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 2026FA0000425Skin · corrodedCORROSION, FORWARD CABIN, RT LOWER SKIN, BFS 125.80 TO 157.00.SDR 3EJA20260525003Control Unit · inoperativeRIGHT ENGINE FIRE LIGHT ILLUMINATE.SDR 3EJA20260525002Anti-Skid Sys · unserviceableANTI-SKID LIGHT FLASHED JUST BEFORE LANDING, NO MAIN BRAKES, USED EMERGENCY BRAKE TO STOP.SDR DXTA2026051808088Brake Sys · faultedDURING LANDING AT APPROX 80KTS, ANTISKID INOP ANNUNCIATION ILLUMINATED. CLEARED & CAME BACK ON. BRAKES WERE INOP DURING BRIEF TAXI OFF OF RUNWAY. THE BRAKES DID GRAB SLIGHTLY JUST BEFORE ACFT CAME TO A FULL STOP. ON POST FLT, ANTI SKID WIRING HARNESS ON RSDR DXTA2026051808079Relay · faultyON FINAL APPROACH INTO CANADA WE HAD THE POWER BRAKE CIRCUIT BREAKER POP AND THE ANTI SKID INOP ANNUNCIATOR ILLUMINATE. WE WENT AROUND AND BROUGHT THE GEAR UP. FOLLOWED BY THE CHECKLIST. WE RESET THE POWER BRAKE CIRCUIT BREAKER AND THE ANNUNCIATOR AND CAUTIOSDR 2026FA0000330Tire · failedAIRCRAFT SUSTAINED DAMAGE FROM LH MAIN LANDING GEAR TIRE TREAD SEPARATION DURING TAKEOFF. AIRCRAFT COMPLETED TAKEOFF, RETURNED TO BASE AND LANDED WITH NO FURTHER INCIDENT. TIRE DID NOT LOSE TIRE PRESSURE. AIRCRAFT TAXIED BACK TO RAMP AS NORMAL.SDR DXTA2026050607912Door Seal · damagedAT FL390 A LOUD HISSING/ WHISTLE SOUND WAS HEARD FROM MAIN CABIN DOOR. IT COULD BE HEARD BY BOTH CREW & PAX. UPON INVESTIGATING NOISE, SOME AIR WAS FELT COMING IN FROM RT FWD CORNER OF DOOR. NO DOOR ANNUNCIATORS OR PRESSURIZATION ISSUES. NOISE APPEARED TO DECRSDR DXTA2026050507920Door Seal · cutAT ALTITUDES ABOVE 16,500' AN ULTRA-HIGH PIERCING FREQUENCY SOUND CAN BE HEARD IN THE CABIN. TOUGH TO PINPOINT, BUT SEEMS TO COME FROM AREA AROUND MAIN CABIN DOOR. PRESSURIZATION SYSTEM SEEMED TO BE HOLDING UP. IN DESCENT FROM HIGH ALTITUDE THE RATE CONTROL FSDR 3EJA202605120226Seal · failedCLIMBING THROUGH ABOUT 8000 FEET, LH ENGINE FIRE LIGHT ILLUMINATION, FOLLOWED BY THE AURAL WARNING. BOTH WENT AWAY AFTER 30 TO 45 SECONDS. INSPECTED ENGINE AND FOUND ALL THREE BLEED AIR DUCT WIGGINS FITTING SEALS BLOWN OUT.SDR 2026FA0000332Bottle · crackedREMOVED NITROGEN BOTTLE FOR EMERGENCY BRAKES AND LANDING GEAR FROM AIRCRAFT AND INSTALLED OVERHAULED BOTTLE FROM PACIFIC SCIENTIFIC COMPANY D/B/A MEGGITT CUSTOMER SERVICES AND SUPPORT. SERVICED BOTTLE TO 1750 PSI. THE NEXT MORNING BOTTLE WAS DOWN 500 PSI. LESDR DXTA2026042707771Door · lack of lubeMAIN CABIN DOOR REQUIRES EXCESSIVE FORCE TO OPEN AND CLOSE DOOR HANDLE FROM INSIDE THE CABIN. UPON ARRIVAL AT AIRCRAFT, CONFIRMED CABIN DOOR IS SLIGHTLY HARDER TO OPEN THAN USUAL. WE NOTED