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 3EJA202410280004Uplock Switch · failedWELL, ON APPROACH INTO DAL WHEN WE CALLED FOR “GEAR DOWN“ THE GEAR WAS SELECTED DOWN AND ONLY THE LEFT MAIN GEAR CAME DOWN AND LOCKED. WE WENT AROUND AND TOWER CONFIRMED WHEN WE FLEW OVERHEAD THAT WE ONLY HAD ONE GEAR DOWN. WE DECLARED AN EMERGENCY RAN APPROPRSDR DXTA2024102300913Motor · faultedPOWER BRAKE CB: ABOUT 5 MINUTES INTO OUR TAXI FROM SIGNATURE TO RUNWAY 30 AT DULLES, JUST AS WE TURNED ON TAXIWAY ZULU GOT AN ANTI SKID ANNUNCIATOR ALONG WITH THE POWER BRAKE CIRCUIT BREAKER POPPED. WE ASKED TO GO TO RUNUP PAD AND AS WE PULLED IN GOT LOW BREAKSDR CVGA20241023005Hydraulic System · leakingLOW BRAKE PRESS/ANTISKID LIGHT ILLUMINATED AFTER LANDING AND A TOTAL LOSS OF BREAKING. NOTICED A PUDDLE OF FLUID UNDER THE RIGHT MAIN GEAR.SDR DXTA2024101400817Pressure Valve · defectiveMAIN HYDRAULICS: UPON APPROACH INTO CHO WE ATTEMPTED TO BRING THE FLAPS TO 15° AND THEY DID NOT MOVE. WE ATTEMPTED TO LOWER THE LANDING GEAR. THE HANDLE CAME DOWN. WE HAD A RED UNLOCK LIGHT AND DID NOT GET ANY LANDING GEAR THREE GREEN LIGHTS. WE ELECTED TO DISDR DXTA2024101400813Battery Pack · dischargedEMERG EXIT SIGN/LIGHT: WITH THE BATTERY SWITCH ON AND EMERGENCY LIGHT SWITCH TO ON, ALL INTERIOR EMERGENCY LIGHTS CHECK NORMAL. WHEN TURNING THE BATTERY SWITCH TO OFF AND EMERGENCY LIGHT SWITCH STILL ON, THE 3 AFT EXIT SIGNS DO NOT ILLUMINATE. CORRECTIVE ACTIOSDR DXTA2024101400814Sight Gauge · out of adjustMAIN DOOR: MAIN CABIN DOOR FLAG SHOWS LOCKED WHEN THE DOOR IS OPEN/UNLOCKED CORRECTIVE ACTION: A REMOVED MCD STEP AND ADJUSTED MIDDLE FWD POSITION SITE AS REQUIRED TO MOVE INTO AND OUT OF SITE HOLE. OPS CK IS GOOD. REINSTALLED MCD STEPS. REF 560XL MM CH 52-10-SDR 3EJA202410040001Unknown · smokeAT ABOUT 5000 FT MSL SMOKE BEGAN ENTERING THE COCKPIT. SHUT OFF APU, REDUCED POWER AND SMOKE SUBSIDED. DECLARED EMERGENCY AND RETURNED TO KPBISDR DRFA202410040001Windshield · crackedDEPARTED KTYS AT 0745 LOCAL. RUNWAY 23L, WEATHER MOSTLY CLEAR WITH FEW SCATTERED CLOUDS. TEMP WAS 18C. WINDS 300 DEGREES AT 3KTS. TAKEOFF WEIGHT 16971LBS. FUEL AT TAKEOFF 4140 POUNDS OR 618 GALLONS. TAKEOFF WAS UNEVENTFUL. SKY CLEAR DURING CLIMB OUT. PASSSDR 3EJA202410020001Unknown · smokeWHILE CRUISING PRIOR TO DESCENT, SMOKE STARTED TO TO SHOW UP ON THE CABIN AND COCKPIT. PUT ON OUR OXYGEN MASK AND