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 DXTA2021060142850Condenser · dirtyCABIN ODOR: STINKY FOUL SMELL COMING OUT OF WEEMACS WITH APU BLEED AIR ON. SUSPECT A DIRTY CONDENSOR SOCK IS THE CULPRIT. UNSUITABLE SMELL FOR PASSENGERS. VERIFIED THE SQK AND REMOVED THE WATER SEPARATOR, AND ONCE IT WAS OPENED IT UP, IT WAS THE EXACT SAME SDR DXTA2021052442490Seal · defectiveMAIN DOOR: MAIN CABIN DOOR OPEN WITH EXTREME DIFFICULTY AFTER BEING AT ALTITUDE FOR ANYTHING OVER ONE HOUR. I.E. ONCE OPEN ON THE GROUND IT OPERATES FINE. REPEAT WRITE UP///SIGN-OFF///REPLACED SHEARED OFF BOLT AND ALL 3 ACCOUSTIC LINER SEALS IAW CE-560XLS AMMSDR O2GA2021052551501Actuator · inoperativeAFTER TAKEOFF, GEAR RETRACTION, NOSE LANDING GEAR DID NOT RETRACT. FOLLOWED CHECKLIST. EMERGENCY DECLARED AND DIVERTED TO KJAX. MAINTENANCE REPLACED THE NLG ACTUATOR. GROUND OPERATIONAL CHECK PERFORMED WITH NO DEFECTS. A SUCCESSFUL OPERATIONAL CHECK FLIGHT WASDR DXTA2021052142370Striker · out of positionMAIN DOOR: REPEAT WRITEUP: AMBER "CABIN DOOR" ANNUNCIATOR LIGHT ILLUMINATED AT 6,000 FEET ON INITIAL CLIMB. NOTE: THE "PRESS SYSTEM SELECT" LEVER HAS BEEN LEFT IN THE "MANUAL" POSITION AS PER THE CHECKLIST. ADJUSTED DOOR PLUNGER STRIKER PLATE UNTIL DOOR LOCKSDR 9JLA2021052510313Fan · defectiveTHE FLIGHT CREW REPORTED THE ENVIRONMENTAL CONTROLLER WOULD NOT WORK IN AUTO MODE. THE MAINTENANCE TEAM TROUBLESHOT AND DETERMINED THE CABIN TEMP SENSOR FAN WAS DEFECTIVE. A NEW CONDITION FAN WAS INSTALLED. FUNCTIONAL CHECKS WERE SATISFACTORY AND THE AIRCRAFT SDR 9JLA2021052521897Bellcrank · brokenTHE FLIGHT CREW REPORTED THE THE LEFT PILOTS SEAT MOVEMENT LEVER WOULD NOT ALLOW THE SEAT TO BE MOVED FORWARD OR BACKWARD. SEAT WAS LOCKED TO SEAT TRACKS. THE MAINTENANCE VENDOR DISCOVERED A BROKEN BELLCRANKS P/N 1B1421-3 AND 1B1421-5. INSTALLED NEW PARTS, OPSSDR DXTA2021051742040Mechanism · lack of lubeMAIN DOOR HANDLE: MAIN CABIN DOOR HANDLE INSIDE WILL ONLY MOVE HALF WAY. UNABLE TO MOVE THE HANDLE ALL THE WAY TO CLOSE THE DOOR FROM THE INSIDE///SIGN-OFF///PERFORMED TROUBLESHOOTING OF MED IAW CE-560XL AMM 52-10-00. FOUND EXCESSIVE FRICTION IN DOOR MECHANISSDR DXTA2021051442030Brake · weakRIGHT MLG BRAKE: AT SLOW SPEED WITH MINIMUM RIGHT SEAT PILOT BRAKE APPLICATION THE RIGHT LANDING GEAR BRAKE LOCKED UP AND RELEASED TWICE IN RAPID SUCCESSION.