[FLTSIM.0] title=Mhkhoyfs_Iran140_EP_SAF sim=Iran 140 model= panel= sound= texture=SAF prop_anim_ratio=-1.6 ui_manufacturer=HESA(Antonov) ui_type=Iran 140 ui_variation=Safiran atc_id=EP-SAF atc_airline=Safiran atc_flight_number=SF1254 visual_damage=1 description=The HESA IrAn-140 or Iran-140 is a short-range twin-turboprop airliner based on the Antonov An-140 and built under license by HESA of Iran. Repainted by Mohamad Heidari Khoei *The Model download from:Avsimrus.com But some iranian Website say :This ACFT is conclusion of their Work.* atc_parking_types=GATE [General] atc_type=ANTONOV atc_model=140 editable=0 performance= \\===================================================================== [WEIGHT_AND_BALANCE] max_gross_weight=47300 // (pounds) empty_weight=39446 // (pounds) reference_datum_position=31.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=-26.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=170, -9.8, -1.75, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=170, -9.8, 1.75, 0.0 //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2=5660, -27.0, 0.0, 0.0 //Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=230701 empty_weight_roll_MOI=71201 empty_weight_yaw_MOI=271691 empty_weight_coupled_MOI=0 ====================================================== [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=0.95 aileron_effectiveness=1.0 rudder_effectiveness=0.85 pitch_stability=1.0 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 ============================================================================= ============================================================================= [GeneralEngineData] engine_type=5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=-28.4, -13.3, 2.7 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=-28.4, 13.3, 2.7 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.0 //Scalar for fuel flow efficiency min_throttle_limit=-0.349915 [propeller] thrust_scalar=1.0 //Propeller thrust scalar propeller_type=0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=13.0 //Propeller Diameter, (feet) propeller_blades=6 //Number of propeller blades propeller_moi=77 //Propeller moment of inertia beta_max=45 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min=12 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm=32520 //Miminum governed RPM prop_tc=0.004 //Prop time-constant gear_reduction_ratio=17.0 //Propeller gear reduction ratio fixed_pitch_beta=0 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available=1 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available=1 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available=1 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather=700 //Minimum RPM for prop feathering beta_feather=79.3 //Feathering pitch angle (degrees) power_absorbed_cf=0.9 //Coefficient of friction for power absorbed by propeller defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available=1 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta=1.0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta=-14.0 //Minimum pitch angle in reverse, (degrees) [TurbineEngineData] fuel_flow_gain=0.011 //Gain on fuel flow inlet_area=1.0 //Square Feet, engine nacelle inlet area rated_N2_rpm=32920 //RPM, second stage compressor rated value static_thrust=200 //Lbs, max rated static thrust at Sea Level [turboprop_engine] power_scalar=1.0 //Scalar on Turboprop power maximum_torque=7878 //Maximum torque available (ft-lbs) ======================================================================================= ======================================================================================= [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor=0, 5 , 17.0 gear_motor=0, 5 , 17.0 autopilot=0, 5 , 17.0 avionics_bus=0, 10, 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 20, 17.0 marker_beacon=1, 2 , 17.0 gear_warning=0, 2 , 17.0 fuel_pump=0, 5 , 17.0 starter1=0, 20, 17.0 light_nav=0, 5 , 17.0 light_beacon=0, 5 , 17.0 light_landing=0, 5 , 17.0 light_taxi=0, 5 , 17.0 light_strobe=0, 5 , 17.0 light_panel=0, 5 , 17.0 //0 Class <0=none,1=wheel, 2=scrape, 3=float> //1 Longitudinal Position (feet) //2 Lateral Position (feet) //3 Vertical Position (feet) //4 Impact Damage Threshold (Feet Per Minute) //5 Brake Map (0=None, 1=Left, 2=Right) //6 Wheel Radius (feet) //7 Steer Angle (degrees) //8 Static Compression (feet) (0 if rigid) //9 Max/Static Compression Ratio //10 Damping Ratio (0=Undamped, 1=Critically