Textron 560XL
Service difficulty reports · 3,806
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 DXTA2025052103571Bungee · defectiveCAPTAIN RUDDER PEDAL: DURING TAXI AND WHILE STATIONARY, WE GET A NOISE IN WHEN YOU MOVE RUDDER PEDALS BACK AND FORTH. YOU CAN HERE THE NOISE FROM THE OUTSIDE IN THE NOSE GEAR WELL. IT APPEARS TO BE COMING FROM THE DAMPNER CYLINDER. CORRECTIVE ACTION; VERIFIED SDR 3EJA20250519001Warning Light · multiple failSTAB MIS COMPARE ILLUMINATION DURING FLAP RETRACTION. NOSE GEAR UNLOCK RED LIGHT ILLUMINATION AFTER GEAR WERE FULLY RETRACTEDSDR DXTA2025052103548None · no discrepancyDAMAGE INSPECTION: SEVERE TURBULENCE WAS ENCOUNTER AT ALTITUDE. CW DAMAGE INSPECTION: DUE TO SEVERE TURBULENCE BEING ENCOUNTER AT ALTITUDE. IAW MM 05-50-00 NO DAMAGE NOTED AT THIS TIME.SDR DXTA2025051903539Wire · brokenEMERGENCY LIGHTING: REPEAT, FRONT HALF OF THE EMERGENCY LIGHTS WILL NOT TURN ON (TRIED: EMER LIGHTS ON, EMER LIGHTS ARM DC POWER OFF AND EMER LIGHTS ON PASS SAFETY ON) CORRECTIVE ACTION; REPAIRED BROKEN WIRING AND PERFORMED OPS CHECKS OF THE SYSTEM AND FOUND NSDR DXTA2025052103535Eec · defectiveAT 80 KNOTS, THE EEC L ANNUNCIATOR ILLUMINATED WITH A LEFT ENGINE REDUCTION OF THRUST. TAKE OFF WAS ABORTED. CORRECTIVE ACTION; REPLACED DEFECTIVE EEC REF. 5455B EMM 71-00-00. NO DEFECTS NOTED.SDR 3EJA20250517002Window · crackedLH FWD SIDE WINDOW SHATTERED IN FLIGHTSDR DXTA2025051903528Precatch · out of adjustMAIN DOOR: CREW LEFT AIRPLANE AND WENT INSIDE FBO. WHEN WE RETURNED, WE WERE UNABLE TO OPEN THE MAIN DOOR. THE HANDLE ACTUATES CORRECTLY WITH NO BINDING. CREW WAS FINALLY ABLE TO OPEN DOOR WITH BOTH PILOTS PUSHING ON THE DOOR AS WE CLOSED IT. WE THEN HAD SDR 2025FA0000359Deck Plate · corrodedFOUND CORROSION ON POTTY DECK LOWER SURFACE DURING 24MO INSPECTION. MEASURED, MAPPED, AND SUBMITTED POTTY DECK LOWER SURFACE CORROSION TO ENGINEERING FOR REPAIR DISPOSITION. REPAIR TOILET DECK SKIN AT LOWER SURFACE. PER: NETJETS RFTS-113845. FABRICATED AND INSSDR DXTA2025051903508Seal · leakingRIGHT ENG FIRE DETECTION LIGHT: CLIMBING OUT OF 11,000 FEET, GOT A RT ENG FIRE INDICATION. FLYING PILOT REDUCED THROTTLE TO APPROX 80 PERCENT AND LIGHT EXTINGUISHED APPROX 10 SECS LATER. RAN QRC & DIVERTED. ENG INDICATIONS WERE NORMAL THROUGHOUT. REMOVED LSDR 3EJA202505140002Indication Sys · illuminatedGEAR SELECTED UP, HEARD THE GEARS SECURE IN THE WHEEL WELLS; HOWEVER, RED GEAR UNLOCK LIGHT ILLUMINATED, NO GREEN.SDR DXTA2025051403447Brake · malfunctionedBRAKE PRESSURE LIGHT: