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 DXTA200601498Apu · overservicedON GROUND AT APA, WITH APU RUNNING AND BLEED AIR ON AND AVIONICS ON, SMOKE IMMEDIATLEY FILLED THE COCKPIT AND FRONT PART OF CABIN. FOUND APU OIL OVER SERVICED, DESERVICED APU AND CLEANED WATER SOCK IAW CE 560XL M/M CH 12-19-02. OPS CHECK GOOD, NO SMOKE OR SMSDR DXTA200601496Relay · failedON LANDING LO BRAKE PRESS/ANTI SKID INOP LIGHT CAME ON. BRAKES FAILED AND EMERGENCY BRAKES APPLIED. ALL ECS NORMAL, ACCUMULATOR NORM, FLUID LEVEL NORM. TROUBLESHOT SYSTEM, REMOVED BRAKE CONTROL MOTOR RELAY KN003 P/N MS2416602, DUE TO INTERNAL FAILURE. REPLSDR CWQR2006014Cable Assy · frayedREQUESTED CABLE INSPECTION OF AFT ELEVATOR TRIM CABLE, BECAUSE AC IN THE FLEET OF THIS SN BLOCK AND TIME SHOWED SIGNS OF FRAYING. DURING INSPECTION FOUND THE CABLE FRAYED AS IT TRANSVERSED THE PULLEY. REMOVED CABLE AND CHAIN ASSEMBLY AND PREFORMED LOOP CHECK, SDR DXTA200601487Control Cable · brokenELEVATOR TRIM MALFUNCTIONED DURING FLIGHT. REMOVED & REPLACED LT & RT AFT ELEVATOR TRIM CABLES AND PULLEY IAW CESSNA 560XL M/M CHAPT 27-31-00& 27-32-02.SDR DXTA200601481Bolt · shearedPLANE ROCKS VIOLENTLY WHEN TRYING TO STEER, NOSE WHEEL STEERING DOES NOT RESPOND. FOUND STEERING GEAR BOLTS SHEARED. REMOVED AND REPLACED NOSE STEERING SHEET BOLTS IAW CESSNA 560XL LMM 32-20-01 AND 560XL M/M 32-50-00.SDR DXTA200601479Fire Warning · unknownRT FIRE DETECT LIGHT ON ANNUNCIATOR PANEL CAME ON DURING DECENT.SDR DXTA200601477Cam · out of adjustAFTER GEAR RETRACTION ON TAKEOFF, ALL THREE GREEN GEAR DOWN INDICATORS WENT OUT BUT RED UNLOCK LIGHT REMAINED ON RECYCLED GEAR DOWN RED UNLOCK LIGHT WENT OUT, 3 GREEN LOCKED LIGHTS ON RAISED GEAR AGAIN, UNLOCKED LIGHT STAYED ON, THREE GREEN LOCKED. TROUBLESHOSDR DXTA200601474Adc · fluctuatesEXPERIENCED PITCH OSCILLATIONS IN CLIMB WITH KP/FD COUPLED TO AUTO PILOT. VIS FLUCTUATED FROM 500FPM TO +5000 FPM. GOT RED X ON VSI AND ALT AND A/S YELLOW FLAGS. APPEARS TO BE NR 1 ADC. REPLACED NR 1 ADC WITH REPAIR UNIT CERTIFIED TO AN ALTITUED OF 59,500 SDR DXTA200601466Control Lever · stuckAFTER T/O, GEAR WOULD NOT RETRACT WITH GEAR HANDLE IN UP POSITION. RECYCLED HANDLE ONCE AND GEAR STILL WOULD NOT RETRACT. ELECTED TO LEAVE GEAR DOWN. NEVER GOT AN UNLOCK LIGHT. SHORTLY BEFORE LANDING, EMERG BLEW "BLOW DOWN" BOTTLE AS A SAFETY PRECAUTION. SDR CWQR2006013Control Cable · frayedDURING A PHASE 1-4 INSPECTION THE ELEVATOR TRIM CABLE ASSEMBLY WAS FOUND TO BE FRAYED WHERE IT PASSES THROUGH THE HORIZONTAL STABILIZER. THE CABLE APPEARS TO HAVE BEEN INSTALLED PROPERLY AND DOES NOT LOOK AS IF IT WAS DAMAGED DURING INSTALLATION. AN SCR HAS BESDR CWQR2006012Control Cable · frayedDURING A PHASE 1-4 INSPECTION THE ELEVATOR TRIM CABLE ASSEMBLY WAS FOUND TO BE FRAYED WHERE IT PASSES THROUGH THE HORIZONTAL STABLIZER. THE CABLE