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 JGVR20170531001Strake · corrodedLT AND RT STRAKES WERE CORRODED, BEYOND LIMITS OF SRM. REPLACED BOTH STRAKES.SDR CVGA20170530001O-Ring · deterioratedWING OVERHEAT RT ANNUNCIATOR ILLUMINATED IN FLIGHT. FOLLOWED ABNORMAL CHECKLIST WHICH INSTRUCTED TO LAND AS SOON AS PRACTICAL AND REFER TO SINGLE ENGINE APPROACH AND LANDING. DECLARED AN EMERGENCY AND LANDED SAFELY. MAINTENANCE FOUND A DETERIORATED O-RING ONSDR JGVR20170526001Skin · corrodedCENTER WING BOND ASSEMBLY HAS CORROSION ON IT'S LAND FOR FUEL PANEL 510BB. FOUND DURING C INSPECTION. REMOVED CORROSION, PERFORMED EDDY CURRENT CHECK OF WING FUEL LAND WITH NO CRACK OR CORROSION INDICATIONS. REPAIRED IN ACCORDANCE WITH CESSNA ENGINEERING MEMO SDR DXTA2017051706404Windshield · damagedDURING CRUISE FLIGHT AT FL400 AFTER 25 MINUTES AT FL400 A STRONG SMELL OF BURNING WIRES. THAT SMELL CONTINUED ON THE FLIGHT DECK THEN AFTER 15 MINUTES OF THE BURNING SMELL THE RIGHT WINDSHIELD HEAT FAULT LIGHT ANNUNCIATOR ILLUMINATED. WE THEN DECLARED AN EMERGSDR JGVR20170516002Support · crackedDURING A 600 HR INSPECTION, FOUND THE MAIN ENTRY DOOR STRUCTURE UNDER C CHANNEL WITH SPRING AND DOOR LOCKED FLAG HAS A CRACK ON THE UPPER AFT CORNER. REMOVED AND REPLACED CRACKED MED SUPPORT.SDR JGVR20170516001Skin · delaminatedLEFT INBD FLAP HAS TWO AREAS OF DELAMINATION ON BOTH THE UPPER AND LOWER SURFACE. FOUND DURING THE FLAP SYSTEM INSPECTION TASK 27-90-50 DURING A C INSPECTION. REMOVED AND REPLACED THE FLAP.SDR EBVR20170508001Strake · corrodedLEFT STRAKE TOP AFT UPPER EDGE RT STRAKE LOWER SURFACE EDGE BELOW COMPOSITE HAS DEEP CORROSION. BLENDED CORROSION, CORROSION WENT THROUGH UPPER SKIN OF LT STRAKE. REPAIRED IAW EO C56-53-0001.SDR 9JLA201705189619Spring · brokenCREW REPORTED THAT WHEN THE MAIN CABIN ENTRY DOOR WAS OPENED THAT THE DOOR COUNTER BALANCE SPRING INSIDE THE DOOR FAILED. THE DOOR TRIM PANELS WERE REMOVED FOR ACCESS WHERE IT WAS FOUND THAT WHEN THE DOOR SPRING FAILED IT CAUSED DAMAGE TO THE DOOR INNER DOOR SSDR DXTR2017050201Channel · crackedMAIN CABIN DOOR FRAME STRUCTURE CRACKED BENEATH AFT SUPPORT ROD LOWER FITTING. ACCOMPLISHED MAJOR REPAIR IAW 5562/05RD.SDR CVGA20170428001Pulley Bracket · crackedWHILE TROUBLESHOOTING CLUNKING NOISE WHEN THE GEAR IS TURNED, FOUND FWD PULLEY BRACKET CRACKED.SDR DXTA2017042306399Engine · power lossWITH EEC IN MANUAL, TAKEOFF POWER OBTAINED. DURING