ON LANDING AFTER APPLYING THE AIRCRAFT BRAKES THE LOW BRAKE PRESSURE AND ANTI SKID ANNUNCIATORS ILLUMINATED. USED THE PNEUMATIC EMER BRAKES TO STOP. THE POWER BRAKE CB DIDN'T TRIP. AFTER THE AIRCRAFT STOPPED THE BRAKE ANNUNCIATOR'S WENT OSDR 3EJA20250512001Engine · power lossLEVELED AT 410. RT ENGINE (WITH NO PRIOR INDICATION) ROLLED BACKSDR 3EJA20250509002Autopilot Sys · malfunctionedAT FRA, A/P WOULD NOT ENGAGE AND THE MESSAGE AP FAIL APPEARED. RESET AND ENGAGED THE AUTOPILOT TWICE, BUT IT FAILED IMMEDIATELY BOTH TIMES. THE AIRPLANE KEPT PITCHING UP AGGRESSIVELY, SO, MOVED THE TRIM ALL THE WAY FORWARD MANUALLY, BUT THAT DIDN’T HELP. REDUCSDR 3EJA20250508001Cabin Pressure · faultedT AT ABOUT 15000FT CABIN ALT LIGHT CAME ON WITH MASTER CAUTION AND MASTER WARNING. ALSO PAX OXYGEN CABIN MASKS DROPPED OUT.SDR 3EJA834JS050825Warning Light · no indicationNO TAKEOFF LIGHT ILLUMINATION ON TAKEOFF. AIRCRAFT WAS AT 50 KNOTS AND TAKEOFF WAS ABORTEDSDR DXTA2025051203378Cartridge · faultedFUEL CROSSFEED HARDWARE: CROSSFEEDING LEFT TO RIGHT, BOTH FUEL BOOST L AND R ILLUMINATED ALONG WITH BOTH LO FUEL PRESS L AND R. CAME OUT OF CROSSFEED AND BOTH LO PRESS L AND R LIGHTS EXTINGUISHED. BOTH L AND R FUEL BOOST REMAINED ILLUMINATED. FOLLOWED THE CSDR DXTA2025050603378Switch · out of positionFUEL CROSSFEED HARDWARE: CROSSFEEDING LEFT TO RIGHT, BOTH FUEL BOOST L AND R ILLUMINATED ALONG WITH BOTH LO FUEL PRESS L AND R. CAME OUT OF CROSSFEED AND BOTH LO PRESS L AND R LIGHTS EXTINGUISHED. BOTH L AND R FUEL BOOST REMAINED ILLUMINATED. FOLLOWED THE CSDR 3EJA20250509001Warning Light · illuminatedAFTER WHEEL OFF GROUND ON TAKE OFF, WHEN GEAR HANDLE WAS UP THE GEAR UNLOCKED LIGHT REMAINED ILLUMINATED.SDR 3EJA20250507002Landing Gear · warning messageGEAR UNLOCK LIGHT REMAINED ILLUMINATED AFTER GEAR UP SELECTED. HYD PRESS LIGHT AND MASTER CAUTION ILLUMINATED FOLLOWED BY STAB MIS COMP LIGHT STEADY ONSDR DXTA2025050903377Bellcrank · defectiveMAIN DOOR: MAIN CABIN DOOR EXTREMELY DIFFICULT TO OPEN. REQUIRED BOTH CREW MEMBERS PUSHING WITH THEIR FEET. IT DOES NOT APPEAR THAT EITHER SEAL WAS INFLATED. CORRECTIVE ACTION; REPLACED FITTING ASSEMBLY IN DOOR PIN BELLCRANK IAW SUPPORT BRACKET ASSY AND DETAILSDR DXTA2025050603377Door · bindingMAIN DOOR: MAIN CABIN DOOR EXTREMELY DIFFICULT TO OPEN. REQUIRED BOTH CREW MEMBERS PUSHING WITH THEIR FEET. IT DOES NOT APPEAR THAT EITHER SEAL WAS INFLATED.SDR DXTA2025050703357Counterbalance · faultedMAIN DOOR: MAIN ENTRANCE DOOR IS VERY HARD/HEAVY TO CLOSE THE LAST 