APPEARS TO HAVE BEEN INSTALLED PROPERLY AND IT DOES NOT LOOK AS IF IT WAS DAMAGED DURING INSTALLATION. AN SCR HASSDR CWQR2006011Control Cable · frayedDURING A PHASE 1-4 INSPECTION THE ELEVATOR TRIM CABLE ASSEMBLY WAS FOUND TO BE FRAYED WHERE IT PASSES THROUGH THE HORIZONTAL STABILIZER. THE CABLE APPEARS TO HAVE BEEN INSTALLED PROPERLY AND IT DOES NOT LOOK AS IF IT WAS DAMAGED DURING INSTALLATION. AN SCR HSDR DXTA200601454Warning Light · erraticAIRCRAFT ON ACTIVE, PUSHED FOR TAKEOFF POWER, GOT FUEL GAUGE ANNUN LIGHT. TAXIED OFF RESET LIGHTS AND TOOK ACTIVE AGAIN WITHOUT PROBLEMS.SDR DXTA200601458Display · inoperativeDURING TAKEOFF ROLL, PILOTS (LEFT SIDE) PFD WENT BLANK (NO RED X). TAKEOFF WAS ABORTED. AFTER CLEARING RUNWAY DISPLAY RETURNED TO NORMAL. ITEM IS UNDER INVESTIGATION.SDR DXTA200601446Apu · smokeAFTER TAKEOFF AIRCRAFT STARTED TO FILL WITH SMOKE. SMOKE WAS COMING FROM THE FLOOR IN COCKPIT & CABIN. SHUTDOWN APU, PULL POWER BACK ON ENGINES FOR DESCENT AND SMOKE STARTED TO CLEAR OUT. SMOKE HAD AN OILY SMELL. OPERATED THE APU AND FOUND A SMOKY SMELL FRSDR CA060704014Fuel Control · malfunctioned(CAN) DURING DESCENT, THE ENGINE WOULD NOT RESPOND TO THROTTLE INPUTS FOR POWER REDUCTION. THE ENGINE WAS SHUT DOWN ON FINAL APPROACH. THE FUEL CONTROL UNIT WAS SUBSEQUENTLY REPLACED. (TC# 20060704014)SDR DXTA200601443Acm · odorDURING CLIMBOUT FROM LUK TO ILG THROUGH 12,000 FT NOTICED STRONG ODOR / BURNING SMELL. SMELL CYCLED ON AND OFF SEVERAL TIMES CLIMBING TO FL 220 AND DESCENDING DOWN TO LANDING. THIS OCCURRED WITH CLIMB POWER AND IDLE WITH APU ISOLATED NO SMOKE OBSERVED. REMOSDR DXTA200601441Actuator · failedLEFT MAIN GEAR WOULD NOT LOCK DOWN. CYCLED THE GEAR, AND STILL NO GREEN LIGHT ON THE LEFT MAIN. -HYD PRESS- LIGHT STARTED FLASHING, AND THE GEAR EVENTUALLY LOCKED DOWN AFTER APPROX 2-3 MINUTES. REMOVED AND REPLACED LT MAIN GEAR ACTUATOR AND OPS CHECKED GOODSDR DXTA200601442Coalescer Bag · dirtyDURING TAKEOFF FROM LUK TO ILM, STRONG ODOR BURNING SMELL NOTICED, RETURNED TO KLUK, NO SMOKE OBSERVED CREW AND PAX SMELLED IT, VERY STRONG ODOR. REMOVED WATER SEPARATOR, CLEANED CONDENSER SOCK THOROUGHLY. REINSTALLED WATER SEPARATOR IAW CE 560XL MM 12-19-02SDR DXTA200601437Windshield · crackedRIGHT FRONT WINDSHIELD HAS MULTIPLE CRACKS BROKE AT FLIGHT LEVEL 390 AND APPEARS TO BE THE OUTER LAYER ONLY. VERIFIED CO-PILOTS WINDSHIELD SHATTERED. REMOVED & REPLACED RT WINDSHIELD. C/W EDGE SEAL. C/W FUNCTIONAL TEST, CHECK GOOD. C/W RETAINER SCREW TORQSDR DXTA200601426Warning System · false activationANTI-SKID LIGHT ILLUMINATED ON SHORT FINAL. LOW BRAKE PRESSURE LIGHT FOLLOWED DURING TAXI. EMERGENCY BRAKE SYSTEM WAS UTILIZED. PWR BRK CIRCUIT BREAKER HAS POPED OUT. INSPECTED PWR BRAKE ANTI SKID SYSTEM. FOUND GEAR BRAKE PNEUMATIC BOTTLE PSI TO BE 1950 PSI SDR DXTA200601420Connector · corrodedDURING