GOOGLES, FOLLOW THE EMERGENCY CHECKLIST AND DESCENDED. LANDED AT THE INTENDED DESTINATION WHICH IS PBI, NO DIVERSION OCCURRED, LANDED SAFELY NO FUSDR 2025F00010Control Cable · wornFOUND RIGHT FORWARD SECONDARY RUDDER CABLE EXCESSIVELY WORN DUE TO RUBBING ON ITS' GUIDE TUBE AND FAIRLEADS THROUGHOUT AIRCRAFT. VERIFIED PROPER CABLE ROUTING AND RIGGING. CABLE WAS REPLACED 2400 HOURS AGO DUE TO SAME ISSUE. CONTACTED MANUFACTURER AND DETERMINSDR 2025F00009Control Cable · wornFOUND LEFT FORWARD SECONDARY RUDDER CABLE EXCESSIVELY WORN DUE TO RUBBING ON ITS' GUIDE TUBE AND FAIRLEADS THROUGHOUT AIRCRAFT. VERIFIED PROPER CABLE ROUTING AND RIGGING. CABLE WAS REPLACED 2400 HOURS AGO DUE TO SAME ISSUE. CONTACTED MANUFACTURER AND DETERMINESDR 2025F00007Control Cable · wornFOUND RIGHT FORWARD PRIMARY RUDDER CABLE EXCESSIVELY WORN DUE TO RUBBING ON ITS' GUIDE TUBE AND FAIRLEADS THROUGHOUT AIRCRAFT. VERIFIED PROPER CABLE ROUTING AND RIGGING. CABLE WAS REPLACED 2400 HOURS AGO DUE TO SAME ISSUE. CONTACTED MANUFACTURER AND DETERMINEDSDR 2025F00006Control Cable · wornFOUND LEFT FORWARD PRIMARY RUDDER CABLE EXCESSIVELY WORN DUE TO RUBBING ON ITS' GUIDE TUBE AND FAIRLEADS THROUGHOUT AIRCRAFT. VERIFIED PROPER CABLE ROUTING AND RIGGING. CABLE WAS REPLACED 2400 HOURS AGO DUE TO SAME ISSUE. CONTACTED MANUFACTURER AND DETERMINED SDR 2025F00005Control Cable · wornFOUND AFT RUDDER TRIM CABLE EXCESSIVELY WORN DUE TO RUBBING ON FAIRLEADS THROUGHOUT AIRCRAFT. VERIFIED PROPER CABLE ROUTING AND RIGGING. CABLE WAS REPLACED 2400 HOURS AGO DUE TO SAME ISSUE. CONTACTED MANUFACTURER AND DETERMINED THERE IS NO APPROVED REPAIR OR ASDR DXTA2024100700726Indication Sys · odorLH AMLCD WENT BLANK AT FL400. WITHIN ABOUT A MINUTE THERE WAS AN ELECTRICAL BURNING SMELL. NO SMOKE WAS VISIBLE. DIVERTED TO DAL. REMOVED FAILED AMLCD ENGINE INDICATING SYSTEM P/N 9912574-5 S/N02060144AB AND INSTALLED OVERHAULED CUSTOMER SUPPLIED AMLCD ENGINSDR DXTA2024100100718Indicator · out of adjustCABIN DOOR LOCKED FLAG THAT IS IN THE STEP IS EXACTLY OPPOSITE TO DOOR FUNCTION. WHEN CABIN DOOR IS UNLOCKED FLAG INDICATES DOOR LOCKED. WHEN DOOR IS LOCKED, FLAG DISAPPEARS FROM WINDOW. CORRECTIVE ACTION: ADJUSTED RAG ARM IAW CE560XLS AMM 52-10-01. OPS CHECKESDR DXTA2024100100691Outflow Valve · malfunctionedAT 40000 HEARD LOUD BOOM ALONG WITH A RUSH OF AIR. CABIN DESCENT RATE WENT TO 1700. RAN QRC AND DESCENDED TO 