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 DXTA2010072204170Display · erraticSTANDBY HSI INDICATIONS ERRACTIC ON BOTH HEADING AND CLIMB AND DESCENT INFORMATION. TESTED AND CONFIRMED ON INITIAL POWER-UP SYS OPERATED NORMALLY. TAXI CHECKED ACFT SYS AND FOUND INDICATOR WOULD ERRATICALLY TILT 5 DEGREES TO THE RT WHILE ACFT WAS STRAIGHT ANSDR DXTA2010072104165Valve · malfunctionedWHILE LEVELING AT 5000 FT RT ENGINE "EEC MANUAL" LIGHT ILLUMINATED. APPROX 30 SEC LATER THE ITT REDLINED. UPON POWER REDUCTION ENGINE BEGAN TO VIBRATE. PERFORMED A PRECAUTIONARY SHUTDOWN CHECKLIST. TROUBLESHOT PROBLEM: DOWNLOADED LT AND RT ENGINE IDLES WITH ISDR DXTA2010072004163Wire · shortedNO BRAKES - POWER BRAKE MOTOR NOT WORKING. LOW BREAK PRESSURE ANNUNCIATOR STAYS ILLUMINATED. TROUBLESHOT & FOUND POWER COMING INTO BRAKE CONTROL MOTOR RELAY KNOB BUT NOT GOING OUT. RUNG OUT RELAY, NO POWER AT X1 OF THE RELAY. JUMPERED A1 & X1 AND RELAY CLOSSDR DXTA2010071504155Control Cable · brokenON DESCENT FOR APPROACH, THE PITCH TRIM LIGHT ON THE PFD CAME ON. AFTER DISCONNECTING AUTOPILOT, THE ELECTRIC TRIM DID NOT MOVE THE TRIM WHEEL. PITCH TRIM CIRCUIT BREAKER REMAINED IN. TRIM WHEEL AND INDICATOR MOVED MANUALLY WITH LITTLE RESISTANCE. ON POST FLIGSDR 2010FA0000784Fcu · malfunctionedWHILE DESCENDING INTO THE BASE AIRPORT, THE NR 2 ENGINE WOULD NOT ROLL BACK TO IDLE WHEN THE THROTTLE WAS CLOSED. THE THROTTLE APPEARED TO HAVE NO AUTHORITY OVER THE ENGINE AT THAT POINT. A SLOW ACCELERATION OF THE NR 2 ENGINE FORCED THE CREW TO SHUT IT DOWNSDR 2010FA0000749Control Cable · frayed( EBVR) CUSTOMER NOTICED ANOMALY IN "FEEL" OF ELEVATOR TRIM. INSP SHOWED (1) ELEVATOR TRIM CABLE FRAYED WITH NUMEROUS BROKEN STRANDS. FRAYED AREA WAS FOUND IN THE AREA OF FS 591, WHERE CABLE EXITS VERTICAL STAB AND ROUTES INTOR HORIZ STAB. CUSTOMER REPLACESDR X7PAN881VP070810Control Arm · brokenFOUND CONTROL LOCK SYSTEM PARTIALLY INOPERATIVE ON POSTFLIGHT INSPECTION, FURTHER INVESTIGATION DETERMINED LEFT AILERON LOCK ARM BROKEN AT LOCK FEATURE CONTACT AREA. CAUSE OF PART FAILURE IS UNKNOWN. PART APPEARS TO HAVE SUFFERED OVERLOADING AT CONTACT POISDR CWQR.2010.04Tube · brokenDURING A SCHEDULED INSP/ OPS CHECK OF THE ECU, WE FOUND THE ASPIRATOR TUBE ASSY BROKEN AT THE FLAIR NUT FITTING ON THE ECU. A SERVICE CONDITION REPORT HAS ALSO BEEN SUBMITTED TO MFG UNDER SCR 520216.SDR DXTA2010070704145Ahrs · malfunctionedHEADING FAIL INDICATED ON LEFT SIDE PFD AND MFD WHILE IN CRUISE FLIGHT AT FL 400. WITH REV MODE SELECTED, INDICATION NORMAL. R & R NR 1 AHRS UNIT. C/W COMPASS SWING. OPS CHECKS GOOD IAW MM 34-21-01.SDR DXTA2010070604143Anti-Skid Sys · malfunctionedPRESS LIGHT FOLLOWED BY AN ANTI SKID INOP LIGHT. WE LANDED AND USED THE EMERGENCY BRAKING SYSTEM. UNABLE TO DUPLICATE. SERVICED GEAR/ BRAKE ACCUMULATOR. BLED BRAKES. R & R ANIT-SKID CONTROL RELAY. INSPECTED GEAR HANDLE WIRES AND SWITCHES; CLEANED AS WELL. ISDR DXTA2010062504131Wire Harness · faultyLEFT ENGINE ITT SPIKED TO 800° IN FLIGHT. TRIED TO CONTROL TEMP WITH THROTTLE, BUT WHEN WE DESCENDED TO 5000', ITT EXCEEDED 760°. SHUTDOWN ENGINE, BUT ITT NEVER DROPPED BELOW 500° - EVEN WHEN ON GROUND. FOUND T1 SENSOR HARNESS OUT OF LIMITS AND ERRATIC. INSTSDR Z5FA061910N549CS1Connector · misinstalledON TAXI OUT CHECKS AFTER UNRELATED MX ACTIVITY CREW WAS UNABLE TO DEPLOY THRUST REVERSERS OR RAISE FLAPS AND RETURNED TO SERVICE CTR. SERVICE CTR MX TROUBLESHOT SYS AND FOUND THE HYD LOADING VALVE CONNECTOR PLUG MISCLOCKED CAUSING WIRE BUNDLE TO CONTACT SURROSDR DXTA2010061804127Lock · brokenAFTER TAKEOFF, STAB MISS COMPARE LIGHT STAYED ON ALONG. WITH THE HYD PRESSURE LIGHT AND THE NOSE GEAR UNLOCK RED LIGHT STAYED ON AS WELL. FOUND LT MAIN GEAR UPLOCK SWITCH NOT BEING MADE WITH GEAR UP DUE TO LT MAIN LAND GEAR ACTIVATOR ROD END LOCK CLIP BROKEN.SDR CWQR.2010.03Torque Tube · corrodedTHIS IS GENERAL INFORMATION REGARDING SURFACE CORROISION ON ELEVATOR TORQUE TUBES.THE TORQUE TUBES ARE A WELDED STEEL ASSY, AND IS NOT UNCOMMON TO FIND SOME CORRISION WHERE IT IS EXPOSED. HAVE FOUND ABOUT 10 ELEVATOR TORQUE TUBES WITH SURFACE CORRISION. OF THSDR DXTA2010061404121Coalescer Bag · dirtySMOKE DETECTED IN COCKPIT & CABIN BY PILOTS ON TAKEOFF (VISUAL & SMELL). SMOKE APPEARED MILDLY ELECTRICAL NOT OIL OR AIR CON BASED. APU RUN PRIOR TO TAKEOFF ROLL, ACM PREVIOUSLY PRODUCED MUSTY ODOR, NOT APPARENT THIS OCCASION. SMOKE DISSIPATED ON LANDING. PSDR DXTA2010060804117Compressor · stalledRT EEC MANUAL ADVISORY LIGHT ILLUMINATED AFTER COMPRESSOR STALL IN CRUISE FLIGHT FL400. SEVERAL MORE (6-7) COMPRESSOR STALLS DURING DESCENT WITH POWER BETWEEN 65 AND 75 PERCENT N1. R & R THE RT ENGINE TORQUE MOTOR W/ O/H UNIT, OBTAINING, ORIGINAL ORIFICE PN 3SDR DXTA2010061104120Bearing · wornRUBBING HEARD/FELT IN YOKE & FLOOR DURING FORE & AFT