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 DXTA2009101903815Bleed Valve · inoperativeRT ENGINE FAILED TO ATTAIN T/O N1 POWER. AFTER MULIPLE ATTEMTS AND AN A/C "RESET" THE BEST N1 ATTITUDE WAS 68%, N1 WITH 100% N2 INDICATED. ON FINAL ATTEMT A COMPRESSOR STALL OCCURRED. REPLACED COMPRESSOR BLEED VALVE. SERVO VALVE/TORQUE MOTOR. INSTALLED SECONDSDR 2010FA0000091Lamp · failedRT MAIN GEAR GREEN LIGHT DID NOT ILLUMINATE DURING GEAR EXTENSION FOR DOWN AND LOCK. RED IN-TRANSIT LIGHT OPERATION NORMAL. CREW BLEW GEAR DOWN, (EMERGENCY AIR EXTENSION) GREEN LIGHT STILL NOT ILLUMINATED. PRESS TO TEST REVEALED LAMP STILL INOPERATIVE. LAMSDR DXTA2009100903809Packing · leakingAT FL 370 RED GEAR "UNLOCK' LIGHT ILLUMINATED. NO NOISES OR OTHER INDICATIONS, NO OTHER LIGHTS WERE PRESENT. GEAR LOWERED NORMALLY WITH 3 GREEN. GEAR EMER EXTENSION BLOWDOWN WAS NOT USED. REPACKED NOSE STRUT ASSEMBLY IAW CMM 32-20-01 LANDING GEAR FUNCTIONASDR DXTA2009100603806Hmu · inoperativeDURING CRUISE AT 3000', REDUCED POWER TO APPROX 60% FOR A SPEED REDUCTION IN SMOOTH AIR, NO TURBULENCE, WITH IGNITIONS ON, THE LEFT ENGINE (QUIT WORKING) SPOOLED DOWN TO ZERO % FOLLOWED BY THE ASSOCIATED ANNUNCIATORS INDICATING AN ENGINE FAILURE. UPON POST FLISDR DXTA2009100203805Actuator · inoperativeHYDRAULIC PRESS LIGHT WOULD NOT EXTINGUISH AFTER TAKEOFF. GEAR WAS UP AND FLAPS WERE 0. WHEN FLAPS WERE PUT DOWN, LIGHT WENT OUT. AFTER LANDING, HYDRAULIC LIGHT CAME BACK ON AND REMAINED ON UNTIL SHUTDOWN. REMOVED SEVERAL ACCESS PANELS ON BELLY TO ACCESS CONNSDR DXTA2009100103802Transducer · inoperativeDURING TAXI ONTO RUNWAY, "ANTI SKID INOP" ANNUNCIATOR ILLUMINATED FOR 15 SEC AND EXTINGUISHED. OCCURRED A SECOND TIME DURING TAXI TO CLEAR RUNWAY. CYCLED THE ANTI SKID SWITCH AND TEST OK. ROTARY TEST OK. RIGHT TRANSDUCER BIT TRIPPED IN NOSE COMPARTMENT. NO LIGSDR DXTA2009092303796Throttle Cable · brokenWHILE ATTEMPTING TO SET T/O POWER, NR 1 THROTTLE WOULD NOT REMAIN IN T/O DETENT. TAKEOFF ABORTED, NR 2 ENG SHUTDOWN NORMALLY. IN THROTTLE CUTOFF, NR 1 ENG ACCELERATED TO APPROX 72 % N1. WITH EECS SELECTED TO MANUAL, NR 2 ENG NORMAL. PRIOR TO SELECTING EECS MSDR DXTA2009091703791Fire Loop · openRIGHT ENGINE "FIRE DET SYS R" ILLUMINATED. TROUBLESHOT TO FAULTY FIRE DETECTION LOOP. REMOVED AND REPLACED TIRE DETECTION LOOP WITH NEW LOOP IAW MM 26-11-01. OPS CHECK GOOD.SDR Z5FA091309N523CS1Bulb · burned outDURING THE APPROACH INTO DTS CREW ATTEMPTED NORMAL GEAR EXTENSION, THE LEFT MAIN LANDING GEAR INDICATION DID NOT ILLUMINATE. THE CREW PERFORMED THE EMERGENCY EXTENSION PROCEDURE PER THE AFM. LANDING WAS UNEVENTFUL. DURING TROUBLE SHOOTING MAINTENANCE DISCOVERESDR DXTA2009091103783Servo · failedLEFT EEC FAILED IN FLIGHT, THE THROTTLE WOULD NOT RESPOND IN AUTOMATIC OR MANUAL MODE, IT