///SIGN-OFF///ARRIVED AT AIRCRAFT AND PERFORMED GVI OF BRAKES. SERVICED SYSTEM AS REQUIRED. PERFORMEDSDR DXTA2021051441990Catcher · inoperativeMAIN DOOR: MAIN CABIN DOOR. WHEN OPENING THE MAIN CABIN DOOR FROM THE OUTSIDE, THE HANDLE UNLOCKS DOOR, BUT PRE-CATCH DOES NOT RELEASE. DOOR WILL NOT OPEN. PUSHING THE PRE CATCH RELEASE BUTTON ALLOWS THE DOOR TO OPEN. REPEAT ITEM FROM 5/12/21.///SIGN-OFF///FOUSDR DXTA2021051441960Relay · intermittentBRAKE PRESSURE LIGHT: DURING TAXI OUT BOTH LOW PRESSURE AND ANTISKID LIGHTS ILLUMINATED ALONG WITH MASTER CAUTION. CIRCUIT BREAKERS DID NOT POP. USED EMERGENCY BRAKES TO STOP THE AIRCRAFT DUE TO COMPLETE LOSS OF BRAKE PRESSURE. // SIGNOFF // TROUBLE SHOT AND SDR 9JLA2021051819052Starter Gen · vibrationTHE FLIGHT CREW REPORTED THAT DURING APU OPERATIONS A LOW FREQUENCY VIBRATION ALONG WITH THE SMELL OF BURNT OIL FROM THE APU BLEED AIR. THE MAINTENANCE VENDOR DETERMINED THAT THE APU STARTER/GEN CAUSING THE VIBRATION. THE STARTER/GEN WAS REMOVED (TOTAL TIME INSDR DXTA2021051341940Fan · defectiveWHILE IN CRUISE FLIGHT AT 39,000FT, WE HAD A STRONG ODOR FILL THE COCKPIT AND CABIN. THE CREW AND PAX BOTH NOTICED THE SMELL AND IT WAS ON THE SIDE OF AN ELECTRICAL BURNING SMELL. THERE WAS NO HAZE OR SMOKE OF ANY KIND. IT TOOK APPROXIMATELY 4 MIN FOR THE ODORSDR DXTA2021051241930Riser · failedDURING MX WHEN QA INSPECTOR WAS EXITING THE AIRCRAFT THE STEP FAILED CAUSING DAMAGE TO THE STEP HINGE. REMOVED AND REPLACED RISER ASSY AND RISER COVER WITH NEW RISER AND RISER COVER IAW CE560XL.S MM S2-10-02 AND SRM 51-40-08. ALL OPS CHECKS OF DOOR AND STEPSSDR 9JLA2021060433250Valve · faultedTHE FLIGHT CREW REPORTED THAT DURING TWO TAKEOFF ATTEMPTS THE LEFT EEC FAILED WHEN THE THROTTLES WERE ADVANCED FOR TAKEOFF. THE MAINTENANCE VENDOR DETERMINED BOV/LVDT FAULTY. THE MX VENDOR REMOVED AND REPLACED THE UNIT WITH AN OVERHAULED UNIT.SDR 9JLA2021052726312Lock · dirtyTHE FLIGHT CREW REPORTED THAT THE CABIN DOOR ANNUNCIATOR LIGHT ILLUMINATED JUST AFTER TAKEOFF. THE CREW RAN THE CHECKLIST AND ELECTED TO RETURN BACK TO THE AIRPORT FOR LAND AND INVESTIGATION. THE MAINTENANCE TECH DETERMINED THE DOOR LOCKING MECHANISM REQUIRED SDR 9JLA2021051826312Latch · dirtyTHE FLIGHT CREW REPORTED THAT THE CABIN DOOR LOCK INDICATION CAME ON AFTER TAKEOFF. THE FLIGHT CREW OPTED TO DIVERT BACK TO THE AIRPORT FOR LANDING AND MAINTENANCE CONSIDERATIONS. THE LANDING WAS UNEVENTFUL. THE DOOR LOCK INDICATION SYSTEM WAS DEFERRED PER MELSDR 9JLA2021051827629Check Valve · leakingTHE