TAKEOFF ROLL, NO TAKEOFF ANNUNCIATOR CAME ON . AC WAS IN PROPER CONFIGURATION. TROUBLESHOT TO SPEED BRAKE SYSTEM. FOUND MOISTURE AND CORROSION IN CONNECTOR JL001 GOING TO THE LT SPEED BRAKE LIMIT MONITORS SWITCHES. REMOVED MOISTURE AND CORROSION. SPSDR DXTA200601419Coalescer Bag · dirtyON DESCENT INTO CRQ AT 5000 FEET NOTICED AND SMELLED SMOKE IN CABIN AND COCKPIT. MADE NORMAL LANDING, SMOKE AND SMELL APPEARED TO LEAVE AFTER ENGINE SHUTDOWN. - OPERATED AIRCRAFT ENGINES AND APU. NOTED MUSTY SMELL AND FOG COMING FROM WEMACS. CLEANED COALESCESDR DXTA200601416Engine · oil consumptionLT ENGINE OIL PRESSURE ANNUNCIATOR ILLUMINATED, MASTER WARNING ILLUMINATED. OIL PRESSURE FELL BELOW 20 PSI THEN CAME BACK UP AND HOVERED AT 40 PSI, SHUT ENGINE DOWN NOTICED NO OIL IN SIGHT GAUGE. DETERMINED THAT THE LT ENGINE WAS BURNING OIL INTERNALLY, REPLSDR DXTA200601415Actuator · failedNOSE GEAR FAILED TO EXTEND FOR LANDING TWICE. 40 SECS PASSED BEFORE GREEN SAFE LIGHT ILLUMINATED ON SECOND TRY. ACCOMPLISHED GEAR EXTENSION AND RETRACTION CYCLE TIME TEST IAW MM 32-01-00 OPS CHECK GOOD. CHECKED WIRING FROM NOSE TO LIGHT, CYCLED GEAR SEVERAL TSDR DXTA200601408Control Unit · failedAFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. WITH LDG GEAR HANDLE UP STILL HAD (3) GREEN INDICATION. CYCLED GEAR HANDLE DOWN AND BACK UP WITH SAME INDICATION. SELECTED LANDING GEAR HANDLE DOWN AND PERFORMED (MANUAL GEAR EXTENSION) IAW CHECKLIST. REMOVED ANDSDR 2006FA0000566Windshield · crackedPILOTS WINDSHIELD OUTER PANE CRACKED AT 39,000 FT. IT IS BELIEVED THAT A HEATING ELEMENT SHORTED CAUSING THE OUTER PANE TO CRACK. WINDSHIELD REMAINS STRUCTURALLY INTERGRAL WITH THE OUTER PANE CRACKED. MFG ENGINEERING IS EVALUATING THE FAILURE. (K)SDR DXTA200601403Manifold · leakingWHILE CLIMBING THRU 10000 FT WE NOTICED SMOKE IN THE CABIN WITH A HEAVY KEROSENE SMELL. WE SHUT DOWN THE APU AND SMOKE CLEARED. - INSPECTED APU-FOUND FUEL LEAKS AT SECONDARY FUEL MANIFOLD, SECONDARY FUEL NOZZLE FLOW DIVIDER, REPLACED SEAL ON FLOW DIVIDER, REPLSDR DXTA200601399Actuator · faultyAFTER TAKEOFF, WHEN LANDING GEAR WAS RETRACTED, RED UNLOCK LIGHT REMAINED ILLUMINATED, HYD PRESS AND STAB MISCOMP LIGHT ILLUMINATED. LANDING GEAR WAS LOWERED NORMALLY. LANDING WAS UNEVENTFUL. FOUND NOSE GEAR FAILED RETRACTION TIME CHECK. INSTALLED SERVICEABLESDR DXTA200601392Unlock Switch · out of adjustDURING GEAR RETRACTION THE 3 GREEN LIGHTS EXTINGUISHED WHILE THE RED UNLOCK LIGHT REMAINED ILLUMINATED. - JACKED ACFT, ADJUST UP-LOCK, SWITCH ON NOSE GEAR, SWING GEAR MULTIPLE TIMES. OPS CHECK GOOD. IAW CE560XL 32-01-00.SDR DXTA200601389Uplock Switch · malfunctionedAFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, UNLOCK LIGHT REMAINED ILLUMINATED. HYD PRESS AND STAB MISCOMP, CAUTION LIGHTS ILLUMINATED. LANDING GEAR WAS LOWERED NORMALLY. LANDING WAS