SAND AND DEBRIS ON THE LOCKING PINS. WE REMOVED THE DOOR TRIM AND INSPSDR 2026FA0000295Skin Panel · corrodedFOUND SEVERAL SPOT OF CORROSION ON FWD FUSELAGE RH LOWER SECTION JUST FWD PANEL 153AC. BLENDED AND REMOVED CORROSION FROM FWD FUSELAGE RH LOWER SECTION JUST FWD PANEL 153AC. BLENDED AREA ON RH SIDE OF FUSELAGE WAS BEYOND LIMITS AND SUBMITTED TO AQRD. COMPLIED SDR 2026FA0000292Vertical Beam · corrodedDURING EMPENNAGE COVE INSP, FOUND VERTICAL AFT SPAR HAS CORROSION ON RH ANGLE ABOVE TOP RUDDER HINGE. BLENDED AND REMOVED ALL VISIBLE SIGNS OF CORROSION ON AFT SPAR RH ANGLE ABOVE TOP RUDDER HINGE. BLENDED AREA WAS BEYOND ALLOWABLE LIMITS AND WAS SUBMITTED TO SDR DXTA2026042307723Support Strut · damagedWHEN OPENING OR CLOSING THE MAIN CABIN DOOR A MECHANICAL GRINDING SOUND IS HEARD AND THE DOOR WILL STOP MID TRAVEL. SOME ADDITIONAL FORCE IS REQUIRED TO MOVE THE DOOR PAST THIS POINT. TECHS REMOVED THE DAMAGED FORWARD SUPPORT STRUT AND INSTALLED RECEIVED NEWSDR DXTA2026042107723Door · bindingWHEN OPENING OR CLOSING THE MAIN CABIN DOOR A MECHANICAL GRINDING SOUND IS HEARD AND THE DOOR WILL STOP MID TRAVEL. SOME ADDITIONAL FORCE IS REQUIRED TO MOVE THE DOOR PAST THIS POINT.SDR 3EJA835JS041226Valve · failedON TAKEOFF CLIMB PRESS FLUCTUATIONS UP TO 4300 ON THE RATE AND BACK DOWN AND BACK UP AGIN ACCOMPANIED WITH A ACM OVERHEAT: REMOVED AND REPLACED LH BILEVEL VALVE IAW AMM 21-11-00. OPS & LEAK CHECKED GOOD.SDR 2026FA0000267Window · crackedDURING CRUISE FLIGHT, THE PILOT OBSERVED DELAMINATION BEGINNING ON THE LEFT-HAND COCKPIT SIDE WINDOW. THE DELAMINATION PROGRESSED AT A RAPID RATE, AND NO MASTER WARNING OR ANNUNCIATION WAS DISPLAYED ON THE INSTRUMENT PANEL. THE DELAMINATION CONTINUED UNTIL THESDR 3EJA202607130003Bracket · bentON TAKEOFF AFTER RAISING THE GEAR THE NOSE GEAR DIDN'T RETRACT. NOSE GEAR LIGHT WAS ON AND THE UNLOCK LIGHT ALSO WAS ON. REMOVED THE DAMAGED LH AND RH NOSE UPLOCK BRACKETS AND INSTALLED NEW BRACKETS REMOVED THE DAMAGED NOSE UPLOCK SWITCH AND INSTALLED A NEWSDR 3EJA202607130004Powerpack · failedDURING TAKE OFF ROLL JUST AFTER 80 KT CHECKS MASTER CAUTION / ANTISKID INOP ANNUNCIATION ILLUMINATED. REMOVED FAILED HYDRAULIC PACK ASSY AND INSTALLED NEW HYDRAULIC POWER PACK ASSY. BRAKE BLEEDING C/W WITH NO DISCREPANCIES NOTED AT THIS TIME. OPS AND LEAK CHSDR U5QA202603240169Warning Message · false activationCLIMBING THROUGH 12,000FT THE CABIN ALT WARNING ANNUNCIATOR CAME ON. MEMORY ITEMS WERE CARRIED OUT AND AN EMERGENCY DECLARED WITH A RETURN TO KPBI. COMPLIED WITH PRESSURIZATION OPERATIONAL CHECKS, CONFIRMED OPERATIONAL CHECKS WERE GOOD