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 DXTA200300161Strut · damagedAFTER TAKEOFF DURING GEAR RETRACTION GEAR UNLOCK LIGHT STAYED ON. TROUBLESHOT AND FOUND NOSE STRUT NOT FULLY EXTENDING WITH WEIGHT OFF WHEELS. REMOVED STRUT AND REPACKED. REINSTALLED AND SERVICED IAW CESSNA 560XL CMM CHAPTER 32-20-01, PERFORMED GEAR SWING. SDR DXTA200300157Brake Assy · contaminatedLEFT BRAKE PEDAL FLUCTUATES IN TRAVEL REQUIRED TO GET THE BRAKE TO APPLY. VERIFIED SQUAWK, ACCOMPLISHED BRAKE BLEEDING PER CESSNA 560XL MM CHAPTER 32-42-00. ACCOMPLISHED TAXI CHECKS FOUND BRAKE PEDAL ACTION EVEN, OPS CHECKED GOOD, NO DEFECTS NOTED.SDR DXTA200300153O-Ring · failedDURING TAXI "LO BRAKE PRESS" AND "ANTISKID INOP" ILLUMINATED. LOST BRAKE PEDAL PRESSURE, STOPPPED AIRCRAFT WITH EMERGENCY BRAKES. HAD AIRCRAFT TOWED TO PARKING POSITION, POST FLIGHT INSPECTION FOUND LEAKING OIL FROM AVIONICS BAY AND NOSE GEAR ASSEMBLY. - FOUNDSDR DXTA200300155Strut · malfunctionedGEAR UNLOCK INDICATOR REMAINED ON AFTER GEAR RETRACTION. TROUBLESHOT TO NOSE GEAR NOT GETTING ON THE UPLOCK STRUT WAS NOT FULLY EXTENDED. PERFORMED A COMPLETE SERVICING OF STRUT IT IS NOW FULLY EXTENDED AND THE GEAR OPERATIONAL CHECK WAS GOOD. ALL WORK PERFORSDR DXTA200300151Engine · making metalAFTER TAKEOFF CLIMBING THRU 3000 FT OIL PRESS LIGHT CAME ON. REDUCED POWER AND LIGHT WENT OUT, ADDED POWER AND INDICATION WAS NORMAL, OIL PRESS AND OIL GAGE AGREED. INSPECTED RT ENGINE CHIP DETECTOR & OIL FILTER FOUND NO DEFECTS, SERVICED ENGINE OIL TO FULLSDR DXTA200300145Switch · failedDURING FLIGHT AT FL370 THE ACM OVERHEATED FOLLOWED BY ACTIVATION OF EMERGENCY PRESSURIZATION . EMERGENCY DECLARED, AIRCRAFT DIVERTED TO CRW AND LANDED SAFELY. REMOVED & REPLACED ACM OVERHEAT SWITCH AND OPS CHECKED GOOD IAW CESSNA 560XL M/M CHAPTER 21-51-00.SDR DXTA200300142Transmitter · malfunctionedAS TAKE OFF POWER WAS APPLIED, THE RIGHT ENGINE OIL PRESSURE DROPPED TO ZERO THEN BEGAN TO JUMP BETWEEN NORMAL LEVELS AND ZERO. NO OTHER LOW OIL PRESSURE INDICATIONS WERE NOTED. TAKE OFF ABORTED. REMOVED AND REPLACED NR 2 ENGINE OIL PRESSURE TRANSMITTER WITH SDR DXTA200300141Proximity Switch · out of adjustRT T/R ARM LIGHT ILLUMINATED IN FLIGHT ACCOMPANIED BY A CONSTANT HYDRAULIC PRESSURE ANNUNCIATOR, FOLLOWED BY INTERMITTENT UNLOCK LIGHT OF LANDING GEAR CAUSING SYSTEM TO RETRACT GEAR. - FOUND RT T/R STOW / DEPLOY SWITCH IN QUADRANT TO BE OUT OF