CLIMB, NOTICED LARGE THROTTLE SPLIT AND NOTICED THAT THE LEFT ENGINE NOT DEVELOPING TAKEOFF THRUST. CONTINUED CHECKING THROUGH CLIMB ONLY GOT 85% N1 101% N2 WITH THROTTLE TO FORWARD STOP.SDR 9JLA2017051914167Carbon Seal · leakingCREW REPORTED THAT WITH THE APU RUNNING AND THE APU BLEED AIR SELECTED ON ON SMOKE ENTERED CABIN. INITIAL FINDING DETERMINED THAT A COMPRESSOR CARBON SEAL FAILED AND ALLOWED ENGINE OIL TO ENTER THE BLEED AIR SYSTEM. THE APU WAS REMOVED FROM THE AIRCRAFT FOR RESDR DXTA2017041606398Warning Message · illuminatedGROUND IDLE ANNUNCIATOR ILLUMINATED FOLLOWED BY MASTER CAUTION AFTER TAKEOFF. EXTINGUISHED AFTER GEAR RETRACTION.SDR DXTR2017041401Skin · corrodedCORROSION FOUND ON RT FUSELAGE BETWEEN RT WING TRAILING EDGE AND FWD SIDE OF LAV SERVICE PANEL DOOR AT FS 405.0. ACCOMPLISHED MINOR REPAIR IAW MEMO DQ7654 DATED 04/04/2017.SDR DXTR2017040801Skin · crackedTHE RT ELEVATOR HAS A CRACK ON THE LOWER SKIN AT THE OUTBOARD HINGE CUTOUT. THE CRACK MEASURES APPROXIMATELY 0.25 INCHES LONG.SDR DXTR2017040702Skin · corrodedCORROSION FOUND ON THE RT UPPER & LOWER WING SKINS & FITTING ON THE RT OUTBOARD FLAP. ACCOMPLISHED MAJOR REPAIR IAW REPAIR DEFINITION 5264/05RD DATED MARCH 31/2017 & FAA FORM 8100-9 DATED APRIL 7/2017. NDT PERFORMED UNDER WORK ORDER 21515 & 21519.SDR DXTR2017040701Skin · corrodedCORROSION FOUND ON THE LT UPPER WING SKIN. ACCOMPLISHED MAJOR REPAIR IAW REPAIR DEFINITION 5264/05RD DATED MARCH 31/2017 & FAA FORM 8100-9 DATED APRIL 7, 2017. NDT PERFORMED UNDER WORK ORDER 21515 & 21519.SDR 3EJA201704060001Relay · defectivePILOT REPORTED WHEN USING REC/TAXI AND LANDING LIGHTS, STRONG ODOR IS NOTICED. PILOT ALSO REPORTED THE LEFT BELLY LIGHT AND LEFT WING LANDING/TAXI LIGHTS INOP. UPON INSPECTING THE SYSTEM, MULTIPLE BURNED WIRES WERE FOUND ON THE REC/TAXI LIGHT SWITCH LOCATED ISDR DXTR2017040601Skin · corrodedTHE STINGER ASSEMBLY HAS THREE (3) AREAS OF CORROSION ON THE OUTER SKIN AT THE 6 O'CLOCK POSITION. REPAIRED IAW AQRD ERO-889608.SDR EBVR20170406001Rib · corrodedCORROSION FOUND ON LOWER RIB OF THE RUDDER AT THE BONDING POINT. REPAIRED EXISTING LOWER RUDDER TORQUE TUBE RIB PER AQRD ERO-891028 REV IR. ATTACHED NEW REPAIR DOUBLER TO LOWER RIB OF RUDDER WET WITH PS870B1/2 LOT# 70540 AND CR3213-4-2 RIVETS.SDR 9JLA201705229615Speed Switch · defectiveDURING APPROACH, AFTER THE FLAPS HAD BEEN SELECTED TO SEVEN DEGREES, RECEIVED A STAB MISCOMPARE