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 DXTA2012022304885Trim System · contaminatedROLL TRIM ANNUNCIATOR ILLUMINATED IN CRUISE. AUTOPILOT MANUALLY DISCONNECTED TO RETRIM AILERONS. AILERON TRIM WHEEL STUCK & WOULD NOT MOVE LT OR RT. ROLL TRIM ANNUNCIATOR STAYED ON FOR 80 PERCENT OF THE FLIGHT. ON GROUND, ABLE TO MOVE AILERON TRIM. CHECKSDR DXTA2012021704877Pressure Switch · inoperativeDURING TAXI, LOW BRAKE PRESSURE AND ANTI-SKID INOPERATIVE ANNUNCIATORS ILLUMINATED AND CREW LOST BRAKE PEDAL PRESSURE. STOPPED ACFT ON TAXIWAY VIA EMERGENCY BRAKES. POWER BRAKE CIRCUIT BREAKER WAS PULLED AND RESET AND BOTH AND ANNUNCIATORS EXTINGUISHED. LOWSDR DXTA2012021404875Bracket · bentWITH LANDING GEAR RETRACTED, RED UNLOCK AND HYD PRESSURE ANNUNIATORS ILLUMAINTED. WITH LANDING GEAR EXTENDED, NO UNLOCK LIGHT OR HYD PRESS ANNUCIATOR LIGHTS ILLUMINATED. INSPECTION FOUND BRACKETS ON NOSE GEAR WHICH HOLD THE CROSS BAR FOR THE UPLOCK TO BE BENTSDR CA120227002Oil System · low pressure(CAN) APPROXIMATELY 7 MINUTES AFTER T/O, THE NR 1 ENGINE OIL PRESSURE STARTED FLUCTUATING AND FELL BELOW LIMITS. THE CREW SHUTDOWN AND SECURED THE ENGINE. THE ACFT DIVERTED TO AIRPORT AND CARRIED OUT AN UNEVENTFUL SINGLE ENGINE LANDING. TROUBLESHOOTING IS ONSDR DXTA2012021304872O-Ring · damagedBRAKES WERE LOCKING UP OR "GRABBING" BRIEFLY AFTER THE ACFT SLOWED TO LESS THAN 20 KTS ON LANDING. REMOVING FEET BRIEFLY FROM BRAKES COMPLETELY, DID NOT CLEAR THE ISSUE. AT NO TIME DID THE BRAKES COMPLETELY FAIL. BRAKE RESERVOIR IS VERY FULL, AND NO LEAKS NOSDR DXTA212021304871Unknown · vaporWITH APU RUNNING AND BLEED AIR ON WE NOTICED LIGHT SMOKE OR VAPOR IN CABIN AND A MUSTY ODOR. TURNED BLEED AIR OFF AND SMOKE/VAPOR SEEMED TO GET WORST. SHUTDOWN APU AND STARTED ENGINES AND SMOKE/VAPOR WENT AWAY.SDR DXTA2012021004868Brake Sys · malfunctionedBRAKES CHECKED NORMAL ON TAXI OUT. WHILE TAXIING & STOPPING AT HOLD SHORT LINE, LT BRAKE FAILED. FURTHER TAXIING REVEALED THAT WITH LIGHT PRESSURE APPLIED TO BRAKES, FIRST APPEAR NORMAL, THEN LEFT SIDE SEEMS TO RELEASE PRESSURE AS IF ANTI-SKID KICKS IN RELEASISDR DXTA2012021004867Control Handle · malfunctionedGEAR WOULD NOT RETRACK WHEN GEAR HANDLE WAS PULLED UP, HAD ALL 3 GREEN INDICATORS, GROUND CONFIRMED GEAR WERE WAS DOWN AND EMERGENCY WAS NOT DECLARED. HANDLE WAS PLACED DOWN TO MATCH CONDITION. PERFORMED GEAR SWING SEVERAL TIMES. DUPLICATED SQK ONCE MOVINGSDR DXTR20120209001Bolt · looseFOUR VERTICAL ATTACH BOLTS ARE LOOSE AT THE VERTICAL STAB AFT SPAR ASSY TO WEB/RIB ASSY FS 588 - WL161.5. RETORQUED TO STANDARD PRACTICES.SDR 9JLA201208023399Solenoid · defectiveCREW REPORTED THAT CABIN DOOR ANNUNICATOR LIGHT REMAINED ILLUMINATED AFTER THE CABIN DOOR WAS CLOSED. THE VENT DOOR SOLENOID WAS FOUND DEFECTIVE.SDR DXTR20120206001Rib · crackedRT WING T/E RIB CRACKED AT WS 167.07. R & R RT T/E RIB.SDR CWQR20120207002Hinge