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 CVGA20200226001Strut · low pressureAFTER TAKEOFF THE CREW SELECTED UP WITH THE GEAR HANDLE, THE THREE GREEN LIGHTS EXTINGUISHED, THE RED GEAR UNLOCK LIGHT REMAINED ILLUMINATED. THE CREW FOLLOWED THE QRH PROCEDURE AND RETURNED TO BOS. APPROACH AND LANDING UNEVENTFUL. MAINTENANCE CHECKED STRUT SESDR O2GA2020021850601Actuator · lack of lubeAT FL400 THE PITCH TRIM ANNUNCIATOR ILLUMINATED WITH AUTOPILOT ON. THE PITCH TRIM WHEEL WAS FROZEN IN PLACE AND REMAINED THAT WAY UNTIL ABOUT 6,000 FT. EMERGENCY DECLARED, DIVERTED TO STL AND LANDING WAS UNEVENTFUL. MAINTENANCE LUBED LEFT AND RIGHT ELEVATOR PISDR O2GA2020021815101Control Handle · intermittentAFTER LANDING AND CLEARING THE RUNWAY EXPERIENCED A PRIMARY BRAKE SYSTEM FAILURE FOLLOWED BY LOSS OF BRAKE PRESSURE/ANTI-SKID MASTER WARNING. APPLIED EMERGENCY BRAKES TO STOP AIRCRAFT WHERE IT WAS THEN TOWED TO FBO. MAINTENANCE REPLACED THE RELAY, DIODE AND LASDR CVGA20200206001Sensor · failedAFTER TAKEOFF, ACM O'HEAT LIGHT AND BLEED AIR O'HEAT LIGHT CAME ON WITH SMOKE IN THE CABIN.SDR 17GRA59A01None · noneWHILE USING LIFE VEST CERTIFIED 1/16/2018 FOR TRAINING FOUND THAT THE C02 INFLATOR CARTRIDGE WAS TO RIGID TO BE PUNCTURED TO INFLATE THE VEST.SDR DXTA2020012103362Lamp · burned outNLG INDICATOR LIGHT BURNT OUT - DURING APPROACH WITH GEAR HANDLE DOWN WE NOTICED WE DIDN'T HAVE GREEN NOSE GEAR DOWN AND LOCKED INDICATION. WE INITIATED A GO AROUND, COMPLETED LANDING GEAR WILL NOT EXTEND QRH EMERGENCY CHECKLIST AND USED GEAR BLOW DOWN PROCEDUSDR O2GA202001190101Uplock Switch · defectiveON CLIMB OUT RED GEAR UNLOCK LIGHT ILLUMINATED FOLLOWED BY 'HYD PRESS' ANNUNCIATOR. FOLLOWED CHECKLIST, DIVERTED TO MCO, AIRPORT EMERGENCY RESCUE TEAM NOTIFIED AND WERE STANDING BY. LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE LEFT AND NOSE GEAR UP-LOCK SWSDR JGVR2020012017004Axle · corrodedFOUND CORROSION ON THE LT MAIN LANDING GEAR AXLE. REPLACED CORRODED AXLE WITH NEW P/N 6641646-1.SDR JGVR2020012017003Hinge · corrodedFOUND CORROSION ON THE MAIN ENTRY DOOR FORWARD HINGE ON THE FUSELAGE SIDE HINGE-HALF. BLENDED CORRODED AREA, PERFORMED NDT AND REPORTED RESULTS FOR DISPOSITION. REPLACED FUSELAGE SIDE OF THE FWD HINGE WITH NEW P/N 6611037-1.SDR JGVR202001197002Stiffener · crackedFOUND CRACKED STIFFENER NEAR THE AFT COUNTERBALANCE SPRING OF THE MAIN ENTY DOOR. REPAIRED STIFFENER BY CUTTING OUT THE CRACKED AREA AND INSTALLING REPAIR DOUBLER AND FILLER IAW ENGINEERING ORDER.SDR JGVR202001197001Trunnion · corrodedFOUND CORRODED AREAS ON THE RT MAIN LANDING GEAR TRUNNION AT THE UPPER BRAKE LINE BAND CLAMP, REMOVED CLAMP BLENDED AREA AND TREATED IAW REPAIR MEMO.SDR