UNEVENTFUL. JACKED AIRCRAFT, REMOVED & REPLACED LT MLG UPLOCK SWITCH. SDR DXTA200601391Pin · disconnectedNOSE WHEEL STEERING PIN DISCONNECTED FROM STEERING ASSEMBLY ON TAKEOFF AT 70K. REMOVED AND REPLACED CUT WORN NOSE WHEEL ASSY WITH NEW SERVICEABLE WHEEL ASSY. INSPECTION THE NOSE GEAR ASSY, TORQUE LINKS, TORQUE LINK PIN, AND RETAINING CLIP. FOUND NO DEFECTS SDR 050906N506CS1Duct · detachedAFTER DEPARTING FROM MCO THE CREW NOTICED THE CABIN ALTITUDE WAS AT 10,000 FEET AND THEN RECEIVED A CABIN ALTITUDE WARNING ANNUNCIATION. ATTEMPTED TO LOWER CABIN ALTITUDE WITH MANUAL MODE WITH NO SUCCESS. DUE TO BOTH AUTO AND MANUAL PRESSURIZATION CONTROL BESDR DXTA200601381Coalescer Bag · dirtyDURING CLIMBOUT SMOKE FILLED FLIGHT DECK AND CABIN. RAN BOTH ENGINES TO 85 PERCENT. COULD NOT FIND ANY DISCREPANCIES. INSPECTED WATER SEPARATOR SOCK & FOUND TO BE WORN AND DIRTY. REMOVED & REPLACED WATER SEPARATOR SOCK IAW CE 560XL MM 21-51-00.SDR DXTA200601377Controller · inoperativeREPEAT WRITE UP - WHEN GEAR WAS LOWERED THE LT MAIN GREEN LIGHT AND THE RED GEAR UNSAFE LIGHT FLICKERED FOR ABOUT 10 SECONDS. THEN ALL MAIN GEAR LIGHTS ILLUMINATED AND THE GEAR UNSAFE LIGHT EXTINGUISHED. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE AND PESDR 2006FA0000472Float Switch · inoperativeTHE RIGHT LOW FUEL LEVEL SYSTEM WAS INOPERATIVE. REMOVED SWITCH AND FOUND SIGNS OF ARCING ON THE TOP SIDE OF THE SWITCH. TROUBLESHOT FURTHER AND FOUND THE PC BOARD WAS DEFECTIVE. IT IS NOT KNOWN IF THE SWITCH DAMAGED THE PC BOARD. THIS IS NOT THE FIRST TIMSDR DXTA200601372Landing Gear · warning lightWHEN GEAR SELECTED DOWN GREEN LT MAIN AND RED UNLOCK LIGHTS WERE FLICKERING RECYCLED GEAR TWICE PROBLEM REMAINED EXECUTED GEAR WILL NOT EXTEND CHECKLIST PROBLEM REMAINED. GEAR BLOWN DOWN AND LANDED WITHOUT INCIDENT. ITEM IS UNDER INVESTIGATION.SDR DXTA200601367Position Switch · out of adjustAFTER TAKEOFF, GEAR RAISED WITH NORMAL INDICATIONS. AT 400FT WHEN FLAPS RAISED TO (0) DEGREE, GOT A STEADY HYD PRESS AND STAB MISCOMPARE LIGHT. AFTER RUNNING CHECKLIST, FLAPS WERE LOWERED TO 15 DEGREES RESULTING IN HYD PRESS AND STAB MISCOMPARE LIGHTS. ADJUSSDR DXTA200601365Landing Gear · warning lightREPEAT WRITE UP, WHEN GEAR EXTENDED LT MAIN NO GREEN AND RED UNLOCK REMAINED ON. CYCLED GEAR ONCE SAME SCENARIO FOLLOWED CHECKLIST AND BLEW GEAR DOWN, GOT FLICKERING LT MAIN GREEN AND FLICKERING UNLOCK LIGHT, LANDING UNEVENTFUL. ITEM IS UNDER INVESTIGATION.SDR CWQR2006010Fork · gougedDURING AN INSPECTION FOUND THE NOSE GEAR STEERING LOWER FORK ASSY (5542304-3) GOUGED. FURTHER INVESTIGATION FOUND THE FORK ASSY IS GOUGED ONLY DURING A MAINTENANCE GEAR RETRACTION TEST, WHEN THE RUDDER PEDALS ARE DEFLECTED FULL RT AND LT. REMOVED FORK ASSY, MESDR DXTA200601364Landing Gear · warning lightON FINAL APPROACH PUT LANDING GEAR DOWN LT MAIN GEAR