Fitting · crackedDURING A VISUAL INSPECTION, FOUND CORROSION ON CABIN DOOR HINGE FITTING, LIMITED TO THE INWARD EDGE OF THE HINGE FITTING, ON CLOSER INSPECTION, FOUND A CRACK THAT WAS .35 INCH LONG ON THE HINGE FITTING RADIUS AREA BETWEEN THE FLANGE ATTACH BRACKETS. THE CRACKSDR CWQR20120207001Hinge Fitting · crackedDURING A VISUAL INSPECTION OF THE FORWARD CABIN DOOR HINGE FITTING, FOUND CRACK. CRACK .35 INCHES LONG AND WAS IN THE RADIUS AREA BETWEEN THE FLANGE AREA THAT ATTACHES TO THE FUSELAGE. THE CRACK WAS VERIFIED USING DYE PENETRANT METHOD. HINGE FITTING WAS REPSDR 9JLA201201293447Solenoid · inoperativeTHE CREW REPORTED AFTER THE CABIN DOOR WAS CLOSED THE CABIN DOOR ANNUNICIATOR REMAINED ILLUMINATED. TROUBLSHOOTING FOUND THE DOOR SOLENIOD INOP.SDR DXTA2012013004857Control Handle · intermittentDURING GEAR RETRACTION AFTER TAKEOFF, THE RED GEAR UNLOCK LIGHT REMAINED ON. SOUNDED LIKE THE GEAR RETRACTED NORMALLY. NO ABNORMAL NOISES OR VIBRATIONS WERE NOTED. RAN THE STAB MISCOMPARE AND HYD PRESSURE ANNUNCIATOR CHECKLISTS. THAT DID NOT FIX PROBLEM. SDR DXTR20120125008Pivot Assy · looseAFT HORIZONTAL PIVOT FITTING, LOOSE (HAND TURN) ATTACH LOCK FASTENERS AND LOOSE ATTACH BOLTS.SDR DXTR20120119007Bracket · crackedRUDDER AUTOPILOT CABLE BRACKET IS CRACKED AT AFT CANTED BULKHEAD.SDR DXTR20120119006Rib · crackedRIGHT WING FLAPWELL T/E RIB AT WS 143.07 IS CRACKED.SDR DXTR20120119005Rib · crackedRIGHT WING FLAPWELL T/E RIB AT WS 88.63 IS CRACKED.SDR DXTR2012004Rib · crackedLEFT WING FLAPWELL T/E RIB AT WS 64.0 IS CRACKED.SDR DXTA2012011704847Actuator · malfunctionedAFTER GEAR WAS EXTENDED, THE RED UNLOCK LIGHT FLICKERED ON/OFF FOR ABOUT 5 MINUTES. 3 GREEN WERE CONTINUOUSLY ILLUMINATED. EVENTUALLY FLICKERING STOPPED. OPTED TO BLOW THE GEAR DOWN WITH THE EMERGENCY BOTTLE. LANDED NORMAL. R & R RT MAIN GEAR ACTUATOR. SDR JEMA2012FA0000029Mount · damagedRT ENGINE AFT MOUNT ASSY FOUND TO BE DAMAGED. CENTER BOLT BENT. DEEP CHECK CUTS IN ENDS OF RUBBER INSERT MATERIAL. ATTACHING ARMS SIEZED TOGETHER AT CENTER BEARING, PN 6651602-4. PART REPLACEMENT RECOMMENDED AT SECOND ENGINE CHANGE (APPROX 10,000 HRS).SDR DXTR2012011105Stiffener · crackedNOSE WHEEL STEERING CABLE STIFFNER FOR PULLEY BRACKET JUST FWD OF CENTER PEDESTAL UNDER FLOORBOARD 141BTC HAS APPROX 0.25 INCH CRACK AT TOP, AFT CORNER RADIUS, FROM EDGE HEADING FWD AND DOWN TOWARDS AFT PULLEY BRACKET.SDR DXTR2012011104Rib · crackedRT FLAP WELL T/E RIB AT WS 88.6 IS CRACKED.SDR DXTR2012011103Rib · crackedLT FLAP WELL T/E RIB AT WS 64.0 IS CRACKED.SDR DXTR2012011102Trim Tab · wornRUDDER TRIM TAB HAS EXCESSIVE PLAY.SDR DXTR2012011101Skin · damagedBOTTOM OF RIGHT INBD FLAP HAS SOFT SPOT FROM IMPACT DAMAGE.SDR CA120115008O-Ring · cut(CAN) SHORTLY AFTER LEVELING AT CRUISE FL410, THE NR 2 ENGINE N1 ROLLED BACK FROM ABOUT 90 PERCENT TO 70 PERCENT WITH ASSOCIATED FUEL FLOW DECREASE. THE