MOVEMENT OF YOKE ONLY WHEN AIRBORNE & AT ALL AIRSPEEDS & CONFIGURATIONS. NO RUBBING INDICATED WITH LT/RT MOVEMENT OF YOKE. RUBBING HEARD/FELT ON BOTH SIDES YOKE & FLOOR OF COCKPIT WITH EACH PILOT CALLING RSDR DXTA201006014106Door · failedMAIN ENTRY DOOR HISS ON CLIMB OUT, DOOR OPENED IN FLIGHT UPON RETURN TO AIRPORT. NO DEFECTS WERE NOTED WITH THE DOOR LATCHING/WARNING SYS. NTSB INVESTIGATION IN PROGRESS, AWAITING CVR SUMMARY.SDR DXTA2010052504101Bulb · inoperativeAFTER LANDING GEAR EXTENSION, GREEN NLG LIGHTS FAILED TO ILLUMINATE. COMPLIED WITH THE LANDING GEAR WILL NOT EXTEND CHECKLIST. LANDING WAS NORMAL. AFTER LANDING, BULBS DID NOT ILLUMINATE ON ROTARY TEST. R & R BOTH NLG DOWN & LOCK LIGHT BULBS. JACKED ACFT, CYCSDR DXTA2010052504100Wire · damagedAFTER TAKEOFF, FLAPS WERE COMMANDED UP AS NORMAL. CREW NOTICED AMBER STAB MISCOMPARE WARNING. FLAP INDICATOR SHOWED FLAPS STUCK AT 7 DEGREES. CREW NOTICED HYD CONTROL CIRCUIT BREAKER POPPED. ONE RESET ATTEMPTED BUT FAILED. MLG HANDLE SELECTED, BUT MLG FAILED TSDR DXTA2010052504102Line · misinstalledWHILE ACCOMPLISHING THE RUDDER BIAS CHECK, WHEN PUSHING RT THROTTLE UP, LT PEDAL ADVANCED. WHEN PUSHING LT THROTTLE UP, RT PEDAL ADVANCED. INSPECTED & FOUND LINES INSTALLED IN WRONG POSITION. REMOVED RUDDER BIAS VALVE. REMOVED FITTINGS GOING INTO VALVE AND SDR DXTA2010051204092Actuator · faultedON GEAR DOWN, RECEIVED GEAR UNSAFE LIGHT, NO LIGHT FOR LT MLG & GOT GREEN LIGHT FOR NOSE & RT MAIN. "HYD PRESS ON" LIGHT REMAINED ON. RAN "MLG WILL NOT EXTEND" CHECK LIST. NO CHANGE IN GEAR INDICATIONS. ON DOWN WIND LEG 1500 FT AGL, GOT NORMAL GEAR DOWN INDICSDR CA100805007Circuit Breaker · poppedCIRCUIT BREAKER POPS OPEN IN FLIGHT (1 OF 3 IN PARALLEL), REPLACED NEW - NOTE THIS CIRCUIT BREAKER AS REPLACED AT 261 HRS, 342 HRS AND 767 HRS.SDR DXTA2010051004089Brake Assy · malfunctionedLT BRAKE INDICATOR IS TRIPPED. ANTI SKID CAUTION LIGHT ILLUMINATED MOMENTARILY UPON TOUCHDOWN AND AGAIN DURING TAXI. LT BRAKE IS SENSITIVE AND OCCASIONALLY MAKES A GRINDING NOISE. REPLACED LT BRAKE ASSY WITH O/H ASSY BLEED BRAKES, TAXIED ACFT ALL CHECKED GOODSDR Z5FA050510N542CS1Light · meltedON APPROACH, SMOKE FROM PEDESTAL AREA NEAR AUTO-PILOT CONTROLLER WITH ODOR. DONNED O2 MASKS, DROPPED PAX O2 MASKS. DECLARED EMERGENCY & LANDED WITHOUT INCIDENT, PAX EVACUATED. FIRE PERSONNEL INSPECTED, UNABLE TO FIND CAUSE FOR SMOKE & ODOR. AREA