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 DXTA2018071601168Engine · malfunctionedRIGHT ENGINE OIL PRESSURE INDICATION NOT READING, RIGHT ENGINE OIL PRESSURE DROPPED TO ZERO IN FLIGHT. ABNORMAL CHECK LIST REQUIRED ENGINE SHUTDOWN. ENGINE ITT TEMP NORMAL AND ENG OIL TEMP NORMAL. INSPECTED RIGHT ENG OIL LEVEL AND FOUND TO BE 1 QUART LOW BUT NSDR DXTA2018071601174Trunnion · lack of lubeLANDING GEAR WARNING HORN ACTIVATED, RT MLG BULB DID NOT ILLUMINATE UPON GEAR EXTENSION AND THE RED UNLOCK LIGHT REMAINED ILLUMINATED. WHEN TESTED, THE RT LG BULB DID ILLUMINATE. WHEN THE EMERGENCY GEAR EXTENSION HANDLE WAS PULLED IAW THE EMERGENCY CHECKLIST SDR PRIA20180706001Control Valve · failedCABIN DUCT OVERHEAT INDICATION ILLUMINATED SHORTLY AFTER TAKE OFF FROM KJAX, RETURNED TO JAX FOR MAINTENANCE. FOUND THAT PN 27241287-14 CABIN TEMP CONTROL VALVE HAD FAILED. REPLACED VALVE AND RESUMED OPERATIONS THE FOLLOWING DAY.SDR JGVR20180703001Strut · corrodedAFTER RE-SERVICING OF THE NLG STRUT PRESSURE HELD BUT THE FLUID BYPASSED SEAL. DURING RE-SEAL OF NLG, FOUND CORROSION IN UPPER BARREL. DISASSEMBLED, CLEANED AND VISUALLY INSPECTED. FOUND MISC BEARINGS, SEALS AND HARDWARE WORN. FOUND RING PACK AND RETAINER CORRSDR DXTA2018062701118Engine · oil consumptionCLIMBING THROUGH 7000 FT CREWS EYES STARTED BURNING FOLLOWED BY DEFINITE OIL SMOKE OR MIST. CONTAMINATION CAUSED BURNING IN THROAT, CREW WENT ON O2 AND RETURNED TO LAND. APU WAS SHUT DOWN. OIL CONTAMINATION IS COMING FROM ENGINES AT HIGHER POWER SETTING. R&RSDR DXTR2018062201Torque Tube · corrodedLEFT ELEVATOR TORQUE TUBE WAS CORRODED.SDR DXTA2018062101106Converter · dirtyCOCKPIT ODOR OIL SMELL. ONE HOUR INTO THE FLIGHT AT 36,000 FT, DISTINCT OIL BURNING SMELL. COPILOT EXPERIENCED PHYSICAL DISCOMFORT. ODOR WAS STRONG IN COCKPIT, NOT SO STRONG IN CABIN. WENT ON OXYGEN REMAINDER OF FLIGHT. CLEANED BOTH OZONE CONVERTORS AND WATER SDR DXTA2018062101105Engine · odorDURING FLIGHT, A STRONG ODOR WAS PRESENT, ESPECIALLY DURING TAKEOFF, AFTER WEIGHT OFF WHEELS. THE ODOR WAS SIMILAR TO BURNING PLASTIC. THE ODOR WAS INTERMITTENT THE REST OF THE FLIGHT. THE APU WAS OFF APPROXIMATELY 3 MINUTES BEFORE TAKEOFF AND STAYED OFF THESDR JGVR201806132004Access Panel · crackedFOUND VERTICAL STABILIZER ACCESS PANEL 340ER CRACKED, REPLACED THE ACCESS PANEL.SDR JGVR201806132003Fitting · corrodedMECHANICALLY BLENDED FOUR AREAS OF CORROSION ON THE LT WING OTBD FLAP PUSHROD ATTACH FITTINGS, PERFORMED AN EDDY CURRENT