CREW INITIATED A DESCENT, NOTICED A KNOB SPLIT BETWEEN THE 2 ENGINES, DID NOT SHUTDOWN THE ENGINE AND A NOSDR DXTA2012010304838Actuator · inoperativeTAKE OFF REQUIRED EXTRA RIGHT RUDDER PRESSURE. ON CLIMBOUT TO 14,000 FT, ACFT REQUIRED FULL RT RUDDER TRIM AND FULL RT RUDDER AND THAT WAS NOT ENOUGH FOR COORDINATED FLIGHT. ON RETURN TO AIRPORT AT LOWER POWER SETTINGS, PLANE REQUIRED HALF OF RT RUDDER TRIM SSDR DXTA2012010404838Trim System · malfunctionedTAKEOFF REQUIRED EXTRA RT RUDDER PRESSURE. ON CLIMBOUT TO 14,000 FT, REQUIRED FULL RT RUDDER TRIM AND FULL RT RUDDER AND THAT WAS NOT ENOUGH FOR COORDINATED FLIGHT. ON RETURN TO AIRPORT AT LOWER POWER SETTINGS PLANE REQUIRED HALF OF RT RUDDER TRIM SETTING FOSDR CVGA20120031Anti-Ice System · inoperativeRIGHT ENGINE ANTI-ICE INOP.SDR Z5FA2011010900001Control Cable · brokenDESCENDING, BOTH ELECTRIC AND MANUAL ELEVATOR TRIM BECAME INOPERATIVE. AN EMERGENCY WAS DECLARED. ACFT LANDING WAS UNEVENTFUL. MX FOUND THE LT AFT ELEVATOR TRIM CABLE BROKEN. THE CABLE WAS REPLACED, SYS RIGGED AND OPS CHECK WAS SUCCESSFUL. ACFT WAS RETURNESDR DXTA2012010304835Control Cable · out of adjustAFTER DEPARTURE AND DURING CLIMBOUT, NOTICED SIGNIFICANT RT AILERON HAD TO BE APPLIED TO KEEP PLANE LEVEL. ACFT ACCELERATED TO 200 KTS AND MORE RT AILERON CONTROL FORCE NEEDED. WITH THE AILERON TRIM CENTERED NEUTRAL, ACFT WOULD BANK HARD LT TO 30 DEGREES WISDR DXTA2011122104829Contactor · inoperativeDURING REPOSITION, ENGINES WERE STARTED WITHOUT APU RUNNING. RT ENGINE STARTED NORMALY & HALF WAY THROUGH LT ENGINE START, A VERY STRONG HOT ELECTRICAL ODOR STRONG ENOUGH TO BURN THE EYES. DISCONTINUED START ON LT ENGINE & SHUTDOWN BOTH ENGINES. ODOR ONLY ISDR DXTA2011121904827Landing Gear · out of adjustAFTER TAKEOFF, MLG SELECTED UP, FOLLOWED SHORTLY WITH FLAP RETRACTION. SOON AFTER, STAB MISCOMPARE ANNUNCIATOR, HYD PRESSURE ANNUNCIATOR & RED MLG UNLOCK INDICATOR ILLUMINATED. MLG SELECTED DOWN WITH NORMAL INDICATIONS OF 3 DOWN & LOCK INDICATORS. STAB MISCSDR X7PA121511Tube · chafedDISCOVERED FAILED ECU ASPIRATOR HIGH PRESSURE TUBE, BROKEN ECU ASPIRATOR TO COASLESCER TUBE & CHAFED RUDDER BIAS BLEED AIR TUBE ON PREFLIGHT. THIS CONDITION APPEARS TO BE DUE TO POOR ROUTING AND ON GOING CHAFING BETWEEN THE ASPIRATOR AND RUDDER BIAS PLUMBING SDR DXTR20111214401Attach Fitting · wornTHE FWD AND AFT HORIZONTAL STAB ATTACH POINTS ARE WORN, ALLOWING HORIZONTAL STAB MOVEMENT BOTH RADIALLY AND UP AND DOWN. THIS MOVEMENT HAS PLAY IN THE HORIZONTAL, SEEMS TO HAVE STARTED TO LOOSEN UP ANOTHER AREA. THE LT SIDE OF THE AFT VERTICAL SPAR HAS AN ARSDR DXTR2011121400000Hydraulic Line · chafedCOPILOTS RT RUDDER PEDAL IS CHAFING ON LT HYDRAULIC BRAKE LINE AT FORWARD BULKHEAD.SDR 2011FA0000778Bracket · crackedDURING A ROUTINE PHASE A/B INSPECTION, TECHS DISCOVERED THAT THE AUTOPILOT RUDDER CABLE BRACKET LOCATED AFT OF THE CANTED BULKHEAD