IN AIR MODE AND NO FAULSDR DXTA2026032407355Door · noiseEXTREMELY LOUD NOISE IN THE LAV IN CUISE AND DECENT COMING FROM THE EMERGANCY EXIT. SOUNDS LIKE THE NOISE FROM THE ENGINE FAN BLADE ALMOST LIKE THE SOUND PROOFING IS MISSING. NO VIBRATION OR ENGINE IRREGLARITIES NOTED. AIRCRAFT PRESSURIZED. UNABLE TO DUPLICSDR 2026FA0000202Skin · corrodedLOWER TAILCONE SKIN CORROSION. COMPLIED WITH NETJETS AQRD ERO-988732 REV.IR, DATED MAR.19,2026. N611QS LOWER TAILCONE SKIN CORROSION.SDR 3EJA2026050100826Hose · failedTHE YAW DAMPER AND AUTOPILOT DISCONNECTED. WE HAD A YELLOW IAS MISCOMPARE INDICATION. R&R #2 PITOT HOSE, R&R LH/RH STATIC DRAIN PACKINGSSDR 3EJA2026050100726Actuator · looseLANDING GEAR WILL NOT RETRACT AFTER TAKEOFF ( RED GEAR UNLOCK LIGHT REMAIN ON) FOLLOWED WITH QRH PROBLEM REMAINED. RETURNED BACK TO RBD AIRPORT SAFELY.//////DISCOVERED LH MAIN LANDING GEAR ACTUATOR JAM NUT TO BE LOOSE PERFORMED ROD ENG ADJUSTMENT AND SECURED JSDR 3EJA202605010002Bracket · bentIMMEDIATELY FOLLOWING TAKEOFF FROM KSYR, THE LANDING GEAR HANDLE WAS SELECTED UP. THE LANDING GEAR FAILED TO RETRACT, AND THE RED GEAR UNLOCKED LIGHT REMAINED ILLUMINATED. R&R NLG BRACKET ASSY WITH NEW BRACKET AND ADJUSTED AND SECURED LH MLG ACTUATOR LOCK NUSDR DXTA2026031607239Controller · defectiveON TAKEOFF WE SELECTED GEAR UP AND THE LANDING GEAR WOULD NOT RETRACT . THEN THE GEAR HANDLE WOULD NOT GO BACK TO THE GEAR DOWN POSITION . WE RAN THE CHECKLIST FOR THE GEAR WILL NOT RETRACT- WHICH DID NOT COMPLETELY APPLY IN THIS SITUATION- AND SUBSEQUENTLY WESDR 2026FA0000171Skin · corrodedRH WINGTIP SKIN UNDER OTBD STATIC WICK BASE IS HEAVILY CORRODED. COMPLIED WITH NETJETS RFTS-116596 REV.0 TITLE: N678QS (560-5616) WING TIP STATIC WICK BASE CORROSION DATED 11MAR26. THIS IS A PERMANENT MINOR REPAIR.SDR 2026FA0000170Deck Plate · corrodedPOTTY DECK CORRODED. REPAIRED POTTY DECK PER NETJETS RFTS-116581 REV.0 TITLE: N678QS (560-5616) TOILET DECK SKIN CORROSION DATED 10MAR26. THIS IS A PERMANENT MINOR REPAIR.SDR DXTA2026030607131G Switch · trippedEMERGENCY LIGHTS STAY ON WHEN EMERGENCY LIGHTING SWITCH PLACED IN THE ARMED POSITION. RECYCLED POWER ON AIRCRAFT WITH SAME RESULTS. ACCESSED AFT EMERGENCY LIGHTING BATTERY PACK, REMOVED ACCESS PANEL LOCATED IN AFT L/H SIDE CLOSET, FOUND G SWITCH TRIGGERED ONSDR 2026F00023Control Handle · faultedCREW REPORTED WHEN THE GEAR UP THE GEAR DIDN'T RETRACT AND ALL THREE GREEN REMAINED. PLACE GEAR HANDLE IN THE DOWN POSITION AND RETURN TO DEPARTURE AIRPORT OF KCHS WITHOUT INCIDENT.SDR 2026FA0000160Tire · damagedON TAKEOFF JUST AFTER ROTATION, PILOT REPORTED