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 DXTA200802842Control Unit · inoperativeAT HIGH POWER SETTING, LT ENGINE FIRE WARNING LIGHT FLICKERED ON AND OFF (VERY DIM) NEVER CAME ON FULL BRIGHT. FOUND FIRE DETECTOR CONTROL UNIT BAD. INSTALLED NEW CONTROL UNIT IAW THE MM 26-11-02. OPS CHECKED GOOD.SDR DXTA200802825Oxygen Mask · leakingCAPT'S 02 MASK HOSE DEVELOPED A LEAK WHERE IT ATTACHES TO MASK AND COULD NOT STOP LEAK. INSTALLED NEW O2 MASK. OPS CHECK GOOD IAW MM CH 35-10-01. (K)SDR DXTA200802822Actuator · malfunctionedWHILE ON DOWNWIND GEAR WAS SELECTED DOWN, WE DID NOT HAVE A GREEN LIGHT FOR LT MAIN. WE HAD PROPER INDICATION FOR RT MAIN AND NOSE (GREEN) AND RED UNSAFE. GEAR WAS CYCLED AND 3 GREEN LIGHTS WERE OBSERVED, NO FURTHER ISSUES AROSE. REPLACED LT MAIN GEAR ACTUATOSDR DXTA200802821Fuel Control · malfunctionedDURING TAKEOFF ROLL THE NR 1 ENG DID NOT DEVELOPE T/O POWER. TARGET N1 WAS 88.6 PERCENT BUT ONLY DEVELOPED 81 PERCENT N1. DOWNLOADED NR1 ENG. DCU AND SENT INFO TO MFG, SWAPPED EEC'S AND RAN FOR PWR OF DAY. DOWNLOADED DCU NR SENT TO MFG. PERFORMED OPS CHECK OSDR DXTA200802816Trimmer · wornTHE TRIM (PITCH) INDICATOR WHILE IN CRUISE IS AT THE MOST FWD PART OF THE TRIM INDICATOR. REMOVED AND REPLACED THE ELEVATOR TRIM TABA CONTROL WHEEL P/N 5565756-3. ALSO REPLACED POINTER ARM ASSY. P/N 5565756. ALSO REPLACED POINTER ARM ASSY P/N 6661053-15, POSDR 020108N509CS1Wire Harness · damagedDURING TAKEOFF ROLL, CREW NOTICED ANTI-SKID INOP ANNUNCIATION. CREW CONTINUED TAKEOFF AND RETURNED TO AIRPORT. AFTER LANDING CREW REPORTED DAMAGE TO TIRE, WHEEL, WHEEL WELL AREA AND FLAP. AC CURRENTLY IN MAINT. MAINT FOUND ANTI SKID DISCREPANCY TO BE CAUSED SDR 020108N547CS1Actuator · failedRT MAIN GEAR DOWN INDICATION FAILED TO ILLUMINATE AFTER GEAR EXTENSION. CREW RAN AFM CHECK LIST PROCEDURES WITH NO CHANGE. GEAR BLOWN DOWN, EMERGENCY DECLARED AND AC LANDED WITHOUT INCIDENT. AC CURRENTLY IN MAINT 02/01/2008. ON SITE MAINT REPLACED RT MAIN GEASDR DXTA200802806Fire Loop · out of positionAT 34.0 FT IB TO MSP LT ENGINE, ENGINE FIRE LIGHT BLINKED ON AND OFF ABOUT 10 TIMES A MIN FOR 10 MIN INSPECTED LT ENGINE FIRE LOOP CONNECTIONS. INSPECTED FIRE LOOP AND FOUND CONTACTING LINE FROM FUEL/OIL HEAT EXCHANGER. REPOSITIONED FIRE LOOP TO MAINTAIN CLEARSDR DXTA200802803Warning Light · illuminatedHYD PRESS LIGHT REMAINED ILLUMINATED FOLLOWED BY THE STAB MISCOMPARE. (2)-POSITION TAIL SYS, OPS CHECK GOOD. STAB LIGHT DUE TO EXTENDED TRAVEL TIME FROM FLAPS, UP TO FLAPS DOWN DURING EMERGENCY GEAR INDICATION DURING TAKEOFF IAW MM CHAP. 27-40-00.SDR DXTA200802799Warning Light · illuminated(EMERGENCY DECLARED) PASSING THRU 10,000 FT, RT WING OVERHEAT LIGHT ILLUMINATED WITH ANTI-ICE SWITCH IN (OFF) POSITION. REDUCED POWER ON RT ENGINE TO IDLE AND LIGHT DIDN’T EXTINGUISH. APPROX 5 