FLIGHT CREW REPORTED DURING PREFLIGHT CHECKS THE LOWER (L) PRE-CHECK LEVER WAS LEAKING FUEL. THE PLANNED FLIGHT WAS CANCELLED. THE MAINTENANCE VENDOR REMOVED AND REPLACED THE PRE-CHECK VALVE ASSEMBLY WITH A NEW UNIT. OPERATION AND LEAK CHECKS WERE SATISFACSDR DXTA2021050541630Converter · defectiveCOCKPIT ODOR: AFTER TAKEOFF EXPERIENCED AN OBNOXIOUS ODOR IN THE COCKPIT. AIRCRAFT HAS HAD A PREVIOUS WRITE UP FOR APU SMOKE, WE RAN THE APU FOR ROUGHLY 45 MINUTES BEFORE DEPARTURE WITH NO UNUSUAL ODORS. APU WAS SHUT DOWN SHORTLY AFTER ENGINE START. RETURNED SDR 3EJA86705/13/21Window · failedCAPTAINS SIDE WINDOW SHATTERED ON CLIMB OUT. R/R LH HEATED SIDE WINDOW IAW CE560 AMM 56-12-00. LEAK CHECK GOOD.SDR DXTA2021042741280Apu · smokeSMOKE IN COCKPIT / CABIN: AFTER COMPLETING THE POWER ON CHECKLIST, WITH THE APU BLEED AIR ON, THE COCKPIT AND CABIN BEGAN TO FILL WITH SMOKE. FOUND APU OIL WAS OVER SERVICED. RE-SERVICED APU OIL TO THE CORRECT LEVEL IAW 680A MM CHAP. 12-20-20. OPERATED APU SDR 2021FA0000110Pan · crackedMULTIPLE AIRCRAFT HAVE COME INTO INSPECTION WITH CRACKED SEAT PANS P/N 1D2016-1 AND 1D2016-2 IN THE PILOT AND COPILOT SEATS. PARTS ARE IN SHORT SUPPLY AND NO REPAIRS ARE AUTHORIZED BY THE OEM.SDR CVGA20210422001Warning Message · illuminatedAFTER TAKEOFF WE HAD A "STAB MISC" LIGHT ILLUMINATE. WE STAYED BELOW 200KTS AND CONTINUED OUR CLIMB BUT THE LIGHT ON HYD LIGHT WENT OUT. AT ALT, WE FOLLOWED THE CHECKLIST TO NO AVIAL. TRIED FLAPS 7 DEGREES TO 15 DEGREES WITH NO CHANGE.SDR DXTA2021041940930Lever · unsecureMAIN DOOR PRECATCH LEVER: PRE-CATCH LEVER FLOPS AROUND. SECURED MAIN DOOR PRECATCH LEVER HANDLE IN REF WITH 52-10-01 OF THE CE-560XL AMM. NO FURTHER FAULTS FOUND AT THIS TIMESDR DXTA2021041340760Socket · out of adjustMAIN DOOR: MAIN CABIN DOOR VERY DIFFICULT TO CLOSE FROM OUTSIDE OF CABIN . SOUNDS LIKE METAL GRINDING. ADJUSTED AFT BOTTOM PIN SOCKET, GAINED SUBSTANTIAL EASE OF OPERATION: OPS CHECK GOOD. ALL WORK DONE IAW AMM 52-10-00.SDR DXTA2021040240370Apu · smokeAPU SMOKE: AFTER LANDING WE STARTED THE APU WITH BLEED AIR ON AND DID TAXI FOR APPROX 8 MIN, DEPLANED THE PAX AND ONCE DONE NOTICED THICK SMOKE IN CABIN AND COCKPIT. WE IMMEDIATELY DID SHUT DOWN THE APU AND THE SMOKE DISSIPATED AFTER ABOUT 15 MIN. NO EXTERIOR SDR DXTA2021033040270Control Valve · defectiveACM OVERHEAT ON TAKEOFF. THERE WAS A HOT/BURN SMELL IN THE AIRCRAFT. COMPLETED CHECKLIST AND LANDED. DID NOT