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 CWQR200803Control Cable · improper partDURING A ROUTINE CABLE REPLACEMENT OF AILERON CABLE PN 6660002-12, WE FOUND THAT THE CABLE HAD A SWAGED BALL AND A CLEVIS END INSTALLED. THIS CABLE ASSY SHOULD HAVE BEEN MANUFACTURED WITH THE SWAGED BALL WITHOUT THE CLEVIS. THE CABLE ASSY HAS BEEN SENT BACK TOSDR 041508N521CS1Bulb · burned outON APPROACH, WHEN GEAR WAS EXTENDED, NOSE GEAR DOWN INDICATION FAILED TO ILLUMINATE. CREW CONTACTED ATC AND ABORTED APPROACH TO WORK AFM CHECK LIST FOR GEAR PROBLEM. STILL UNABLE TO GET GEAR DOWN INDICATION, CREW DECLARED EMERGENCY, BLEW GEAR DOWN AND LANDEDSDR DXTA200803000Unknown · unknownGEAR RETRACTED DURING LANDING ROLLOUT. MALFUNCTION UNDER INVESTIGATION.SDR DXTA200802992Bleed Valve · bypassingUPON APPLICATION OF TAKEOFF THRUST THERE IS A OSCILLATING PRESSURE SURGE THAT CAN BE FELT STRONGLY AND HEARD. REMOVED P/N 9912492-1(1988-00-3) S/N 2317. INSTALLED OVERHAULED UNIT BY DUKES INC. CRS WUERE79L. OPERATIONAL AND LEAK CHECK GOOD. WORK DONE IAW MM 21SDR DXTA200802984Actuator · stuckFLAPS WILL NOT RETRACT BEYOND 7 DEG WITH THE FLAP HANDLE IN THE 0 POSITION. RECEIVED ACFT WITH FLAPS STUCK HARD AT 15 DEGREES. ATTACHED HYDS AT EXTEND AND RETRACT LINES OFF OF FLAP CONTROL VALVE. FLAPS WOULD NOT EXTEND OR RETRACT WITH APPLIED HYD PRESSURE. MESDR DXTA20082984Flap System · malfunctionedFLAPS WILL NOT RETRACT BEYOND 7 DEG WITH THE FLAP HANDLE IN THE 0 POSITION.SDR DXTA200802954Engine · power lossLT ENGINE WILL NOT MAKE TAKEOFF POWER IN THE TAKEOFF DETENT AND WITH EECS IN AUTO AND FAILED TO MANUAL. RAN ENGINES AT 88.4 PERCENT N1 WITH SEVERAL ACCELERATIONS AND DECELERATIONS WITH NO FAULTS FOUND IAW FAULT ISOLATION SECTION OF MM 72-00-00.SDR DXTA20082954Engine · power lossLT ENGINE WILL NOT MAKE TAKEOFF POWER IN THE TAKEOFF DETENT AND WITH EECS IN AUTO AND FAILED TO MANUAL. RAN ENGINES AT 88.4 PERCENT N1 WITH SEVERAL ACCELERATIONS AND DECELERATIONS WITH NO FAULTS FOUND I/A/W FAULT ISOLATION SECTION OF MM 72-00-00.SDR DXTA20082953Uplock Switch · out of adjustWHILE FLYING AT FL400 A LOUD (THUNK) WAS HEARD COMING FROM THE BACK. THE GEAR UNSAFE LIGHT ILLUMINATED WITH HYD PRESS STEADY. ADJUSTED NOSE GEAR UPLOCK HOOK AND UP LOCK SWITCH IAW MM 32-30-05 GEAR SWING OPERATIONAL CHECK GOOD.SDR DXTA20082952Latch · obstructedAC DOOR LIGHT (TAIL) ILLUMINATED ON TAKEOFF. FOUND BAGGAGE AFT UPPER LATCH STIFF. CLEANED SLIDE (BAYONET) AND HINGE POINTS AND LUBED. REMOVED UNIT FROM BAYONET RECEPTACLE. ADJUSTED SPRING TENSION. FOUND TAILCONE FWD ACCESS DOOR AFT UPPER LATCH STIFF AND RSDR N568CS032008Circuit Breaker · defectiveAFTER LOWERING LANDING GEAR, DID NOT GET 3 GREEN DOWN AND LOCKED LIGHTS. FOLLOWED AFM PROCEDURES AND LANDING GEAR INDICATION NORMAL: (3 