PRIA2020011400001Bracket · bentUPON ESTABLISHING A POSITIVE RATE OF CLIMB, THE LANDING GEAR WAS RETRACTED. AT V2 PLUS 10 THE FLAPS WERE RETRACTED. AT WHICH POINT A STAB MISCOMPARE WAS NOTICED. WE REQUESTED A LEVEL OFF AT 8,000 FT. WE SLOWED THE AIRCRAFT TO BELOW 200 KNOTS. WE THEN NOTICED ASDR DXTA2020011303328Actuator · unserviceableBOTH FLAP EXTENSION FAIL - ON APPROACH FLAPS WHERE SELECTED TO 15. "HYD PRESS" LIGHT INITIALLY ILLUMINATED NORMAL. THEN STARTED TO FLASH WITH THE "MASTER CAUTION" LIGHT. THE FLAPS NEVER TRAVELED PASS 3 DEGREES. WE MOVED THE FLAP SWITCH BACK TO FLAPS 0 DEGRESDR DXTA2020011303325Coalescer Bag · dirtyCABIN ODOR - ACM PRODUCES A WET SOCK SMELL WHEN RUNNING IN WARM HUMID CONDITIONS.//SIGNOFF// GAINED ACCESS AND REMOVED OLD CONDENSER BAG P/N: 83237-12, NSN AND INSTALLED A
NEW CONDENSER BAG P/N: 83237-12, NSN. PERFORMED APU AND ENGINE RUNS AGAIN WITH NO ODOR.SDR CVGA20200103001Warning System · activatedCOMING IN FOR LANDING IN FLL, LEFT MAIN GEAR INDICATOR DID NOT ILLUMINATE WITH GEAR HANDLE DOWN. GEAR HORN BLEW AND RED GEAR UNSAFE LIGHT WAS ON. COMPLETED THE EMERGENCY CHECKLIST WHICH INITIALLY DIDN'T HELP UNTIL A FEW MINUTES LATER, 3 GREEN, NO RED PRIOR TO SDR DXTA2019123073256Converter · dirtyBURNED FUEL ODORS IN BOTH COCKPIT AND CABIN WHILE ENGINE OR APU IS RUNNING, SAME ODOR IS FOUND WHEN HELL HOLE DOOR IS OPENED AND WHEN STANDING UP IN THE AFT ACCESS SPACE. ODOR IS MORE SUBSTANTIAL WITH APU ON AND ENGINES OFF, THAN JUST ENGINES ALONE. BOTH PIC ASDR DXTA2019121703213Sensor · defectiveCOCKPIT ODOR - VERY STRONG, ACRID ODOR COMING FROM THE AIR CONDITIONING SYSTEM. REMOVED PRECOOLER TEMP SENSOR AND INSTALLED NEW SERVICEABLE TEMP SENSOR AND PERFORMED OPS TEST OF PRECCOOLER RAM AIR DOOR WITH NO DEFECTS NOTED. ALL MAINTENANCE PERFORMED IAW AMMSDR DXTA2019121303196Actuator · failedRIGHT MLG LANDING GEAR UNLOCK LIGHT ILLUMINATED, AFTER GEAR SELECTED DOWN, THE RIGHT MLG LIGHTS DID NOT ILLUMINATE AND THE GEAR UNSAFE LIGHT REMAINED ON. AFTER COMPLETING THE EMERGENCY GEAR CHECKLIST, STILL WAS THE UNSAFE LIGHT, GEAR HORN ON AND NO LIGHTSDR DXTA2019121303193Apu · odorSHORTY AFTER TO A VISIBLE SMOKE WITH ENVIRONMENTAL SMELL APPEARED IN THE COCKPIT, DISSIPATED AFTER APU SHUTDOWN. BY TIME WE LANDED SMOKE AND SMELL WHERE GONE. ALL APPROPRIATE COMPANY PROCEDURES AND FAR'S WHERE COMPLIED WITH. REMOVED AND REPLACED THE APU. RAN SDR DBCA2019121730006Static Wick · failed1) AFTER DEPARTING CLT CREW REPORTED BOTH #1 COMM AND #2 COMM HAVE HEAVY STATIC DURING CLIMBOUT AND INTERMITTENT AT LEVEL FLIGHT. MODERATE PRECIP THROUGHOUT THE FLIGHT. 2) CREW RETURNED TO HOME BASE. LANDING WAS UNEVENTFUL. 