DECLARE AN EMERGENCY. DID NOT LAND OVER WEIGHT. COMPLIED WITH OPERATIONAL PROCEDURE. REMOVED AND REPLACED RH FLOW CONTROL VALVE. IAW 560XL MM 21SDR DXTA2021032940030Seal · crackedCOCKPIT/CABIN NOISE: ON TAKEOFF ROLL APPROACHING 50 KTS, WE HEARD A LOUD POPPING NOISE ( LIKE GUN SHOT)COMING FROM THE MAIN CABIN DOOR. FOLLOWED BY LOUD HISSING FROM AFT INBOARD MAIN CABIN DOOR. AFTER BLOCK IN FOUND HOLE IN RUBBER SEAL INSIDE THE CABIN DOOR FRSDR DXTA2021032539970Coalescer Bag · dirtyAIR CONDITIONING COMPRESSOR: WITH APU BLEED AIR RUNNING, THERE WAS A DIRTY SOCK SMELL IN THE AFT CABIN AREA. POWERED UP AIRCRAFT WITH APU. CONFIRMED WITH APU BLEED AIR THERE IS A SMELL TO THE AIR COMING FROM THE DUCTS. ACCOMPLISHED TC-5XL-21-120902M ENVIRONMESDR DXTA2021032239770Door · bindingMAIN DOOR: MAIN ENTRY DOOR EXTREMELY DIFFICULT TO OPEN, HAD TO CYCLE FOUR TIMES FROM LOCK TO UNLOCK IN ORDER TO ALLOW THE MAIN ENTRY DOOR TO OPEN ,IT FELT LIKE THE BAYONET LUGS WERE NOT RELEASING, ATTEMPTED TO RELEASE IT USING PRE-CATCH AND IT HAD NO EFFECT. SDR 9JLA2021032427546Line · leakingTHE FLIGHT CREW REPORTED UPON POST FLIGHT INSPECTION, NOTICED POOL OF HYDRAULIC FLUID ON GROUND NEAR LEFT MAIN BRAKE, AND FLUID ON BRAKE LINES DRIPPING. THE MAINTENANCE TEAM DISCOVERED THAT THE LEFT BRAKE SHUTTLE VALVE WAS LEAKING. THE VALVE WAS REMOVED AND RESDR 9JLA2021032427544Transmitter · faultedTHE FLIGHT CREW REPORTED THAT THE LH OIL PRESSURE INDICATOR "TAPE JUMPS". THE MAINTENANCE TEAM DETERMINED THAT THE LEFT ENGINE OIL PRESSURE TRANSMITTER WAS DEFECTIVE. A NEW TRANSMITTER WAS INSTALLED FUNCTIONAL AND LEAK CHECKS WERE SATISFACTORY. THE AIRCRAFT WASDR O2GA2021032350201Switch · inoperativeON GEAR RETRACTION FELT A SHUTTER AND THE LANDING GEAR UNLOCK ANNUNCIATOR REMAINED ILLUMINATED. STAB MIS-COMPARE AND THE HYDRAULIC PRESSURE ANNUNCIATOR ALSO REMAINED ILLUMINATED. MAINTENANCE REPLACED THE LEFT AND RIGHT LANDING GEAR UPLOCK SWITCHES. A SUCCESSFUSDR O2GA2021032351201Water Separator · contaminatedAFTER ENGINE START WITH APU RUNNING FUNNY SMELL IN COCKPIT AND LIGHT SMOKE IN CABIN. ENGINES/APU SHUT DOWN AND CREW DEPLANED THE PASSENGERS. EMERGENCY VEHICLES WERE STANDING BY. NO EVIDENCE OF HOT SPOTS NOTED. MAINTENANCE ISOLATED THE DISCREPANCY TO A FAULTY ASDR DXTA2021031539490Sign · inoperativeCABIN EMERG LIGHT: RED EXIT SIGN ABOVE PRECATCH (FORWARD OF MAIN CABIN DOOR) IS INOP. WHEN ACTUATING AND/OR JIGGLING THE PRECATCH LEVER, SOMETIMES