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 W9FA20120418001Bearing · displacedNR 2 MAIN OLEO STRUT LOWER BEARING DISPLACED FROM HOUSING.SDR DXTA2012041604948Indication Sys · malfunctionedAFTER GEAR SELECTED UP, GEAR UNSAFE LIGHT AND GREEN NOSE GEAR DOWN LIGHT STAYED ON AN EXTRA 3 TO 5 SECONDS BEFORE EVENTUALLY EXTINGUISHING. PRIOR TO THE LIGHTS GOING OUT, AN UNUSUAL NOISE WAS HEARD FROM NOSE GEAR. GEAR SELECTED DOWN FOR LANDING NO ABNORMALISDR CWQR20120412029Hinge Bracket · crackedDURING A SCHEDULED MX, FOUND ON THE LT ELEVATOR HINGE BRACKET CRACKED ON THE LOWER FLANGE. REMOVED THE BRACKET ASSY AND FOUND THE UPPER FLANGE WAS CRACKED USUING EDDY CURRENT INSPECTION.SDR CWQR20120412028Hinge Bracket · crackedDURING A SCHEDULED MX, FOUND THE RT ELEVATOR HINGE BRACKET CRACKED ON THE LOWER FLANGE. REMOVED THE BRACKET ASSY AND FOUND THE UPPER FLANGE WAS CRACKED USING EDDY CURRENT INSPECTION.SDR DXTA2012082105100Skin · crackedTAILCONE SKIN CRACK DAMAGED AT APU HEAT SHIELD ATTACHMENTS. COMPLETED MFG REPAIR DEFINITION ATA53/03RD.SDR CWQR20120410027Support Channel · crackedDURING A SCHEDULED INSPECTION, FOUND THE FWD CARGO DOOR HINGE SUPPORT CHANNEL CRACKED IN SEVERAL PLACES. THIS ACFT HAD SB560XL-52-13 INSTALLED AT THE FACTORY, AND STILL HAD CRACKS IN THE SUPPORT CHANNEL.SDR 9JLA2012071704505Cvr · no testCREW REPORTED THE COCKPIT VOICE RECORDER WOULD NOT TEST. WAS REMOVED FOR REPAIRS. SAME UNIT INSTALLED AFTER REPAIRED.SDR 9JLA2012040604504Solenoid · defectiveTHE CREW REPORTED THE CABIN DOOR ANNUNCIATOR WOULD NOT EXTINGUISH. TROUBLESHOOTING FOUND THAT THE CABIN VENT DOOR SOLENOID WAS DEFECTIVE. THIS HAS BEEN OUR THIRD DEFECTIVE SOLENOID IN THE LAST 12 MONTHS.SDR Z5FA2012040550601Actuator · contaminatedON LEVEL OFF, AUTO PILOT DISENGAGED AND PITCH MISTRIM ANNUNCIATOR ILLUMINATED. EXCESSIVE PITCH TRIM REQUIRED TO MAINTAIN LEVEL FLIGHT. ACFT DIVERTED & LANDING UNEVENTFUL. MX INSPECTED ELEVATOR TRIM CABLE TENSION AND TRAVEL. NO DEFECTS FOUND. LT AND RT ESDR CWQR2012040326Hub · crackedDURING A SCHEDULED INSPECTION OF THE CABIN DOOR, FOUND THE FORWARD CABIN DOOR COUNTERBALANCE SPRING REEL HUB TO BE CRACKED WHERE THE ROLL PIN GOES THROUGH THE HUB. PICTURES AND A SERVICE CONDITION REPORT HAS BEEN SENT TO MFG UNDER SDR 614143.SDR CA120411004Bleed Valve · faulty(CAN) DURING DEPARTURE TAKEOFF POWER WAS SET FOR 3-5 SECONDS, LT ELECTRONIC ENGINE CONTROL ANNUNCIATOR ILLUMINATED AND ENGINE REVERTED TO MANUAL MODE, TAKEOFF WAS ABORTED AT 50 KNOTS. ACFT WAS SENT TO MFG, TROUBLESHOOTING