INSPECTION AND AN ULTRASONIC THICKNESS INSPECTION. FOUND INBOARD FITTING BEYOND LIMITS. PROTECTED BARE METAL IAW SRM 51-10-02 TO AREAS WITSDR JGVR20180613002Axle · corrodedFOUND THE LEFT MAIN LANDING GEAR AXLE CORRODED OUT OF LIMITS, REPLACED THE AXLE.SDR JGVR20180612001Access Panel · corrodedCORROSION FOUND UNDERNEATH THE ACCESS PANEL 340CR, LOWER AFT ON THE RT SIDE OF THE VERTICAL STAB. BLENDED THE CORROSION, CLEANED, CHEMICALLY TREATED, AND PRIMED AREAS IAW ENGINEERING MEMO.SDR DXTA2018061101059Unknown · odorDESCENDING OUT OF 23000 FEET, DETECTED A DIRTY SOCK/BURNT OIL ODOR ALL THE WAY DOWN TO LANDING. REMOVED AND REPLACED THE CONDENSER BAG. RAN APU, NR 1 AND 2 ENGINES. OPS CHECKED GOOD. WORK PERFORMED IAW AMM 21-51-00, FOUND CONDENSER BAG TO HAVE NORMAL WESDR O2GA2018061150001Seal · failedA LOUD POP SOUND FROM MAIN ENTRY DOOR FOLLOWED BY CONTINUOUS SOUND OF AIR LEAKING PAST DOOR. CABIN REMAINED PRESSURE. DIVERTED. MAINTENANCE REPLACED MAIN ENTRY DOOR LOWER ACOUSTIC SEALS. OPS CHECKED OK. AIRCRAFT WAS RETURNED TO SERVICE.SDR DXTA2018060651040Converter · odorHAD A MUSTY ODOR IN THE CABIN DURING PREFLIGHT, ATTRIBUTED TO MAINTENANCE DONE PREVIOUSLY ON THE SOCK. CLIMBING OUT ABOVE 10,000 FT, SHUT OFF THE APU, SWITCHED TO BLEEDING OFF THE ENGINES. RECEIVED AN ODOR OF HOT METAL OR OIL IN THE CABIN. WAITED A FEW MINUTESDR 17GR060518Anti-Ice Valve · failedDURING START, THE ANTI-ICE LIGHT WARNING ILLUMINATED. FOUND THE STATOR ICE VALVE FAILED.SDR DXTA2018060501036Unknown · odorCLIMBING THRU 10K, PAX NOTIFIED CREW OF A SMOKE ODOR IN THE CABIN. CREW CONFIRMED AND FO WENT BACK TO CHECK WHILE CAPTAIN SHUT DOWN APU. ODOR IMMEDIATELY DISSIPATED. GROUND VISUAL CHECK REVEALED NO EVIDENCE OF A PROBLEM. PERFORMED BOROSCOPE APU INLET INSPECSDR CVGA20180608001Light · no indicationNOSE GEAR LIGHT DID NOT COME ON DURING APPROACH. COULD NOT VERIFY NOSE GEAR DOWN. EMERGENCY GEAR BOTTLE WAS BLOWN AND AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED AND TAXIED IN WITHOUT INCIDENTS.SDR DXTA2018052951004Eec · malfunctionedRIGHT ENGINE LOW POWER, ENGINE DID NOT MAKE TAKE OFF POWER BY 4 OR 5 %, RIGHT ITT WAS HIGHER THAN THE LEFT, ALL THE REST THE ENGINE PARAMETERS WERE MATCHED. AT 10000 FEET THE ENGINES WERE MATCHED. PERFORMED RECOMMENDED PROCEDURES. PERFORMED T/R OPS TESTS SDR DXTA201805250991Engine · power lossRIGHT ENGINE NOT DEVELOPING FULL POWER DURING CLIMB. COULD NOT DUPLICATE DISCREPANCY. REMOVED AND REPLACED EEC INTERFACE PCB AS A PRECAUTIONARY