THE EXIT SIGN WILL ILLUMINATE INTERMITTENTLY. REMOVED AND REPLACED CABIN EMERGENCY LIGHT FORWARD OF MED IAW CE-5SDR DXTA030220213893Bolt · backed outENTRANCE STAIR HARDWARE: FORWARD TELESCOPING MAIN DOOR BRACE HAS ATTACHMENT HARDWARE THAT IS BACKING OUT. INSPECTED PIN AND CONFIRMED WRITE-UP. RE-SECURED PIN AS REQUIRED, USING ORIGINAL HARDWARE, I.R.W. CE-560XLS AMM 52-10-01-2. THE DOOR AND TELESCOPE ROD SDR DXTA0301202138800Engine · failedRIGHT ENGINE OIL PRESSURE LOW ANNUNCIATOR WITH MASTER WARNING. AT 13,000FT, DURING CLIMB OUT, WITH CLIMB POWER SET AIRSPEED 250 KNOTS OIL PRESSURE INDICATES ZERO FOR APPROX 3 MINUTES. RAN QRH OIL. *** CORRECTIVE ACTION *** PER PWC ENGINEERING, PCE·DD0355 IS TOSDR DXTA030120213880Warning Message · activatedRIGHT ENGINE OIL PRESSURE LOW ANNUNCIATOR WITH MASTER WARNING. AT 13,000FT, DURING CLIMB OUT, WITH CLIMB POWER SET AIRSPEED 250 KNOTS OIL PRESSURE INDICATES ZERO FOR APPROX 3 MINUTES. RAN QRH OIL [T2PL6D0083DX5]SDR JGVR20210225001Structure · corrodedFOUND THE UPPER TRAILING EDGE EXTRUSION ON THE RUDDER TO BE CORRODED BEYOND LIMITS. REPLACED UPPER TRAILING EDGE EXTRUSION WITH NEW CESSNA PN 5533000-30. PAINTED AND BALANCED RUDDER AS REQUIRED.SDR DXTA022320213856Linkage · out of adjustMAIN DOOR HARDWARE: MAIN CABIN DOOR OVER CENTER DOWN LOCK WHEN DOOR IS OPEN DISENGAGES AND WILL NOT LOCK DOWN. AFTER DOOR IS OPEN DOOR WILL POP UP AND ATTEMPT TO CLOSE WITHOUT GRABBING HANDLE TO DO SO. (POST FLIGHT) // SIGN OFF // ADJUSTED DOOR OVER CENTER SDR DXTA022220213845Screw · brokenMAIN DOOR HANDLE: MAIN ENTRANCE DOOR INSIDE HANDLE BROKEN. HANDLE MOVES FREELY. REMOVED STEPS AND INSPECTED HANDLE ASSY, FOUND BOTH SCREWS ATTACHING THE HANDLE TO THE SHAFT SHEARED OFF. REMOVED FAILED FASTENERS AND REPLACED WITH NEW. REINSTALLED STEPS. DOSDR JGVR20210216001Torque Tube · corrodedLH ELEVATOR TORQUE TUBE IS CORRODED. REMOVED CORRODED INBOARD TORQUE TUBE DUE TO LEVEL 2 CORROSION FROM L/H ELEVATOR P/N 6634200-809LH S/N 0000210. INSTALLED NEW CUSTOMER SUPPLIED TORQUE TUBE P/N 6634002-15 PER CESSNA 560XL SRM 51-40-03, 51-40-06, AND 55-20-02SDR DXTA2021021504744Rod · inoperativeMAIN DOOR TELESCOPING ROD: MAIN CABIN DOOR WILL NOT CLOSE. TELESCOPING ARMS WILL NOT FULLY RETRACT. AIRCRAFT DEPARTED SC IN MODERATE TO HEAVY RAIN. OUTSIDE AIR TEMPERATURE IN MDW IS CURRENTLY -18C. FBO WILL NOT PROVIDE HANGAR SPACE. REMOVED AFT STRUT ANDSDR DXTA2021021204719Switch · defectiveCABIN