10000. DURING DESCENT RATE DECREASED. COMPLIED WITH THE FOLLOWING OPS CHECKS, PRESSURIZE AIRPLANE WITH APU. OUTFLOW VALVES OPENED AT 9.2. SECONDARY OUSDR CVGA20240930246Unknown · smokeON DEPARTURE AND INITIAL CLIMB OUT CREW NOTICED SMOKE IN THE COCKPIT AND INCREASING IN VOLUME AND SMELL. CREW CONFIRMED WITH EACH OTHER THERE WAS SMOKE IN THE COCKPIT AND SMELLED ELECTRICAL IN ORIGIN. CREW SHUT DOWN THE APU AND IT ALMOST IMMEDIATELY STOPPED PRSDR 2024FA0000792Uplock Switch · defectiveTHIS IS TO INFORM YOU THAT ON 24 SEPTEMBER 2024, NASJET AIRCRAFT N142AA MSN 560-5281 RETURNED TO LSZH DUE CREW REPORTED THAT THE NLG DOOR LIGHT DID NOT EXTINGUISH WHEN THE GEAR HANDLE WAS UP. ON GROUND, CONTRACTED MAINTENANCE REPLACED NOSE LANDING GEAR DOOR USDR DXTA2024092500648Door · out of adjustMAIN CABIN DOOR NEEDS ADJUSTED. AFTER LANDING WITH COLD SOAKED AIRCRAFT, MAIN CABIN DOOR WILL NOT STAY IN DOWN LOCKED POSITION USING CABIN DOOR HANDLE. CORRECTIVE ACTION: ADJUSTED SUPPORT STRUT ASSY AS NEEDED. NO DEFECTS FOUND AT THIS TIME OPS CHECKS GOOD. PERSDR 2024FA0000738Trim Tab · out of adjustON 22 SEPTEMBER 2024, NASJET AIRCRAFT N142AA MSN 560-5281 RETURNED BACK/FLIGHT (LSZH) DUE TO CREW REPORTED THAT WHEN AIRCRAFT REACHED 200 KTS ABOVE, THE SLIP SKID DISPLACED TO THE LEFT AND NEED TO TRIM RUDDER HALFWAY TO THE LEFT TO CENTER IT. THE AIRCRAFT LANDSDR DXTA2024092300610Powerpack · failedDURING TAXI TO RAMP, NORMAL AC BRAKES FAILED AND AC STRUCK THE BUILDING. REMOVED ANTI-SKID MOTOR AND REPLACED WITH A OVERHAULED UNIT IAW CESSNA 560XL/XLS MM 32-44-00. REMOVED ANTI-SKID PUMP ASSEMBLY AND COUPLING AND ALSO REPLACED WITH NEW IAW CESSNA 560XL/XLSDR DXTA2024091700546Anti-Skid Sys · defectiveWHILE HOLDING SHORT OF RWY 06 IN TEB THE ANTI-SKID INOP/LOW BRAKE PRES. CAUTION LIGHT CAME ON, WE ACCOMPLISHED THE QRH CHECKLIST. WE TAXIED BACK TO SIGNATURE SOUTH, DURING THE TAXI LOST ALL MAIN BRAKE CONTROL PRESSURE,I USED THE EMERGENCY BRAKES TO STOP THE SDR 3EJA844JS091224Engine · faultedON TAKEOFF, AIR CIRCULATION NOISES INCREASED AS ENGINE POWER WAS APPLIED. INTO THE TAKEOFF, THE ACM OVERHEAT LIGHT WAS NOT NOTED UNTIL AFTER V1, SO THE TAKEOFF WAS CONTINUED. AFTER ROTATION, THE ITT INDICATIONS ON THE LEFT ENGINE WENT COMPLETELY RED IN COLORSDR DXTA2024090900452Unknown · odorCOCKPIT ODOR: WHILE TAXIING FOR TAKEOFF, WE SUDDENLY GOT A STRONG HOT BURNING SMELL, IT HAD AN ELECTRICAL SMELL