3) TECHNICIANS TESTED ALL STATICSDR 2019FA0000407Limit Switch · intermittentAFTER LANDING @ KCHT AND DURING TAXI, NO TAKEOFF CAS MESSAGE WAS DISPLAYED. PILOTS REPORTED THAT AFTER SHUTDOWN THE AIRCRAFT STABILIZER WAS IN THE HIGH SPEED CONFIGURATION. FLAPS WHERE AT 7 DEGREES AND THERE WAS NO CAS MESSAGE DISPLAY OF STABILIZER MIS-COMPARESDR EBVR20191212001Trim Tab · crackedFOUND CRACK ON LOWER TRAILING EDGE OF RUDDER TRIM TAB. FABRICATED AND INSTALLED DOUBLER ON RUDDER TRIM TAB LOWER TRAILING EDGE. WORK ACCOMPLISHED IAW AQRD ERO-965397 DATED 12-11-19 AND 8110-3 DATED 12-11-19SDR DXTA2019120603170Unknown · odorDURING DEPARTURE WITH APU ON AND APU BLEED AIR ON , HAD A STRONG SMELL OF JET A COMING THRU VENTS IN CABIN. AND COCKPIT. WE SHUT THE APU AND BLEED AIR OFF AND SMELLED REMAINED. WE TURNED THE SOURCE TO OFF TO ISOLATE, THE SMELL OF JET A STOPPED AFTER SOURCSDR W9FA20191205001Access Panel · corrodedCORROSION WAS DISCOVERED ON NINE WING FUEL ACCESS PANEL DOUBLERS. THE CORRODED LOCATIONS WERE BLENDED OUT AND THE REMAINING THICKNESSES WERE MEASURED USING ULTRASOUND. BLEND MINIMUM REMAINING THICKNESSES. FIGURE 1 IS A SKETCH OF THE DAMAGE LOCATIONS. SDR DXTA2019120213138Circuit Card · defectiveRIGHT ENGINE FIRE DETECTION LIGHT INTERMITTENT - IN FLIGHT AT FL280, THE R/H ENGINE FIRE WARNING LIGHT FLICKERED ON AND OFF CONTINUOUSLY FOR APPROXIMATELY FIVE MINUTES. THERE WERE NO SECONDARY INDICATIONS OF A POSSIBLE ENGINE FIRE. WING AND ENGINE ANTI ICE WERSDR DXTA201912023129Actuator · defectiveALL LANDING GEAR RETRACTION - AFTER TAKEOFF SELECTED GEAR UP. RED UNLOCK LIGHT ILLUMINATED. PERFORMED APPROPRIATE CHECKLIST. ON EXTENSION THREE GREEN LIGHTS ON THE GEAR. DECLARED AN EMERGENCY AND RETURNED FOR AN OVERWEIGHT LANDING AT 19900 POUNDS. ACCOMPLISHEDSDR 2GYR201911250005Oil System · low pressureDURING TAKEOFF FROM GYY, 883SC EXPERIENCED AN IN FLIGHT EMERGENCY WITH THE RIGHT ENGINE. THE CREW GOT A LOW OIL PRESSURE INDICATION AND THERE WAS SMOKE IN THE COCKPIT AND CABIN. THEY SHUT THE ENGINE DOWN, DECLARED AN EMERGENCY, AND RETURNED TO GYY WITHOUT FURTSDR DXTA2019112503113Motor · defectiveBOV INTERMITTENT - AT FL410, FO MADE A SLIGHT POWER INCREASE WHEN WE HEARD A FLUTTERING FOUND/POSSIBLE COMPRESSOR STALL FROM LEFT ENGINE. LEFT ENGINE ITT WENT UP AND DOWN ABOUT 100 POINTS. THE RANGE WAS BETWEEN 500 AND 600 DEGREES. THIS HAPPEN TWICE IN FLIGHSDR DXTA2019112103110Landing Gear · unknownNLG INDICATOR LIGHT INTERMITTENT - ON APPROACH LANDING GEAR DOWN WAS SELECTED. THE NOSE GEAR DID NOT ILLUMINATE. THE RED UNLOCK LIGHT DID EXTINGUISH. FLAPS WERE AT 15. WE EXECUTED A GO AROUND TO TROUBLESHOOT AND RUN CHECKLISTS. THE NOSE GEAR LIGHT STILL SDR DXTA2019111983091Condenser · dirtyCOCKPIT ODOR - ON DESCENT INTO PBI WITH POWRAN APU AND