GREEN LIGHTS). COMPLETED NORMAL LANDING. REMOVED AND REPLACED LANDING GEAR WARNING CIRCUIT BREAKER. LANDING GEAR OPERATIOSDR DXTA20082951Rmu · odorNR 1 RMU SWITCHED ON AND OFF TWICE IN FLIGHT. EACH TIME THIS HAPPENED A STRONG ELECTRICAL ODOR WAS NOTICED. NR 1 COMM CB WAS PULLED. REMOVED RMU AND INSTALLED SERVICEABLE UNIT IAW MM 23-80-01. SYSTEM OPERATIONAL CHECKS GOOD.SDR DXTA20082942Warning Light · illuminatedWHEN THE LANDING GEAR WAS LOWERED THE RT DOWN AND LOCKED LIGHT DID NOT ILLUMINATE, RES (UNLOCK) LIGHT REMAINED ON, BLED HYDRAULICS SYSTEMS ON AIRCRAFT IAW MM 32-30-00, 27-50-00, 27-40-00, AND 27-60-00. OPS CHECKS GOOD.SDR DXTA20082941Actuator · false indicationLANDING GEAR IND UNSAFE (LEFTSIDE- NOGREEN- RED UNLOCK ON). INSTALLED REPAIRED LT MAIN LANDING GEAR ACTUATOR, PERFORMED CAMBER CHECK, SLOW CYCLE GEAR AND PURGED AIR FROM SYSTEM, SERVICED EMERGENCY AIR BOTTLE, CYCLED GEAR NUMEROUR TIMES, OPS CHECK GOOD. REF FESDR DXTA20082945Display · failedDURING CLIMBOUT PFD NR2 SCREEN WENT DARK, PFD FAILURE WAS ACCOMPANIED BY A BURNING ODOR. REMOVED AND REPLACED PFD NR 2 WITH A REPAIRED UNIT AND SECURED. OPS CHECKED SATISFACTORY IAW MM CHAPTER 34-25-01.SDR DXTA200802933Control Handle · inoperativeDURING GEAR RETRACTION RED UNLOCK LIGHT STAYED ILLUMINATED, FOLLOWED BY STAB MISCOMPARE AND HYD PRESS CAUTION LIGHTS. WITH GEAR EXTENDED UNLOCK LIGHT WENT OUT. WHILE COMPLETING HYD PRESS CHECKLIST (GEAR RETRACTED), A LOUD THUNK WAS HEARD IN THE L WING ROOT ASDR DXTA20082933Control Handle · inoperativeDURING GEAR RETRACTION RED UNLOCK LIGHT STAYED ILLUMINATED. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE IAW MM 32-30-01 ALSO REMOVED AND REPLACED LANDING GEAR PCB IAW MM 24-51-02. C/W LANDING GEAR FUNCTIONAL CHECKS IAW MM 32-01-00. OPERATIONAL CHECKSSDR DXTA20082932Pump · inoperativeWHILE TAXING, ANTI SKID INOP LIGHT CAME ON , FOLLOWED BY LOW BRAKE PRESS LIGHT AND SUBSEQUENT LOSS OF NORMAL BRAKING. REPLACED POWER BRAKE HYDRAULIC PUMP WITH NEW CUSTOMER SUPPLIED. REPLACED ANTI-SKID RELAY WITH NEW P/N: MS2416602, REMOVED RELAY P/N: MS241660SDR DXTA20082931Signal Cond Unit · inaccurateDURING TAKEOFF ROLL BELOW 70 KNOTS, (LT FUEL GAGE) AND MASTER CAUTION LIGHTS CAME ON. REPLACED FUEL QUANTITY SIGNAL CONDITIONER IAW MM CHAPTER 28-41-00. PERFORMED FUEL SYSTEM ADJUSTMENT AND TEST IAW MM CHAPTER 28-41-00. TEST GOOD.SDR DXTA20082930Master Cylinder · failedDURING TAXI, NO BRAKE FUNCTION UNTIL MAXIMUM PRESSURE IS APPLIED AND THEN LT BRAKE LOCKS. REPLACED CAPTAINS LEFT BRAKE MASTER CYL WITH NEW UNIT AND BLEED SYSTEM IAW MMCH 32-42-02, NO LEAKS, OPS CHECK GOOD. TAXIED AIRCRAFT MADE SEVERAL LEFT AND RIGHT TURNS.SDR DXTA20082929Actuator · false indicationDURING DESCENT, WE NOTICED THE LT MAIN DOWN AND LOCK GREEN ANNUNC ON, WITH NO