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 DXTA200500523Pedal · damagedPILOTS LEFT BRAKE PEDAL WENT TO FLOOR ON LANDING ROLL. CO-PILOTS BRAKES WORKED FINE. ITEM IS UNDER INVESTIGATION.SDR CA050120006Line · cracked(CAN) AIRCRAFT DEPARTED. AS THE AIRCRAFT ACCELERATED THE CREW BECAME CONCERNED DUE TO A VIBRATION. THE AIRCRAFT WAS DIVERTED TO INTERNATIONAL AIRPORT. INVESTIGATION FOUND A CRACK IN THE HYDRAULIC LINE FROM THE LT ENGINE DRIVEN HYDRAULIC PUMP WHERE IT CONNECTSDR DXTA200500520Cylinder · malfunctionedRED UNLOCK LIGHT ON GEAR FLASHED (OR CYCLED) AFTER GEAR RETRACTION. UPON EXTENDING GEAR, HAD 2 "BUMPS" LIKE HYDRAULIC ACTUATION RESULTING IN MOMENTARY LOSS OF DOWN & LOCKED INDICATIONS. GEAR WAS BLOWN DOWN. RT ACTUATOR LEAKING EXCESSIVELY, REMOVED AND REPSDR DXTA200500516Bulb · inoperativeDURING LANDING CHECK WHEN SELECTING LANDING GEAR DOWN, DID NOT GET GREEN SAFE NOSE GEAR INDICATION. CHECKED ROTARY TEST AND INDICATED NOSE GEAR GREEN LIGHT INOP. PERFORMED MANUAL GEAR EXTENDED IAW CHECKLIST AND BLEW THE NOSE GEAR DOWN. TROUBLESHOT TO BAD NOSDR DXTA200500514Limit Switch · failedNO TAKEOFF LIGHT WILL NOT GO OUT ON GROUND, HORN SOUNDS WHEN POWER IS ADVANCED ALL ASSOCIATED SYSTEMS CHECKED / NO PROBLEMS INDICATED. FOUND STAB POSITION SWITCHES OUT OF ADJUSTMENT AND CORROSION ON SPEED BRAKE SWITCH CONNECTORS. ADJUSTED HORIZONTAL STAB POSISDR DXTA200500512Reservoir · lowLANDING GEAR WOULD NOT RETRACT. INSPECTED SYSTEM PER M/M 32-30-00, RAN GEAR UP & DOWN SEVERAL TIME NO DEFECTS NOTED, OPS CHECK GOOD. SERVICED HYD RESERVOIR.SDR DXTA200500511Master Cylinder · malfunctionedLEFT BRAKE PEDAL ON LEFT SIDE GOES ALL THE WAY DOWN WHEN BRAKES APPLIED. TROUBLESHOT LEFT BRAKE TO MASTER CYLINDER. REMOVED AND REPLACED PILOT'S LT WHEEL BRAKE MASTER CYLINDER WITH A SERVICEABLE INSPECTED BRAKE MASTER CYLINDER IAW ESSNA 560XL MM CHAPTER 32-4SDR DXTA200400502Uplock · out of adjustAFTER TAKEOFF NOSE GEAR WOULD NOT FULLY RETRACT. CYCLED ON UPLOCK ON & OFF (UNLOCK LIGHT). ADJUSTED NOSE GEAR UPLOCK. OPS CHECK GOOD. WORK DONE IAW CESSNA 560XL MAINTENANCE MANUAL 32-30-05.SDR 5285001Thrust Reverser · lack of lubeLT THRUST REVERSER WOULD NOT DEPLOY AFTER LANDING. OCCURRED AFTER A FLIGHT 2 HOURS IN CLEAR AIR AND DESCENT INTO HAZY BELOW FREEZING MOISTURE CONDITIONS. MAINTENANCE FOUND LUBRICATION NEEDED. LUBRICATED AND F/C SATISFACTORY.SDR DXTA200400501Brake · fireON TAXI IN, GROUND PERSONNEL NOTICED THE LT WHEEL WELL HAD A FIRE, FLIGHT CREW DID NOT NOTICE ANY GRINDING, PULLING, OR VIBRATION INDICATING A PROBLEM. INSPECTED LT MAIN LANDING GEAR AND SURROUNDING WING AREA FOR DAMAGE, NONE NOTED. REMOVED LT MAIN WHEEL ASSSDR DXTA200400500Switch · malfunctionedAFTER GEAR UP/FLAPS UP HAD HYD PRESS, STAB MISCOMPARE ANNUNCIATORS AND UNLOCK GEAR LIGHT. PULL HYD C/B, AND LOUD THUMP HEARD AND FELT IN NOSE GEAR AREA. PUSH HYD C/B IN GET SAME NOISE. ALL LIGHTS OUT AND SYSTEMS WORKED FINE WITH GEAR DOWN AND FLAPS FULL AT SDR DXTA200400499Landing Gear · malfunctionedAFTER TAKEOFF NOSE GEAR WOULD NOT GET INTO UPLOCK AND CONTINUED TO CLUNK IN WHEEL WELL. HYDRAULIC PRESSURE LIGHT WOULD NOT GO OUT. ITEM IS UNDER INVESTIGATION.SDR DXTA200400487Connector · dirtyWHEN GEAR WAS SELECTED DOWN, RIGHT MAIN GEAR LIGHT DID NOT ILLUMINATE AND GEAR UNLOCKED LIGHT REMAINED ON. AFTER RECYCLING THE GEAR, THE GEAR LOCKED WITH RECEIVED THREE GREEN LIGHTS. JACKED AIRCRAFT CLEANED/RESEATED ALL GEAR WIRING CONNECTORS COMPLIED WITH (2SDR DXTA200400489Module · failedRIGHT GEAR LIGHT CAME ON DURING FLIGHT (GEAR HANDLE UP) FOLLOWED BY LOW BRAKE PRESS & ANTI SKID INOP CAUTION LIGHT ON. AFTER 20 MIN ALL 3 LIGHTS EXTINGUISHED, DURING DESCENT (10,000 FT) OPERATION OF GEAR AND BRAKES DURING LANDING WAS NORMAL. REPLACED LANDINSDR DXTA200400470Warning System · activatedLOW BRAKE PRESSURE/ANTISKID INOP (IN-FLIGHT) ANNUNCIATOR ILLUMINATED WITH RT GEAR LIGHT ILLUMINATED. CHECKLIST CONDUCTED EMERGENCY BRAKES USED. ITEM IS UNDER INVESTIGATION.SDR DXTA200400461Fuel Filter · warning lightDURING TAKEOFF ROLL FUEL FILTER L-ANNUNCIATOR ILLUMINATED. TAKEOFF ABORTED, ANNUNCIATOR EXTINGUISHED DURING ABORT. REPLACED LEFT AND RIGHT ENGINE FUEL FILTER AND ASSOCIATED PACKING. PERFORMED SATISFACTORY ENGINE RUNS AND LEAK CHECKS. REFERENCE P + W 545 AMSDR CWQR200400006Tube · crackedAIRCRAFT WAS LEAKING FUEL. TECHNICIAN FOUND A 1.3 INCH CRACK IN -Y- TUBE IN PRESSURE REFUELING SYSTEM. NO EVIDENCE OF DAMAGE TO TUBE ASSY. REPLACED TUBE ASSY, AND LEAK CHECKED GOOD.SDR DXTA200400460Filter · warning lightDURING TAKEOFF ROLL MASTER CAUTION ILLUMINATED TRIGGERED BY RIGHT ENGINE FUEL FILTER BY-PASS ANNUNCIATOR. REMOVED AND REPLACED RT FUEL FILTER IAW P&W 545 MM CHAPTER 73-10-07. LEAK CHECK GOOD, FILTER INSTALLED IS NEW. OPERATIONAL CHECK SATISFACTORY.SDR CA050107001Hmu · failed(CAN) RT ENGINE WOULD NOT START.SDR CA041202004Control Cable · broken(CAN) DUE TO THE RISK ASSOCIATED TO BROKEN MAIN CONTROL CABLES, FOLLOWING THE BROKEN RT WING DOWN OB AILERON CABLE P/N 6660001-62 AT RWS 54 (REF. SDR NR 20031113014), WE DECIDED TO INSPECT THE AILERON WING CABLES MORE FREQUENTLY THAN THE 1200 HRS REQUIRED BY SDR DXTA200400455Landing Gear · malfunctionedLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF, BLEW GEAR DOWN AND LANDED SAFELY. RESECURED EMERGENCY GEAR HANDLE CABLE CLEVIS ASSY AND REAFFIXED EMERGENCY GEAR BOTTLE SAFETY WIRE, EMERGENCY