WAS STUCK IN FLIGHT IDLE. AFTER FOLLOWING TAB O1, PERFORMED AN ENGINE FAILURE PRECAUTIONARY SHUTDOWN. PERFORMED FUEL CONTAMINATION CHECK AND INSPECTION OF LT ENGINE FUESDR DXTA2009091103784Uplock · bindingAFTER GEAR RETRACTION, GEAR UNLOCK LIGHT REMAINED ILLUMINATED. UPON PULLING AND RESETTING HYD PRESS CIRCUIT BREAKER, NOISE WAS HEARD FROM NOSE AND MALFUNCTION CLEARED. TROUBLESHOOTING FOUND LT MAIN GEAR UPLOCK HOOK INTERMITTENTLY BINDING. CLEANED AND LUBED USDR 2009F00067Gcu · malfunctionedLEFT GEN CAUTION LIGHT ON DURING T/O ROLL. ABORTED T/O. RESET GEN AS PER CHECKLIST. GOOD VOLTAGE OBSERVED BUT GEN WOULD NOT RESET TO ON. ON POSTFLIGHT OBSERVED FLASHING SYS LIGHT ON LT GCU IN APU COMPARTMENT.SDR DXTA090907002Generator · failedDUAL GENERATOR FAILURE WITH ACCOMPANYING GEN ANNUNCIATOR L/R AND MASTER WARNING. FAILURE OCCURED WHILE CLIMBING THROUGH 15,000' WITH APU GEN ON AND LASTED 3-4 SECS. BOTH AMPHERES READ "0" BEFORE RETURNING ON LINE.SDR DXTA20090908037Control Cable · out of adjustCHECKED ALL FLT. CONTROL CABLES (PRIMARY) IAW MM 27-10-00, 27-20-00 & 27-30-00. ADJUSTED & CHECKED AILERON WING, FUSELAGE & SERVO CABLE TENSION IAW MM 27-10-00. ADJUSTED & CHECKED ELEVATOR & RUDDER CABLES IAW MM 27-31-00 & 27-20-00.SDR DXTA2009090803777Control Handle · inoperativeLANDING GEAR WILL NOT RETRACT ON TAKEOFF (REMAINED 3 DOWN AND LOCKED INDICATION). R & R CONTROL HANDLE IAW MM 32-30-01. OPS, GEAR SWING CHECK GOOD.SDR DXTA2009090803775Control Column · vibrationEXCESSIVE VIBRATION IN CONTROL YOKE/COLUMN STARTING AT 230 KTS, APPROX 9-10K FT, CONTINUED AT ALL A/S AND ALTITUDES ABOVE THAT. REPEAT WRITE-UP. VIBRATES WITH AUTOPILOT ON OR OFF.SDR DXTA2009090303770Actuator · inoperativeLEFT GREEN DOWN AND LOCKED ANNUNCIATOR ILLUMINATED INTERMITTENTLY IN FLIGHT. HYDRAULIC PRESS LIGHT DID NOT ILLUMINATE. ALL OTHER INDICATIONS NORMAL. INSTALLED REPAIRED ACTUATOR IAW THE MM 32-30-04. OPS CKED GOODSDR DXTA2009082103763Pushrod · out of adjustAFTER TAKEOFF ACFT ROLLED LEFT. EXCESSIVE PRESSURE NEEDED TO FLY STRAIGHT. A/P WAS OFF AND TRIMS WERE NEUTRAL. YOKE TURNED APPROX 45 DEG TO THE RT TO MAINTAIN HEADING. ADJUSTED AILERON TRIM TAB PUSH RODS AND SAFETIED REF MM 27-10-00. TRAVEL CHECKS ARE GOOD.SDR DXTA2009081703759Acm · leakingAFTER RUNNING APU FOR APPORX 5 MINUTES A WAVERING SQUEAL WAS HEARD AND SMOKE FILLED THE COCKPIT. APU WAS THEN IMMEDIATELY SHUTDOWN. NO SMOKE VISIBLE OUTSIDE. OIL FOUND DRIPPING FROM BOTTOM OF ACM. T/S AND FOUND APU HAD OIL IN INLET CAUSING SMOKE IN COCKPITSDR DXTA2009081403758Brake Assy · chatteringBRAKES CHATTER AND PLANE SUTTER WHEN APPLYING THE RT BRAKE DURING TAXI AND LANDING, REPLICATED ON BOTH SETS OF BRAKE PEDALS. T/S SYS TO DEFECTIVE ANTISKID VALVE, ANTI-SKID PUMP AND BRAKE METERING VALVE. REMOVED AND REPLACED ALL UNITS. BLED SYSTEM. OPS AND LEASDR 2009FA0000676Engine · reads highLT ENG WAS INSTALLED ON THIS ACFT, 22 HOURS OF FLIGHT PRIOR TO THIS INCIDENT. 