ONGOING. PERFORMED GROUND RUN AND CASDR CWQR2012040225Support Channel · crackedDURING A SCHEDULED INSPECTION OF THE TAIL BAGGAGE DOOR HINGE, FOUND THE LOWER FORWARD HINGE SUPPORT CHANNELS CRACKED, SB560XL-52-13 HAD BEEN COMPLIED WITH AT THE FACTORY. BUT BOTH THE 66120692 AND THE 6612069-11 CHANNELS WERE CRACKED IN 2 PLACES. THE CRACKS SDR CWQR2012040224Control Cable · frayedDURING A SCHEDULED INSPECTION THE ELEVATOR TRIM CABLE WAS FOUND TO BE FRAYED BEYOND LIMITS. THIS CABLE ASSY IS LOCATED WHERE THE CABLE TRANSITIONS FROM A VERTICAL RUN TO THE HORIZ AT A PULLEY LOCATED IN THE HORIZ STABILIZER. WE HAVE SEEN NUMEROUS THIS SAME COSDR DXTA2012040204941Windshield · crackedRT FWD WINDSHIELD CRACKED. R & R RT HEATED WINDSHIELD IAW MM 56-11-00. PERFORMED WIRING CHECKS. NO DEFECTS NOTED.SDR DXTA2012040204935Brake · malfunctionedDURING A SHARP RT TURN AT TAXI, CO-PILOT`S RT BRAKE PEDAL LOST PRESSURE, & NEEDED TO BE PUMPED TO STOP ACFT FROM A 1 OR 2 MPH. CAPTAIN`S SIDE NEEDED A LOT OF MOVEMENT TO GET PRESSURE AFTER ACFT STOPPED. COPILOT`S RT PEDAL NEEDS A LOT MORE MOVEMENT TO GET PRESDR DXTA2012040204936Brake Sys · noneBRAKES WON'T KEEP THE ACFT STOPPED WITH POWER SET TO TAKEOFF SETTING. INSPECTED BRAKE ASSEMBLIES, FOUND NO DEFECTS. ALL CHECKED GOOD AT THIS TIME IAW MM 30-44-20.SDR DXTA2012040204937Uplock Switch · inoperativeDURING TAKEOFF, WITHIN 2 SECONDS OF SELECTING THE GEAR LEVER UP, HEARD A LOUD "THUMP". ALL THE GEAR GREEN LIGHTS EXTINGUISHED AND THE RED UNLOCK ANNUNCIATOR REMAINED ILLUMINATED. RAN EGINES INDEPENDENTLY APPLYING HYDRAULIC LOADS. DID NOT OBSERVE A "LOW HYDSDR CWQR20120330023Control Cable · frayedDURING A SCHEDULED INSPECTION, THE ELEVATOR TRIM CABLE WAS FOUND TO BE FRAYED BEYOND LIMITS. THIS CABLE ASSY IS LOCATED WHERE THE CABLE TRANSITIONS FROM A VERTICAL RUN TO THE HORIZONTAL AT A PULLEY LOCATED IN THE HORIZONTAL STABILIZER.SDR CWQR20120330022Control Cable · frayedDURING A SCHEDULED INSPECTION, THE ELEVATOR TRIM CABLE WAS FOUND TO BE FRAYED BEYOND LIMITS. THIS CABLE ASSY IS LOCATED WHERE THE CABLE TRANSITIONS FROM A VERTICAL RUN TO THE HORIZ AT A PULLEY LOCATED IN THE HORIZ STABILIZER.SDR CWQR20120330021Control Cable · frayedDURING A SCHEDULED INSPECTION, THE ELEVATOR TRIM CABLE WAS FOUND TO BE FRAYED BEYOND LIMITS. THIS CABLE ASSY IS LOCATED WHERE THE CABLE TRANSITIONS FROM A VERTICAL RUN TO THE HORIZONTAL AT A PULLEY LOCATED IN THE HORIZONTAL STABILIZER.SDR CWQR20120330020Control Cable · frayedDURING A SCHEDULED INSPECTION THE ELEVATOR TRIM CABLE