MIN LATER WHILE ENROUTE TO LANDING, LIGHT DID EXTINGUISH. LANDED SDR DXTA200802792Switch · inoperativeHAD A (NO TAKEOFF) ANNUN AFTER ADDING TO THRUST AND REACHING APPROX 30 KTS, THE LIGHT CAME ON ALONG WITH HORN. ABORTED TAKEOFF. REMOVED LT SPEEDBRAKE SWITCH P/N 602EN16-6. INSTALLED NEW LT SPEED BRAKE SWITCH P/N 602EN16-6 IAW 27-61-06 OF MM. OPS CHECK GOOD.SDR DXTA200802791Display · malfunctionedAT FL340, LT ENGINE INSTRUMENT LCD WENT BLANK, SHORTLY AFTER WE DETECTED AN ELECTRICAL BURNING ODOR AND RETURNED TO AIRPORT. REMOVED AMLCD AND INSTALLED MODIFIED AMLCD IAW MM 77-40-00. OPS CHECKS GOOD.SDR CA080206009Oil System · empty(CAN) DURING CLIMB AT APPROX FL190, THE CREW RECEIVED A LOW OIL PRESSURE WARNING AND PERFORMED A COMMANDED SHUTDOWN OF THE ENGINE. THE AC WAS DIVERTED TO AN ALTERNATE LANDING SITE. POST FLIGHT INSP REVEALED NO INDICATION OF OIL ON THE SIGHT GLASS. NO SIGNS OFSDR CA080125001Oil System · unknown(CAN) APPROXIMATELY 5 -7 MINUTES AFTER TAKEOFF, THE WARNING LIGHT (LOW OIL PRESS R ) WAS OBSERVED ON THE M.A.P. AND (0) ON THE OIL PRESSURE INDICATOR TAPE . A PRECAUTIONARY ENGINE SHUTDOWN WAS PERFORMED FOLLOWED BY THE DECLARATION OF AN EMERGENCY. ENG IS STILLSDR DXTA200802787Trim Motor · sticksCLIMBING FROM FL 380 TO FL 410 AT 18,600 LBS AND 180 KTS WHEN WE RAN OUT OF FWD NOSE DOWN TRIM. REPLACED ELECTRIC TRIM MOTOR FOR TROUBLESHOOTING PURPOSES AND FOR POSSIBLE COLD SOAK OF OLD TRIM MOTOR CAUSING OVER TORQUE CONDITION. OPS. CHECKED OKAY. LOWERINSDR DXTA200802790Control Column · vibrationVERY HIGH DEGREE OF VIBRATION IN CONTROL COLUMN AND YOKE AT ALL SPEEDS ABOVE 250 KNOTS AND AT ALL ALTITUDES ABOVE THAT SPEED. PERFORMED ELEVATOR AND ELEVATOR TRIM CABLE TENSION CHECK, PERFORMED FREE PLAY CHECK ON RT/LT AILERON, ALSO PERFORMED INSPECTION OF CASDR DXTA200802777Fire Loop · out of positionLT ENGINE FIRE WARNING LIGHT FLASHES INTERMITTENT IN CRUISE FLIGHT. NO SECONDARY INDICATIONS OBSERVED. REMOVED BOTH UPPER AND LOWER COWLINGS, INSPECTED FIRE LOOP, FOUND LOOP CONTACTING ENG. REPOSITIONED FIRE LOOP, CLEANED CONNECTORS, SWAPPED FIRE DETECTION CSDR DXTA200802775Light · fireAFTER APU START AND TAIL FLOOD LIGHTS TURNED ON , BOTH PILOT AND FUEL LINEMAN OBSERVED BLUE FLAME AND SMOKE COMING FROM RT TAIL FLOOD LIGHT. RAN APU SEVERAL TIMES, TURNED FLOOD LTS. ON/OFF DURING START AND NORMAL OPERATION. NO INDICATION OF HIGH APU ITT. NSDR DXTA200802771Relief Valve · stickingGEAR WOULD NOT RETRACT AFTER TAKEOFF. R & R LT UPLOCK ACTUATOR WITH NEW. FOUND HYD RELIEF VALVE OUT OF TOLERANCE, REPLACED WITH OVERHAULED UNIT FROM PNEUDRAULICS RS PD6R469J, PRESSURE SWITCH & LT MLG ACTUATOR WITH SERVICEABLE UNIT FROM CESSNA ICT RS CNQB9181 WSDR DXTA200802769Actuator · intermittentON ILS APPROACH GEAR WAS EXTENDED BUT LT MAIN GEAR LIGHTS DID NOT ILLUMINATE. REMOVED LT MLG ACTUATOR