ANNUNCIATION, FOLLOWED BY A SIGNIFICANT CLIMB MOVEMENT. THE AIRCRAFT LANDED WITHOUT INCIDENT. TROUBLESHOOTING DETERMINED THAT THE SPEED SWITCH OF THE TWO-SPEED POSSDR 9JLA201705199613Lamp · inoperativeTHE CREW REPORTED THAT DURING APPROACH, AFTER THE GEAR WAS SELECTED DOWN, THERE WAS NO LT GEAR DOWN AND LOCK INDICATION. AFTER COMPLETING THE PILOTS CHECKLIST THE CREW ACTIVATED THE EMERGENCY GEAR BLOW DOWN SYSTEM. THERE WAS STILL NO LT GEAR DOWN AND LOCK INDISDR 9JLA201705229610Wire · damagedMAINTENANCE CREW HAD A REPORT THAT THE LT ENGINE IGNITION SYSTEM FAILED. VERIFIED THAT THERE WAS NO IGNITION OPERATION WHEN SELECTED TO THE IN THE ON POSITION. TROUBLESHOOTING A COLD SOLDERED CONNECTION ON ONE PIN OF THE LT IGNITION SWITCH. SOLDERED WIRE TO PSDR 9JLA201705229609Relay · faultedTHE MAINTENANCE NOTED THAT WHEN THE AIRCRAFTS MAIN SHIP BATTERY MASTER SWITCH WAS SELECTED ON, THE AVIONICS SYSTEMS ENERGIZED UNCOMMANDED. TROUBLESHOOTING IDENTIFIED BOTH AVIONICS POWER RELAYS FAULTY (KZ001 AND KZ002). REMOVED THE RELAYS AND REPLACED WITH NSDR CVGA20170329001Lamp · inoperativeON APPROACH, CREW RECEIVED LANDING GEAR UNSAFE LIGHT INDICATION WARNING AND NO DOWN LIGHT INDICATION ON LEFT MAIN AND NOSE GEAR. DETERMINED TO DIVERT FOR LOW PASS APPROACH FOR ATC GEAR DOWN OBSERVATION. AIRCRAFT LANDED UNEVENTFUL AND TAXIED TO FBO. MX VERIFISDR EBVR20170327002Skin · crackedCRACK IN THE VERTICAL STAB CAP, REPAIRED CRACK IN VERTICAL STAB CAP IAW REPORT S-750-ATA51/01RD (STRUCTURAL REPAIR OF COMPOSITE LAMINATE STRUCTURES). REPAIRED.SDR EBVR20170327001Torque Tube · corrodedRUDDER TORQUE TUBE AREA IS RUSTED, REMOVED THE RUDDER TORQUE TUBE AND INSTALLED NEW TORQUE TUBE. CORROSION WAS FOUND ON THE LOWER RUDDER RIB WHILE REPLACING THE TORQUE TUBE. REPAIRED THE LOWER RUDDER TORQUE TUBE RIB IAW ERO-889729, REV IR.SDR 2017FA0000121Strut · chafedACCOMPLISHED MINOR REPAIR TO OLEO IAW MEMO DQ7482.SDR 2017FA0000115Window · failedDURING CRUISE FLIGHT, THE RIGHT FORWARD ELECTRICALLY HEATED SIDE WINDOW FAILED. THE WINDOW FAILED IN SUCH A MANNER THAT THE EXTERIOR PORTION OF THE LAMINATED GLASS BURST INTO FRAGMENTS SENDING GLASS DEBRIS AFT INTO THE ENGINE.SDR 9JLA2017040614162Bellcrank · crackedDURING FLIGHT, THE CREW REPORTED THAT THE MAIN CABIN DOOR ANNUNCIATOR ILLUMINATED. DIVERTED FOR FURTHER INVESTIGATION AND REPAIR. LANDING WAS UNEVENTFUL. TROUBLESHOT TO DETERMINE THE CAUSE. THE AIRCRAFT WAS GROUNDED. DISCOVERED