HAS A 1" CRACK AT THE BASE OF THE BRACKET PASSING THROUGH THE TOP MOUNT HOLE.SDR DXTA2011120804818Connector · damagedAFTER DEPARTING IN HEAVY RAIN, GEAR WAS SELECTED UP. GEAR RETRACTED BUT RED GEAR UNLOCK LIGHT REMAINED ILLUMINATED. FLAPS WERE SELECTED UP BUT DID NOT RETRACT. HYD PRESSURE LIGHT ILLUMINATED. STAB MISCOMPARE LIGHT ILLUMINATED. GROUND IDLE LIGHT ILLUMINATEDSDR CVGA 11 339 2Wire Harness · openNR 2 ENGINE ITT INDICATION; BOTH DIGITAL AND TAPE INDICATOR INOPERATIVE.SDR 9JLA201112053394Display · defectiveTHE CREW REPORTED THAT DURING CRUISE FLIGHT THE STANDBY ATTITUDE INDICATOR DISPLAY SCREEN WENT BLANK. THE DEFECTIVE SECONDARY FLIGHT DISPLAY (STANDBY) WAS REMOVED SN M001386. AN O/H UNIT WAS INSTALLED. FUNCTIONAL CHECKS WERE SATISFACTORY. SN M001386 WAS O/H ISDR CVGA 11 338 1Altimeter · malfunctionedRADAR ALTIMETER READING ZERO AT ALTITUDE, SETS OFF GEAR HORN AND GPWS.SDR Z5FA2011120757601Actuator · contaminatedDURING DEPARTURE, JUST BEFORE LEVEL OFF AT FL410, PITCH TRIM MISCOMPARE ON PFD ILLUMINATED. IAW CHECKLIST THE AUTOPILOT WAS DISCONNECTED AND CREW HAD TO USE CONSIDERABLE AMOUNT OF CONTROL COLUMN FORWARD PRESSURE TO MAINTAIN LEVEL FLIGHT. FOUND PITCH TRIM WHEESDR 9JLA201112073392Display · defectiveTHE CREW REPORTED THAT DURING ACFT POWER UP THE STANDBY ATTITUDE INDICATOR DISPLAY WOULD INTERMITTENTLY LOCK UP. THE DEFECTIVE UNIT WAS REMOVED. AN OVERHAULED UNIT WAS INSTALLED, FUNCTIONAL CHECKS SATISFACTORY.SDR DXTA2011120104809Indication Sys · malfunctionedGEAR UNLOCK LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION SELECTED. HYD PRESS ALSO REMAINED ILLUMINATED. AIRSPEED NEVER EXCEEDED 196 KTS. ONCE GEAR WAS SELECTED TO EXTEND, THE SYS CYCLED NORMALLY (3 GREEN NO RED). PERFORMED HYD EXTENSION AND RETRACTION MANSDR DXTA2011120104808Landing Gear · malfunctionedAFTER TAKEOFF GEAR WAS SELECTED UP, RECEIVED THE RED UNLOCK LIGHT, GEAR WAS CYCLED AGAIN WITH SAME OUTCOME. DECIDED TO KEEP GEAR DOWN AND LOCK, AND LANDED.SDR DXTA2011112804798Uplock Switch · inoperativeON GEAR RETRACTION, NOSE GEAR LIGHT AND GEAR UNSAFE LIGHT REMAINED ILLUMINATED. EXTENDED GEAR AND LEFT IT DOWN FOR REMAINDER OF FLIGHT. AFTER FLAP EXTENSION TO BOTH 15 AND 35 DEGREES HYD PRESSURE LIGHT REMAINED ILLUMINATED AND ACTIVATED MASTER CAUTION. WITHISDR A59A2012F00020Engine · multiple failDURING A CLIMB, NOTICED RT ENGINE LOW OIL PRESSURE (RED) ANNUNCIATOR ILLUMINATE. ALSO NOTICED RT ENGINE MANUAL MODE WHITE ANNUNCIATOR ILLUMINATED AND THE OIL PRESSURE GAUGE TO ZERO. PILOTS NOTICED SMOKE IN THE COCKPIT, BOTH VISUALLY AND THROUGH ODOR. DECLASDR DXTA2011111604793Actuator · contaminatedCAPTAIN`S AND F/O RUDDER PEDALS BECAME INCREASINGLY STIFF AT HIGHER ENGINE POWER SETTINGS. FOUND RUDDER BIAS ACTUATOR CORRODED AND FULL OF WATER. REPLACED ACTUATOR IAW THE MM 27-20-05. OPS CHECKED GOOD.
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