AND INSTALLED REPAIRED ACTUATOR I.A.W. CESSNA 560XL MAINT. MAN. CHAP. 32-30-04, OPS AND LEAK CHECK GOOD.SDR DXTA200802764Switch · malfunctionedAFTER TAKEOFF UPON FLAP RETRACTION THE "STAB MISCOMPARE ANNUNCIATOR LIGHT" ILLUMINATED. REPLACED SWITCHES SC050 AND SC051 PER MM 27-90-40. GROUND OPERATIONAL CHECK GOODSDR DXTA200802762Indicator · unknownEXCESSIVE BACK PRESSURE (MORE THAN NORMAL) REQUIRED FOR ROTATION. REMOVED AND REPLACED ELEVATOR TRIM WHEEL POINTER IAW MM 27-32-01. CHECKED ELEVATOR TRIM RIGGING PER CE-5460XL M/M 27-31-00.CHECKS GOOD.SDR DXTA200802761Downlock Switch · malfunctionedRT GEAR INDICATOR LIGHT SHOWED RT GEAR NOT DOWN AND LOCKED. PEFORMED GEAR SWING MANY TIMES WITH NO FAULTS. APPLIED FREEZE-IT SPRAY TO RT GEAR DOWNLOCK SWITCH GIVING US A FAULTY LIGHT AT GEAR INDICATION. REMOVED RT MAIN ACTUATOR AND INSTALLED REPAIRED ACTUASDR DXTA200802758Uplock Switch · malfunctionedUPON GEAR RETRACTION - GEAR UNLOCK LIGHT WOULD NOT EXTINGUISH. REMOVED AND REPLACED ALL THREE UP LOCK SWITCHES WITH NEW PER CESSNA 560XL MAINT. MANUAL CHAP 32-30-05 & 32-60-02. SYS GROUND OPS CHECKED GOOD.SDR DXTA200802745Connector · dirtySELECTED GEAR DOWN AND RECEIVED A DOWN INDICATION FOR RT MAIN AND NOSE ONLY. RED UNLOCK LIGHT ILLUMINATED ACCOMPANIED WITH NO LT MAIN INDICATION. SERVICED GEAR BLOW DOWN BOTTLE AND SAFETIED AS REQUIRED. BLEED MLG HYD SYSTEM. T/S LANDING GEAR SYSTEM. CLEANED LSDR DXTA200802739Brake Assy · failedWHILE TAXIING, WE LOST OUR BRAKES AND USED EMERGENCY BRAKES TO STOP. FOUND PWR BRAKE CB PULLED. BLED BRAKES COMPLETED OPERATIONAL CHECK OF ANTI-SKID SYSTEM AND OPERATIONAL CHECK OF EMERGENCY BRAKE SYSTEM. TAXIED ACFT TO ACCOMPLISH OPS CEHCK OF BRAKES OPS CHECSDR DXTA200802738Brake Assy · contaminatedRT BRAKE PEDAL SOFT. GOES TO THE THE STOPS WHEN PRESSED. HOOKED UP BRAKE BLEEDER HOSES AND C/W LT & RT BRAKE BLEEDING. FOUND NUMEROUS AIR POCKETS ON LT & RT BRAKE SYSTEMS. C/W BRAKE BLEEDING ON LH & RH BRAKES. OPS CHECKED GOOD AND TAXI CHECKED GOOD IAW 560SDR DXTA200702737Actuator · leakingON TAKEOFF, GOT A STAB MISCOMPARE LIGHT AND THE HYDRAULIC PRESS LIGHT. REPLACED ACTUATOR DUE TO EXCESS LEAKAGE IN ACTUATOR IAW 560XL M/M 23-40-00. OPS AND LEAK CHECK GOOD.SDR CA080116012Fuel Control · malfunctioned(CAN) DURING APPROACH AT 3000 FEET, THE LOW FUEL FLOW WARNING CAME ON, FOLLOWED BY ENGINE SHUTDOWN. THE FUEL CONTROL HAS BEEN REMOVED AND SUBMITTED FOR INVESTIGATION. UPDATES WILL BE PROVIDED WHEN AVAILABLE. (TC NR 20080116012)SDR DXTA200702722Control Wheel · damaged(EMERGENCY DECLARED) ON ROTATION AN UNUSUAL NOSE UP FORCE WAS NOTED REQUIRING FULL NOSE DOWN TRIM. BOTH PILOTS APPLIED NOSE DOWN PRESSURE AND CONDITION WORSENED AS SPEED INCREASED. FOUND PITCH TRIM WHEEL IMPROPERLY CLOCKED & PART OF INDICATOR TRACK MISSING. SDR DXTA200702724Wheel · crackedTRIM INDICATOR