WAS FOUND TO BE FRAYED BEYOND LIMITS. THIS CABLE ASSY IS LOCATED WHERE THE CABLE TRANSITIONS FROM A VERTICAL RUN TO THE HORIZ AT A PULLEY LOCATED IN THE HORIZ STABILIZER. HAVE SEEN NUMEROUS WITH THIS SAME SDR CWQR20120327019Hinge Bracket · crackedDURING A SCHEDULED INSPECTION, FOUND RT ELEVATOR INBD HINGE CRACKED, VERIFIED WITH NDT, R & R HINGE ASSY.SDR DXTA2012032604432Bulb · inoperativeDURING APPROACH AND LANDING THE "GREEN" LEFT MLG LIGHTS NEVER ILLUMINATED. RAN THE "GEAR WOULD NOT EXTEND" CHECK LIST TO MAKE SURE IT WAS DOWN AND LOCKED. REPLACED 2 BULBS FOR THE GREEN LT MLG INDICATION IAW MM 33-10-00, OPS TEST GOOD. RESET EMERGENCY BLOWDSDR CWQR20120323018Hinge Bracket · crackedDURING A SCHEDULED INSPECTION, FOUND RT ELEVATOR OTBD HINGE CRACKED, VERIFIED WITH NDT, R & R HINGE.SDR CWQR20120323017Hinge Bracket · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK ON THE ELEVATOR RT INBD HINGE THAT ATTACHES TO THE STABILIZER. VERIFIED CRACK WITH NDT, R & R HINGE.SDR DXTR20120322002Drip Tray · debondedDURING ACCOMPLISHMENT OF SB-53-13, 1 AREA OF BOND SEPARATION NOTED ON RT SIDE AT FS 90.20, FROM LOWER EDGE OF NOSE COMPARTMENT DOOR OPENING UP TO 14". C/W SB-53-13 R1-- FUSELAGE NOSE DRIP CAP REPAIR OF MARKED AREA IAW SB-53-13 R1.SDR DXTR20120322001Web · crackedWEB HAS 3 CRACKS AT DOOR HANDLE ATTACH POINT. REMOVED DAMAGE AS REQUIRED AND INSTALLED NEW STIFFENER IAW SRM 51-40-03 AND 51-40-06 AND SB-52-14.SDR CWQR20120320016Hinge · crackedDURING A SCHEDULED INSPECTION, FOUND AN AREA OF CORRISION ON THE FWD MAIN CABIN DOOR HINGE, THAT IS ATTACHED TO THE DOOR FRAME. FOUND THE CORRISION ON THE FWD EDGE OF THE HINGE, PREFORMED A DYE-PEN CHECK AND FOUND THE HINGE TO BE CRACKED. THIS IS THE THIRD SDR CA120329005Oil System · failed(CAN) DURING FLIGHT, ACFT WAS ON FINAL APPROACH TO VENICE WHEN ENGINE OIL PRESSURE WENT TO ZERO. PILOTS SHUTDOWN AND SECURED THE ENGINE. AN UNEVENTFUL SINGLE ENGINE LANDING PERFORMED AT PLANNED DESTINATION. TROUBLESHOOTING ONGOING.SDR CA120319001Indicator · malfunctioned(CAN) DURING FLIGHT, THE NR 1 ENGINE OIL PRESSURE WENT INTO THE YELLOW. IT THEN WENT BELOW 20 PSI, MASTER WARNING AND LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED. THE ENGINE WAS SHUTDOWN IAW CHECKLIST. ACFT DIVERTED TO NORFOLK WHERE AN UNEVENTFUL SINGLE ENGINESDR CWQR20100308014Hinge · corrodedDURING A SCHEDULED INSPECTION, FOUND CORROSION ON THE FWD CABIN DOOR HINGE FROM THE CORNER EDGE OF THE PART TO BEYOND THE FIRST FASTENER ATTACH HOLE, BEYOND ALLOWABLE LIMITS. REMOVED