3 DAYS PRIOR TO INCIDENT LT ENG EXPERIENCED A 15-20PSI RISE IN OIL PRESSURE. ON MORNING OF INCIDENT FLIGHT, PILOT NOTED NO OIL SHOWING IN SIGHT GLASS. CONTACTED MX WHO INFORMED THEM SDR DXTA2009080703754Blower · smokeDURING FLIGHT CREW OBSERVED WHAT SOUNDS LIKE A FAN HUMMING SOUNDS COMPARABLE TO WHAT IT SOUNDS LIKE WHEN ENGINES ARE OUT OF SYNCH. UPON LANDING PAX INFORMED US THAT SHE NOTICED SMOKE IN THE CABIN FOR 10 MIN PRIOR TO LANDING. TROUBLESHOT SYS, FOUND DEFOG BLOWESDR DXTA2009080403750Elevator · obstructedDURING TAKE OFF, THE ELEVATOR FLIGHT CONTROL WOULD NOT TRAVEL BEYOND THE NEUTRAL POSITION WHEN ATTEMPTING TO ROTATE DUE TO A BLOCKAGE WHICH FELT LIKE A METAL TO METAL OBSTRUCTION. FOUND BOLT MISSING FOR AFT STOP. STOP ROTATED INTO PATH OF BELLCRANK. LOCATEDSDR DXTA2009072903743Motor · malfunctionedAFTER PREFLIGHT WHERE ALL SYS TESTED NORMAL, TAXIED OUT OF RAMP. ON FIRST BRAKE CHECK OF CHECKLIST BOTH HAD BREAKS. AFTER ABOUT 200 YRDS TAXING THE "ANTISKID INOP" LIGHT STARTED FLASHING AND THE CIRCUIT BREAKER POPPED. TRYED TO RESET (IAW CHECKLIST) BUT IT PSDR CWQA072709N595SActuator · failedSTAB MIS-COMPARE AFTER TAKEOFF. UNSCHEDULED LANDING ACCOMPLISHED. STAB ACTUATOR REPLACED.SDR DXTA2009072703741Actuator · malfunctionedON TAKEOFF, GEAR DID NOT RETRACT NORMALLY; HAD RED UNSAFE INDICATION. AFTER 6 MIN, WITH SPEED BELOW 200 KIAS, CREW HEARD A LOUD CLUNK AND RED UNSAFE INDICATOR EXTINGUISHED. GEAR EXTENSION WAS NORMAL. LANDING WAS UNEVENTFUL. POST FLIGHT VISUAL INSP SHOWED NO APSDR DXTA2009072303736Indicator · out of positionEXTREME NOSE DOWN YOKE PRESSURE REQUIRED AFTER TAKEOFF. ELECTRIC TRIM CAN NOT KEEP UP WITH NOSE DOWN PRESSURE REQUIRED. COMPLIED WITH SYSTEM OPS CHECKS FOUND INDICATOR PANEL TO BE OUT OF POSITION. REPOSITIONED THE INDICATOR AND OPS CHECK GOOD. IAW MM 27-32SDR DXTA2009071703731Seal · leakingDURING TAKEOFF APPROX 500FT, CREW GOT A RT 'LO OIL PRESS' INDICATION LIGHT. CREW FOLLOWED CHECKLIST AND LANDED THE ACFT SAFELY. OIL PRESSURE WAS AT APPROX 30 PSI. ALL OTHER INDICATIONS WERE NORMAL. RAN ACFT AT TAKEOFF PWR AND FOUND GARLOCK SEAL ON FCU LEAKINSDR DXTA2009071503729Bleed Valve · malfunctionedEEC MANUAL LIGHT ILLUMINATED ON NR 2 ENGINE DURING DESCENT FOLLOWED BY LOSS OF THRUST AND CONTINUOUS COMPRESSOR STALLS. AFTER DOWNLOADING DCU FILES AND SENDING TO MANUFACTURER. REMOVED REPLACED AND OPS CHECK GOOD OF RT BLED AIR TORQUE MOTOR IAW MM 73-20-03, SDR Z5FA070909N523CSController · defectiveDURING CRUISE LT WINDSHIELD FAULT LIGHT ILLUMINATED FOLLOWED SHORTLY BY THE LT WINDSHIELD SHATTERING.SDR Z5FA070809N514CSController · defectiveDURING CLIMB NOTICED RAPID