THAT A BELLCRANK IN THE MAINSDR O2GA2017032451501Indicator · out of adjustAFTER TAKE-OFF WITH TRIM INDICATOR IN T.O. POSITION, THE "NO TAKEOFF" WARNING HORN SOUNDED. NOSE DOWN TRIM REQUIRED TO KEEP AIRCRAFT BALANCED. TRIM INDICATOR DID NOT AGREE WITH TRIM POSITION. MAINTENANCE ADJUSTED THE ELEVATOR TRIM INDICATOR. TRAVEL, RIGGING ANSDR DXTA2017030206377Coffeemaker · failedON DESCENT INTO DESTINATION, SMELLED AN ODOR. ON SHUTDOWN THE COFFEE POT AS WELL AS THE WATER POT WERE EXTREMELY HOT WITH THE SWITCHES IN THE OFF POSITION. INSPECTED SWITCHES, WIRING AND CONNECTORS FOR UPPER AND LOWER HOT LIQUID TANKS. NO DEFECTS NOTED. FOUNSDR DXTA2017022206374Light · meltedDURING DESCENT, THERE WAS SMOKE COMING FROM THE LEFT CIRCUIT PANEL. AN EMERGENCY DESCENT WAS PERFORMED AND ELECTRICAL FIRE OR SMOKE CHECKLIST G1 WAS INITIATED AND COMPLETED. INSPECTED THE AIRCRAFT FOR SOURCE OF SMOKE AND FOUND AISLE LIGHTS ON LEFT SIDE MELTESDR DXTR2017022501Web · crackedMED HAS ONE CRACK EACH ON THE FWD & AFT WEB ASSY. EACH CRACK MEASURES APPROXIMATELY 0.25 INCHES LONG. ACCOMPLISHED MAJOR REPAIR IAW ERO-886507 DATED FEB 23/2017 & FAA FORM 8110-3 DATED FEB 23/2017.SDR DXTA2017022106372Brake Sys · contaminatedPWR BRKS CB POPPED. ANTISD INOP ANNUNCIATOR ILLUMINATED. RESET CB ONCE AND IT POPPED AGAIN. AFTER 5 MIN TAXI, LO BRK PRESS ANNUNCIATOR ILLUMINATED FOLLOWED BY LOSS OF BRAKES. DRAINED AND FLUSHED BRAKE SYSTEM HYDRAULIC FLUID AND SERVICED RESERVOIR TO CORRECT SDR DXTA2017021006366Switch · failedNORMAL DEPARTURE ACCELERATING THROUGH 200 KTS, NOTICED THE TRIM WHEEL BUCKED AND RAN OUT OF FORWARD TRIM. SIMULTANEOUSLY, THERE WAS EXTREME PRESSURE ON THE YOLK IN ORDER TO REMAIN LEVEL. THE STAB MISCOMPARE LIGHT ILLUMINATED MOMENTARILY. THE CREW RAN THE STSDR DXTR2017020600001Hinge · bentRIGHT OUTBOARD ELEVATOR HINGE WAS FOUND BENT.SDR DXTR2017020601Support Bracket · gougedELEVATOR BELLCRANK ASSEMBLY HAS CONTACTED THE SUPPORT BRACKET AND GOUGED THE METAL. DAMAGE LOCATED LT AFT CORNER OF THE ELEVATOR BELLCRANK CUTOUT AT FS 589.0 & WL 148.0. ACCOMPLISHED MINOR REPAIR IAW AQRD ERO-884036.SDR DXTA2017012506366Tire · out of balanceAC EXPERIENCED STRONG VIBRATIONS ON NOSE FLOOR AND RUDDER PEDALS AFTER GEAR RETRACTION. INDICATIONS NORMAL. LOWERED GEAR AND LANDED. VIBRATIONS STOPPED PRIOR TO LOWERING GEAR. FOUND NOSE TIRE/WHEEL UNBALANCED AND NOT TORQUED TO PROPER SPECS. BALANCED NOSE WHEESDR O2GA2017011850702Circuit