SIGNIFICANT VIBRATION FROM LEFT WING. PILOT TAPPED BRAKES AND VIBRATION STOPPED AND PILOT ASSUMED BLOWN TIRE ON LH WHEEL. UPON LANDING IT WAS NOTED THAT THE TIRE WAS STILL INFLATED BUT 3/4 OF THE TREAD IN BETWEESDR 3EJA868JS030326Pressure Switch · failedON THE TAKEOFF ROLL PRIOR TO 80, THE R LO FUEL PRESS ILLUMINATED FOLLOWED IMMEDIATELY BY R FUEL BOOST LIGHT.SDR DXTA2026030307075Door · bindingWHEN OPENING OR CLOSING THE MAIN CABIN DOOR YOU CAN HEAR AND PHYSICALLY FEEL THAT SOMETHING IS BINDING. IT HAPPENS WHEN YOU OPEN THE DOOR IS ABOUT 3/4 OPEN AS WELL AS ALMOST CLOSED VERIFIED PROPER TENSIONS OF PAX DOOR COUNTERBALANCE FWD AND AFT CABLES PER MSDR DXTA2026030307085Light · inoperativeA SEGMENT OF THE FLOOR EMERGENCY LIGHTING IS INOPERATIVE BELOW SEAT THREE. DURING T/S GAINED ACCESS TO THE LT AISLE EMERGENCY LIGHT HAD FEW LED LIGHT WERE OUT. REMOVED INOP EMERGENCY LIGHT AND INSTALLED A NEW LED LIGHT ASSY. OPS CHECKED GOOD. REF AMM 33-50SDR DXTA2026022607017Valve · faultyAFTER FLIGHT WITH APU ON IT TAKES UP TO 30 SECONDS FOR SEAL TO DEFLATE ENOUGH TO ALLOW OPENING OF THE MAIN CABIN DOOR. SUBSEQUENTLY AFTER FLIGHT WITH APU ON IT TAKES UP TO 10 SECONDS FOR SEAL TO DEFLATE ENOUGH TO OPEN THE MAIN CABIN DOOR. REMOVED FAILED DEFLASDR FKEA202602260001Brake · draggingHIGH SPEED REJECTED TAKE OFF IN APF, LOSS OF DIRECTIONAL CONTROL AS AIRCRAFT ACCELERATED TO V1 DUE TO A DRAGGING LEFT MAIN MOUNT. DRAG DUE TO EITHER A HUB/BEARING FAILURE OR BRAKING SYSTEM FAILURE ALLOWING LEFT BRAKE TO STICK. THE BRAKE WAS REMOVED AND FOUNDSDR FKEA202602230001Turbine Case · crackedCREW AND PASSENGERS NOTICED THE SMELL OF EXHAUST AFTER THE APU WAS STARTED ON THE DECENT FOR LANDING. MAINTENANCE WAS CALLED TO TROUBLESHOOT THE CAUSE AFTER LANDING. ON INSPECTION, THEY FOUND THE APU TURBINE HOUSING HAD A CRACK IN IT AT ABOUT THE 5 O'CLOCK POSSDR 3EJA202603250004Acm · false indicationDURING TAKEOFF AT 100 FEET ACM OVERHEAT LIGHT ILLUMINATED ALONG WITH AN ODOR OF PLASTIC MELTING. TROUBLE SHOT AND COULD NOT DUPLICATE.SDR DXTA2026021706916Lever · looseMAIN DOOR PRECATCH LEVER IS EXTREMELY LOOSE. INSPECTED MAIN DOOR PRECATCH SYSTEM FOUND NUT THAT SECURE LEVER LOOSE. TIGHTEN NUT, OPS CHECK OF PRECATCH SYSTEM OK I/A/W CE-560XLS AMM 52-10-01.SDR DXTA2026021606905Sign · inoperativeEMERGENCY EXIT SIGN LIGHT ON FRONT OF LAV IS INOP CORRECTIVE ACTION: REMOVED OLD LAV EXIT LIGHT AND INSTALLED A NEW EXIT LIGHT. FUNCTION TEST IS GOOD AT THIS TIME. WORK PERFORMED IAW AMM 33-50-02.SDR 2026FA0000129Bulb · burned outWHEN AIRCRAFT BEGAN ITS FINAL DECENT AS GEAR WAS SELECTED DOWN GEAR BEGAN MOVEMENT AND AT