HINGE, INSPECTED AND PREFORMED NDT INSP OF ATTACH POINT, NO DEFECTS NOTED. TSDR DXTA2012030904913Coalescer Bag · odorPAX DESCRIBED A STRONG ACRID BLEED AIR ODOR IN THE CABIN ON TAKEOFF. CLEANED COALESER SOCK IN WATER SEPERATOR. OPS CHECK OF ECS OK WITH ENGINES AND APU. WORK PERFORMED IAW MM 12-19-02 & 21-51-00.SDR DXTA2012030904912Garlock Seal · leakingNR 1 OIL PRESSURE WENT INTO THE YELLOW. PROCEDURE COMPLETED. THEN WENT BELOW 20 PSI, MASTER WARNING AND LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED. ENGINE SHUTDOWN IAW CHECKLIST. ON POSTFLIGHT, SIGHT GAUGE EMPTY (WAS FULL AT DEPARTURE) AND OIL ALL OVER COWLINSDR DXTA2012030804908Apu · leakingSMOKE IN CABIN AFTER APU BLEED AIR TURNED ON. OPERATED APU AND BLEED AIR AND VERIFIED DISCREPANCY. NOTED AN OIL ODOR WHEN CABIN WAS FILLED WITH SMOKE. TURNED OFF APU. ACCESSED APU AND DISCONNECTED MAIN BLEED AIR LINE AND FOUND EVIDENCE OF OIL LEAKING INTERSDR CWQR20120306015Hinge · corrodedDURING A SCHEDULED INSPECTION, FOUND CORROSION ON THE AFT CABIN DOOR HINGE FROM THE CORNER EDGE OF THE PART TO BEYOND THE FIRST FASTENER ATTACH HOLE. BEYOND ALLOWABLE LIMITS. REMOVED HINGE, INSPECTED AND PREFORMED NDT INSP OF ATTACH POINT, NO DEFECTS NOTED. THSDR CWQR20120305009Support Bracket · crackedDURING SCHEDULED MX THIS ECU SUPPORT BRACKET WAS FOUND CRACKED IN 2 PLACES. ONE CRACK IS 1.80 INCHES LONG, THE SECOND CRACK IS .80 INCHES LONG. THIS IS THE SECOND SUPPORT BRACKET TO BE INSTALLED ON THIS ACFT. WE HAVE SEEN SIMULAR SUPPORT BRACKET CRACKS ON OTSDR DXTA2012030504904Actuator · malfunctionedLEFT MLG INDICATOR DID NOT SHOW SAFE DOWN WHEN EXTENDED AND RED UNSAFE LIGHT ILLUMINATED. YAWED ACFT TO ACHIEVE GOOD DOWN & LOCKED INDICATION. LANDED NORMALLY. ROLLOUT NORMAL. DURING A 180 DEGREE LT TURN ON RAMP LT MLG INDICATED UNSAFE & RED UNSAFE LIGHT ISDR DXTA2012030504901Uplock Switch · illuminatedAFTER TAKEOFF, RETRACTED MLG AND RECEIVED A RED UNSAFE INDICATION THAT STAYED ON WITH ALL 3 GREEN LIGHTS EXTINGUISHED. LEVELED OFF AT 5,000 FT & MAINTAINED SPEED BELOW 200 KTS WHILE RUNNING CHECKLISTS & THEN RETUNED TO LAND. NO OTHER INDICATION WAS DETECTEDSDR DXTR20120302001Hinge Fitting · corrodedCABIN DOOR AFT LOWER HINGE AIRFRAME SIDE, UPPER FORWARD CORNER CORRODED.SDR DXTA2012030204896Acm · seizedSTARTED APU AND TURNED ON BLEED AIR. BOTH CABIN AND COCKPIT AIR SUPPLY TEMPS WENT TO 250. COULDN'T GET THE TEMPS LOWERED EITHER MANUALLY OR AUTOMATICALLY. CABIN BEGAN TO FILL WITH SMOKE AND HAD A PLASTIC BURNING ODOR. R & R SEIZED ACM