IAW MM 24-51-01. RAN ENGINES A SECOND TIME IDLE,CRUISE,CLIMB AND TAKE-OFF NUMBERS ALL MATCH, NO DEFECTS NOTED. OKSDR DXTA2018052200985Unknown · odorWHEN THE COCKPIT TEMP SELECTOR WAS MOVED TO WARM (10 O'CLOCK POSITION), THERE WAS AN OIL ODOR IN THE COCKPIT. REMOVED AND REPLACED CONDENSER BAG. INSPECTED BLEED DUCTS AND APU INLET FOR OIL RESIDUE. NO OIL RESIDUE NOTED. PERFORMED ECS DUCT BURN OUT. NO OIL ODSDR DXTA2018052100977Fuel Sys · contaminatedENROUTE CREW FELT SLIGHT ENGINE SURGES, THEN AT 24K, THE RIGHT ENGINE ROLLED BACK TO APPROXIMATELY 44% N1 WITH NO THROTTLE INPUT.. CONTINUED FOR ABOUT 5 MINUTES AND THEN RETURNED TO PREVIOUS POWER SETTING. PERFORMED FUEL CONTAMINATION CHECKS ON THE LT AND RTSDR DXTA2018051700968Control Valve · faultyALL LANDING GEAR EXTENSION DELAY, GEAR WAS SELECTED DOWN AT 200 KTS. FOR AT LEAST 30 SECONDS THERE WAS ONLY THE RED GEAR UNSAFE LIGHT ILLUMINATED, NO HYDRAULIC LIGHT CAME ON AND THERE WAS NONE OF THE USUAL GEAR NOISE. AFTER THIS DELAY , THE GEAR UNLOCKED , HYDSDR 20188051000938Valve · inoperativeSUBSEQUENT ACTION: REPLACED THE PARKING BRAKE VALVE, ANTISKID CONTROL SERVO VALVE AND THE POWER BRAKE VALVE
IAW CE560XL MM 32-42-03 AND 32-42-05. BLED BRAKES. LEAK CHECKS ARE GOOD. OPERATIONAL CHECKS ARE GOOD. TAXI
CHECK IS GOOD. PART DETAILS: PARKING BRAKE SDR 2019F00003Skin · crackedRIGHT NOSE LG DOOR SKIN CRACKED AT THE LATCH.SDR DXTA20180430885Pump · failedDURING CLIMB, APPROXIMATELY 5 MINUTES AFTER LAST USE OF HYD SYSTEM, THE HYD LOW LEVEL ILLUMINATED. ON POST FLIGHT INSPECTION, HYD LEVEL APPROX 1 1/2 ABOVE EMPTY LINE. REMOVED AND REPLACED THE LT ENGINE DRIVEN HYDRAULIC PUMP IAW MM 29-11-03. OPS AND LEAKSDR DXTR2018042601Stringer · crackedSTRINGER 15L, BS 580 WAS FOUND CRACKED AT AFT END IN THE AFT MOST TAIL COMPARTMENT.SDR EBVR20180423001Strake · corrodedRIGHT WING, TOP SPAR HAS A COUPLE OF AREAS OF SUSPECTED CORROSION ON THE LT AND RT STRAKES NEAR THE COMPOSITES. FABRICATED AND INSTALLED REPAIR DOUBLERS.SDR DXTA201804240867Unknown · odorCOCKPIT HAD AN OIL ODOR, COCKPIT TEMP CONTROLLER SELECTED AT 11 O'CLOCK POSITION. AT FL360. REMOVED THE WATER SEPARATOR FROM AIRCRAFT. CLEANED THE CONDENSER IAW MM 12-19-02. INSPECTED CONDITIONED AIR DUCTING FOR EVIDENCE OF OIL. NONE FOUND. REINSTALLED THESDR O2GA2018042350201Circuit Breaker · failedANTI-SKID INOPERATIVE LIGHT ILLUMINATED DURING GEAR EXTENTION STAGE OF FLIGHT. POWER BRAKE CIRCUIT BREAKER WAS NOTICED TO BE EXTENDED. LANDING WAS UNEVENTFUL. EMERGENCY