Damped) //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) ============================================================================= ==================================================================================== [contact_points] point.0=1, -5.0, 0.00, -7.45, 1500, 0, 1.617, 25.0, 0.500, 2.5, 0.9, 5.0, 6.0, 0, 100, 250 point.1=1, -29.0, -12.99, -7.55, 3000, 1, 0.633, 0.0, 0.675, 2.5, 0.8, 6.0, 7.0, 2, 100, 250 point.2=1, -29.0, 12.99, -7.55, 3000, 2, 0.633, 0.0, 0.675, 2.5, 0.8, 6.0, 7.0, 3, 100, 250 point.3=2, -31.6, -42.50, 5.39, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 5 point.4=2, -31.6, 42.50, 5.39, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 6 point.5=2, -68.6, 0.00, 1.22, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 9 point.6=2, 0.0, 0.00, -3.92, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 4 max_number_of_points=21 static_pitch=-0.4 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=7.1 //feet, altitude of CG when at rest on the ground ========================================================================================= =============================================================================== gear_system_type=0 [Views] eyepoint=-8.8, -1.45, 2.1 //(feet) longitudinal, lateral, vertical distance from reference datum [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.8 // 0.0 .. 1.0 extending-time=5 // seconds flaps-position.0=0 // degrees, KIAS flaps-position.1=10 // degrees, KIAS flaps-position.2=20 // degrees, KIAS flaps-position.3=35 // degrees, KIAS damaging-speed=250 // KIAS blowout-speed=300 // KIAS ========================================================================= [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [SMOKESYSTEM] smoke.0=-3.400,-44.00,-16.48, fx_smoke_rx smoke.1=-3.400,-44.00,16.48, fx_smoke_rx =========================================================================== [fuel] LeftMain=-31.1, -9.1, 3.9, 717.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=-31.1, 9.1, 3.9, 717.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 =========================================================================== electric_pump=0 [Reference Speeds] flaps_up_stall_speed=92.0 //Knots True (KTAS) full_flaps_stall_speed=72.0 //Knots True (KTAS) cruise_speed=265.0 //Knots True (KTAS) max_indicated_speed=265.000000 max_mach=0.579980 [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator=150.0, 250.0 aileron=150.0, 250.0 rudder=150.0, 250.0 ============================================================= [autopilot] autopilot_available=1 flight_director_available=1 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=105.000000 pitch_takeoff_ga=8.000000 ============================================================= max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 default_vertical_speed=1000.000000 [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=27000 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -30.6, -38.5, 6.3, fx_navred , light.1=3, -30.6, 38.5, 6.3, fx_navgre , light.2=2, -30.6, 38.5, 6.3, fx_strobe , light.3=2, -30.6, -38.5, 6.3, fx_strobe , light.4=1, -51.0, 0.00, -4.1, fx_beacon , \\\1.4 light.5=4, -7.91, 0.00, 3.64, fx_vclight, light.6=4, -8.91, 0.00, 3.64, fx_vclight, light.7=4, -50.9, 0.00, 1.64, fx_vclight, light.8=4, -52.9, 0.00, 1.64, fx_vclight, \\light.9=4, -20.9, 0.00, 1.34, fx_vclight, [direction_indicators] direction_indicator.0=3,0 ===================================================================== [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second ===================================================================== [airplane_geometry] wing_area=585.000000 wing_span=85.000000 wing_root_chord=7.000000 wing_dihedral=2.499390 wing_incidence=0.999756 wing_twist=-2.999268 oswald_efficiency_factor=0.850061 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=-29.250000 wing_pos_apex_vert=0.000000 htail_area=97.000000 htail_span=26.000000 htail_pos_lon=-66.000000 htail_pos_vert=0.000000 htail_incidence=0.999756 htail_sweep=0.000000 vtail_area=106.000000 vtail_span=11.738824 vtail_sweep=0.000000 vtail_pos_lon=-57.000000 vtail_pos_vert=3.416667 elevator_area=53.500000 aileron_area=12.100000 rudder_area=46.400000 elevator_up_limit=16.999658 elevator_down_limit=15.498508 aileron_up_limit=18.002334 aileron_down_limit=18.002334 rudder_limit=30.000070 elevator_trim_limit=15.000035 spoiler_limit=59.988681 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [brakes] toe_brakes_scale=1.062532 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=30.022988 flap_limit_idle=15.011494 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
