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 DXTA200500819Odor · detectedUPON DESCENT THROUGH 14000 FT, MFD SCREEN WENT BLANK ABRUPTLY. STRONG ODOR OF BURNED PLASTIC FILLED COCKPIT, BUT NO SMOKE DETECTED. PERFORMED USER INITIATED SELF TEST. ALL ITEMS DISPLAY PASS AND VALID. SWITCH SG FROM NORM TO SG1 AND SG 2. SELF TEST ALSO PASSDR CA050704009Engine · malfunctioned(CAN) DURING CLIMB, THE ENGINE WOULD NOT RESPOND TO THROTTLE INPUT TO REDUCE POWER. THIS WAS ACCOMPANIED BY AN ELECTRONIC ENGINE CONTROL (EEC) REVERSION. THE FLIGHT WAS DIVERTED AND THE ENGINE WAS SHUT DOWN ON FINAL APPROACH. P&WC WILL INVESTIGATE THE EVENTSDR DXTA200500811Actuator · out of adjustAFTER TAKEOFF AND RETRACTING GEAR AND FLAPS-GEAR UNLOCK (RED) LIGHT REMAINED LIT AND STAB MISCOMPARE LIGHT CAME ON. ADJUSTED LT MAIN LANDING GEAR ACTUATOR IAW MM. OPS TESTED LANDING GEAR TEN TIMES WITH NO FAULTS.SDR DXTA200500809Control Cable · shearedLT RUDDER PEDAL WILL NOT MOVE RUDDER. RT RUDDER PEDAL WILL MOVE RUDDER. LT RUDDER PEDAL MOVES FREELY WITH NO RESISTANCE. ALSO NOTED RUDDER CABLE BOWS BEHIND PEDAL AND FIREWALL. FOUND RUDDER CONTROL CABLE ASSY (UPPER) BROKEN AT 9 O' CLOCK POSITION. REPLACED RSDR DXTA200500808Brake Assy · leakingLOW BRAKE PRESSURE AND ANTI-SKID INOP LIGHTS CAME ON JUST AFTER TAXI OFF RUNWAY THE BRAKE FLUID IS COMING OUT OF THE OVERFLOW NEAR THE NOSE WHEEL. WOULD NOT CANCEL. ITEM IS UNDER INVESTIGATION.SDR DXTA200500807Warning Light · illuminatedUPON GEAR EXTENSION, LO BRAKE PRESS AND ANTI-SKID INOP LIGHT ILLUMINATED, FLUID IS LEAKING ON TO NOSE GEAR. ITEM IS UNDER INVESTIGATION.SDR CWQR2005005Drain · poppedFORWARD RT FUSELAGE STATIC DRAIN VALVE NOT FLUSH. NEW UNIT ORDERED AND INSTALLED, LEAK CHECKED. DURING REMOVAL OF SUSPECTED BAD PART, ENTIRE CORE POPPED OUT, CONDITION WOULD HAVE DIRECTLY OPENED STATIC SYSTEM. CORE OF UNIT APPEARS TO BE PRESSED AND GLUED INSDR DXTA200500792Engine · malfunctionedON TAKEOFF WITH THROTTLE IN THE T/O DETENT, THE LT ENGINE ITT EXCEEDED 720 DEG CELSIUS WITHIN 10 SECS. THE LT ITT INDICTED 724 DEG CELSIUS AND WAS STILL SLOWLY INCREASING. LT THROTTLE REDUCED TO CLIMB. DETENT AND ITT INDICATION IMMEDIATLY DECREASED BELOW 720SDR DXTA200500762Apu · smokeTAXIING FOR T/O ENGINES RUNNING, APU & BLEED AIR ON, ALL AVIONICS ON, THE CABIN & COCKPIT FILLED WITH SMOKE. SMOKE STOPPED WHEN I SHUT EVERYTHING DOWN AND TURNED ELECTRICAL POWER OFF. A LARGE AMOUNT OF WATER DRIPPING FROM BOTTOM OF APU. INSPECTED ENGINE INTSDR DXTA200500761Line · leakingBRAKE SYSTEM FAILURE ON GROUND. AIRCRAFT PUMPED BRAKE LINE FLUID OUT OF NOSE COMPARTMENT ON TO GROUND AROUND NOSE WHEEL. ASSOCIATED AMBER ANNUNCIATORS + M/C (LOW BRAKE