IS NOT INDEXED CORRECTLY. TRIM WAS CHECKED AND SET TO TAKEOFF RANGE BEFORE START. JUST PRIOR TO ENGINE START, BOTH PILOTS NOTICED TRIM INDICATOR FULL FORWARD. TRIM WAS RESET TO TAKEOFF RANGE, TAXI AND TAKEOFF WERE BEGUN. DURING TAKEOFF, YOKE STSDR DXTA200702727Circuit Board · inoperativeCLIMBING TO ALTITUDE THE LEFT GREEN INDICATOR LIGHT STARTED FLICKERING ON AND OFF. NO HYDRAULIC OR GEAR UNSAFE LIGHTS WERE PRESENT. AT FL300 IT CONTINUED TO FLICKER AND STYING ON LONGER AND LONGER, IT DID THIS FOR 1/2 HOUR. AT GEAR EXTENSION ALL GREEN LIGHTS.SDR DXTA200702726Actuator · bypassingEMERGENCY DECLARED. ON POST FLT DISCOVERED LEFT FLAP EXTENDED ABOUT ONE INCH & RT FLAP FULLY RETRACTED FLUSH WITH THE FLAP HANDLE IN THE FULL UP POSITION. ' HYD PRESS' AMBER ANNUNCIATOR REMAINED ILLUMINATED IN FLT AFTER FLAP RETRACTION. PERFORMED 'HYD PRESS' ASDR DXTA200702719Actuator · inoperativeFAILED TO GET LT MAIN GEAR LIGHT UPON EXTENDING MLG. JACKED A/C, REMOVED NR 2 ENG HYD PUMP TO FACILITATE HYD PWR W/ROBO MULE, REMOVED & REPLACED LT MLG ACTUATOR, SWING GEAR MULTIPLE TIMES NO DEFECT NOTED. DOWNJACKED A/C, REINSTALLED NR 2 ENGINE RAN, OPS & LEASDR DXTA200702704Brake Assy · weakRT BRAKE PEDAL SERVING BOTH PILOT STATIONS IS SPONGY. AIRCRAFT EXHIBITS ASSYMETRIC BRAKING DURING LANDING, BRAKE APPLICATION YAWS ABRUPTLY. BLED RIGHT BRAKE IN REF. TO CE-560XL MM 32-42-00. OPS AND LEAK CHECK GOOD. TAXIED ACFT. NO DEFECTS NOTED.SDR DXTA200702709Wire · damagedAFTER GEAR EXTENSION, RT MAIN GEAR DID NOT INDICATE DOWN AND ASSOCIATED UNLOCK LIGHT DID ILLUMINATE. ATTEMPTED MANUAL GEAR EXTENSION VIA CHECKLIST BUT GEAR STILL INDICATED UNSAFE. NORMAL LANDING AFTER GEAR BLOW DOWN BOTTLE WAS USED. TROUBLESHOT TO BRAKE X1 SDR 122107N540CS1Actuator · failedLT MAIN GEAR DOWN INDICATION FAILED ON GEAR EXTENSION. AFM EMERGENCY PROCEDURES DID NOT REMEDY SITUATION. DIVERTED FROM SCHEDULED DESTINATION. DECLARED EMERGENCY AND LANDED AIRCRAFT WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED SUSPECT GEAR ACTUATOR AND OSDR DXTA200702698Water Separator · odorNOXIOUS FUMES ENTER COCKPIT WHEN COCKPIT TEMPERATURE CONTROL IS RAISED TO HEAT COCKPIT. REMOVED & CLEANED WATER SEPARATOR. REINSTALLED WATER SEPARATOR IAW CESSNA 560XL MM CH 12-19-02. OPS & LEAK CHECK GOODSDR DXTA200702696Mount · looseON TAKEOFF, F/O HAD TO USE FULL FORWARD PRESSURE TO KEEP NOSE DOWN. FOUND ELEVATOR TRIM WHEEL MOUNTING SCREWS LOOSE CAUSING THE POINTER TO SKIP ITS TRACK. REINDEX POINTER TO TRIM WHEEL AND TAKEOFF MARKER INDEX. RESECURED TRIM WHEEL SCREWS AS ORIGINAL REF CESSDR DXTA200702693Check Valve · bypassing(LO HYD FLOW RT) ANNUNCIATOR ILLUMINATED ON TAKEOFF ROLL AT 40 KNOTS. NO SECONDARY INDICATIONS. ABORTED TAKEOFF. REMOVED AND REPLACED R/H LO HYD. FLOW CHECK VALVE WITH A NEW UNIT. PERFORMED OPS TEST. CHECKED SATISFACTORY NO LEAKS