DOOR ANNUNCIATOR CAME ON INFLIGHT AND STAYED ON CLIMBING THROUGH FL360. NO OTHER INDICATIONS PRESENT. TROUBLESHOT CABIN DOOR ANNUNCIATOR COMING ON IN FLIGHT AND STAYING ON CLIMBING THROUGH FL360 AND FOUND ELECTRICAL CONNECTOR PM007 LOOSE. TIGHTENED CONSDR XCGA20210212001Actuator · false indicationWHILE ON FINAL APPROACH TO KPIT WHEN THE FLIGHT CREW LOWERED THE LANDING GEAR THE GEAR UNSAFE LIGHT REMAINED ON AND THE RIGHT GEAR GREEN LIGHT DID NOT COME ON. AT THAT TIME, THE FLIGHT CREW ADVISED AIR TRAFFIC CONTROL THAT THEY WOULD NOT CONTINUE THE APPROACH SDR DXTA2021021004705Pcb · defectiveUPON REACHING FL390 THE CABIN DOOR ANNUNCIATOR ILLUMINATED. ALL GREEN FLAGS WERE VISIBLE AND NO OTHER WARNING LIGHTS (SIX PACK) WERE ILLUMINATED.///SIGN-OFF///REMOVED MAIN CABIN DOOR STEPS PER CE-560XL MM 52-10-02. OPERATED MAIN CABIN DOOR WITH NO FAULTS FOUNDSDR 9JLA2021021222617Computer · defectiveTHE FLIGHT CREW REPORTED THAT THE AUTO-PILOT KICKED OFF IN FLIGHT AT THE TOP OF DESCENT. THE MAINTENANCE PROVIDER REMOVED THE NO2 FLIGHT GUIDANCE COMPUTER P/N 822-1108-143 S/N 3N3BX AND INSTALLED AN OVERHAULED FGC. OPERATIONAL CHECKS WERE SATISFACTORY AND THE SDR DXTA2021020304672Battery Pack · inoperativeREPEAT WRITE: THE WHITE EMER EXIT LIGHT OVER THE MAIN ENTRANCE DOOR AND THE TWO RED EXIT LIGHTS FWD AND AFT OF THE MAIN ENTRANCE DOOR ARE ALL INOP. ALSO, THE FWD FLOOR PATH LIGHTING IS INOP. THE EMER LIGHTS OVER SEATS 10 AND 3 WORK NORMALLY WITH THE READINGSDR 9JLA2021020421323Boot · failedTHE FLIGHT CREW REPORTED THAT IN FLIGHT WHEN THE AIRCRAFT WAS COLD SOAKED THE RIGHT TAIL DEICE FAILED. THE MAINTENANCE VENDOR DETERMINED THAT THE RIGHT TAIL DEICE BOOT HAD FAILED. THE DEFECTIVE BOOT WAS REMOVED AND A NEW BOOT WAS INSTALLED. OPERATIONAL CHECKS SDR 9JLA2021020411098Switch · defectiveTHE FLIGHT CREW REPORTED THAT THE LANDING GEAR WARNING HORN WOULD NOT TEST ON ROTARY CHECK. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THAT THE ROTARY TEST SWITCH WAS DEFECTIVE. THE SWITCH WAS REPLACED WITH A NEW UNIT. OPERATIONAL CHECKS WERE SATISFACTOSDR 9JLA2021021215735Torque Motor · inoperativeTHE FLIGHT CREW REPORTED OF AN INTERMITTENT RIGHT ELECTRONIC ENGINE CONTROL ANNUNCIATOR WHILE IN FLIGHT. THE FLIGHT CREW RAN THE APPROPRIATE CHECKLIST. LANDING WAS UNEVENTFUL. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THE TORQUE MOTOR WAS INOP. P/N 30J
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