PRESS, ANTI-SKID FAIL). ITEM IS UNDER INVESTIGATION.SDR DXTA200500756Line · leakingLEFT BRAKE PEDAL (PILOTS SIDE) DEPRESSED TO FLOOR WITH NO RESISTANCE AND NO BRAKING UPON LANDING. DURING TAXI, PEDAL WAS DEPRESSED TO FLOOR WITH NO RESISTANCE OR BRAKING. RIGHT SIDE PEDAL OK, RIGHT SEAT L/R PEDAL OK. FOUND COPILOT, LEFT BRAKE PEDAL, UPPER BSDR CA050608005Duct · loose(CAN) DEPARTURE AFTER MAINTENANCE, AT FL 22,000 CLIMBING, CREW HEARD A LOUD BANG, THEN THE CABIN ALTITUDE BEGAN TO RISE ( DELTA PRESSURE DROPPED). THE CREW STOPPED CLIMB AND DESCENDED BELOW 10,000 FEET AND ELECTED TO RETURN TO POINT OF DEPARTURE. MAINTENANCE SDR DXTA200500740Wire Harness · faultyDURING TAKEOFF ROLL LEFT ENGINE PRODUCED 80% N1. SCHEDULED TAKEOFF POWER WAS 90.1% - REMOVED AND REPLACED ENGINE WIRING HARNESS PER P&WC M/M CH 76-20-02 OPERATIONAL CHECKS SATISFACTORY. BOTH AUTO AND MANUAL MODES.SDR DXTA200500738Windshield · failedRIGHT FRONT WINDSHIELD SHATTERED DURING FLIGHT. REMOVED RT RAIN SHROUD, REMOVED RT HEATED WINDSHIELD, INSTALLED NEW SEAL ON NEW WINDSHILED IAW MM 56-11-00. PERFORMED STEP C1-C8 RETORQUED BOLTS IAW 560XL MM 56-11-00. PERFORMED FUNCTIONAL CABIN PRESSURIZATISDR DXTA200500739Apu · overservicedAFTER TAKEOFF, HAD A SMOKE SELL FROM AN UNIDENTIFIABLE SOURCE. NO SMOKE WAS VISIBLE. NO UNUSUAL INDICATIONS, NO C/B OPENED, SMELL DISSIPATED WITH APU SHUT DOWN) - FOUND APU OIL TANK OVERSERVICED, OPERATED APU FOR AN EXTENSIVE PERIOD WAS ABLE TO DUPLICATE SMESDR CA050518010Uplock Switch · unserviceablePILOT NOTED THAT THE GEAR WOULD NOT RETRACT AFTER TAKEOFF. IT MADE A REPETATIVE CLUNKING SOUND AND THE RED GEAR INDICATION LIGHT FLASHED ON AND OFF. CYCLED THE GEAR BACK DOWN NORMALLY AND LANDED. THE RT MLG UPLOCK SWITCH WAS REPLACED. PERFORMED GEAR EXTENSDR DXTA200500712Engine · malfunctionedON TAKEOFF , ITT ON LT ENGINE REACHED 725 - 730 INITIALLY DECREASED THROTTLE TO IDLE W/IN 2-3 SECONDS DUPLICATED IN RUN UP PAD ITT ON LT ENGINE REACHED 720 IN CLIMB DETENT DECREASED THROTTLE TO IDLE W/IN 2-3 SECONDS. PERFORMED COMPRESSOR WASH ON LT AND RT ENGSDR CA050527008Hmu · failedIN DESCENT, THE ENGINE EXPERIENCED AN UNCOMMANDED SHUTDOWN. A RELIGHT ATTEMPT WAS UNSUCCESSFUL. THE HYDROMECHANICAL FUEL CONTROL UNIT WAS SUBSEQUENTLY REPLACED.SDR DXTA200500687Relay · failedLO BRAKE PRESS & ANTISKID INOP ANNUNCIATOR ILLUMINATED AT START OF T/O ROLL CAUSING WHEEL BRAKE FAILURE, THE EMERGENCY BRAKING SYSTEM WAS USED. TROUBLESHOT TO POWER BRAKE CONTROL RELAY KN003. RELAY WOULD NOT CLOSE. REMOVED AND REPLACED RELAY IAW CC 560XL WISDR CWQR20050004Support Bracket · misinstalledDURING PHASE 1-4 INSPECTION FOUND LOWER OUTBOARD BARREL SUPPORT BRACKETS INSTALLED