JASC 2710

Service difficulty reports · 2,967

Reports filed under 2710 · Aileron Control System, newest first.

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 jasc_code = '2710'
  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.

SDR 2010FA0001005Frame · crackedTHE PN 6760141-5 FRAME IS PART OF THE AILERON POWER CONTROL UNIT SUPPORT ASSY AND IS APPLICABLE TO ACFT 750-0001 TO 750-0149 THAT HAVE NOT BEEN MODIFIED BY SB750-27-44. DURING SCHEDULED INSP, THE FRAME WAS FOUND TO BE FATIGUE CRACKED. THE PART WAS REPLACED. Sep 8, 2010 · N948QS · Cessna 750SDR MASA2010090800968Control Panel · defectiveEXCESSIVE ROLL 45 DEGREES UNCOMMANDED [AFTER] T/O. MX REMOVED AND REPLACED AIL/RUD TRIM CTL PNL.Sep 7, 2010 · N905J · Cndair CL6002D24SDR A6WA201040671Strip · dirtyAS SOON AS FLAPS ARE SELECTED TO 45 DEG, ACFT BECOMES UNSTABLE AROUND A LONGITUDINAL AXIS. ACFT SNAPS TO THE LT AND RT WITHOUT AILERON INPUT, AND WHEN APPLYING AILERON , CORRECTION AILERONS DOS100-0080-01 EFFECTIVE UNTIL SIGNIFICANT. CLEANED AND PAINTED INBDSep 3, 2010 · N419AW · Cndair CL6002B19SDR SWAA105157Bearing · faultyAILERONS BINDING AT 30 DEGREE LEFT CONTROL WHEEL ON GROUND CYCLED TO FULL LEFT AILERON SEVERAL TIMES. FELT THE BIND AND A POP ON RETURN TO CENTER. REMOVED AND REPLACED CAM FOLLOWER BEARING ON AILERON FEEL AND CENTERING MECHANISM PER MM.Sep 1, 2010 · N551WN · Boeing 73776QSDR REXA20100124Warning System · activatedKMLI - FIRST OFF, HAD THE AILERON TRIMMED LEFT WING DOWN FROM PREVIOUS FLIGHT AS FAR AS THE GREEN WOULD ALLOW TO GET THE TAKEOFF CONFIG OK MSG. TOOK THE RUNWAY (27) FOR DEPARTURE. WINDS WERE 190/18 GUSTING TO 21KTS. DIRECT CROSSWIND. AS CREW SET TAKEOFF Aug 31, 2010 · N841AY · Cndair CL6002B19SDR CA100826011Balance Weight · cracked(CAN) DURING THE COURSE OF A COMPASS SWING ON A/C, THE RT WING TIP WAS REMOVED TO ADJUST THE FLUX VALVE. AT THIS TIME IT WAS NOTICED THAT THE RT AILERON OUTBOARD BALANCE HORN WEIGHT WAS CRACKED THROUGH THE ATTACHMENT HOLES APPROXIMATELY 90 PERCENT OF THE WAY Aug 26, 2010 · Bag JETSTM3112SDR 2010FA0000992Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N549ER · Cessna 172SSDR 2010FA0000990Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N549ER · Cessna 172SSDR 2010FA0000989Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N549ER · Cessna 172SSDR 201001095Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH AAug 23, 2010 · N549ER · Cessna 172SSDR 2010FA0000988Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N540ER · Cessna 172SSDR 2010FA0000987Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N540ER · Cessna 172SSDR 2010FA0000986Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N540ER · Cessna 172SSDR 201001094Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N540ER · Cessna 172SSDR 2010FA0000985Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N552ER · Cessna 172SSDR 2010FA0000984Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH AAug 23, 2010 · N552ER · Cessna 172SSDR 2010FA0000983Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N552ER · Cessna 172SSDR 201001089Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N552ER · Cessna 172SSDR 2010FA0000982Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH AAug 23, 2010 · N546ER · Cessna 172SSDR 2010FA0000981Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH AAug 23, 2010 · N546ER · Cessna 172SSDR 2010FA0000980Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N546ER · Cessna 172SSDR 201001079Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH AAug 23, 2010 · N546ER · Cessna 172SSDR 2010FA0000979Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH AAug 23, 2010 · N556ER · Cessna 172SSDR 2010FA0000978Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH AAug 23, 2010 · N556ER · Cessna 172SSDR 2010FA0000977Control Cable · frayedCABIN OVERHEAD CTR PANEL REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WAS ABLE TO CATCH FRAYED WIRES WITH A RAG & COULDAug 23, 2010 · N556ER · Cessna 172SSDR 201001043Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N556ER · Cessna 172SSDR 2010FA0000976Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N557ER · Cessna 172SSDR 2010FA0000975Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N557ER · Cessna 172SSDR 2010FA0000974Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N557ER · Cessna 172SSDR 201001006Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH AAug 23, 2010 · N557ER · Cessna 172SSDR 2010FA0000973Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH AAug 23, 2010 · N551ER · Cessna 172SSDR 2010FA0000972Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH AAug 23, 2010 · N551ER · Cessna 172SSDR 2010FA0000971Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH AAug 23, 2010 · N551ER · Cessna 172SSDR 201000738Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH AAug 23, 2010 · N551ER · Cessna 172SSDR 2010FA0000969Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N548ER · Cessna 172SSDR 2010FA0000968Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N548ER · Cessna 172SSDR 201000930Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH AAug 23, 2010 · N548ER · Cessna 172SSDR 2010FA0000967Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH AAug 23, 2010 · N541ER · Cessna 172SSDR 2010FA0000966Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH AAug 23, 2010 · N541ER · Cessna 172SSDR 2010FA0000965Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH AAug 23, 2010 · N541ER · Cessna 172SSDR BF8R201000987Control Cable · frayedCABIN OVERHEAD CENTER PANEL REMOVED FOR INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, ABLE TO CATCH FRAYED WIRES WITH A RAG AND COULD SEE A SUBSAug 23, 2010 · N541ER · Cessna 172SSDR 2010FA0000939Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED OR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSP, FLAT SPOTS WERE NOTICED ON 3 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH A RAG ANAug 23, 2010 · N554ER · Cessna 172SSDR 2010FA0000938Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED OR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSP, FLAT SPOTS WERE NOTICED ON 3 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH A RAG ANAug 23, 2010 · N554ER · Cessna 172SSDR 201000338Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED OR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSP, FLAT SPOTS WERE NOTICED ON 3 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH A RAG ANAug 23, 2010 · N554ER · Cessna 172SSDR DXTA2010081804199Actuator · inoperativeROLL SYSTEM CONTROL FAULT AMBER CAS ILLUMINATED IN FLIGHT. ACCESSED THE ROLL RATIO CHANGER ACTUATOR. NOTED GOOD CONNECTIVITY. ACTUATOR & AREA CLEAN. CONNECTED PITOT/STATIC. PERFORMED THE RAIO CHANGER POSITION CHECK. AT 300 KNOTS DIMENSION OF MALMENT IS IAug 17, 2010 · N376QS · Cessna 680CESDR A6WA201040610Trim Panel · faultyON CLIMBOUT AT 4000`, RUDDER TRIM (NOSE LT) AND AILERON (LWD) RUNAWAY. R & R TRIM PANEL ASSY IAW AMM 27-12-01.Aug 13, 2010 · N461AW · Cndair CL6002B19SDR SIMA201022802Fitting · wornDURING MAINTENANCE BASE VISIT INSPECTION FOUND THE LEFT POWER CONTROL ACTUATOR ATTACH FITTING OUTBOARD BUSHING TO BE MIGRATING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AILERON POWER CONTROL ACTUATOR FITTING IAW EO EM-27MR-112. TAug 12, 2010 · N636AE · Emb EMB145LRSDR HALA2010080900358Actuator · inoperativeETOPS SIGNIFICANT SYS - EICAS AILERON LOCKOUT CAME ON AT 300KTS. C/W R & R LT AILERON LOCKOUT ACTUATOR IAW TASK 27-11-44-022-004. OPS CHECK GOOD.Aug 9, 2010 · N596HA · Boeing 767332SDR CA100908001Seal · wornWHILE CRUISING AT FL380, AUTOPILOT HEADING CONTROL BEGAN BEHAVING ABNORMALLY. WHEN THE FLIGHT CREW DISCONNECTED THE AUTOPILOT THEY WERE UNABLE TO MOVE AILERON CONTROLS, ALTHOUGH LIMITED CONTROL WAS AVAILABLE AT THE CO-PILOT STA AND LEVEL FLIGHT WAS MAINTAINEDAug 4, 2010 · Gulstm G100SDR CA100806002Actuator · failedFLIGHT CREW REPORTED THAT AN EXCESSIVE FORCE WAS REQUIRED WHEN TURNING THE AILERON CONTROL WHEEL AFTER THE AUTOPILOT HAD BEEN DISCONNECTED. MX WAS DISPATCHED TO THE ACFT AND FOUND THE AILERON SERVO ACTUATOR AT FAULT. THE AILERON SERVO ACTUATOR IS EQUIPPED WITAug 3, 2010 · Cndair CL6002B19
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