ADJUSTMENT. READSDR DXTA200300129Uplock Switch · malfunctionedAFTER TAKE-OFF FROM HYA NOSE GEAR WOULD NOT STAY UP AND LOCKED AFTER RETRACTION, DIVERTED INTO SWF. JACKED AIRCRAFT AND PERFORMED GEAR SWINGS, UNABLE TO DUPLICATE SQUAWK ON GROUND. FOUND EMERGENCY GEAR RELEASE CABLE HAS EXCESSIVE TENSION, RE-RIGGED CABLE IAWSDR DXTA200300135Cdu · inoperativeDURING FLIGHT FMS CIRCUIT BREAKER TRIPPED AND ELECTRICAL ODOR WAS PRESENT IN COCKPIT. - INSPECTED COCKPIT AND FOUND CDU INOPERATIVE, REPLACED UNIT IAW WITH CESSNA 560XL MM CHAPTER 34-10-00.SDR DXTA200300125Bellcrank · misinstalledDURING ENGINE RUN FOR POST INSTALLATION OF MFG SB 560XL7603R1 (THROTTLE CUT OFF IMPROVEMENT) FOUND ENGINES FAILED TO STAY IN FLIGHT IDLE, WHEN POWER IS REDUCED TO IDLE, ENGINES WOULD GO TO CUT OFF, INSPECTED THROTTLE LINKAGE AND FOUND THE BELLCRANK ASSEMBLIES SDR DXTA200300124Bellcrank · misinstalledON LANDING AT TEB, LT ENGINE FAILED UPON STOWING THRUST REVERSERS, TROUBLESHOT AND FOUND THE LEFT ENGINE WHEN POWER IS ABRUPLY REDUCED TO IDLE, ENGINE FAILED (THROTTLE WENT TO CUT-OFF) - FERRIED AIRCRAFT TO CMH FOR REPAIR, CONFIRMED DISCREPANCY TROUBLESHOT ANDSDR DXTA200300112Handle · inoperative"GEAR UNLOCK" LIGHT REMAINED ILLUMINATED AFTER GEAR HANDLE PLACED IN THE UP POSITION. PERFORMED LANDING GEAR FUNCTIONAL TEST, CHECKED GOOD. CHECKED RIGGING ALL UP LOCK SWITCHES AND HOOKS, FOUND THE NOSE LANDING GEAR UPLOCK TO BE OUT OF RIG, ADJUSTED UPLOCK HOOSDR 2003FA0000883Panel · crackedDURING INSPECTION FOUND RT WING, INBOARD LEADING EDGE BLEED AIR TUBE HEATSHIELD PANEL LOWER MOUNT FLANGE CRACKED APPROXIMATELY HALF WAY LENGTHWISE. THIS IS THE THIRD C-560XL THAT WE HAVE FOUND THIS CONDITION ON. REPLACED THE PANEL WITH NEW.SDR DXTA200300108Pushrod · chafedDURING ROUTINE INSPECTION FOUND MAIN ENTRY DOOR PUSHROD (OPENING/CLOSING) RUBBING AGAINST THE CUTOUT IN THE DOOR STRUCTURE. ADJUSTED PUSHROD TO PREVENT CHAFING, PERFORMED BLEND OUT REPAIR TO CABIN DOOR FORMER IAW MFG REPAIR DEFINITION REPORT NR S-560XL-5227/01SDR 2003FA0000905Pushrod · chafedDURING A ROUTINE INSPECTION OF THE MAIN ENTRY DOOR, IT WAS DISCOVERED THAT THE DOOR OPENING / CLOSING PUSHROD WAS RUBBING AGAINST THE CUT OUT IN THE DOOR STRUCTURE.SDR DXTA200300101Control Handle · defectiveAFTER TAKEOFF THE GEAR WOULD NOT RETRACT, NO UNLOCK LIGHT OR ANY FLICKERING OF THE 3 GREEN LIGHTS, ACCOMPLISHED AIR TURN BACK TO SJC. - FOUND LANDING