TO IT. CORRECTIVE ACTION: PERFORMED MULTIPLE ENGINE RUNS AND APU RUNS. PERFORMED TC-5XL-21-120902MR1 (ENVIRONMENTAL CONTROL SYSTEM BLEED AND TRIM AISDR DXTA2024090900445Solenoid Valve · defectiveRUDDER: REPEAT WRITE UP. AFTER APPLYING TAKEOFF POWER AND BEGINNING TAKEOFF ROLL AIRCRAFT PULLS SEVERELY TO THE RIGHT AND WITH FULL LEFT RUDDER UNABLE TO MAINTAIN RUNWAY CENTERLINE. BOTH ENGINES ADVANCED TOGETHER AND WERE PRODUCING EQUAL POWER. ACHEIVED A MAXISDR 3EJA202409030024Engine · failed#2 ENG FUEL FLOW WENT TO ZERO, OIL PRESSURE DROPPED TO ZERO. PRECAUTIONARY ENGINE SHUTDOWN COMPLETEDSDR DXTA2024090300393Switch · defectiveSTAB MISCOMPARE LIGHT: ON 5 MILE FINAL PRIOR TO LANDING, WE GOT THE STAB MISCOMPARE ANNUNCIATOR LIGHT AND ALSO THE HYD PRESS LIGHT ( FLASHING ). TOOK A LOT OF CONTROL FORCE TO HOLD ALTITUDE. RAN QRH CHECK LIST AND LANDED UNEVENTFULLY. PHOTO ATTACHED. PRIOR TO SDR 3EJA202409032924Solenoid · failedCABIN DEPRESSURIZED DURING CLIMB. WOULD MAINTAIN A MAXIMUM PRESSURE DIFFERENTIAL OF ONLY 1.5 PSIDSDR 2024FA0000670Skin · corrodedREPAIRED THE LH UPPER WING SKINS BY BLENDING CORRODED AREAS, PERFORMING NDT, AND REPORTING FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREAS FOUND ACCEPTABLE, AND FABRICATED & INSTALLED TWO REPAIR DOUBLERS AS REQUIRED IN ACCORDANCE WITH TEXTRON FIELD SDR 2024FA0000669Skin · corrodedMECHANICALLY REMOVED 3 AREAS OF CORROSION FOUND AROUND E-EXIT DOOR SKIN AROUND EXTERIOR HANDLE. FOUND 1 CORROSION BLEND TO BE BEYOND LIMITS IAW C560XL SRM 51-70-08. COMPLIED WITH TEXTRON FR-560-5574-12462, TITLE FIELD REPAIR- CORROSION, EMERGENCY EXIT, SKIN, ASDR 2024FA0000668Skin · corrodedREPAIRED 54 AREAS OF CORROSION ON THE DROP AISLE FUSELAGE SKIN AND STRINGERS BETWEEN FUSELAGE STATION 175 THRU 355. PERFORMED AN EDDY CURRENT AND ULTRASONIC THICKNESS INSPECTION OF THE BLENDED AREAS. CLEANED, TREATED AND PRIMED AREAS FOUND ACCEPTABLE. FABRICATSDR 2024FA0000666Skin · corrodedMECHANICALLY BLENDED LH FUSELAGE PSE SKIN CORROSION LOCATED AROUND LH FWD CABIN WINDOW WITH 1 AREA OF CORROSION, 2ND CABIN WINDOW WITH 1 AREA OF CORROSION, 3RD CABIN WINDOW WITH 5 AREAS OF CORROSION, 4TH CABIN WINDOW WITH 3 AREAS OF CORROSION AND 5TH WINDOW WISDR DXTA2024082600313Counterbalance · damagedMAIN DOOR: MAIN DOOR HAS NO TENSION WHEN YOU CLOSE IT. SLAMS SHUT. AS A RESULT, THE TRIM ON THE BOTTOM OF THE DOOR IS STARTING TO CRACK. CORRECTIVE