GEAR BOTTLE FOUND PROPERLY SERVICED. PERFORMED LANDING GEAR HYDRAULICSDR DXTA200400451Line · leakingBRAKE PEDALS ARE SOFT AND GO TO THE FLOOR ON LANDING, ALSO ON POST AIRCRAFT INSPECTION THERE APPEARS TO BE A PUDDLE OF HYDRAULIC FLUID UNDER THE CO-PILOTS BRAKE PEDAL. FOUND CO-PILOTS LEFT BRAKE PEDAL VALVE HAS A BROKEN LINE AT TOP OF CYLINDER. REMOVED & REPSDR CA041117004Engine · fire(CAN) SHORTLY AFTER TAKEOFF, THE CREW WERE ADVISED OF SMOKE AND FLAMES EMANATING FROM THE ENGINE. THE ENGINE WAS SECURED AND AN UNSCHEDULED LANDING WAS PERFORMED AT POINT OF DEPARTURE. P&WC WILL INVESTIGATE THE EVENT AND WILL REVISE THIS REPORT TO REFLECT ROSDR DXTA200400448Controller · inoperativeDURING T/O ROLL, AT 70 KIAS A LOUD BANG FROM TAIL AREA FOLLOWED BY A PRESSURE BUMP. STRONG SMOKE ODOR, NONE VISIBLE. COULDN’T DETERMINE WHERE SMOKE ODOR WAS COMING FROM, SEEMED TO COME FROM AIR VENTS. GND IDLE LIGHT REMAINED ILLUM UNTIL 1000 FT AGL. PRESS SEESDR DXTA200400445Anti-Skid Sys · inoperativeON APPROACH, BROUGHT THE LANDING GEAR DOWN BOTH ANTI-SKID INOP AND LOW BRAKE PRESSURE ANNUNCIATORS REMAINED ILLUMINATED. CYCLED THE GEAR AND RAN THE CHECKLIST, THE POWER BRAKES CB WAS IN WHEN RUNNING THE CHECKLIST. EMERGENCY BRAKES WERE USED TO STOP AIRCRAFTSDR 100704Starter Gen · meltedENGINE WOULDN'T START. BRUSHS HOUSING ON STARTER GENERATOR MELTED.SDR CA050324009Uplock Switch · failed(CAN) AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT, THE AIRCRAFT RETURNED TO THE AIRPORT. THE NOSE GEAR UPLOCK SWITCH WAS FOUND TO BE FAILED. THE SWITCH WAS REPLACED, MULTIPLE SATISFACTORY GEAR SWINGS WERE CARRIED OUT AND THE AIRCRAFT WAS RETURNED TO SERVSDR 092904Starter Gen · meltedLT ENGINE FAILED TO START. SEVERE ARCING ON COMMUTATOR, AND BRUSHES. CAUSING BRUSHES TO MELT.SDR 2004FA0000852Windscreen · distortedON DELIVERY OF NEW A/C, DAY ACCEPTANCE CHECK CARRIED OUT AND A/C ACCEPTED. DURING NIGHT FLYING LT WINDSCREEN OBSERVED TO HAVE PARALLAX DISTORTION ERROR. DAY TESTS CARRIED OUT OF GRID TEST AND WATER TEST. WINDSCREEN CERTIFIED SERVICEABLE BY VENDOR & MANUFACTURSDR 2004FA0000851Windscreen · distortedON DELIVERY OF A NEW AIRCRAFT, DAY ACCEPTANCE CHECK CARRIED OUT AND AIRCRAFT ACCEPTED. DURING NIGHT FLYING LT WINDSCREEN OBSERVED TO HAVE PARALLAX DISTORTION ERROR. DAY TESTS CARRIED OUT OF GRID TEST AND WATER TEST. WINDSCREEN CERTIFIED SERVICEABLE BY VENDOR SDR DXTA200400386Arm · unsecureDURING CLIMB OUT, THE GEAR UNLOCK LIGHT CAME ON, RECYCLED GEAR AND PROBLEM DID NOT GO AWAY. ACCOMPLISHED AIR TURN BACK TO MRY. FOUND THE EMERGENCY GEAR BOTTLE ARM NOT SAFETIED AND THE ARM PARTIALLY ACTUATED SUPPLYING NITROGEN TO THE GEAR EXTEND SYSTEM. RESESDR DXTA200400377Engine · bird ingestionON TAKEOFF ROLL INGESTED A BIRD IN LEFT ENGINE, ABORTED TAKEOFF AND RETURNED TO BLOCK. PRELIMINARY INSPECTION FOUND EVIDENCE OF INGESTION NOTED ON ENGINE INLET AND EXHAUST. INSPECTED LT ENGINE AS REQUIRED, CLEANED REMAINS OF BIRD FROM INTAKE. BORESCOPED ENGSDR DXTA200400370Strut · damagedON GEAR RETRACTION RED UNLOCK LIGHT ON GEAR. EXTENDED GEAR, 3 GREENS, NO RED LANDED UNEVENTFULLY. TROUBLESHOT LANDING GEAR SYSTEM. FOUND NLG STRUT NOT EXTENDING COMPLETELY, CAUSING UPLOCK LOCK TO CONTACT UPLOCK ROLLERS NOT ALLOWING GEAR TO RETRACT. DISASSEMBSDR 2004F00412Radio · dislodgedON BEGINNING DEPARTURE FROM KSWF, WHEN THE STANDBY COMMUNICATION RADIO HEAD SLID OUT OF ITS RACK APPROXIMITY SIX INCHES ON INITIAL ACCELERATION FOR TAKEOFF. THE TAKEOFF WAS ABORTED AT SEVENTY KNOTS WITHOUT INCIDENT. THE AIRCRAFT RETURNED TO THE CESSNA SERVICSDR DXTA200400349Squat Switch · out of adjustAFTER TAKEOFF, FOUND LANDING GEAR WOULD NOT RETRACT, DIVERTED AIRCRAFT TO GTF AND LANDED SAFELY. JACKED UP AIRCRAFT AND ADJUSTED LT MLG SQUAT SWITCH IAW CESSNA 560XL MAINTENANCE MANUAL CHAPTER 32-61-00. SERVICED LT & RT MLG OLEO'S IAW CESSNA 560XL MM CHAPTERSDR CWQ2004F00005Vapor Barrier · crackedDURING ROUTINE PHASE INSP. 1-4 HAD TO REMOVE RT IB LE FOR ANOTHER PROBLEM (REF SCR NR 156504) BEFORE REINSTALLATION OF REPAIRED LE INSPECTED AREA AND FOUND THE HEAT SHIELD/ VAPOR BARRIER PN 6621281-30 CRACKED ON LOWER ATTACH FLANGE 4 FT 2 IN LONG. A CAUSE DUSDR DXTA200400344Mount · failedAFTER TAKEOFF DOOR SEAL & CABIN DOOR ANNUNCIATOR ILLUMINATED, LOUD WIND NOISE FROM AROUND DOOR. ACCOMPLISHED AIR TURNBACK AND UPON LANDING THE MAIN ENTRANCE DOOR FELL OPEN. REPLACED AFT DOOR STRUT MOUNTING FRAMES IAW CESSNA 560XL B/P 6611267, BOTH DOOR CABLESDR CWQ2004F00006Diffuser · crackedFOUND LT AND RT IB LE SKIN WHERE IT JOINS CUFF SKIN RIVETS FOUND COCKED IN HOLES WITH HEAD COCKED ABOVE SURFACE. TO REPLACE RIVETS THE LE HAD TO BE REMOVED, UPON REMOVAL, NOTICED DIFFUSER WAS CRACKED 2 PLACES AND KRINKLED IN 2 PLACES WITH A LITTLE BROWNING ONSDR 2004F00238Transmitter · malfunctionedTHE ELT TRANSMITTER WOULD ACTIVATE ITSELF WHILE THE AIRCRAFT WAS STATIC IN THE HANGAR. THE UNIT WOULD ALSO SELF ACTIVATE WHILE SITTING ON THE BENCH. THE ON/OFF SWITCH ON THE ELT COULD BE TURNED ON THEN BACK TO OFF AND THE ELT WOULD REACTIVATE WITHIN A FEW MISDR 2004F00231Fuel Control · shearedAT 16,000 MSL CRUISE, RT ENGINE FLAMED OUT. INSPECTION FOUND ENGINE DRIVEN FUEL PUMP SHEARED.SDR DXTA200400338Indicator · failedON TAKEOFF ROLL THE LEFT ITT IND FAILED MESSAGE CAME ON, ABORTED TAKEOFF. VERIFIED INDICATOR FAILED. REMOVED FAILED INDICATOR AND REPLACED WITH AN INSPECTED INDICATOR. OPS