BRAKING USED TO STOP THE AIRCRAFT. NOTICED HYDRAULIC FLUID LEAKING FROM NOSE COMPARTMENT. MSDR DXTA2018041700852Connector · dirtyALL LANDING GEAR DID NOT RETRACT, LANDING GEAR UNLOCK LIGHT REMAINED ILLUMINATED AFTER GEAR WAS RETRACTED. ALL GREEN LIGHTS EXTINGUISHED. COULD HEAR THE NOSE WHEEL SPINNING DURING GEAR RETRACTION. RAN CHECKLIST AND EXTENDED GEAR WITH ALL NORMAL INDICATIONS. SDR 9JLA2018041816166Wire · out of positionPILOT REPORTED THAT DURING A POST-FLIGHT CHECK, FOUND THAT THE TAT PROBE WAS COVERED IN ICE THAT HAD COLLECTED DURING THE PREVIOUS FLIGHT. TROUBLESHOOTING DETERMINED THAT THE TAT PROBE WAS NOT HEATING AND THE CAUSE WAS DETERMINED TO BE A FAULT WITH THE X1/X2 WSDR 9JLA2018071117324Fastener · obstructedDURING A ROUTINE PREFLIGHT CHECKS OF THE AIRCRAFT THE MAINTENANCE TECH NOTED WHILE MOVING THE ELEVATOR THROUGH ITS TRAVEL, BINDING WAS FELT. IT WAS DISCOVERED THAT THE RIGHT ELEVATOR BELLCRANK HARDWARE IN THE STAB WAS CONTACTING THE STRUCTURE. THERE IS A SERVISDR DXTA2018041200829Unknown · odorAT 40000 FT, DETECTED AN OIL ODOR IN THE COCKPIT AND CABIN. RAN THE CHECKLIST FOR ODOR. INSPECTED APU INLET DUCT FOR PRESENCE OF OIL. NONE FOUND. REMOVED AND INSPECTED THE CONDENSOR BAG IAW MM 21-51-00, LEAK CHECKED GOOD. PERFORMED A GROUND RUN ON APU SDR DXTA2018041200830Condenser · odorTHERE WAS A VERY STRONG DIRTY SOCK ODOR IN THE COCKPIT AND CABIN, WHEN THE CABIN AIR CONDITIONING WAS OPERATING. REMOVED AND REPLACED CONDENSER SOCK WITH NEW CONDENSER SOCK IAW AMM 21-21-00. CHECKED GOOD.SDR DXTA2018033000781Shuttle Valve · malfunctionedJUST PRIOR TO FINAL APPROACH, PUT THE GEAR DOWN. RT GEAR DOWN INDICATOR LIGHTS DID NOT ILLUMINATE. MISSED APPROACH AND TROUBLESHOT SYSTEM. SELECTED THE FLAPS 35 AND GEAR HORN DID NOT GO OFF. ACCOMPLISHED A ROTARY TEST AND THE RIGHT GEAR DOWN INDICATOR LISDR DXTR20180321001Skin · gougedTHE MAIN ENTRY DOOR HAS A GOUGE ON THE INNER SURFACE OF THE DOOR SKIN IN THE FWD COUNTERBALANCE SPRING BAY. THERE IS A DENT ON THE EXTERIOR SURFACE AT THE SAME LOCATION.SDR CVGA20180402001Release Cable · tightGEAR UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF. NOSE GEAR WOULD NOT LOCK IN THE UP POSITION. AIR RETURN WITH GEAR DOWN. TROUBLESHOOTING FOUND NOSE GEAR EMERGENCY RELEASE CABLE TOO TIGHT AND NOT ALLOWING UPLOCK TO FULLY ENGAGE ROLLER TO MAKE SWITCH. ADJUSTED ESDR 2018F00102Stiffener · mislocatedSTIFFENER MISLOCATED.SDR 2018F00101Pulley Bracket · brokenNOSE WHEEL STEERING PULLEY BRACKET