OTHER ABNORMAL INDICATIONS. T/S TO BAD ACTUATOR. REPLACED L/H MAIN LANDING GEAR ACTUATOR IAW 560XL MM CH 32-30-04. ADJUSTED CAMBER IAW 560XL MM CH 32-10-00. OP'S & LK CK GOODSDR DXTA20082927Apu · smokeAPU RUNNING, WITH BLEED ON AND ENGINES RUNNING, SMOKE ENTERED THE CABIN. REMOVED AND REPLACED APU. SERVICED OIL TO FULL. OPERATIONAL AND LEAK CHECK GOOD. WORK PERFORMED IAW MM 49-10-00.SDR DXTA20082923Brake · contaminatedUPON SHUTDOWN , SUFFICENT SMOKE FROM RT MAIN GEAR. SMOKE PERSISTED FOR 15 MIN. REMOVED RT MAIN WHEEL AND INSP WHEEL AND BRAKE ASSY FOUND EXCESSIVE GREASE ON INSIDE OF WHEEL, CLEANED GREASE AND FOUND SMALL SUPERFICIAL BURN MARKS. REINSTALLED RT MAIN WHEEL IAW SDR DXTA20082920Brake · contaminatedPILOT'S RT BRAKE PEDAL VERY SOFT GOES ALMOST TO STOP. FOUND AIR IN SYSTEM, BLED BRAKES AS REQUIRED PER CESSNA 560XL M/M 32-42-00 FUNCTION CHECK GOOD.SDR DXTA20082922Brake · contaminatedPILOTS RT BRAKE PEDAL GOES TO THE STOP WITH LITTLE OR NO RESISTANCE. FOUND AIR IN SYSTEM, BLED BRAKES AS REQUIRED PER MM 32-42-00 FUNCTION CHECK GOOD.
SDR CA080402002Bleed Valve · malfunctionedTHE CREW EXPERIENCED ENGINE VIBRATIONS, FOLLOWED BY AN EEC MANUAL LIGHT. ENGINE POWER INCREASED AS EXPECTED, BUT THE CREW WAS UNABLE TO FURTHER MODULATE POWER BY MOVING THE THRUST LEVER. THE ENGINE WAS SHUT DOWN AS A RESULT AND THE FLIGHT CONTINUED TO PLANNESDR DXTA20082917Actuator · intermittentDURING INITIAL LANDING ATTEMPT, LT MAIN GEAR DID NOT INDICATE DOWN AND LOCKED. PERFORMED GEAR SWING MANY TIMES AND COULD NOT DUPLICATE PROBLEM. REMOVED LT MLG ACTUATOR WHICH INCORPORATES THE DOWN AND LOCK SWITCH AND INSTALLED INSPECTED ACTUATOR IAW MM 32-30-04SDR DXTA20082914Uplock Switch · damagedAFTER TAKEOFF WHEN GEAR HANDLE PLACED IN UP NOSE WHEEL UNLOCK. RED LIGHT STARTED FLASHING AND THUMPING NOISE CAME FROM NOSE AREA. DURING ARRIVAL INSPECTION. RH MAIN UPLOCK SWITCH WAS FOUND DAMAGED PUT AIRCRAFT ON JACKS. REMOVED AND REPLACED DAMAGED UPLOCK SSDR DXTA20082915Metering Unit · malfunctionedNR1 ENGINE FUEL BOOST PUMP LIGHT FLASHED UPON DESCENT. A FEW SECONDS AFTER THE FLASH THE NR1 ENGINE FAILED. REMOVED/REPLACED FUEL METERING UNIT, FUEL FLOW DIVIDER, AND FUEL FLOW TRANSMITTER. REMOVED FUEL LINES AND INSPECTED FOR CONTAMINATION, NONE FOUND, REINSDR DXTA20082913Apu · overservicedWHILE RUNNING APU, ELECTRICS AND BLEED ON, RT WING O'HEAT ANN ILLUMINATED. RAN BOTH ENGINES W/APU ELECTRICS AND BLEED ON, O`HEAT ANN DID NOT ILLUMINATE, BUT STRONG BLEED AIR ODOR AND SMOKE FILLED THE AIRCRAFT. REMOVED APU BLEED AIR CHECK VALVE. NO DEFECTS FOSDR DXTA20082908Trim Tab · misriggedTRIM INDICATOR GOES .5 IN BEYOND FWD WHITE BAND AND ONLY BACK AS FAR AS THE O IN (TO) EXCESSIVE FWD CONTROL PRESSURES REQUIRED DURING TAKEOFF WITH INDICATOR IN TO RANGE. PERFORMED