2 FEET OF MOVEMENT. WHEN OPENING DOOR, IT POPS OPEN ABOUT 2 FEET AND PULLED CREWMEMBER INTO DOOR. CORRECTIVE ACTION: OPENED AND DOSED DOOR MULTIPLE TIMES, FOUND DOOR COUNTER BALANCE ASSIST NOT SDR DXTA2025050403357Door · malfunctionedMAIN DOOR: MAIN ENTRANCE DOOR IS VERY HARD/HEAVY TO CLOSE THE LAST 2 FEET OF MOVEMENT. WHEN OPENING DOOR, IT POPS OPEN ABOUT 2 FEET AND PULLED CREWMEMBER INTO DOOR.SDR DXTA2025050303336Rheostat · failedCOCKPIT FLOOD LIGHT: WITH APU RUNNING TRIED TO DIM THE FLOOD LIGHTS WITH THE RHEOSTAT KNOB. RESULTED IN A BRIGHT FLASH BEHIND THE KNOB, BURNING ODOR, AND THE CIRCUIT BREAKER POPPING CORRECTIVE ACTION: GAINED ACCESS TO FLOOD LIGHT RHEOSTAT BY REMOVING SWITCH PASDR DXTA2025050303344Light · inoperativeEMERG EXIT SIGN OVER SEAT 7 DOES NOT ILLUMINATE W/ EMERG LIGHT SWITCH ON CORRECTIVE ACTION: REMOVED LIGHT PN:9919040-6 SN:118004048 IAW 560XL MM 33-20-04 INSTALLED NEW LIGHT PN:99190404-23 SN:202200000034039 IAW 560XL MM 33-20-04 OPS CHECK GOOD VERIFIED INSTALSDR DXTA2025050203319Light · inoperativeFLOOR EMERG EXIT LIGHT: FORWARD STRIP OF AISLE EMERGENCY LIGHTS ON LEFT SIDE OF AIRCRAFT ARE INOP. ALL OTHER EMERGENCY LIGHTS ARE OPERATING NORMAL. CORRECTIVE ACTION: REMOVED L/H FWD EMERGENCY/ PATH LIGHT STRIP FROM AIRCRAFT P/N: 9919040-9 S/N: 121003902. INSTSDR DXTA2025043003254Yoke · multiple failCAPTAIN CONTROL YOKE MAKES GRINDING NOISE WHEN ROLLED LT & RT. CAN ALSO FEEL BINDING/GRINDING. RIGHT SIDE IS SMOOTH BUT CAN STILL HEAR THE GRINDING. REMOVED DAMAGED SHAFT & INSTALLED NEW SHAFT IAW AMM 27-10 04 WITH NO DEFECTS NOTED. REMOVED DAMAGED DRUM ASSESDR 3EJA20250424001Lamp · failedAFTER THE GEAR WAS EXTENDED THE CREW SAW ONLY 2/3 GREEN LIGHTS INDICATING THAT THE NOSE GEAR WAS NOT EXTENDEDSDR 9JLA20250425002Servo · failed"AUTO PILOT FAIL" CAS MESSAGE REMAINS ILLUMINATED AFTER PREFLIGHT TESTSDR DXTA2025042403161Switch · failedWHEN SELECTING FLAPS TO 15 ON APPROACH TO LANDING RECEIVED A STAB MIS COMP CAUTION. AIRSPEED WAS AT 190 KTS. RAN QRH AND IT DID NOT CLEAR. CORRECTIVE ACTION: POWERED UP AIRCRAFT STAB MISCOMPARE STILL THERE. RESET CB AND RAN ENGINES BUT LIGHT REMAINS ON. SLAVEDSDR 3EJA20250414002Gauge · faultedL FUEL GAUGE ANNUNCIATOR WARNING AND THE L FUEL GAUGE WAS READING ZERO.SDR DXTA2025041703057Powerpack · defectiveBRAKE PRESSURE LIGHT: WHILE HOLDING SHORT OF RUNWAY AMBER ANTI SKID ANNUCIATOR ILLUMINATED AND POWER BRAKE CIRCUIT BREAKER TRIPPED. CALLLED MAINTENACE DID ONE RESET AND TOLD TO NOT TAKEOFF . BACK TAXIING RUNWAY 10 LOST POWER