INCORRECTLY DURING MANUFACTURE.SDR DXTA200500668Smoke · detectedSMOKE AND ELECTRICAL SMELL IN CABIN AFTER T/O. EMERGENCY PRESS ON AND AIR DUCT OVERHEAT CAUTIONS LIGHTS ON. ALL CAUTION LIGHTS OUT PRIOR TO LANDING. T/S RAN ENGINE OPS CHECKED A/C ENVIRONMENTAL SYS, NO DEFECTS NOTED. CHECKED CABIN, PRESSURIZATION SYS NO DESDR CWQR20050003Sensor · arcedDURING INSPECTION FOUND LOW LEVEL FUEL SWITCH INOP AND THE APPEARANCE OF MISSING MATERIAL AND ARCING BETWEEN FLOAT AND SWITCH BODY WHEN FLOAT WAS IN THE UP POSITION. THIS SWITCH HAS BEEN SENT TO CESSNA FOR EVALUATION AND SUBMITTED CITATION SERVICE CONDITION RSDR DXTA200500657Pressure Switch · dirtyRIGHT LO FUEL PRESS CAUTION LIGHT ILLUMINATES INTERMITTENTLY WITH ENGINE RUNNING. STILL ILLUMINATES WITH RT BOOST PUMP ON OR OFF. REMOVED & INSPECTED FUEL FILTER, FOUND FILTER TO BE DIRTY. REMOVED & REPLACED FUEL FILTER OPERATED RT ENGINE AT TAKEOFF POWER FSDR DXTA200500640Engine · malfunctionedAFTER APPLYING TAKEOFF POWER, RIGHT EEC REVERTED TO MANUAL MODE, ABORTED TAKEOFF. ITEM IS UNDER INVESTIGATION.SDR DXTA200500639Control Box · malfunctionedAFTER TAKEOFF GEAR WOULD NOT RETRACT. TROUBLESHOT SYSTEM AND FOUND LANDING GEAR CONTROL UNIT NOT FUNCTIONING PROPERLY. REMOVED CONTROL UNIT S/N - 0110 AND INSTALLED CONTROL UNIT S/N - 0088. PERFORMED OPERATIONAL CHECK, NO DEFECTS NOTED AT THIS TIME IAW CE56SDR DXTA200500626Uplock Cable · out of adjustWHILE IN CRUISE AT FL410, CREW HEARD CLUNK SOUND FROM GEAR AREA, RED GEAR UNSAFE LIGHT ILLUMINATED AND HYD PRESS LIGHT ILLUMINATED STEADY. PULLED HYD CONTROL CB, HYD PRESS EXTINGUISHED, GEAR UNSAFE REMAINED ILLUMINATED. FOUND NOSE GEAR FREEFALL CABLE TO BE TSDR DXTA200500624Support Bracket · damagedNO TAKEOFF LIGHT AND HORN CAME ON AT TAKEOFF POWER AND TAKEOFF ROLL INITIATION. FLAPS 15, SPEED BRAKE RETRACTED, TRIMS SET FOR T/O). FOUND RT SPEED BRAKE SWITCH JAM NUT BEING PUSHED UP BY SPEED BRAKE DOOR SUPPORT BRACKET, CAUSING PLUNGER TO RELAX. ADJUSTED SDR DXTA200500618Rudder · malfunctionedAIRCRAFT REQUIRES EXCESSIVE EFFORT FOR RUDDER CONTROL IN HIGH POWER SETTINGS ON GROUND AND INFLIGHT "AIRSPEED IS NOT AN ISSUE". FEELS AS IF YAW DAMPER IS ON, SUSPECT RUDDER BIAS SYSTEM. ITEM IS UNDER INVESTIGATION.SDR 5285002Uplock Switch · defectiveAFTER DEPARTURE FROM FSM, LANDING GEAR UNLOCK LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. EXTENDED GEAR SUCCESSFULLY, RETURN TO FSM UNEVENTFUL. FOUND FAULTY UPLOCK SWITCH.SDR CA050224008Engine · shutdown(CAN) THE ENGINE EXPERIENCED AN UNCOMMANDED SHUTDOWN IN CRUISE. SUBSEQUENT RELIGHT ATTEMPTS WERE UNSUCCESSFUL. THE CREW DECLARED AN EMERGENCY AND THE FLIGHT DIVERTED. MFG WILL INVESTIGATE THE EVENT AND