CHANGES IN CABIN RATE OF CLIMB ON THE PRESSURIZATION CONTROLLER. AT FLIGHT LEVEL 340 EXPERIENCED RAPID DEPRESSURIZATION WITH NO OTHER FAULTS OR INDICATIONS.SDR DXTA2009070703721Line · leakingFUEL FUMES IN COCKPIT AND CABIN WITH APU BLEED AIR ON. SECURED APU AND FUMES STOPPED. REMOVED SECONDARY FUEL MANIFOLD P/N 38838991 DUE TO A FITTING ON LINE LEAKING. INSTALLED A NEW LINE P/N 3883899-1. ALL WORK DONE IAW MM 49-30-06 RAN APU AND ACCOMPLISHED A SDR DXTA2009070203713Sensor · inoperativeACM OVERHEAT LIGHT ILLUMINATES DURING TAKEOFF ROLL BETWEEN 70KTS AND V1. ALSO EXPERIENCED RUSH OF AIR IN CABIN AND COCKPIT WITH HOT AIR RUBBER ODOR. TROUBLESHOT BLEED AIR SYSTEM PER MM 36-11-00. FOUND NO FLOW FROM LT PRECOOLER EXHAUST. REMOVED AND REPLACED LTSDR DXTA2009070103711Bulb · burnedSMOKE FROM CABIN LIGHTS IN BETWEEN SEATS 4 AND 6 AFTER ABOUT 40 MINUTES OF USE. SMOKE AND ELECTRICAL ODOR DISSIPATED WHEN CABIN LIGHT SWITCH TURNED OFF. R & R BURNED BULB & BULB CLIP WITH NEW BULB & CLIP. LIGHT OPERATES NORMAL AT THIS TIME IAW MM 33-20-01.SDR DXTA2009062503704Windshield · unknownREMOVED LT WINDSHIELD AND INSTALLED NEW WINDSHIELD WITH NEW HARDWARE, PERFORMED WINDSHIELD SYS PCU/ALTERNATOR AND CONTROLLER FAILURE CHECK AND NO DEFECTS NOTED. OPS CHECK AND LEAK CHECK FOUND NORMAL, APPLIED FILLET SEAL. OPS CHECK NORMAL WORK DONE IAW MM, CHPSDR DXTA2009062903704Windshield · failedLT MAIN WINDSHIELD OUTER PANE SHATTERED AT 38,000 FT.SDR DXTA2009062203694Pressure Switch · malfunctionedSTAB MIS-COMPARE LIGHT CAME ON WHEN FLAPS WERE SELECTED FLAPS 15. REMOVED AND REPLACED AIRSPEED SWITCH. OPS AND LEAK CHECKS GOOD IAW MM CH 27-40-00.SDR DXTA2009061803691Downlock Switch · failedIN CRUISE NLG GREEN LIGHT ILLUMINATED. MLG RETRACTED, LIGHT EXTINGUISHED. EXTENSION NORMAL, BLEW DOWN TO INSURE DOWNLOCK. JACKED ACFT, RELEASED PRESSURE FROM MLG SYS, RE-SEATED MLG SHUTTLE VALVES, CYCLED MLG. BLED AIR FROM SYS IAW MM 32-01-00. RANG OUT NLG SDR DXTA2009061503686Brake Assy · weakON LANDING, "LO BRAKE PRESSURE" AND "ANTI SKID INOP" LIGHTS ILLUMINATED; ANTI-SKID BITE LIGHTS ARE NORMAL. ACFT PULLS TO THE RT WHEN BRAKES ARE APPLIED ON THE GROUND AND FEEL SPONGY. NOTICABLE FLUID MISSING FROM BRAKE RESEVOIR, ONLY .3333 FULL NOW. INSPECTESDR DXTA2009061503689Actuator · inoperativeNOSE GEAR INDICATOR LIGHT ILLUMINATED IN CRUISE FLIGHT. STEADY AT FIRST, THEN INTERMITTENT. ACCOMPLISHED "GEAR WILL NOT EXTEND" CHECKLIST BLOW DOWN PROCEDURE PRIOR TO LANDING. REMOVED INOP ACTUATOR. INSTALLED CUSTOMER SUPPLIED INSPECTED ACTUATOR . OPS CHECK GSDR DXTA2009060803682Metering Valve · malfunctionedUPON LANDING AND SLOWING TO TAXI SPEED LT BRAKE PEDAL APPLICATION RESULTS IN LT BRAKE GRABBING. THIS HAPPENS ON THE CO-PILOTS SIDE AND CONTINUES DURING TAXI. BRAKES FEEL SPONGY ON CO-PILOTS