HAD NO ODOR. RAN RIGHT ENGINE ONLY AND NO ODOR. RAN LEFT ENGINE ONLY AND NO ODOR. REPOSISTION AIRCRAFT AND PERFORMED POWER RUNS ONE AT A TIME AT POWER AND EITHER ENGINE DID NOT PRODUCE A MUSTY ODOR. // SIGSDR 2020F00052Apu · odorN227MC WAS EN-ROUTE FROM RYY-BNA EMPTY FOR A CHARTER TRIP, AND THE CREW NOTED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED, AND THEY DIVERTED TO DALTON, GA. AIRCRAFT LANDED WITH OUT INCIDENT. UPON INVESTIGATION BY CESSNA, IT WAS DISCOVERED THE ROOT CAUSE OFSDR 2019FA0000358Eec · defectiveR/H ENGINE EEC ANNUNCIATOR LIGHT (EEC IN MANUAL MODE - NOT AUTOMATIC) CAME ON DURING TAKE OFF ROLL AT AROUND 80 KTS. THE CREW ABORTED THE TAKE OFF AND RESET THE EEC AND THE CIRCUIT BREAKER PER THE QRH CHECKLIST. THE ANNUNCIATOR LIGHT EXTINGUISHED AND THE CREW SDR 2019FA0000357Eec · defectiveR/H ENGINE EEC ANNUNCIATOR LIGHT (EEC IN MANUAL MODE - NOT AUTOMATIC) CAME ON DURING TAKE OFF ROLL AT AROUND 80 KTS. THE CREW ABORTED THE TAKE OFF AND RESET THE EEC AND THE CIRCUIT BREAKER PER THE QRH CHECKLIST. THE ANNUNCIATOR LIGHT EXTINGUISHED AND THE CREW SDR 2019FA0000356Eec · defectiveR/H ENGINE EEC ANNUNCIATOR LIGHT (EEC IN MANUAL MODE - NOT AUTOMATIC) CAME ON DURING TAKE OFF ROLL AT AROUND 80 KTS. THE CREW ABORTED THE TAKE OFF AND RESET THE EEC AND THE CIRCUIT BREAKER PER THE QRH CHECKLIST. THE ANNUNCIATOR LIGHT EXTINGUISHED AND THE CREW SDR O2GA2019111651101Trim Motor · faultyDURING DESCENT FROM FL410 TO FL310 THE CREW RECEIVED A PITCH TRIM AMBER ANNUNCIATION ON THE PFD'S AT AROUND FL320. AUTOPILOT WAS DISCONNECTED. MANUAL AND ELECTRIC PITCH TRIM WAS UNRESPONSIVE. EMERGENCY WAS DECLARED AND CHECKLIST FOLLOWED. AS THE AIRCRAFT DESCESDR O2GA2019102851201Wheel · bindingDURING DESCENT FROM FL410 'PITCH TRIM' FLAG APPEARED IN PFD. AUTO-PILOT WAS DISCONNECTED AND ELEVATOR TRIM WHEEL FOUND TO BE JAMMED. CHECKLIST WAS FOLLOWED AND AN EMERGENCY DECLARED. DURING THE DESCENT TO LOWER ALTITUDE AND IN ABOVE FREEZING AIR THE ELEVATOR TSDR CVGA20191025001Indicator · brokenWHILE BEING VECTORED FOR APPROACH AT 2000FT INTO PWM, FLAP INDICATOR POINTER MALFUNCTIONED AND STUCK AT 0. WEATHER WAS LOW OVERCAST AND TURBULENT, PIC COULDN’T DETERMINE A NOTICEABLE CHANGE AIRCRAFT AND DETERMINED IT WAS
UNSAFE TO EXIT SEAT AND WALK TO CABIN SDR DXTA2019102402972Sensor · unknownLEFT ENGINE ENGINE OIL TEMPERATURE INDICATION HIGH TEMPERATURE - #1 OIL TEMPERATURE FLUCTUATION. DURING CLIMB (PASSING 35,000?) WITH THROTTLE IN CLIMB DETENT, #1 OIL TEMPERATURE FLUCTUATION FROM NORMAL TO MAXIMUM REDLINE. ON LEVEL OFF AND IN CRUISE POWER, #1 OSDR DXTA2019102192964Condenser · dirtyCOCKPIT ODOR - DIRTY SOCK SMELL. NOTICED DURING DESCENT APU OFF. REMOVED AND REPLACED WATER