COOLING TURBINE AND ISDR DXTA2012030204895Connector · corrodedRED MLG UNLOCK LIGHT REMAINED ILLUMINATED WITHOUT GREEN LIGHTS, AFTER RETRACTION OF MLG. MLG EXTENDED INDICATING THREE GREEN, NO RED. RETACTED MLG, RED UNLOCK REMAINED ILLUMINATED, NO GREEN. RETURNED TO AIRPORT AND LANDED NORMALLY WITH THREE GREEN. FOUNDSDR CWQR20120229008Closeout Panel · crackedDURING A SCHEDULED MX CHECK, FOUND THE RT WHEEL WELL AFT SPAR CLOSE-OUT PANEL TO BE CRACKED AT 3 LOWER INBD RIVET LOCATIONS THAT ATTACH IT TO THE LOWER WING SKIN. UPON DISASSEMBLE IT WAS FOUND THAT 1 OF THE CRACKS WENT FROM RIVET TO RIVET. THE PANEL ALSO HOLDSSDR CA120224007Pump · failed(CAN) AFTER CREW SELECTED GEAR DOWN, THEY HAD A LOW BRAKE PRESSURE WARNING, DECLARED EMERGENCY AND LANDED USING EMERGENCY PNEUMATIC BRAKE SYSTEM TO STOP. AFTER EVALUATION, SERVICE CENTER DETERMINED THAT THE ELECTRIC MOTOR PORTION OF PUMP WAS FUNTIONAL BUT THE SDR CA120224004Spring · broken(CAN) ONE OF THE DOOR SPRINGS FOUND BROKEN. AFTER A DETAILED INSPECTION, FOUND THAT THE SPRING ITSELF WAS BROKEN ALONG WITH A ROD END AND A COVER PLATE. NO STRUCTURAL DAMAGE WAS FOUND ON THE DOOR OR THE HINGES. REPLACED BEFORE NEXT FLIGHT.SDR DXTR20120223002Casting · looseFOUND FOUR BOLTS LOOSE AT HORIZONTAL STAB REAR ATTACH CASTING. TORQUED BOLTS IAW MM 20-10-01.SDR DXTR20120223001Skin · crackedRUDDER SKIN CRACKED ON LOWER L/E. R & R SKIN WITH NEW PN 6633000-5.SDR CA120222002Pushrod · corroded(CAN) WHILE PERFORMING PHASE 5, FOUND RT ELEVATOR TRIM TAB PUSH RODS CORRODED AT NUT. PUSH ROD WERE REPLACED BEFORE THE NEXT FLIGHT.SDR DXTA2012022204883Handle · malfunctionedAT 220 KTS, 1500 FT, MOVED THE GEAR HANDLE TO THE DOWN POSITION. HANDLE MOVED NORMALLY AND LOCKED INTO PLACE BUT ONLY THE RED GEAR UNSAFE LIGHT CAME ON AND NO SOUNDS OF THE GEAR DOORS OPENING. AFTER WIGGLING THE HANDLE BACK AND FORTH FOR 4-5 SECONDS IN THE DSDR 2012FA0000123Circuit Board · damagedAFTER POST INSPECTION, ENGINE RUNS FOUND RT ENGINE ECS FAULT INDICATOR TRIPPED AFTER SHUTDOWN. RESET INDICATOR, AND PERFORMED NORMAL ENGINE START, AND IDLE. SHUTDOWN ENGINE AND REINSPECTED FAULTED INDICATOR AND FOUND IT HAD TRIPPED AGAIN. DOWN LOADED EEC DASDR CA120228003Engine · power loss(CAN) SHORTLY AFTER INITIATING DESCENT AT FL390, THE PILOT RECEIVED AN ELECTRIC ENGINE CONTROL REVERSION TO MANUAL WARNING AS POWER WAS BEING REDUCED. ACFT VIBRATIONS WERE ALSO NOTICED. THE CREW RAN THE EMERGENCY CHECK LIST TWICE TO RESTORE ENGINE CONTROL WIT
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