[fltsim.0] title=Antonov An-32B sim=Antonov An-24RV model= panel= sound= texture=sdc checklists= ui_manufacturer=Antonov ui_type=An-32B ui_variation=Sadelca atc_id=HK-4427X visual_damage=1 description=This is the Sadelca (Sociedad aérea del Caquetá) Antonov AN-32, Sadelca is a Colombian Cargo Airline that operates cargo in the south of the country with An-32's/Model by Samdim Design (AN-24RV) and texture by Jorge Andrés Calderón C. // --- do not modify afer this line --- [General] performance=48 Passenger\nTwin Turboprop\nRegional Commuter\n\nDevelopment version atc_type=Antonov atc_model=AN24 [GeneralEngineData] engine_type=5 Engine.0=11.780, -12.400, -0.500 Engine.1=11.780, 12.400, -0.500 fuel_flow_scalar=0.944 min_throttle_limit=-0.01 [Propeller] thrust_scalar=1.08 propeller_type=0 propeller_diameter=12.795 propeller_blades=4 propeller_moi=350 beta_max=49.99 beta_min=8.0 //19.0 for LSL min_gov_rpm=13900.00 prop_tc=0.009 gear_reduction_ratio=12.1285 fixed_pitch_beta=15 low_speed_theory_limit=180.000 prop_sync_available=1 prop_deice_available=1 prop_feathering_available=1 prop_auto_feathering_available=0 min_rpm_for_feather=500.000 beta_feather=93.320 power_absorbed_cf=1.000 defeathering_accumulators_available=0 prop_reverse_available=0 //1 minimum_on_ground_beta=0.0 minimum_reverse_beta=0.0 //19.0 for LSL rotation=-1 -1 [Turboprop_engine] power_scalar=1.0 maximum_torque=10614.3602 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 [TurbineEngineData] fuel_flow_scalar=1.0000 fuel_flow_gain=0.0030 inlet_area=1.000 rated_N2_rpm= 15100 static_thrust=625 afterburner_available=0 [flight_tuning] cruise_lift_scalar=1.30 pitch_stability=1.0 roll_stability=1.000 yaw_stability=1.000 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=1.0 aileron_effectiveness=1.00 rudder_effectiveness=1.50 elevator_trim_effectiveness=0.7 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [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 [Weight_and_balance] MTW=46305 //21000 kg MLW=46305 //21000 kg empty_weight=30430.000 //13800 kg empty_weight_cg_position=0.470, 0.000, 0.00 reference_datum_position=0.000, 0.000, 0.000 empty_weight_roll_MOI=149345.2 empty_weight_pitch_MOI=223887.1 empty_weight_yaw_MOI=295687.8 empty_weight_coupled_MOI=1800.000 max_gross_weight=46305.000 //21000kg CG_forward_limit=1.000 CG_aft_limit=1.000 max_number_of_stations=50 station_load.0=5000.000,0.47000,0.000000,0.000000 [electrical] max_battery_voltage=27 generator_alternator_voltate=28.5 max_generator_alternator_amps=600.0 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, 15, 17.0 additional_system=0, 2 , 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 starter2=0, 20, 17.0 light_nav=0, 5 , 10.0 light_beacon=0, 5 , 10.0 light_landing=0, 5 , 17.0 light_taxi=0, 5 , 17.0 light_strobe=0, 5 , 10.0 light_panel=0, 5 , 10.0 [fuel] LeftMain=0.470, -17.400, -1.860, 485.760, 0.000 //1476kg LeftAux=0.470, -10.000, -1.860, 187.440, 0.000 //568kg RightMain=0.470, 17.400, -1.860, 485.760, 0.000 //1476kg RightAux=0.470, 10.000, -1.860, 187.440, 0.000 //568kg fuel_type=2.000000 number_of_tank_selectors=2 electric_pump=0 [airplane_geometry] wing_area=806.27 wing_span=95.8 wing_root_chord=10.4992 wing_dihedral=0.000 wing_incidence=1.3 wing_twist=0.00 oswald_efficiency_factor=0.700 wing_winglets_flag=0 wing_sweep=0.0 wing_pos_apex_lon=-1.860 wing_pos_apex_vert=-0.920 htail_area=185.37 htail_span=29.8 htail_pos_lon=-41.535 htail_pos_vert=0.000 htail_incidence=0.000 htail_sweep=22.000 vtail_area=142.9 vtail_span=16.920 vtail_sweep=24.000 vtail_pos_lon=-40.480 vtail_pos_vert=16.740 elevator_area=55.51 aileron_area=32.92 rudder_area=53.79 elevator_up_limit=10.0 elevator_down_limit=10.00 aileron_up_limit=12.002 aileron_down_limit=12.002 rudder_limit=30.000 elevator_trim_limit=36.000 spoiler_limit=1.000 spoilerons_available=1 aileron_to_spoileron_gain=0.000 min_ailerons_for_spoilerons=0.000 min_flaps_for_spoilerons=0.000 //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] static_pitch=0.000 static_cg_height=7.80 gear_system_type=0 point.0=1.000, 19.200, 0.00, -7.35, 800.0, 0, 1.147, 45.0, 