LIGHT FLICKERED AND RED GEAR UNLOCK LIGHT FLICKERED, CYCLED GEAR DID NOT CURE. WENT AROUND CYCLED GEAR AGAIN GOT THREE GREEN AND LANDED. INSPECTED LT MAIN GEAR DOWNLOCK SWITCH AND WIRING WITH NO DISCREPANCSDR DXTA200601359Position Switch · contaminatedSHORTLY AFTER TAKEOFF POWER APPLIED NO TAKE OFF LIGHT ILLUMINATES AND AUARAL WARNING. AFTER CLEARING RUNWAY LIGHT GOES OUT. TROUBLESHOT SYSTEM. CLEANED LT AND RT SPEED BRAKE SWITCHES AND CONNECTORS, CHECKED OPERATION OF FLAP POS SWITCH, RT STAB SWITCH, ELEVSDR DXTA200601357Ahrs · defectiveON TAKEOFF ROLL COPILOT ATT FAIL AND HDG FAIL PFD ENUNCIATORS ILLUMINATED WITH CHECK PFD 2 ENUNCIATOR COULD NOT RESET. REMOVED FAULTY AHRS UNIT NR 2 S/N 1110 AND INSTALLED UNIT S/N 2020 REPAIRED BY FAA REPAIR STATION NR M31R0300 SYSTEM OPERATIONAL CHECKS GOODSDR CWQR2006009Cable Assy · damagedDURING A SCHEDULED MAINTENANCE VISIT BEFORE REPLACING A CABLE ASSEMBLY ON A THE CABLE TERMINAL END WAS FOUND TO HAVE BEEN DRILLED TO A DEPTH OF .3750-.5 INCH AT AN ANGLE AND DAMAGED THE THREADS. THIS CABLE ASSEMBLY WAS ORDERED FROM AND DOCUMENTED AS NEW.SDR DXTA200601346Position Switch · malfunctionedMASTER WARNING AND RT THRUST REVERSER ARM LIGHT ILLUMINATED IN FLIGHT. REMOVED AND REPLACED BOTH RT T/R STOW SWITCHES IAW MM 78-30-11. OPERATIONAL CHECKS GOOD.SDR DXTA200601345Clip · faultyDURING TAKEOFF ROLL (NO TAKEOFF) LIGHT ILLUMINATED AND WARNING HORN SOUNDED. TAKEOFF WAS ABORTED. DURING TROUBLESHOOTING NOTICED THAT EXTENDING THE SPEED BRAKES WHILE CONFIGURING FOR TAKEOFF CAUSED THE (NO TAKEOFF) LIGHT TO EXTINGUISH MOMENTARILY AND COME BACSDR DXTA200601334Wire Harness · failedANTI-SKID INOP AND MASTER CAUTION ANNUNCIATORS ILLUMINATED DURING INITIAL TAKEOFF ROLL. NORMAL DIFFERENTIAL BRAKE PRESSURE WAS LOST AND EMERGENCY BRAKING WAS USED TO STOP AIRPLANE. REMOVED AND REPLACED LT MAIN GEAR WIRE BUNDLE ASSY IAW 560XL WIRING MANUAL CHSDR DXTA200601333Fire Detector · malfunctionedAT APPROX FLIGHT LEVEL 1200, LEFT ENGINE FIRELIGHT CAME ON, THROTTLE WAS REDUCED TO IDLE, LIGHT CYCLED ON/OFF. 1ST BOTTLE WAS DISCHARGED AS PER CHECKLIST, LEFT FIRE LIGHT CONTINUED TO CYCLE ON/OFF. 2ND BOTTLE WAS DISCHARGED AS PER CHECKLIST, LIGHT EXTINGUISHSDR CA060425004Oil System · leakingDURING CRUISE, ENGINE OIL PRESSURE WAS SEEN TO FLUCTUATE ACCOMPANIED BY SMOKE AND ODOR IN THE CABIN AIR. ENGINE OIL PRESSURE SUBSEQUENTLY REDUCED TO ZERO AND THE ENGINE WAS SHUT DOWN IN FLIGHT. PWC WILL INVESTIGATE THE EVENT AND WILL ADVISE OF ROOT CAUSE, ONSDR DXTA200601325Engine · low pressureAFTER TAKEOFF AT CLIMB-OUT POWER DETENT, LT LOW OIL PRESSURE ANNUNCIATER ILLUMINATED. LOW PRESSURE WAS VERIFIED ON TAPE, DIGITS WERE RED AND PRESSURE WAS ZERO. REDUCED POWER AND PRESSURE REMAINED ZERO FOR ABOUT 10 SEC THEN RETURNED TO NOMAL. POST FLIGHT INS
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