GEAR CONTROL HANDLE DEFECTIVE, REMOVED DEFECTIVE LANDING GEAR CONTROL HANDLE AND INSTALLED NEW UNIT IAW MFG 5SDR CWQ2004F00003Line · chafedREPORT 110840, INSPECTED WHEEL WELL AREAS LT AND RT, FOUND THE LT WHEEL WELL LINES TO BE OK AT THIS TIME. RT WHEEL WELL BRAKE LINE ASSY , PN 6627100-34 AND THE FLAP RETRACT LINE ASSY PN 6627000-68, TO BE CHAFED BEYOND ALLOWABLE LIMITS STATED IN MM. REMOVED ASDR DXTA200300081Line · chafedWHILE PERFORMING NJA'S ONE TIME INSPECTION OF THE HYDRAULIC/PNEUMATIC LINES IN THE WHEEL WELLS, FOUND THE RT EMERGENCY BRAKE LINE CHAFFED THROUGH, THE LT EMEGENCY BRAKE LINE, LT AND RT HAND FLAP RETRACT AND EXTEND LINES, SPEED BRAKE RETRACT AND EXTEND LINES CHSDR 2003FA0000816Line · chafedLT FLAP RETRACTION HYDRAULIC LINE, RT AND LT EMERGENCY BRAKE PNEUMATIC LINES CHAFING ON PILLOW BLOCK CLAMPS.SDR DXTA200300080Line · chafedWHILE PERFORMING NJA'S ONE TIME INSPECTION OF THE HYDRAULIC/PNEUMATIC LINES IN THE WHEEL WELLS, FOUND THE RT EMERGENCY BRAKE LINE CHAFED THROUGH, AND FLAP RETRACT LINE CHAFED BEYOND LIMITS. - REMOVED AND REPLACED DEFECTIVE HYDRAULIC AND PNEUMATIC LINES IAW CESSDR DXTA200300078Line · leakingDURING POST FLIGHT INSPECTION FOUND HYDRAULIC FLUID LEAKING OUT OF RIGHT WHEEL WELL. INSPECTED RIGHT WHEEL WELL AND FOUND FLUID LEAKING OUT FROM SPEED BRAKE RETRACT LINE. FURTHER INSPECTION FOUND SPEED BRAKE EXTEND LINE, FLAP EXTEND AND RETRACT LINES CHAFED SDR DXTA200300076Odor · detectedUPON DESCENT STRONG EXHAUST SMELL OF JET FUMES, APU WAS NOT RUNNING AT THE TIME, AND ENVIRONMENTAL SOURCES SHOWED 50 DEGREES. INSPECTED BOTH ENGINE INLETS AND TAILPIPES FOR TRACES OF OIL, NONE FOUND. OPENED LOWER COWLS AND RAN BOTH ENGINES INDIVIDUALLY FOR SDR DXTA20030076Odor · detectedUPON DESCENT STRONG EXHAUST ODOR OF JET FUMES, APU WAS NOT RUNNING AT THE TIME, AND ENVIRONMENTAL SOURCES SHOWED 50 DEGREES. - ITEM IS UNDER INVESTIGATION.SDR DXTA200300067Hub Cap · out of positionABORTED TAKE-OFF DUE TO ANTI SKID LIGHT THEN BRAKES FAILED, USED EMERGENCY BRAKE TO STOP AIRCRAFT. - NOTED LEFT WHEEL HUB CAP TRANSDUCER CLIP POSITIONED INCORRECTLY, REPOSITIONED HUB CAP. BLED BRAKES, OPERATIONAL CHECK GOOD. ALL WORK DONE IAW CHAPTER 32-42-SDR CNQ8200360111Engine · burnedRT ENGINE OIL PRESSURE DROPPED ON CLIMBOUT. ALSO HAD A 10 PERCENT POWER LOSS. PILOT SHUT DOWN ENGINE. FOUND ENGINE HAD A FIRE MELTING PARTS OF ENGINE.SDR 5300063003Seal · leakingLT AND RT