CHECKED GOOD DURING LEFT/RIGHT ENGINE RUNS, ALL INDICATIONS NORMAL IAW THE CESSNA 560SDR DXTA200400337Proximity Switch · out of adjustON TAKEOFF ROLL OUT OF LUK, THE EMERGENCY CAUTION LIGHT ILLUMINATED, ABORTED TAKEOFF. REMOVED EMERGENCY EXIT DOOR, REMOVED EMERGENCY EXIT PROX SWITCH FROM DOOR JAM, PERFORMED VISUAL INSPECTION OF SWITCH AND WIRING, NO DEFECTS NOTED. ADJUSTED PROX SWITCH TO WSDR DXTA200400334Selector Knob · out of positionDURING CRUISE AT 22,000 FT, MASTER WARNING CAME ON FOR LOSS OF CABIN PRESSURIZATION. DECLARED EMERGENCY AND DESCENDED DOWN TO 10,000 FT, PROBLEM WENT AWAY. DIVERTED AND AIRCRAFT LANDED SAFELY. FOUND SELECTOR KNOB POINTING INCORRECTLY, REPOSITIONED CABIN SOUSDR DXTA200400331Engine · malfunctionedWITH POWER AT TAKEOFF THRUST AIRCRAFT YAWS SHARPLY LEFT, POWER ON BOTH ENGINES MATCHED. RAN AIRCRAFT TO TAKEOFF POWER, TAXI CHECKED BRAKES, TOP CHECKED RUDDER BIAS, COULD NOT DUPLICATE. FOUND RIGHT ENG ACCELERATING FASTER AND HIGHER THRUST THAN LEFT, COULD NSDR 2004FA0000828Wheel · damagedAC WAS TOWED, WITH BRAKES RELEASED, WITHOUT ANY BRAKING ACTIVITIES BY PILOT, SHEARING NOISE WAS NOTED, TOWING PROCESS WAS STOPPED. HYD FLUID WAS SPILLED OUT FROM LT BRAKE UNIT. FIRST INVESTIGATION OF INSTALLED LT CARBON BRAKE UNIT DID SHOW, THAT ATTACHING SDR DXTA200400322Position Switch · malfunctionedAFTER TAKEOFF NOSE WHEEL LANDING GEAR GREEN LIGHT REMAIN ILLUMINATED, DID NOT EXTINGUISH AFTER GEAR WAS RECYCLED. REMAINED ON FOR THE DURATION OF FLIGHT, UPON LANDING GEAR CYCLED DOWN, ALL 3 GREEN LIGHTS CAME ON. JACKED AIRCRAFT, COMPLIED WITH GEAR SWING ANDSDR DXTA200400315Support Bracket · crackedDURING INSPECTION FOUND LOWER HALF OF MAIN ENTRY DOOR STEPS SUPPORT BRACKETS AND A COVER PLATE / WEB ASSEMBLY CRACKED. REPLACED BOTH SUPPORT BRACKETS, PLATE ASSEMBLY AND WEB ASSEMBLY PER CESSNA SERVICE BULLETIN 560XL-52-12.SDR DXTA200400311Brake · firePERFORMED HIGH SPEED TAXI AFTER BRAKE MAINTENANCE, TAXIED BACK USING NORMAL BRAKING PROCEDURE. UPON RETURN TO RAMP, LEFT WHEEL/BRAKE ASSEMBLY WAS ON FIRE, RIGHT WHEEL/BRAKE ASSEMBLY SMOKING. EXTINGUISHED FIRE WITH PURPLE K, DRY CHEMICAL (B-C) EXTINGUISHER. SDR DXTA200400305Warning System · activatedAFTER TAKEOFF THE GEAR WAS RETRACTED, THE THREE GREEN INDICATORS WENT OUT BUT THE RED LIGHT REMAINED ON, FLAPS AND STAB WERE NOT COMMANDED TO MOVE. RED LIGHT REMAINED ON AND THE HYDRAULIC PRESSURE LIGHT FLASHED, CYCLED GEAR SECOND TIME WITH SAME RESULTS. ITEMSDR DXTA200400302Landing Gear · malfunctionedAFTER TAKE OFF FROM FFC NOSE LANDING GEAR WOULD NOT RETRACT, DIVERTED TO ATL AND LANDED SAFELY. ITEM IS UNDER INVESTIGATION.
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