SUPPLEMENT THIS REPORT TO REFLECT ROOT CAUSE ONCE ESTABSDR 022405N523CS1Engine · malfunctionedDURING CRUISE AT ALTITUDE 40,000 FEET, THE RIGHT ENGINE DID A UNCOMMANDED SHUTDOWN. THE CREW PUT THE AIRCRAFT INTO THE RESTART ENVELOPE AND ATTEMPTED TWO INFLIGHT RESTARTS. THE ENGINE WOULD NOT START SO AN EMERGENCY WAS DECLARED AND THE AIRCRAFT SAFELY LANDESDR DXTA200500603Landing Gear · malfunctionedAFTER ROTATION, GEAR SELECTED UP, AFTER 3-4 SEC GEAR MADE A CYCLING THUMPING NOISE FOR APPROX 3 SECONDS. RECEIVED A HYD FLOW & A HYD LOW CAUTION LIGHT. CYCLING STOPPED, GEAR LOCKED UP & HYD FLOW LIGHT WENT OUT. KEPT FLAPS AT 15 DEG AND RE-EXTENDED GEAR. HYSDR DXTA200500601Engine · leakingDURING FLIGHT CREW & PASSENGERS NOTICED FUMES IN CABIN. AFTER LANDING FOUND OIL LEAKING FROM NR 1 ENGINE & NO OIL SHOWING ON SIGHT GAUGE. ENGINE CHANGE CURRENTLY IN WORK.SDR DXTA200500599Pump · failedLOW BRAKE PRESSURE AND ANTI-SKID INOP. ANNUNCIATORS ILLUMINATED WITH MASTER CAUTION. BRAKE PUMP WOULD NOT RUN. SMELL OF ELECTRICAL BURN IN COCKPIT. AFTER APPROX 5 MINUTES LIGHTS EXTINGUISHED AND PUMP OPERATED AGAIN.SDR DXTA200500596Fire Loop · intermittentRIGHT FIRE LIGHT ILLUMINATED MOMENTARAILY FOR A FEW SECONDS DURING CRUISE. WENT OUT WHEN POWER WAS REDUCED. REPLACED RT FIRE DETECTOR LOOP WITH NEW REF 560 XL CH 26-11-01. OPERATIONAL CHECK SATISFACTORY.SDR DXTA200500591Line · leakingBRAKES ARE SPONGY, LEFT SIDE IS WORSE THAN THE RIGHT SIDE. LEFT BRAKE ALMOST GOES TO HTE FLOOR FOR ANY REACTION. FOUND AIR IN BRAKE SYSTEM, BLED BRAKE SYSTEM IAW 560XL MM 32-42-00, TAXI CHECK GOOD.SDR 2005FA0000276Heat Shield · contaminatedAFTER LANDING, SMOKE AND SMALL FLAME OBSERVED FROM LT MAIN GEAR WHEEL. FIRE WAS EXTINGUISHED, NO DAMAGE TO LANDING GEAR OR AIRCRAFT. LT MAIN GEAR WHEEL ASSEMBLY WAS REPLACED AS A PRECAUTION. THE LT WHEEL HAD BEEN RECENTLY CLEANED WITH A WATER BASED SOLVENT IAWSDR DXTA200500583Handle · inoperativeAFTER TAKEOFF GEAR HANDLE WOULD NOT MOVE, THEREFORE COULD NOT RETRACT THE GEAR. ITEM IS UNDER INVESTIGATION.SDR DXTA200500577Warning System · malfunctionedWHILE IN DESCENT THE LT GREEN LANDING LIGHT CAME ON ALONG WITH THE "LO BRAKE PRESS" AND "ANTISKID INOP" ANNUNCIATORS & MASTER CAUTION. ALL LIGHTS WENT OUT AFTER A COUPLE OF MINUTES AND LANDING WAS NORMAL. COULD NOT DUPLICATE AT THIS TIME. JACKED ACFT, PERFORSDR CWQR20050002Nut · wrong partPILOT FOUND ELEVATOR TRIM OUT OF RIG. TECHICIAN FOUND EXCESSIVE PLAY IN TRIM WHEEL, ALLOWING TRIM INDICATOR POINTER TO JUMP GROOVE IN TRIM WHEEL. FOUND TRIM WHEEL BOLT (P/N AN3-57) NOT TO HAVE NUT (P/N MS21044N3) INSTALLED. NUT WAS FOUND IN AIRCRAFT BELLY. SDR CWQR20050001Heat Shield · crackedDURING