END OF CYCLE LH GEAR DID NOT SHOW DOWN AND LOCKED. CREW DECLARDED AN EMERGENCY AND PROCEEDED WITH A NORMAL LANDING . UPON INSPECTION IT WAS NOTED THAT BOTH INDICATOR BULBSDR DXTA2026021306862Battery Pack · defectiveTHE FRONT EMERGENCY BATTERY PACK IS DEAD. WITH BATTERY SWITCH ON AND EMER LIGHT SWITCH ON, ALL EMERGENCY LIGHTS CHECK NORMAL. TURNING THE BATTERY SWITCH TO OFF, THE FRONT EMERGENCY LIGHTS DO NOT ILLUMINATE. T2PL6D00DP743- REMOVED FRONT EMERGENCY BATTERY PACK SDR 3EJA202603250006Bracket · bentAFTER TAKEOFF WITH THE GEAR HANDLE SELECTED IN UP POSITION THE GEAR UNLOCK LIGHT REMAINS ILLUMINATED. FOUND NOSE GEAR FORK MOUNTED UPLOCK ROLLER BRACKETS BENT DOWN OVER 1/16 OF AN INCH CAUSING IMPROPER TOO LITTLE CONTACT TO THE NOSE UPLOCK SWITCH, R & R BRACSDR DRFA2026021000802Door Seal · leakingDURING DEPARTURE FROM TUCSON INTERNATIONAL AIRPORT, (KTUS) IN N567MC FEB 8, 2026 AT 0900 LOCAL TIME, WHILE CLIMBING THROUGH APPROXIMATELY 23,000 FEET MSL, A LOUD AND ABNORMAL WHISTLING NOISE WAS NOTED FROM THE MAIN CABIN DOOR SEAL AREA. AIRCRAFT PRESSURIZATIOSDR 3EJA202603250005Uplock Switch · failedGEAR UNLOCK LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. R & R LH MLG UPLOCK SWITCHSDR 3EJA202603250003Control Valve · failedTHE GEAR UNLOCK LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. REMOVED LANDING GEAR CONTROL VALVE P/N 71839-1 S/N 0110 AND INSTALLED OVERHAULED LANDING GEAR CONTROL VALVE P/N 71839-1 S/N 0111,SDR 3EJA202603250002Switch · dirtyON DEPARTURE AT 2000 FEET T/R LIGHT ARM, AND UNLOCKED CAME ON, WITH ASSOCIATED HYDRAULIC PRESSURE CAS MESSAGE. CLEANED AND INSPECTED TR SWITCHES, FUNCTION CHECK, NDFSDR DXTA2026020906803Door · bindingMAIN ENTRANCE DOOR, HARD TO MOVE HANDLE TO DOOR CLOSED, LOCK, AND ALSO HARD TO MOVE THE HANDLE TO OPEN DOOR. WITH DOOR OPEN THE HANDLE MOVES NICE AND EASILY LIKE IT SHOULD. BUT WITH DOOR CLOSED HANDLE IS VERY HARD TO MOVE. WE HAD TO PUT OUR BODY WEIGHT INTO ISDR DXTA2026020606796Gauge · out of positionMAIN CABIN DOOR SIGHT GAUGE INDICATOR: WITH THE DOOR FULLY CLOSED, UNABLE TO VERIFY THE GREEN CONFIRMATION FLAG. THIS IS THE SIGHT GUAGE BELOW THE DOOR HANDLE. IN ADDITION, WHILST OPENING/CLOSING MAIN CABIN DOOR, AT MID POINT UP/DOWN MOTION, THERE IS SUBSTANTSDR DXTA2026020306745Light · inoperativeEMERGENCY EGRESS LIGHTS REMAIN ON THE RIGHT SIDE OF THE FUSELAGE WITH THE BATTERY OFF, PASSENGER SAFETY OFF AND THE EMERGENCY LIGHT SWITCH OFF. INSIDE THE CABIN, TWO EXIT LIGHTS REMAIN ON IN THE REAR OF THE CABIN AND ONE RIGHT SIDE AISLE. LIGHT STAYS ILLUMINAT
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