0.260, 2.500, 0.999, 4.000, 4.000, 0.000, 0.000, 0.000 point.1=1.000, -6.5620, -12.400, -7.54, 1400.0, 1.0, 1.475, 0.000, 0.311, 1.500, 0.890, 3.500, 4.500, 2.000, 0.000, 0.000 point.2=1.000, -6.5620, 12.400, -7.54, 1400.0, 2.0, 1.475, 0.000, 0.311, 1.500, 0.850, 3.700, 4.700, 3.000, 0.000, 0.000 //point.0=1.000, 21.390, 0.00, -7.00, 600, 0, 0.618, 58.000, 0.115, 2.500, 0.990, 4.000, 4.000, 0.000, 162.000, 166.000 //point.1=1.000, -0.800, -12.400, -7.80, 800.0, 1.000, 0.618, 0.315, 0.799, 0.850, 0.831, 3.500, 5.000, 2.000, 162.000, 166.000 //point.2=1.000, -0.800, 12.400, -7.80, 800.0, 2.000, 0.618, 0.315, 0.799, 0.850, 0.831, 3.500, 5.000, 3.000, 162.000, 166.000 point.3 =2.00, 24.33, -0.00, -4.90, 9000, 0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 4, 0, 0 point.4 =2.00, -5.96, 0.00, -5.24, 6000, 0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 4, 0, 0 point.5 =2.00,-44.75, 0.00, -1.00, 6000, 0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 9, 0, 0 point.6 =2.00, -8.92, -47.50, 3.42, 3000, 0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 5, 0, 0 point.7 =2.00, -8.92, 47.50, 3.43, 3000, 0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 6, 0, 0 point.8 =2.00, -4.92, -47.50, 3.42, 3000, 0, 0.0, 0.0, 0.00, 0.0, 0.00 , 0.00, 0.00, 5, 0, 0 point.9 =2.00, -4.92, 47.50, 3.42, 3000, 0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 6, 0, 0 point.10=2.00, -1.00, -12.50, -1.30, 6000, 0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 5, 0, 0 point.11=2.00, -1.00, 12.50, -1.30, 6000, 0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 6, 0, 0 point.12=2.00,-41.75, 0.00, 20.00, 3000, 0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 8, 0, 0 point.13=2.00,-36.50, 0.00, 9.00, 3000, 0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 8, 0, 0 point.14=2.00, 0.75, 0.00, 5.50, 3000, 0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 7, 0, 0 point.15=2.00, 20.50, 0.00, 3.75, 3000, 0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 8, 0, 0 point.16= 5, -30.9, -5.25, -7.30,1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 8.0, 8.2, 0, 0.0, 0.0 [Flaps.0] type=1 span-outboard=0.600 extending-time=16.000 system_type=1 damaging-speed=162.000 blowout-speed=170.000 lift_scalar=2.0 drag_scalar=0.1 pitch_scalar=1.000 flaps-position.0=0.000, 0 flaps-position.1=5.000, 162.0 flaps-position.2=10.000, 0.0 flaps-position.3=15.000, 0 flaps-position.4=20.000, 135.0 flaps-position.5=25.000, 0 flaps-position.6=30.000, 0 flaps-position.7=38.000, 0 [TailHook] tailhook_length=4 tailhook_position = -15.0, 0.0, -1.0 cable_force_adjust = 1.0 [folding_wings] wing_fold_system_type=4 fold_rates=0.075,0.075 [exits] number_of_exits = 2 exit_rate.0 = 0.09 exit_rate.1 = 0.2 [Reference Speeds] flaps_up_stall_speed=102.000 full_flaps_stall_speed=82.800 cruise_speed=215.000 max_indicated_speed=292.000000 max_mach=0.650000 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 1 Adf.1=1 Transponder.1=1 Marker.1=1 [autopilot] autopilot_available=0 flight_director_available=0 default_vertical_speed=1000.000000 autothrottle_available=0 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 use_no_default_bank=0 //For no wing leveler when AP On use_no_default_pitch=0 //For no pitch holding when AP On autoland_available=0 [Lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -5.96,-47.67, 3.24, fx_navredm , light.1 = 3, -5.96, 47.67, 3.24, fx_navgrem , light.2 = 2, -37.53, 0.00, 9.21, fx_beaconb , light.3 = 2, -8.50, 0.00, -4.21, fx_beaconh, light.4 = 3, -49.50, 0.00, 4.00, fx_navwhi , light.5 = 4, 18.13, 0.00, 2.3, fx_vclight , light.6 = 5, -2.00, 26.42, 3.7, fx_landing , light.7 = 5, -2.00, -26.42, 3.7, fx_landing , [brakes] toe_brakes_scale=0.518815 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.099976 flap_limit_power=30.022988 flap_limit_idle=55.011494 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 [pitot_static] vertical_speed_time_constant=10 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=18.0, -1.76, 2.04 [direction_indicators] direction_indicator.0=3,0 [Effects] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1