TMotor · failedCOMPLETE BRAKE FAILURE DURING TAXI OUT. ANTI-SKID LIGHT AND POWER PRESSURE CIRCUIT BREAKER TRIPPED. THEN LOW BRAKE PRESSURE LIGHTS. HYD FLUID ON NOSE GEAR DURING POST FLIGHT. INSPECTED BRAKE SYSTEM FOR SIGNS OF DAMAGE, NONE FOUND. OPS CHECKED BRAKES, COULD NOTSDR JGVR20171110001Skin · corrodedFOUND CORRODED AREA ON THE EXTERNAL SKIN OF THE EMERGENCY EXIT DOOR, JUST FORWARD OF THE LATCH HANDLE. PERFORMED MECHANICAL BLENDING, NDT, TREATING AND TOP COATING OF THE AREA.SDR CVGA20171106001Display · failedMASTER CAUTION PFD2 AMBER ANNUNCIATOR, COPILOT PFD WENT BLANK, RED X DURING LIFT OFF, AFTER TAKEOFF.SDR DBCA2017110400004Valve · failedDURING TAKEOFF ROLL, CREW NOTED UNCOMMANDED HOT AIR COMING INTO CABIN AND FLUCTUATIONS IN CABIN PRESSURIZATION RATE. RETURNED TO BASE, LANDING WAS UNEVENTFUL. TROUBLESHOT AND FOUND EMERGENCY PRESSURE VALVE INTERMITTENT. REPLACED THE VALVE WITH AN OVERHAULSDR DBCA201711060001Unknown · odorAFTER TAKEOFF, CREW NOTED UNCOMMANDED HOT AIR COMING INTO CABIN AND FLUCTUATIONS IN CABIN PRESSURIZATION RATE. RETURNED TO BASE, LANDING WAS UNEVENTFUL. COULD NOT DUPLICATE. AIRCRAFT RETURNED TO SERVICE. NO DISCREPANCIES ON RETURN FLIGHT.SDR CVGA20171031001Apu · smokeSMOKE FILLED COCKPIT/CABIN ON CLIMB OUT. EMERGENCY DECLARED. AFTER APU SHUTDOWN SMOKE CLEARED. AIRCRAFT RETURNED TO KPBI.SDR DXTA201711070001Pump · failedDURING TAXI, THE ANTI-SKID LIGHT ILLUMINATED FOLLOWED BY POWER CIRCUIT BREAKER. LOW BRAKE PRESSURE ILLUMINATED. FINALLY EMERGENCY BRAKE HAD TO BE USED TO STOP THE AIRPLANE ON THE RAMP. REMOVED AND REPLACED A WORN HYDRAULIC PUMP ASSEMBLY WITH A NEW UNIT. REPLASDR O2GA2017103101Actuator · leakingAFTER TAKEOFF GOT HYD PRESS AND STAB MISCOMPARE ANNUNCIATORS. FOLLOWED THE CHECKLISTS PULL A HYDRAULIC CONTROL CIRCUIT BREAKER. ONCE THAT WAS DONE THE GEAR UNSAFE LIGHT CAME ON AND THEN THE NOSE GEAR DROPPED DOWN AND LOCKED (GEAR HANDLE WAS UP). DIVERTED TO KSSDR DXTAT2PL6D005FZGSUnknown · odorSTRONG ODOR OF EXHAUST EXPERIENCED DURING CRUISE FLIGHT. TURNED THE BLEED SOURCE TO THE LEFT SIDE ONLY AND THE ODOR WENT AWAY. AFTER 10 MINUTES, PUT THE BLEED SOURCE ON THE RIGHT SIDE AND THE ODOR RETURNED. BORESCOPED FRONT CORE OF ENGINE AND REAR TURBINESDR O2GA2017101650701Engine · failedDURING CLIMBOUT, THE RIGHT FUEL BOOST PUMP CAUTION LIGHT ILLUMINATED. RAN CHECKLIST AND RESET THE RIGHT BOOST PUMP. WHEN THE PUMP WAS RESET, RIGHT LOW FUEL PRESSURE MASTER CAUTION ILLUMINATE, FOLLOWED BY THE RIGHT FUEL BOOST PUMP LIGHT. RAN THE CHECKLIST FORSDR 17GR2017100500001Bracket · defectiveVENT DOOR IN MAIN CABIN DOOR WILL INTERMITTENTLY NOT CLOSE. VENT DOOR CAN THEN BE MANUALLY CLOSED OR AFTER MULTIPLE LOCK UNLOCK ATTEMPTS VENT DOOR CLOSES IN SEQUENCE WITHOUT MANUAL OPERATION. VENT DOOR IS STRIKING BRACKET 6611391-10 DURING SOLENOID ACTUATION ASDR JGVR20171003001Spar Cap · corrodedMECHANICALLY BLENDED 5 AREAS OF CORROSION ON THE RT WING UPPER SPAR CAP AT WING STATIONS 190, 121.7, 99.7, 96.7 AND 88.7 AND 4 AREAS OF CORROSION ON THE LT WING UPPER SPAR CAP AT WING STATIONS 104.5, 119.5, 130.5 AND 141.0. FOUND TO BE BEYOND LIMITS IAW SRM 51SDR O2GA2017100550702Uplock Switch · intermittentLANDING GEAR UNLOCK LIGHT ILLUMINATED AFTER GEAR RETRACTION. STAB MISCOMPARE LIGHT ALSO ILLUMINATED WITH FLASHING HYD PRESSURE LIGHT. MAINTENANCE REPLACED THE LEFT AND RIGHT LANDING GEAR UPLOCK SWITCHES. GROUND OPS CHECK SUCCESSFUL, OPERATIONAL CHECK FLIGHTSDR O2GA2017100550401Motor · defectiveDURING TAKEOFF, CREW SET TAKEOFF POWER, RIGHT ENGINE WAS SLOW TO ACCELERATE. TAKE OFF POWER WAS SET AT 70-80 KNOTS THE RIGHT ENGINE POWER DROPPED BACK 20 PERCENT. ABORTED TAKEOFF AND RETURNED TO THE RAMP. MAINTENANCE REPLACED THE RIGHT ENGINE TORQUE MOTOR. ASDR JGVR20171003002Axle · corrodedNLG AXLE IS CORRODED. FOUND DURING TC-5XL-32-160207 NOSE GEAR INSPECTION. REMOVED AND REPLACED THE AXLE IAW MM 32-41-01.SDR O2GA2017100250701Warning Light · false activationGEAR UNLOCK LIGHT ILLUMINATED WITH GEAR RETRACTION. MAINTENANCE PERFORMED A FULL SYSTEM OPERATIONAL CHECK TO INCLUDE GEAR SWINGS. NO DEFECTS NOTED. A SUCCESSFUL OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.SDR O2GA2017092251301Pressure Switch · defectiveNO PITCH TRIM PASSING 200 KTS, AUTO OR MANUAL. STAB MISCOMPARE ANNUNCIATOR ILLUMINATED AND AUTOPILOT DISENGAGED. EMERGENCY DECLARED AND DIVERTED. LANDING WAS UNEVENTFUL. MAINTENANCE TROUBLESHOT THE DISCREPANCY TO A FAULTY AIRSPEED DIFFERENTIAL PRESSURE SWISDR DXTR2017090801Skin · corrodedLEFT LOWER WING SKIN HAS 4 AREAS OF CORROSION AT LWS 255.5, 263.5, 265.5, 285.5
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