ENGINE AC GENERATOR DRIVE SEALS LEAKING OIL.SDR DXTA200300051Display · lightning strikeAIRCRAFT STRUCK BY LIGHTNING, AVIONICS SCREENS LOOK LIKE TIE DYE SHIRTS. SEEMS TO HAVE ENTERED THROUGH THE NOSE (CO-PILOT SIDE DIVERTER SCREW) EXITED OUT A BURNED HOLE OVER CO-PILOT SIDE SECOND PAX WINDOW. ITEM IS UNDER INVESTIGATION.SDR DXTA2003MD001Duct · misalignedINSTALLATION OF NEW UPGRADED APU STARTER/GENERATOR P/N 9912499-29 IN LIEU P/N 9912499-22, REF: CE-560XL IPC 80-11-00 FIG 01 ITEM NR 1 AND NR 1A. THE NEW STARTER/GENERATOR END BELL IS 1INCH LONGER WHICH CAUSES A MISALIGNMENT IN THE INLET COOLING DUCT, AND HAND SDR DXTA200300050Bleed Valve · closedDURING TAKEOFF ROLL, WINDSHIELD HEAT AND MASTER WARNING ANNUNCIATORS ILLUMINATED. VALVES WERE CLOSED AND SWITCHES WERE OFF. - RAN AIRCRAFT AND DUPLICATE SQUAWK. REMOVED AND REPLACED BLEED AIR VALVE IAW 560 MM CH 30-41-00.SDR DXTA200300049Apu · failedDURING CLIMBOUT SMOKE WAS NOTICED IN THE COCKPIT AND CABIN. APU FAIL LIGHT ILLUMINATED AND APU SHUTDOWN. FOUND APU OIL QTY EMPTY, RESERVICED & OIL LEAKS INTO APU INLET. ALSO FOUND METAL ON MAGNETIC OIL PLUG. REMOVED AND REPLACED APU IAW CESSNA 560 MM & HONSDR DXTA200300044Relay · inoperativeLOST BRAKES ON LANDING ROLLOUT. USED EMERGENCY BRAKES TO STOP ACFT. POWER BRAKES AND ANTI SKID ANNUNCIATORS DID COME ON WHEN ACFT LOST BRAKES. POST FLIGHT REVEALED A PUDDLE OF FLUID ON THE GROUND AND ON THE NOSE GEAR, UNDER THE NOSE OF THE ACFT. TROUBLESHOSDR DXTA200300041Ground Wire · damagedLEFT ENGINE FIRE WARNING LIGHT ILLUMINATED DURING CLIMB THRU FL260 WITH ENGINE/WING ANTI-ICE ON. REDUCED POWER TO 72 PERCENT ON EFFECTED ENGINE AND LIGHT EXTINGUISHED. REMOVED AND REPLACED LT ENGINE FIRE LOOP WITH A NEW PART IAW CESSNA 560XL MAINTENANCE MANUSDR DXTA200300039Tube · leakingLT ENGINE FIRE WARNING LIGHT ILLUMINATED ON CLIMBOUT AT 14,000 FT. TROUBLESHOT FIRE DETECTION SYSTEM. PERFORMED FIRE LOOP CONTINUITY RESISTANCE CHECK IAW CE-560 XL MAINTENANCE MANUAL CHAPTER 26-1-0. PERFORMED HIGH POWER RUNS ON LT ENGINE FOUND ANTI-ICE PLUMSDR DXTA200300036Fire Loop · misroutedDURING FLIGHT 120124-1 FROM MIA TO CHS DIVERTED TO MCO DUE TO LT ENGINE FIRE LIGHT CAME ON AT FL240. REDUCED POWER TO HALF THROTTLE AND LIGHT EXTINGUISHED, NO EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. REMOVED LT ENG COWLS AND RAN FOR LEAK CHECK. NO LEAKS SDR 5300051903Control Valve · failedNO CONTROL OF COCKPIT