INSPECTED,SDR DXTA2010050304084Eec · malfunctionedCLIMBING THROUGH FL280 HAD PARTIAL LOSS OF POWER ON THE RT ENGINE, POWER LEVERS IN CLIMB. MAX POWER WAS 64.5 % WITH FUEL FLOW OF 360. LT ENG APPROX 85 % & FUEL FLOW AROUND 800. DESCENDING THROUGH FL250 ENG POWER RETURNED TO NORMAL. R & R RT ENG EEC IAW MM 7SDR DXTA2010042904078Actuator · malfunctionedRT LANDING GEAR WOULD NOT INDICATE DOWN AND LOCKED AFTER NORMAL EXTENSION. RAN THE EMERGENCY CHECKLIST, PULLED THE HANDLE AND BLOW DOWN AND STILL NO GREEN INDICATION. YAWING ACFT WOULD NOT GIVE DOWN AND LOCKED INDICATION. LIGHT WAS CONFIRMED TO WORK WITH ROTARSDR DXTA2010042604076Brake Assy · weakCAPTAINS LT BRAKE PEDAL GOES ABOUT HALF WAY TO FLOOR BEFORE BRAKES BEGIN TO TAKE EFFECT. ONCE THAT POINT IS REACHED, BRAKES SEEMS TO WORK OK, BUT LT AND RT PEDALS DO NOT MATCH. CHECKED MASTER CYL FOR LEAKAGE, NONE NOTED. CHECKED HISTORY OF SQUAWK. FOUND WITHISDR DXTA2010042604075Brake Assy · weakBRAKE PEDALS FEEL MUSHY. THEY REQUIRE SIGNIFICANTLY MORE PRESSURE THAN NORMAL TO BRAKE THE AIRPLANE. ALL 4 PEDALS FEELS THE SAME. INSPECTED BRAKE SYS FOR LEAKS, NONE FOUND. PERFORMED BRAKE SYS BLEEDING TO HYD BRAKE SYS IAW MM 32-44-00. BRAKE SYS, OPS CHECKSDR DXTA2010041904072B-Nut · looseLT BRAKE PEDAL ON THE CAPTAIN'S SIDE GOES ALL THE WAY TO THE STOP WITH LITTLE TO NO BRAKING EFFECT. FOUND LOOSE B-NUT ON LOW SIDE OF SYS. TIGHTENED B-NUT; BLED BREAKS. TAXI CK GOOD. WORK DONE IAW MM CHAP 32-42-00.SDR DXTA2010041404066Unknown · odorSTRONG ACRID/EXHAUST SMELL BEGAN WHEN COCKPIT TEMP CONTROL WAS INCREASED TO APPROX 70 DEGREES. SUPPLY TEMP WAS BETWEEN 150 AND MAX OBSERVED OF 205 DEGREES. REMOVED AND CLEANED WATER SYS AND INSTALLED IAW MM 21-51-00 THEN RAN APU SELECTED TEMP CONTROL IN AUTOSDR DXTA2010040604061Brake Sys · weakCAPTAIN SIDE, LT BRAKE FEELS MUSHY AND TRAVELS TO THE FLOOR BEFORE ENGAGING THE BRAKE. COPILOTS BRAKES APPEAR NORMAL. PERFORMED BLEEDING PROCEDURE FOR THE BRAKE MASTER CYLINDER. PEDAL TRAVEL IS NOW EQUAL ON THE PILOT SIDE LT AND RT PEDAL. NO FURTHER ACTION RSDR Z5FA41510N546CSFuel Control · failedLANDING, THE LT ENGINE AUTO SHUTDOWN. NO ABNORMAL INDICATIONS PRIOR TO SHUTDOWN. CREW IDENTIFIED ENGINE FAILURE DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. TROUBLESHOOTING REVEALED THE FUEL CONTROL UNIT TO BE AT FAULT. THE FCU WAS REPLACED AND THE ACFT SDR Z5FA032510N546CS1Engine · shutdownLANDING, THE LT