NOTED. I.AW. CE-560XL M.M. CSDR DXTA200702691Brake Assy · malfunctionedCO-PILOTS RT BRAKE FADES TO STOP AND WILL NOT HOLD . TAXIED AIRCRAFT AROUND RAMP AND PERFORMED SEVERAL BRAKE CHECKS USING PILOT'S AND CO-PILOT'S BRAKES WITH NO DEFECTS NOTED. MADE SEVERAL TURNS USING AIRCRAFT RUDDER PEDALS ONLY WITH NO DEFECTS BEING NOTED. INSDR DXTA200702690Pitot Tube · contaminatedABORTED TAKEOFF DUE TO NO AIRSPEED INDICATION ON PILOTS SIDE. DRAINED MOISTURE FROM LT PITOT TUBE. PERFORMED PURGE TO PILOTS SYSTEM. TESTED LT PITOT SYSTEM. OPERATIONAL CHECK SATISFACTORY IAW MANUAL 34-11-08.SDR DXTA200702682Controller · inoperativeAUTOPILOT INOP AMBER TURN KNOB INDICATION ON PFD'S. TURN KNOB WAS IN THE CENTER POSITION. POSITION. REMOVED AUTOPILOT CONTROLLER & INSTALLED SERVICEABLE AUTOPILOT CONTROLLER REMOVED FROM A/C 560XL-5176 N876QS FOR CONTINUED SERVICE ON 560-5264 N664QS AUTO PILOSDR CA080207002Actuator · leaking(CAN) LT THRUST REVERSER INBD ACTUATOR. WEEPING HYDRAULIC FLUID. NOTE: THIS ACTUATOR WEEPED FLUID FROM DAY ONE ON 560 S/N 0648 HAD 2 ACTUATORS I/B LT REPLACED FOR HYDRAULIC FLUID LEAKS OVER APPROX 1800 HRS.SDR CA080207001Actuator Valve · sticking(CAN) RT BLEED AIR OVERTEMP WARNING LITE CAME ON DURING T/O. TWICE IN 42 T/O. THE HEAT EXCHANGER VALVE WAS STICKING IN CLOSED POSITION - VALVE ACTUATOR PIN IE50-2 WAS REPLACED.SDR DXTA200702679Latch · bindingCABIN DOOR WARINING LIGHT CAME ON IN FLIGHT. FOUND CABIN DOOR UPPER AFT LATCH BINDING. ADJUSTED UPPER AFT LATCH AS NEEDED TO FREE UP PIN TO CONTACT DOOR LATCH SWITCH. OPS CHECKED GOOD. ALL WORK COMPLETED I/A/W CESSNA 560XL MM 52-10-00.SDR CA071214008Valve · failed(CAN) AT LANDING GEAR SELECTION, THE LANDING GEAR DID NOT COME DOWN AND NONE OF THE FOLLOWING INDICATIONS WERE OBSERVED: HYD PUMP OPERATION GEAR MOVEMENT / NOISE GEAR DOWN LIGHTS INDICATION ON THE CONTROLLER, NOTE: ALL OTHER HYD CONSUMERS WERE OPERATIONAL THSDR CA071221003Motor · defective(CAN) VIBRATION, (RUMBLE) AND EEC REVERSION WAS EXPERIENCED DURING DESCENT. THE CREW ELECTED TO PERFORM AN INFLIGHT SHUTDOWN OF THE ENGINE AND CONTINUE TO DESTINATION. TROUBLESHOOTING REVEALED A DEFECTIVE BLEED VALVE TORQUE MOTOR CAUSING THE COMPRESSOR SURGES/SDR DXTA200702674Bleed Actuator · inoperativeDURING DESCENT FROM CRUISE ALTITUDE, CREW EXPERIENCED ENGINE VIBRATION ACCOMPANIED BY EEC MANUAL L ADVISORY WITH NO ENG VIB ANNUNCIATOR. THROTTLE AY IDLE ITT= 650. EEC CHECKLIST DID NOT EFFECT VIBRATION. PERFORMED PRECAUTIONARY S/D. VISUALLY INSPECTED CHIP SDR DXTA200702667Overheat Sensor · inoperativeIN CRUISE FLT WITH WING + ENGINE ANTI-ICE ON, MASTER CAUTION FLICKERED THEN LATER CAME ON AND RT (WING OVERHEAT) ANNUNCIATOR FLASHED. REPLACED TEMP SENSOR TT02 WITH NEW. LEAK & OPERATIONAL CHECK NORMAL IAW 560XL MM 36-11-01.
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