ACTION: REMOVED AND REPLACED CABIN ENTRY DOOR COUNTERBALANCE ASSEMBLY AND PERFORMED RIGGING IAW CE-560XL AMM 52-SDR 2024FA0000634Proximity Switch · out of adjustAIRCRAFT RETURNED BACK/FLIGHT (LSZH - LGIR) DUE TO AT CLIMB STATE, PASSING FL 230, THE CABIN DOOR CAS MSG (STEADY) APPEARED. THE AIRCRAFT LANDED SAFELY BACK TO LSZH. ON GROUND, CONTRACTED MAINTENANCE PERFORMED TROUBLESHOOTING AND FOUND CABIN DOOR UPPER AFT PRSDR DXTA2024082200295Oil System · overservicedMUSTY AND OILY ODOR IN AC SYSTEM DURING ENTIRE FLIGHT WITH OCCASIONAL FLUCTS IN AIR FLOW CORRECTIVE ACTION: DESERVICED THE APU TO THE PROPER LEVEL AND REMOVED AND REPLACED THE COALESCER SOCK. PERFORMED MULTIPLE OPERATIONAL CHECKS AND LEAK CHECKS OF THE APU ANDSDR DXTA2024082100272Control Valve · faultedMAIN CABIN DOOR DIFFICULT TO OPEN & CLOSE FROM INSIDE & OUTSIDE OF ACFT. WHEN APU BLEED AIR IS ON, THERE`S APPROX A 10 SEC DELAY FOR DOOR SEAL TO DEFLATE AFTER OPENING DOOR. WHEN CLOSING DOOR, PRECATCH WILL HOLD DOOR CLOSED, BUT WILL NOT RELEASE WHEN HANDLE SDR DXTA2024081900251Plunger · out of adjustMAIN DOOR: WITH DOOR SEAL INFLATED , MAIN CABIN DOOR DOES NOT OPEN PROPERLY. THERE IS A LONG DELAY WAITING FOR DOOR SEAL TO DEFLATE. CORRECTIVE ACTION: ADJUSTED PLUNGER ON ACOUSTIC DOOR SEAL VALVE. OPS CHECKS GOOD. REF. CE560XL MM 52-10-04.SDR DXTA2024081500196Support · damagedMAIN CABIN DOOR IS DIFFICULT TO CLOSE. WHEN LOCKING THE DOOR CLOSED, RESISTANCE IS FELT IN THE HANDLE. TO LOCK THE DOOR IT TAKES MORE FORCE THAN NORMAL. THIS HAPPENS FROM BOTH OUTSIDE AND INSIDE. ALSO, A LOUD BINDING SOUND CAN BE HEARD FROM THE SIDE PINS ASDR DXTA2024081200182Switch · brokenEMERGENCY LIGHTING: WHEN RUNNING POWER ON CHECKLIST. EMERGENCY LIGHT TEST FAILS. NO LIGHTS AT ALL. TROUBLESHOT DOWN TO FAULTY EMERGENCY LIGHTING SWITCH. REMOVED PILOT SEAT FOR EASE OF ACCESS TO SWITCH REMOVED FAULTY SWITCH PN: AL-1269 AND SOLDERED IN NEW SWITCSDR 3EJA803JS081124Cabin Pressure · faultedDURING CLIMB THROUGH 14000, THE CAB ALT ANNUNCIATOR ILLUMINATED, WITHIN 30 SECONDS TO A MINUTE THE EMERGENCY PRESSURIZATION ACTIVATEDSDR DXTA2024080500106Precatch · faultedMAIN DOOR PRECATCH HOLDS THE MAIN DOOR CLOSED BUT DOES NOT RELEASE IT. TROUBLESHOT THE MAIN ENTRY DOOR PRECATCH NOT CATCHING THE DOOR WHEN CLOSING, GAINED ACCESS TO THE PRECATCH LEVER, INSPECTED AND FOUND THE LEVER DRIED OUT AND HOLDING BACI< THE PRECATCH