BRAKES AND LOW BRAKE PRESS LIGHT SDR DXTA2025041003031Solenoid · faultedAFTER CLOSING AND SECURING MAIN CABIN DOOR, THE CABIN DOOR ANNUNCIATOR LIGHT REMAINED ILLUMINATED. AFTER A COUPLE OF UNSUCCESFUL ATTEMPTS TO PROPERLY SECURE THE DOOR BY MANUALLY CLOSING THE VENT DOOR, THE COCKPIT ANNUNCIATOR REMAINED ILLUMINATED AND ALSO THE RSDR DXTA2025040803003Handle · malfunctionedMAIN DOOR HANDLE: MAIN ENTRANCE DOOR EXTERIOR HANDLE WILL NOT STAY STOWED. IT DOES NOT SPRING STOWED. CORRECTIVE ACTION: REMOVED EXTERIOR DOOR HANDLE AND REPLACED BROKEN DOOR SPRING WITH NEW UNIT P/N: SL5204-2 AND REPLACED COTTER PIN WITH NEW UNIT P/N: MS24665SDR DXTA2025040432920Lamp · inoperativeCABIN EMERG LIGHT: SEAT 7 READING LIGHT (PART OF EMER LIGHTING SYSTEM) IS INOP. ATTEMPTED TO MANUALLY TURN READING LIGHT ON WITHOUT SUCCESS. CORRECTIVE ACTION: REMOVED AND REPLACED LED LAMP WITH NEW IAW CE560XL AMM 33-20-02. OPS CHECK GOOD PER CE560XL AMM 33-5SDR DXTA2025040102856Shaft · failedMAIN DOOR PRECATCH LEVER: WHILE OPERATING PRE-CATCH LEVER, RED HANDLE FELL OFF. RED HANDLE LEFT IN SEAT 10. CORRECTIVE ACTION: REMOVED AND REPLACED PRECATCH SHAFT PN: 6211315-31 AND HANDLE PN: 6211315-38 REF CE560XLS AMM 52-10-01. PERFORMED OPERATIONAL CHECKSSDR DXTA2025032802812Solenoid · faultyDURING DOOR CLOSURE, BOTH LIGHTS GO OUT BRIEFLY. WITHIN A FEW SECONDS THE "CABIN DOOR" LIGHT COMES BACK ON. IT BAS BEEN INTERMITTENT ALL WEEK. IT WOULD GO OUT AFTER OPENING AND CLOSING. THIS TIME WE TRIED NUMEROUS TIMES, INCLUDING MANUALLY TRYING TO PUSH THE SDR 2025FA0000203Strake · corrodedLH AND RH STRAKES HAVE SEVERAL AREAS OF CORROSION ON UPPER AND LOWER SURFACES. PERFORMED 4 EACH DOUBLER REPAIRS TO LH STRAKE AND PERFORMED 6 EACH DOUBLER REPAIRS TO RH STRAKE. ALL WORK WAS ACCOMPLISHED IN ACCORDANCE WITH EO NO: C56-53-0001 TITLED: MINOR REPAIRSDR DXTA2025032602798Buss Bar · corrodedWHEN GEAR WAS SELCTED DOWN THE ANTI-SKID ANNUNCIATOR ILLUMINATED AND ABOUT 60 TO 90 SECONDS LATER POWER BRAKE CIRCUIT BREAKER TRIPPED. RESET THE CIRCUIT BREAKER & WITHIN 60/90 SECONDS THE POWER BRAKE CIRCUIT BREAKER TRIPPED AGAIN. TROUBLESHOOTING REVEALED CSDR DXTA2025032502788Control Cable · out of adjustHIGH VIBE IN YOKE AND PEDALS STARTING AT 250KTS. INCREASED INTENSITY AS SPEED INCREASED. CHECKED ELEVATOR AFT CONTROL CABLE TENSIONS, TENSIONS WERE WITHIN LIMITS IAW MM 27-31-00. CHECKED RUDDER CABLE TENSIONS, ALL TENSIONS WERE WITHIN LIMIT IAW MM 27-20-00. SDR W9BA2025032200000Brake Sys · faultedWE HAD A REPEAT OCCOURANCE OF THE BRAKE SYSTEM