SIDE. DURING TAXI THE MAIN LANDING GEAR IS MAKING A LOUD GROWLING NOSDR DXTA200906043678Actuator · bypassingSTAB MISCOMPARE ILLUMINATED AFTER TAKOFF, RAN CHECKLIST AND LIGHT WENT OUT AFTER THE HYD CONTROL C/B WAS CYCLED. FOUND HORIZ STAB ACTUATOR BYPASSING HYDRO FLUID. REMOVED AND REPLACED STAB ACTUATOR. LEAK AND OPS CHECK GOOD. IAW MM 27-40-00.SDR DXTA2009060403677Circuit Board · inoperativeWHILE ON APPROACH, FLAPS WERE SELECTED TO 15(DEG). FLAP INDICATOR DID NOT MOVE & STAB MISCOMP ANNUNCIATOR ILLUMINATED. WHEN MLG SELECTED DOWN, THEY DID NOT MOVE. APPROXIMATELY 30 SECONDS AFTER MLG WAS SELECTED DOWN, FLAPS MOVED, MLG MOVED & STAB MISCOMP ANNSDR DXTA2009060403676Trim System · malfunctionedELECTRIC TRIM WILL NOT TRIM NOSE UP FROM EITHER THE PILOT OR CO PILOT ELECTRIC TRIM. MANUAL TRIM WORKS FULL TRAVEL. REMOVED LT AND RT ELEVATOR TRIM TAB ACTUATORS DUE TO STIFF TRIM. INSTALLED NEW ACTUATORS IAW MM CH 27-32-02, OPS CHECKED AND TRAVEL CHECKED GOSDR DXTA200905213662Display · inoperativeCLIMBING THROUGH 15,000 FT, THE CO-PILOTS SIDE PFD DISPLAYED AN ATTITUDE AND HEADING FAIL. SWAPPED AHRS REFERENCE UNITS FOR TROUBLESHOOTING. NO FAIL. SWAPPED BACK TO ORIGINAL POSITIONS. CHANGED CO-PILOT AHRS REFERENCE UNIT LCR-93 WITH INSPECTED UNIT. POWEREDSDR DXTA2009052103659Track · damagedDURING FATS NOTICED TRIM FWD OF T/O & NO TAKEOFF LIGHT. TRIMMED ACFT TO TAKEOFF POSITION, LIGHT EXTINGUISHED. RAN FULL PREFLT EARLIER & NO BINDING & FULL RANGE. AT 80 KIAS ON TAKEOFF ROLL ACFT NEEDED FORWARD PRESSURE TO KEEP NOSE ON GROUND. ONCE AIRBORNE WITSDR DXTA2009051103643Valve · failedDURING STATIC T/O POWER APPLICATION AT APPROX 90 PERCENT N1, RT RUDDER MOVED FWD UNCOMMANDED, THEN RUDDER BIAS LIGHT ILLUMINATED. INSPECTED RUDDER BIAS PLUMBING IN TAILCONE, NO DEFECTS NOTED. INSPECTED RUDDER BIAS ACTUATOR. NO DEFECTS NOTED. C/W GROUND RUN, CSDR DXTA2009050803641Control Handle · malfunctionedGEAR DID NOT RETRACT WHEN GEAR HANDLE WAS SELECTED IN THE UP POSITION. ALL GREEN LIGHT WERE ILLUMINATED WITH NO RED LIGHT. THE GEAR HANDLE WAS TAPPED AND THE GEAR RETRACTED NORMALLY. REMOVED AND REPLACED GEAR CONTROL HANDLE ASSY. PERFORMED GEAR FUNCTIONAL CHESDR DXTA2009050803639Actuator · bindingIN CRUISE, PITCH TRIM WHEEL (AUTOPILOT ENGAGED) WAS FELT JERKING BUT NOT MOVING. AUTOPILOT DISCONNECTED TO FIND EXCESSIVE NOSE DOWN FORCE REQUIRED TO MAINTAIN LEVEL FLT. NOSE DOWN ELECTRIC TRIM DID NOT MOVE TRIM WHEEL. ONLY TWICE NORMAL HAND PRESSURE ON WHESDR DXTA2009050703638Coalescer Bag · odorWITH APU AND ENGINE BLEED AIR ON A STRONG MUSTY ODOR IS OBVIOUS THROUGHOUT THE COCKPIT AND CABIN. FOUND ODOR COMING FROM ACM WATER SOCK, CLEANED SOCK AND RE-INSTALLED, RAN APU AND ENGINE. RAN COCKPIT AND CABIN TEMP. THROUGH FULL HOT AND COLD NO STRONG ODOR NO
Back to Textron 560XL