INSPECTION FOUND THE LEADING EDGE HEAT SHIELD FLANGE CRACKED ON BOTH LEFT AND RIGHT WINGS. SUBMITTED CESSNS/CITATION SERVICE CONDITION REPORT 181187 WITH PICTURES.SDR DXTA200500561Circuit Board · failedNO GEAR INDICATION LIGHTS WHEN LANDING GEAR EXTENDED. GEAR CIRCUIT BREAKER POPPED. DURING CHECKLIST, WHEN C/B WAS RESET, MOMENTARILY GOT 3 GREEN LIGHTS, THEN C/B POPPED AGAIN. GEAR WAS BLOWN DOWN PER CHECKLIST. TROULBLESHOT SYSTEM, CHECKED POWER WIRES 1PC0SDR DXTA200500552Handle · stuckCOULD NOT RAISE GEAR HANDLE TO RETRACT GEAR AFTER T/O. INSPECTED GEAR HANDLE AND FOUND IT TO BE BINDING. REMOVED GEAR HANDLE WHEEL AND CLEANED SLIDING SAFETY SHAFT INSTALLED GEAR HANDLE WHEEL AND PERFORMED GEAR SWING, OPS CHECK GOOD. WORK DONE IAW 560XL M/MSDR DXTA200500551Wire Harness · chafedDURING APPROACH, SELECTED GEAR DOWN, HEARD THE GEAR DEPLOY BUT GOT NO SAFE LIGHT INDICATION. GEAR WARN C/B POPPED & RESET IT TO FIND 3 GREEN, LANDED NORMAL. TROUBLESHOT FAULT WITH TEAM XL AND ISOLATED FAULT TO A CHAFED WIRE HARNESS IN THE LEFT WHEEL. REPAIRSDR DXTA200500548Connector · dirtyLANDING GEAR UNLOCK LIGHT WILL NOT EXTINGUISH AFTER GEAR RETRACTION. HYDRAULIC SYSTEM STAY PRESSURIZED, IT SOUNDS AND FEELS LIKE THE GEAR IS RETRACTING. GROUND OBSERVER ALSO SAID THE GEAR APPEARED TO BE RETRACTING. INSPECTED ALL GEAR, NO DEFECTS NOTED. CLESDR DXTA200500544Support Bracket · crackedTHE RIGHT SIDE SUPPORT BRACKET IS CRACKED C/T THE ECM. REMOVED AND REPLACED BRACKET REF 560XL IPC 21-51-00 AND 560XL SRM 51-40-03.SDR DXTA200500543Attach Bracket · crackedACM SUPPORT BRACKET CRACKED WHERE RUDDER BIAS CONTROL VALVE ATTACHES. REMOVED AND REPLACED THE CRACKED BRACKET IAW THE 560 XL MM 21-50-00 SRM 51-40-03; 04; 06; AND 08.SDR DXTA200500545Bulb · inoperativeLANDING - RIGHT GEAR DOWN LIGHT WOULD NOT TURN GREEN. RECYCLED GEAR, CHECK ROTARY TEST, LIGHT OUT. EMERGENCY GEAR EXTEND AND LANDED. REPLACED RIGHT GEAR DOWN LIGHT BULB P/N 387. RESET EMERGENCY GEAR EXTEND AND CARRIED OUT GEAR RETRACTION REF A/C M/M CH32-0SDR DXTA200500557Downlock Switch · malfunctionedDID NOT GET ANY GEAR INDICATION LIGHTS WHEN LANDING GEAR WAS EXTENDED GEAR CIRCUIT BREAKER WAS POPPED. RESET C/B & IT POPPED AGAIN. RESET C/B A 2ND TIME AND IT STAYED IN. BLEW GEAR DOWN MANUALLY PER THE CESSNA EMERGENCY CHECKLIST. FOUND MINOR CORROSION ON SDR DXTA200500530Warning Light · illuminatedON APPROACH WHEN FLAPS WERE SELECTED TO 15 DEG LOW HYD FLOW LT & RT CAUTION LIGHTS ILLUMINATED. THAT WAS FOLLOWED BY LOW HYD LEVEL AT AROUND THE SAME TIME THE FLAPS REACHED 15 DEG BECAUSE OF THE POTENTIAL FOR HYDRAULIC FLUID LOSS, AND EMERGENCY GEAR EXTENSION
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