NOT WORKING PROPERLY. THE CREW LANDED AND THE BRAKES WORKED AS INTENDED BUT AFTER STOPPING THE BRAKES STOPPED WORKING (HYDRAULIC PUMP TURNED OFF THAT SUPPLIES PRESSURE TO THE BRAKES). THE CREW USED THE BACKUP BRAKSDR 2025FA0000201Strake · corrodedLH STRAKE TRAILING EDGE WEDGE FITTINGSDR U5QA202503200149Pitot Head · obstructedN643TX-250320-1 FO PFD INSTRUMENTS FROZE AT FL400. AIRSPEED INDICATIONS INCREASED TO 450KTS (NOT ACTUAL AIRSPEED). WITH ASSICIATED AURAL WARNING. MX C/A: DRAINED ALL STATIC PORTS AND PURGED PITOT/STATIC SYSTEM, OPS AND LEAK CHECKS NORMAL AT 40000 FT AND 200 KSDR 3EJA202503210001Condenser · dirtyDURING FINAL APPROACH RECEIVED SMOKE DETECTOR LIGHT FOLLOWED BY SMOKE APPEARING OUT OF CABIN AND COCKPIT VENTS. CLEANED WATER SEPARATOR AND RAN ENGINES AND APU AND COULD NOT DUPLICATE SMOKE N CABIN OR COCKPIT.SDR DXTA2025032102744Solenoid Valve · defectiveMAIN DOOR SECONDARY SEAL: WITH APU ON AND BLEED AIR OFF THE ACOUSTIC SEAL IN DOOR FRAME INTERFERES WITH OPENING AND CLOSING MAIN CABIN DOOR. BINDING BETWEEN THE DOOR HARDWARE AND THE INFLATED SEAL. THE SEAL APPEARS DAMAGED IN ALL OF THE AREAS WHERE THERE IS BSDR 3EJA2025031800005Unknown · smokeDURING FINAL APPROACH RECEIVED SMOKE DETECTOR LIGHT FOLLOWED BY SMOKE APPEARING OUT OF CABIN AND COCKPIT VENTSSDR DXTA2025031902735None · no discrepancyON DESCENT THROUGH 17000FT AT 295 KIAS, WE ENCOUNTERED SEVERE TURBULENCE FOR APPROXIMATELY 10SECONDS. WE HAD THE FLAPS AND GEAR UP, CLEAN CONFIGURATION, BUT THE AIRCRAFT ACCELERATED TO 310KIAS FOR THE DURATION OF THE EVENT. CORRECTIVE ACTION; ACCOMPLISHED 560XSDR DXTA2025032002713Servo Valve · stalledLEFT ENGINE ENGINE COMPRESSOR STALL: UPON REACHING FL410 AND BEGINNING TO REDUCE THRUST FOR CRUISE, WE EXPERIENCED THREE DISTINCT COMPRESSOR STALLS WITH AIRCRAFT YAW AND A NOTICEABLE DROP IN N1 INDICATION ON THE NUMBER ONE ENGINE. CORRECTIVE ACTION; SWAPPED EESDR DXTA2025032002719Windshield · failedCAPTAIN COCKPIT WINDOW: CLIMBING THROUGH 30,000' PILOT SIDE FRONT WINDSHIELD SHATTERED. IT APPEARS TO BE THE OUTER PANE. CORRECTIVE ACTION; REPLACED FAILED PILOTS SIDE WINDSHIELD IAW CE560XLS MM 56-11-00. OPS AND LEAK CHECK GOOD.SDR DXTA2025031902710Windshield · crackedFIRST OFFICER COCKPIT WINDOW CRACKED COMING INTO EGE. REMOVED RH COCKPIT WINDOW DUE TO CRACKED GLASS DAMAGE. REMOVED COCKPIT WINDOW INSTALLED REPAIRED COCKPIT WINDOW. APPLIED FILLET SEAL AND WAITED FOR PROPER CURE. PERFORMED PRESSURIZATION SYSTEM OPS CHECK.
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