SEPARATOR CONDENSER BAG AND PERFORMED SYSTEM OPERATIONAL CHECK. NO DEFECTS NOTED. REF: CE 560XL MM 21-51-00SDR DXTA2019100702925Engine · contaminatedCOCKPIT ODOR - REPEAT WRITEUP. DURING TAKEOFF WITH THE APU OFF WE GOT A BAD ODOR OF SOME SORT OF CHEMICAL SMELL. POSSIBLY OIL? DEFINITELY NOT EXHAUST OR BAD SOCK OR MUSTY SMELL. SMELL WAS WORST AT HIGH POWER SETTING. WITH APU ON WHILE ON THE GROUND AND TAXI OUSDR DXTA2019100402917Engine · contaminatedCOCKPIT ODOR - AT FL410 STARTED TO GET A JET EXHAUST ODOR IN THE COCKPIT. BOTH CREWMEMBERS STARTING EXPERIENCE NAUSEOUS SYMPTOMS. CONTINUED BUT STARTED AN EARLY DESCENT. ONCE BELOW 10,000FT, SYMPTOMS IMPROVED AND THE SMELL DISSIPATED. THE APU WAS OFF DURING SDR DXTA2019093002908Water Separator · odorCOCKPIT ODOR - DESCENDING FROM CRUISE ALT OF FL400. STARTED GETTING A STRONG ORDER SIMILAR TO JET EXHAUST. IT SMELLED DIFFERENT THAN WHEN THE HEAT IS TURNED UP. REMOVED CLEANED INSTALLED ECS WATER SEPARATOR AND PERFORMED SATISFACTORY ECS DUCT BURN OUT THEN ISDR EBVR20190923001Skin · crackedRUDDER TRIM TAB SKIN IS CRACKED PROXIMATELY .5" ON BOTTOM AFT CORNER LT SIDE. COMPLIED WITH 8110-3 AND ERO-962724 REV IR DATED 9/22/2019 RUDDER TRIM TAB TRAILING EDGE REPAIR.SDR CVGA20190914001Fluid · dirtyUPON RETRACTION OF LANDING GEAR, RED UNLOCK AND HYD PRESS LIGHTS REMAINED ILLUMINATED. MAINTENANCE FOUND DIRTY FLUID COMING FROM NLG STRUT WHEN CHECKING PRESSURE. SERVICED NLG STRUT. ALL OPS TESTS NORMAL FOLLOWING SERVICING.SDR XCGA2019091000000Unknown · odorFLIGHT CREW REPORTED THAT DURING ENGINE START SMOKE ENTERED THE CABIN THROUGH THE AIR CONDITIONING DUCTS. THE FLIGHT CREW SHUT DOWN AND TURNED THE AIRPLANE OVER TO MAINTENANCE. MAINTENANCE INSPECTED ENGINE AND APU DRAINS AND INLETS. NO EVIDENCE OF OIL LEAKS WASDR 2019FA0000295Rib · crackedHORIZONTAL STABILIZER RIB CRACKED. REFERENCE ENGINEERING REPAIR MEMO REF: DQ22759M1 DATED 8/20/19.SDR 2019FA0000289Piccolo Tube · chafedLH AND RH WING ANTI-ICE PICCOLO TUBES CHAFED. REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ22819M1 DATED AUGUST 28, 2019.SDR 2020F00021Skin · chafedREPAIR OF LEFT WING LEADING EDGE DAMAGE (CHAFING AGAINST PICCOLO TUBE). REPAIR MEMO DQ22885M1 DATED 8/28/2019.SDR 2020F00020Tube · chafedREPAIR OF LH AND RH LEADING EDGE PICCOLO TUBE DAMAGE (CHAFE). TEXTRON AVIATION REPAIR MEMO DQ22817M1 DATED 8/28/2019.SDR DXTA2019082702803Coffeemaker · odorCLIMBING OUT OF 12,000 FEET, WE TURNED OFF THE APU. IMMEDIATELY HAD A BURNING ODOR. SHUT OFF COFFEE POT AS WELL. INVESTIGATED THE CABIN, SLIGHT SMELL. RETURNED TO COCKPIT, ODOR COMPLETELY DISSIPATED . 19600 FEET. RAN AIRCRAFT WITH BOTH ENGINES BLEED AIR AND
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