ELEVATOR TRIM SURVEY. FOUND EXCESSIVE CLEARENCE BETWEEN PIN AND SPACER. REMOVESDR CA080305016Engine · power loss(CAN) DESCENDING THROUGH FL370, THE ENGINE ELECTRONIC CONTROL REVERTED TO MANUAL AND ENGINE N2 SPEED REDUCED TO 41 PERCENT ASSOCIATED WITH VIBRATION. THE ENGINE DID NOT RESPOND TO THRUST LEVER INPUT AND THE CREW ELECTED TO SHUTDOWN THE ENGINE. TROUBLESHOOTING SDR 030108N577CS1Bleed Valve · defectiveENROUTE, CREW EXPERIENCED NR 2 ENGINE EEC ANNUNCIATION FOLLOWED BY ENGINE VIBRATION. CREW FOLLOWED CHECKLIST AND FOR PRECAUTIONS, SHUTDOWN RT ENGINE, DIVERTED AND DECLARED AN EMERGENCY. AC LANDED WITHOUT INCIDENT. CURRENTLY CAUSE IS YET TO BE DETERMINED AND SDR DXTA20082905Actuator · malfunctionedUPON LOWERING THE LANDING GEAR THE RED (UNSAFE) LIGHT REMAINED ILLUMINATED AND THE LT MAIN GEAR GREEN LIGHT REMAINED OFF. LT GEAR ACTUATOR REPLACED WITH RENTAL UNIT. SYS TESTED IAW MM 32-30-04. ACTUATOR REPLACED DUE TO SUSPECTED INDICATION FAILURE.SDR CA080227002Spindle · worn(CAN) CREW SNAGGED MAIN CABIN DOOR OUTER HANDLE AS BEING SLOPPY. DISASSEMBLED DOOR HANDLE AND FOUND OUTER DOOR HANDLE SPINDLE TO BE EXESSIVELY WORN WHERE PIN FOR ATTACHING OUTER HANDLE FITS. MEASURED REMAINING MATERIAL AND FOUND TO BE 0.028 INCH ON ONE SIDE ANSDR DXTA20082901Actuator · malfunctionedSELECTED GEAR DOWN LT MAIN NO GREEN ANNUNCIATOR AND RED UNLOCK ANNUNCIATOR ON. REMOVED ACTUATOR P/N 9912537-3 S/N 0760. CLEANED AND INSPECTED GEAR ASSY. INSTALLED REPAIRED ACTUATOR P/N 9912537-3 S/N 0441. RESERVICED N2. CHECKED CAMBER, OPS CK OF GEAR GOOD.SDR DXTA20082898Rmu · odor10 MINUTES AFTER TAKEOFF CREW SMELLED A BURNING PLASTIC LIKE ODOR. REMOVED NR 1 RMU PN 7012100-825 SN 98112277 AND INSTALLED REPAIRED UNIT PN 7012100-825 SN: 00102968. OPERATIONAL TEST IS GOOD REF EXCEL AMM 23-80-01SDR DXTA20082893Actuator · malfunctionedWHILE RESETTING HYD CONTROL CIRCUIT BREAKER , L T MAIN GEAR EXTENDED AND GREEN DOWN AND LOCKED LIGHT ILLUMINATED. REMOVED AND REPLACED LT MAIN GEAR ACTUATOR WITH RENTAL UNIT IAW MM 32-30-04. OPS AND LEAK CHECK GOOD. INSTALLED UNIT HAS 2089 CYCLES.SDR CA080305012Eec · malfunctioned(CAN) DURING TAKEOFF ROLL, THE ENGINE ELECTRONIC CONTROL DROPPED OFF LINE. THE CREW ADVANCED THE THRUST LEVER TO ACHIEVE REQUIRED THRUST, BUT THE POWER LEVEL REMAINED 10 PERCENT LESS THAN THE REQUIRED LEVEL.THE FLIGHT WAS ABORTED AND THE AIRCRAFT RETURNED TO TSDR 021708N554CS1Line · defectiveDURING APPROACH THE (LOW HYD LEVEL) AND (LT/RT LOW HYD FLOW) INDICATION ILLUMINATED. CREW FOLLOWED THE ABNORMAL CHECKLIST, MANUALLY EXTENDED THE LANDING GEARS, AND DECLARED AN EMERGENCY LANDING. LANDING WAS UNEVENTFUL. MAINT FOUND A DEFECTIVE LT HYDRAULIC PUMPSDR DXTA20082876Actuator · failedAFTER TAKEOFF, DURING GEAR RETRACTION, NOSE GEAR STAYED DOWN AND LOCKED (GREEN ) MAIN GEARS OPERATED NORMALLY. REMOVED NOSE GEAR ACTUATOR DUE TO INTERNAL FAILURE. INSTALLED RENTAL ACTUATOR IAW MM CH 32-30-03. PERFORMED GEAR FUNCTIONAL TEST IAW MM CH 32-01-00SDR DXTA20082874Probe · reads lowON TAKEOFF ROLL, MASTER CAUTION CAME ON, REJECTED TAKEOFF, LT FUEL GAUGE ANNUNCIATOR LIGHT ON. CONNECTED TEST SET, FOUND PROBE NR 6 READING LOW. REMOVED NR6 PROBE, CLEANED AND REINSTALLED, PROBE NOW READING IN SAME RANGE AS OTHER PROBES, C/W WET CAL IAW MM CHSDR DXTA200802867Pressure Switch · malfunctionedCAB ALT 10, 000 CAME ON AT 10,500 FEET WITH MASTER WARNING. REMOVED CABIN ALTITUDE PRESSURE SWITCH. REPLACED WITH NEW SWITCH. OPERATIONAL CHECK GOOD. WORK IAW MM 21-30-00.SDR DXTA200802864Engine · shutdownLT ENGINE QUIT SHORTLY AFTER TAKEOFF. FIRST NOTICED EEC MANUAL ANNUNCIATOR, FOLLOWED BY (DASHES) ON LT FUEL FLOW INDICATOR. ENG WAS ROTATING FREELY & LT BOOST PUMP CAME ON AUTOMATICALLY. R & R NR 1 ENG WITH REPAIRED UNIT IAW MM 71-00-03. OPS & LEAK CHECKED GOOSDR DXTA200802859Uplock Switch · inoperativeAFTER TAKEOFF, THE GEAR UNLOCK LIGHT, STAB MISCOMPARE AND HYD PRESS ANNUNCIATORS ILLUMINATED CONTINUOUSLY AFTER THE GEAR HANDLE WAS RAISED TO THE (UP) POSITION. THE HYD PRESS LIGHT NEVER FLASHED. REPLACED UPLOCK SWITCH IAW CH 32-60-01 WHILE ADJUSTING SWITCH, NSDR DXTA200802857Controller · malfunctionedAFTER LIFTOFF CABIN WOULD NOT PRESSURIZE. CABIN WAS CLIMBING AT SAME RATE AS AC. M2B- COMPLIED WITH KOLLSMAN DYNAMIC TEST, TEST FAILED. REMOVED AND REPLACED CONTROLLER IAW MM 21-30-00. OPERATIONAL CHECKS GOOD.SDR DXTA200802855Spring · weakAFTER TAKEOFF, THE GEAR UNSAFE LIGHT ILLUMINATES AFTER THE GEAR HANDLE IS PLACED IN THE UP POSITION. THE HYD PRESS AND STAB MISCOMPARE ANNUNCIATOR ALSO ILLUMINATE. PULLING THE HYD CONT CB, DOES NOT DROP ANY LANDING GEAR ASSEMBLIES OR EXTINGUISH THE UNLOCK LIGHSDR DXTA200802853Thermal Switch · malfunctionedRT BLEED AIR OVERHEAT ANNUNCIATOR ILLUMINATED ON DEPARTURE, RT THROTTLE RETARDED TO BELOW 80 PERCENT N1 AND LIGHT WENT OUT. TROUBLESHOT SQUAWK DOWN TO RT BLEED AIR OVERTEMP SWITCH. REMOVED AND REPLACED RT BLEED AIR OVERTEMP SWITCH AND OPS AND LEAK CHECKED GOSDR DXTA200802849Uplock Switch · out of adjustAFTER TAKEOFF , THE GEAR UNLOCK LIGHT ANNUNCIATOR ILLUIMINATED CONTINUOSLY AFTER THE GEAR HANDLE WAS RAISED TO THE UP POSITION. ADJUSTED L/R MAIN UPLOCK SWITCHES IAW MM CHPT 32-30-05. OPS CHECK GOOD IAW MM CHPT 32-01-00.SDR DXTA200802848Uplock Switch · looseWHEN THE GEAR IS SELECTED UP AND IT'S UP AND STOWED, A LOUD CLUNK OCCURS FROM THE NOSE AREA. FOUND NOSE GEAR UPLOCK AFT JAM NUT LOOSE AND NOT MAKING ADEQUATE CONTACT WITH UPLOCK ROLLER. RIGGED AND SAFETIED NOSE GEAR UPLOCK SWITCH IAW MM 32-61-00. COMPLIED WITH
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