ENGINE AUTO SHUTDOWN. NO ABNORMAL INDICATIONS PRIOR TO SHUTDOWN. CREW IDENTIFIED ENGINE FAILURE DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. ACFT IS CURRENTLY IN MX.SDR CWQR.2010.01Stringer Clip · crackedDURING DISASSEMBLY TO REPLACE THE AFT ENG CARRY-THRU BEAM ASSY, WE FOUND PN 6612029-36 STRINGER CLIP CRACKED 0.84 INCHES. THIS PART IS LOCATED ON THE LT SIDE OF THE TAIL BAGGAGE AREA, AND IS BETWEEN THE AFT ENGINE BEAM AND THE TAIL BAGGAGE DOOR FRAME STRUCTURESDR DXTA2010031504030Oil System · reads highAT CLIMB TO FL370. RT ENGINE OIL PRESSURE EXCEEDED RED LINE TO 190/200PSI. REDUCED THROTTLE & BEGAN TO DESCEND. AT FLT IDLE, OIL PSI STAYED ABOVE RED LINE UNTIL BELOW FL200. KEPT THROTTLE AT FLT IDLE. PSI HIGHER THAN LT ENGINE BUT STAYED IN GREEN AT 120PSI. ASDR DXTA2010030804016Brake · weakBRAKE PUMP CYCLES ON AND OFF EVERY 5 TO 10 SECONDS. PIC RT BRAKE PEDAL HAS .5 INCH MORE PLAY COMPARED TO LT BRAKE. BRAKES SLIGHTLY MUSHY. PERFORMED BRAKE BLEED ON PIG RT BRAKE. BLED SEVERAL TIMES AND BRAKES FEEL FIRM. SERVICED RESERVOIR TO LIMITS. LEAK CHECKSDR DXTA2010030804022Strut · underservicedWHEN THE GEAR WAS SELECTED UP, THE RED UNLOCK LIGHT REMAINED ON AND ALL 3 GREEN LIGHTS WENT OUT. THE PLANE FLEW AS THOUGH ALL THE GEAR WERE UP IN THE WELLS. SERVICED NOSE STRUT IAW MM 12-14-00. VERIFIED RIG OF NLG UPLOCK IAW MM 32-30-05. CHECKS GOOD.SDR 2010F00027Tube · shortTHE RUDDER CONTROL CABLES PASS THROUGH A PLASTIC GUIDE TUBE BETWEEN WING AND FUSELAGE. THIS GUIDE TUBE IS NOT SUPPORTED AT AFT END. IT IS TOO SHORT TO PASS THROUGH THE SUPPLIED SUPPORT CLAMP. SB560XL-27-20 ADDRESSES THIS CONDITION BUT IS NOT APPLICABLE TO TSDR DXTA2010030304010Wire Harness · faultedRT THRUST REVERSER UNLOCK LIGHT ILLUMINATED ON THE DESCENT TO DESTINATION. PERFORMED APPROPRIATE EMERGENCY/ABNORMAL PROCEDURES CHECKLIST. AFTER RUNNING THE CHECKLIST THE UNLOCK LIGHT EXTINGUISHED INITIALLY BUT THEN STARTED FLICKERING ON AND OFF UNTIL LANDINGSDR DXTA2010030104007Brake · weakLT BRAKE PEDAL FROM BOTH LT AND RT VERY MUSHY AND VERY LITTLE BRAKING ACTION. FROM LT SEAT, LT PEDAL ALMOST GOES ALL THE WAY TO THE FLOOR BEFORE ANY BRAKING ACTION. BLED ANTI SKID BRAKE SYS AND TAXIED ACFT MULTIPLE TIMES IAW MM 32-42-00. ALL OPS CHECKS AND LSDR CA101027002Transmitter · failedENG OIL PRESSURE IN FRITE INDICATING LOSS OF OIL PRESSURE FOUND WITH TROUBLE SHOOTING ON GROUND, THE ENG OIL PRESSURE WAS