TEMPERATURE.SDR CA030528012Wheel · unbonded(CAN) AT LIFT OFF PILOT HEARD AND FELT STRONG VIBRATIONS ON THE NOSE WHEEL. HE DECLARED AN EMERGENCY AND RETURNED TO BASE. DURING THE INVESTIGATION FOUND NOSE WHEEL OUT OF BALANCE. NOSE WHEEL ASSY WAS STRIPPED MAY 27/03 AND FOUND BALANCE PATCH GLUED TO TIRE UNSDR 5300051803Cowling · crackedRIGHT ENGINE COWL CRACK FORMING FROM OIL SERVICE DOOR.SDR DXTA200300033Odor · detectedWHILE ENROUTE AT FL280 NOTICED STRONG ODOR IN COCKPIT + CABIN. PIC + SIC DEVELOPED HEADACHE + BURNING EYES. USED O2. ONCE AT 3000' , SELECTED OFF ON PRESSURIZATION SOURCE. ODOR DIMINISHED. ITEM IS UNDER INVESTIGATIONSDR 5300051203Display · faultyNR 2 RMU DISPLAY IS UNREADABLE.SDR DXTA200300030Warning Light · illuminatedRIGHT "T/R ARM LIGHT" , "HYD PRESS" & "MASTER WARNING" LIGHT ILLUMINATED WHILE CRUSING LEVEL AT FL330, MACH 7.0. ENGAGED EMERGENCY STOW SWITCH AND DECLAIRED AN EMERGENCY WHILE SLOWING TO 200 KTS INDICATED. NOTICED NO UNSUAL AIRCRAFT MOVEMENT OR ANY DAMAGE. SDR DXTA200300018Motor · lack of lubeCLIMBING THROUGH 35,000 FT YOKE JERKED ABRUPTLY, AUTOPILOT WAS DISCONNECTED AND AIRCRAFT NEED NOSE DOWN TRIM. FIFTEEN SECONDS LATER WITH AUTOPILOT OFF SECOND JERK OCCURRED IN YOKE.SDR 5300040403Control Valve · failedNO CONTROL OF CABIN TEMPERATURE AVAILABLE.SDR 5300010503Generator · wornAC BEARING CAUTION ON RIGHT ENGINE ILLUMINATED.SDR 5300123102Transmitter · failedLOST LEFT ENGINE OIL PSI, INDICATION.SDR 2002FA0001244Clip · crackedCRACKS AT TWO FASTENER HOLES ATTACHING NOTED CLIP TO THE VERTICAL STABILIZER AFT SPAR.SDR CWQ2002F00006Lens · crackedFOUND LT WING TIP LIGHT ASSEMBLY LENS CRACKED AROUND FORWARD AND AFT FLANGE. POSSIBLE CAUSE: OVER-TORQUE OF ATTACHING HARDWARE. REPLACED WING TIP LIGHT ASSEMBLY LENS.SDR CA020502027Servo · malfunctioned(CAN) DURING A PHASE INSPECTION, THE AUTO-PILOT SERVO CABLE AND THE SECONDARY RUDDER CABLE WERE FOUND CROSSING EACH OTHER BETWEEN THE LOWER AFT RUDDER SECTOR AND PULLEYS AT THE 63 PERCENT VERTICAL SPAR IN ZONE 340.THE AUTO-PILOT SERVO CABLE HAS BEEN RE-ROUTED SDR DXT2001F00003Cable · chafedCABLE RUN JUST FORWARD OF BATTERY COMPARTMENT, INBOARD SIDE OF HYDRAULIC PRESSURE LINE, RUBBING ON BULKHEAD.STATION FS390.(K)SDR DXT2001F00000Control Cable · chafedCABLE RUN JUST FWD OF BATTERY COMPARTMENT, I/B SIDE OF HYDRAULIC PRESSURE LINE RUBBING ON BULKHEAD.
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