Board · failedAFTER TAKE-OFF AND GEAR RETRACTION THE GEAR UNLOCK INDICATOR LIGHT REMAINED ILLUMINATED WITH AN ASSOCIATED FLASHING HYDRAULIC PRESSURE ANNUNCIATOR. IAW CHECKLIST CYCLED HYD CTL CIRCUIT BREAKER AND LIGHTS EXTINGUISHED. NORMAL GEAR EXTENSION AT DESTINATION. MASDR 9JLA201703067734Circuit Breaker · defectiveTHE CREW REPORTED THAT WHILE TAXIING THE AIRCRAFT THE POWER BRAKE CIRCUIT BREAKER TRIPPED. FUNCTIONAL CHECKS FOUND NO DISCREPANCIES WITH THE BRAKE SYSTEM. DURING ANOTHER TRIP FOLLOWING THIS EVENT, THE CREW REPORTED AGAIN THAT THE POWER BRAKE CIRCUIT BREAKER TRSDR O2GA2017010550702Manifold · intermittentAFTER TAKE-OFF AND GEAR RETRACTION, GEAR UNLOCK ANNUNCIATOR REMAINED ON, AS DID HYDRAULIC PRESSURE. IAW CHECKLIST CYCLED HYDRAULIC CONTROL CIRCUIT BREAKER. BOTH ANNUNCIATORS WENT OUT AND GEAR EXTENDED NORMALLY. MAINTENANCE REPLACED THE HYDRAULIC MANIFOLD. A SDR O2GA2016010550701Landing Gear · malfunctionedAFTER TAKE-OFF AND GEAR RETRACTION, GEAR UNLOCK ANNUNCIATOR REMAINED ON, AS DID HYDRAULIC PRESSURE. IAW CHECKLIST CYCLED HYDRAULIC CONTROL CIRCUIT BREAKER. BOTH ANNUNCIATORS WENT OUT AND GEAR EXTENDED NORMALLY. DIVERTED, AND LANDING WAS UNEVENTFUL. MAINTENANCSDR DXTA2016123006352Outflow Valve · failedAT FL400 CABIN ALTITUDE WARNING ILLUMINATED. CABIN ALT INCREASED TO FL 200. CABIN ALTITUDE STABILIZED PASSING 10000 FEET. ACCOMPLISHED PRESSURE CHECK OF SERVICE AIR SYSTEM AT OUTFLOW VALVE AND FOUND SYSTEM TO PROVIDE 23 PSI WHICH IS CORRECT. ACCOMPLISHED ELESDR DXTA2016123006351Coalescer Bag · dirtyACM PRODUCED A SOCK ODOR. REMOVED & REPLACED DIRTY WATER SEPARATOR CONDENSER CLOTH IAW MM 12-19-02. OPS & LEAK CHECKS WERE GOOD.SDR DXTR2016122901Skin · dentedRIGHT LOWER WING SKIN AT RWS 143.07 DENTED, REPAIRED IAW ERO-877762.SDR DXTR2016122801Structure · corrodedCORROSION FOUND UNDER THE DATA PLATE ON THE TAILCONE. REPAIRED CORROSION IAW DQ6626.SDR DXTR2016122702Structure · corrodedCORROSION FOUND IN MULTIPLE LOCATIONS ON THE UPPER SIDE OF THE LT AND RT WINGS. REPAIRED IAW REPAIR S-560XL-5805/06RD.SDR DXTR2016122701Structure · corrodedCORROSION FOUND IN MULTIPLE LOCATIONS ON THE UPPER SIDE OF THE LT AND RT WINGS. REPAIRED IAW REPAIR S-560XL-5805/06RD.SDR EBVR20161223001Support Angle · crackedBAGGAGE DOOR FWD SUPPORT ANGLE IS DAMAGED. COMPLIED WITH AQRD REPAIR ERO-876975 REV A DATED 12/22/2016 AND FAA FORM 8110-3.
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