NORMAL AND INDICATION AT FAULT OIL PRESSURE TRANSMITTER WAS FAILING GIVING LOWER OIL PRESSURE INDICATION THAN THE ENGINE WAS GENERATING. SDR DXTA2010022203997Heating Element · failedAT FL230 SAT WAS -30C. NOTICED SPARKS AT THE TOP RT PORTION OF PILOT SIDE WINDSHIELD AND WITHIN 5 SECONDS THE WINDSHIELD COMPLETELY SHATTERED, "WINDSHIELD FAIL R" ANNUNCIATOR ILLUMINATED SIMULTANEOUSLY. TROUBLESHOT & FOUND PILOTS WINDSHIELD HEATING ELEMENTS SDR Z5FA021510N547CSWindshield · failedDURING CRUISE, RT WINDSHIELD SHATTERED. EMERGENCY CHECKLIST WAS FOLLOWED. ACFT DIVERTED. MX REPLACED THE WINDSHIELD. LEAK AND OPS CHECK WAS GOOD. ACFT WAS RETURNED TO SERVICE.SDR DXTA2010021503984Warning Light · illuminatedAFTER TAKEOFF, GEAR UNLOCKED LIGHT REMAINED ON WITH NO GREEN GEAR POSITION LIGHTS ON. HYD PRESS LIGHT REMAINED ILLUMINATED STEADY. STAB MISCOMPARE ANNUCIATOR CAME ON FOR APPROX 30 SECONDS AND THEN WENT OFF. WHEN HYD SYS CB WAS PULLED PER CHECKLIST, NOSE GEAR SDR CA100218001Windshield · broken(CAN) WINDSHIELD OUTER PLY SHATTERED AS ACFT CLIMBED THROUGH 10,000 FT, ACFT RETURNED TO LAND WITH NO FURTHER DIFFICULTY. (TC 20100218001)SDR DXTA2010021203980Uplock Switch · out of adjustAFTER TAKEOFF; STAB MISCOMPARE. CONFIRMED BELOW 200KTS & CYCLED FLAPS; STILL RECEIVING MISCOMPARE. RAN CHECKLISTS, PULLED HYD CTRL CB THEN NOTICED GEAR UNLOCK LIGHT ON WITH NO GREEN LIGHTS. ON APPCH; CB PUSHED IN & FLAPS 15-STAB MISCOMPARE WENT OUT, HYD PRESSSDR Z5FA020810N554CS1Actuator · defectiveDURING APPROACH, WHEN GEAR WAS EXTENDED, CREW DID NOT GET LT GEAR DOWN INDICATION. CREW ABORTED THE APPROACH AND DID A GO AROUND, WHERE THEY WORKED ABNORMAL/EMERGENCY CHECK LIST. LANDING GEAR WAS BLOWN DOWN, LT MAIN GEAR DOWN INDICATION ILLUMINATED AND ACFT SDR VQMA0208201000001Actuator · failedFLIGHT CREW REPORTED THE STAB MISCOMPARE LIGHT ILLUMINATED IN FLIGHT. MX REMOVED AND REPLACED THE HORIZONTAL STABILIZER ACTUATOR, PERFORMED THE 2 POSITION HORIZONTAL STABILIZER OPS CHECK AND LEAK CHECK WITH SATISFACTORY RESULTS AND APPROVED THE ACFT FOR RETURNSDR DXTA2010020803974Uplock Switch · faultedGEAR RAISED ON TAKEOFF. GREEN LIGHTS WENT OUT BUT RED INTRANSIT REMAINED ON FOLLOWED BY STAB MISCOMPARE. CREW LOWERED GEAR. GEAR LOCKED DOWN . HYD PRESS & STAB MISCOMPARE LIGHTS WENT OUT. FLAPS WERE UP. WE RAISED GEAR AGAIN. ALL GREEN LIGHTS WENT OUT BUT R
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