LEVSDR DXTA2024080200058Precatch · engagedREPEAT WRITE UP. WHEN OPENING THE CABIN, THE PRECATCH IS STILL ENGAGED. PUSH BUTTON FROM THE OUTSIDE OR THE HANDLE FROM THE INSIDE MUST BE USED TO OPEN THE DOOR. ATTEMPTED TO OPEN FOUR TIMES FROM THE EXTERIOR AND INSIDE THE CABIN. ADJUSTED PRE-CATCH IAW TC-5XLSDR 3EJA2024080124Indicator · inoperativeNO GREEN LEFT LANDING GEAR LIGHT ON APPROACH. UNSAFE GEAR CONDITION. DECLARED EMERGENCY. DIVERTED TO PBI. DID THE LOWER APPROACH BURN OFF SOME FUEL AND HAD AN UNEVENTFUL LANDING. THE LIGHT DID COME ON, FINALLY ON SHORT APPROACH INTO PALM BEACH.SDR 2024FA0000551Skin · corrodedMECHANICALLY REMOVED 2 AREAS OF CORROSION FOUND IN ZONE 513 AT WING STATION 97.00 THROUGH 99.00 AND FRAME STATION 335 OF THE LH UPPER WING SKIN, FWD OF SPAR CAP PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION.SDR JGVR202407290001Door Frame · chafedEMERGENCY EXIT CUT OUT, HAS A CHAFE LOCATION ON AN EXISTING REPAIR ON INNER WEB BETWEEN F.S. 123.46 AND 131.04. RE COMPLIED WITH EXISTING AQRD ERO-868105 REV IR DATED 10/25/2016 TITLED: CHAFE REPAIR. REMOVED EXISTING REPAIR THAT WAS CHAFED BEYOND ALLOWABLE LIMSDR DXTA2024072412454Precatch · failedMAIN DOOR PRECATCH: MAIN DOOR PRECATCH HOLDS THE DOOR CLOSED BUT FAILS TO OPEN WHEN PUSHED. THIS HAS BEEN WRITTEN UP TWICE BEFORE. ACCESSED THE PRECATCH RELEASE MECHANISM BY MOVING THE DOOR TRIM FROM THE FOWARD DOOR FRAME, ADJUSTED THE PRECATCH CABLE TO BE ABSDR DXTA2024072212439G Switch · trippedEXIT LIGHT ABOVE MAIN CABIN DOOR,¿ EXIT SIGN LEFT AND RIGHT OF MAIN CABIN DOOR AND READING LIGHT AT SEAT NR. 3 AND NR. 10 ARE STEADY ILLUMINATED. THEY WILL EXTINGUISH WITH THE EMER LTS IN THE OFF POSITION. WITH THE EMER LTS IN THE ON OR ARM POSITION THEY ARE ASDR JGVR202407220003Door Frame · chafedPERFORM REPAIR TO EMERGENCY EXIT DOUBLER CHAFE LOCATIONS. PER: ERO-980291. PERFORMED REPAIRS TO 5 EACH CHAFE LOCATIONS IN CABIN SURROUNDING EMERGENCY EXIT AND LH AND RH SUBSTRATE MOUNTING LOCATIONS. RE PROTECTED AREAS WITH ETCH, ALODINE AND EPOXY PRIMER. REPAISDR DXTA2024072212427Door · unknownMAIN DOOR WILL NOT CLOSE UNDER NORMAL OPERATIONS. WITH THE DOOR FULLY OPEN THE HANDLE WILL MOVE TO THE LOCK POSITION WITH EASE. DURING OPS CHECK OF MED, DOOR BAYONETS GOT STUCK IN THE DOOR. DOOR WOULD NOT OPEN YET THE ENTRY HANDLE ROTATES. T. FURTHER DISSASSEM
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