BROKEN.SDR EBVR20180212001Skin · delaminatedDURING INSPECTION, FOUND THE LT OUTBOARD FLAP IS DELAMINATED. INSTALLED A REPAIR IAW MM 57-50-01, AND 27-51-00.SDR O2GA2018021251301Computer · malfunctionedNR 2 AHRS FAILED SHORTLY AFTER TAKE OFF. DIVERTED AND LANDED. NO HISTORY ON THE OCCURRENCE. SWAPPED THE NR 1 & 2 AHRS COMPUTER. SYSTEM OPS CHECKED PERFORMED AND NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE.SDR CVGA20180215001Actuator · leakingCREW NOTICED A DIFFERENCE IN FLAP ANGLE FROM ONE WING VERSUS THE OTHER WHILE EN ROUTE. CREW ELECTED TO PERFORM A NO FLAP LANDING. DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT.SDR 9JLA2018021311289Bracket · brokenDURING A POST-FLIGHT CHECK, AN INSPECTION OF THE NOSE LANDING GEAR DOOR CENTER HINGE ATTACH BRACKETS. FOUND THE LEFT DOOR FOREWORD BRACKET ON THE CENTER HINGE WAS CRACKED. THE BRACKET WAS REMOVED AND REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR 9JLA2018021317005Bracket · crackedDURING THE POST-FLIGHT CHECK, AN INSPECTION OF THE NOSE LANDING GEAR DOOR CENTER HINGE ATTACH BRACKETS. FOUND THE LEFT DOOR FOREWORD BRACKET ON THE CENTER HINGE WAS CRACKED. THE BRACKET WAS REMOVED AND REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR EBVR20180201Casting · corrodedINSPECTION OF SECTOR REVEALED CORROSION ON BOTH THE ALUMINUM CASTING AND STEEL SHAFT. REPLACED SECTOR WITH NEW
ASSEMBLY P/N 6660303-18.SDR JGVR20180201001Closeout Panel · corrodedAPU CLOSEOUT PANEL IS SEVERELY CORRODED ON THE INSIDE, AROUND THE OIL SERVICE DOOR LATCHES, AND AROUND THE CAMLOCKS. REMOVED CORRODED APU ACCESS DOOR ASSY. AND INSTALLED NEW APU ACCESS DOOR ASSY IAW MM 52-40-02.SDR DXTA2018010100519Coalescer Bag · dirtyCOCKPIT ODOR OIL SMELL - DURING LAST COUPLE OF FLIGHTS, HAD NOXIOUS FUMES AND "DIRTY SOCK" SMELL IN THE COCKPIT. VERIFIED DISCREPANCY, INSPECTED SYSTEM GAINED ACCESS TO WATER SEPARATOR AND FOUND CONDENSER BAG DIRTY. REMOVED CONDENSER BAG AND INSTALLED A NEW BASDR JGVR20180131003Skin · corrodedBLENDED TWO AREAS OF CORROSION ON THE EXTERIOR FUSELAGE SKIN FWD OF THE CABIN DOOR AT BS 187, PERFORMED EDDY CURRENT CRACK AND ULTRASONIC THICKNESS INSPECTIONS, PREPPED AND TREATED IAW SRM 51-10-03, MM 51-10-00, AND 51-70-08.SDR JGVR20180131002Skin · corrodedBLENDED 10 AREAS OF CORROSION ON THE LT UPPER WING SKIN, PERFORMED EDDY CURRENT CRACK AND ULTRASONIC THICKNESS INSPECTION, PREPPED AND TREATED AREAS IAW SRM 51-10-03, AND MM 51-10-00.
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