[fltsim.0] title = CV-10T sim = CV-10T model = panel = sound = texture = panel_alias = sound_alias = kb_checklists = CheckList__CV-10T kb_reference = atc_id = atc_id_color = 0xffffffff atc_airline = atc_flight_number = 1 ui_manufacturer = North American ui_type = CV-10T ui_variation = Air America description = Proposed, but unbuilt, cargo version of the OV-10 Bronco FAC aircraft. The OV-10T was proposed to the USAF by North American Rockwell as a small tactical transport and spec ops plane. In the end USAF interest waned, and no prototype was ever built. This "what if" CV-10T represents a production plane in service with Air America in the late '60's. Such a plane would have suited the secretive air service perfectly. [General] atc_type = atc_model = editable = 1 performance = * Weight: 11906 lbs Max 14849 lbs * Power: 1040 hp MIL 1040 hp WEP * 4.5g Corner speed: 209 mph * Max speed @ SL: 234 mph * Max speed: 281 mph @ 25000 ft * Climb rate: 3475 ft/min @ 109 mph Flight Model By: Tim Piglet Conrad Piglet's Peculiar Planes 11/4/03 04:11 AM Flight Model Workbook V2.83.56 [pitot_static] vertical_speed_time_constant = 2 [WEIGHT_AND_BALANCE] max_gross_weight = 14849 empty_weight = 7066 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0.7, 0, 0 CG_forward_limit = 0 CG_aft_limit = 1 max_number_of_stations = 6 station_load.0 = 170, 9, -1.3, -0.21 station_load.1 = 170, 9, 1.3, -0.21 station_load.2 = 4500, 0, 0, -1.66 station_load.3 = 0, 0, 0, 0 empty_weight_pitch_MOI = 28471 empty_weight_roll_MOI = 14959 empty_weight_yaw_MOI = 39194 empty_weight_coupled_MOI = 0 [flight_tuning] cruise_lift_scalar = 1 parasite_drag_scalar = 1 induced_drag_scalar = 1 elevator_effectiveness = 1 aileron_effectiveness = 1 rudder_effectiveness = 1 pitch_stability = 1 roll_stability = 1 yaw_stability = 1 elevator_trim_effectiveness = 1 aileron_trim_effectiveness = 1 rudder_trim_effectiveness = 1 [GeneralEngineData] engine_type = 5 Engine.0 = 2.68, -7.4, 0 Engine.1 = 2.68, 7.4, 0 fuel_flow_scalar = 1 [propeller] thrust_scalar = 1 propeller_type = 0 propeller_diameter = 8.8 propeller_blades = 3 propeller_moi = 18.6 beta_max = 65 beta_min = 0 min_gov_rpm = 7500 prop_tc = 0.01 gear_reduction_ratio = 4.5 fixed_pitch_beta = 30 low_speed_theory_limit = 80 prop_sync_available = 1 prop_deice_available = 1 prop_feathering_available = 1 prop_auto_feathering_available = 1 min_rpm_for_feather = 700 beta_feather = 88.5 power_absorbed_cf = 0.9 defeathering_accumulators_available = 0 prop_reverse_available = 1 minimum_on_ground_beta = 1 minimum_reverse_beta = -14 rotation = 1, -1 [TurbineEngineData] fuel_flow_gain = 0.011 inlet_area = 4.43393437777121E-02 rated_N2_rpm = 10000 static_thrust = 150 afterburner_available = 0 reverser_available = 0 [turboprop_engine] power_scalar = 1 maximum_torque = 2458.64175291736 [contact_points] max_number_of_points = 8 point.0 = 1, 15.265, 0, -6.482, 3181, 0, 0.9, 30, 0.35, 2.5, 0.952, 5.8, 6.8, 0, 0, 0 point.1 = 1, -1.492, -7.817, -6.515, 3574, 1, 1.1, 0, 0.5, 2.5, 0.915, 5.5, 7.5, 2, 0, 0 point.2 = 1, -1.492, 7.817, -6.515, 3574, 2, 1.1, 0, 0.5, 2.5, 0.915, 6.3, 8.3, 3, 0, 0 point.3 = 2, 0, -25.107, 1.225, 787, 0, 0, 0, 0, 0, 0, 0, 0, 5 point.4 = 2, 0, 25.107, 1.225, 787, 0, 0, 0, 0, 0, 0, 0, 0, 6 point.5 = 2, -7.599, 0, -4.317, 787, 0, 0, 0, 0, 0, 0, 0, 0, 9 point.6 = 2, 17.564, 0, -3.5, 787, 0, 0, 0, 0, 0, 0, 0, 0, 4 point.7 = , , , , , , , , , , , , , static_pitch= 0 static_cg_height= 6.6 [Views] eyepoint= 9.306, -1.267, 1.069 [flaps.0] //Trailing Edge Flaps type = 1 span-outboard = 0.5 extending-time = 7 flaps-position.0 = 0 flaps-position.1 = 15, 208 flaps-position.2 = 25, 199 flaps-position.3 = 35, 190 flaps-position.4 = 45, 181 damaging-speed = 208 blowout-speed = 226 system_type = 1 lift_scalar = 0 drag_scalar = 0 pitch_scalar = 1 [flaps.1] //Leading Edge Flaps - Lift type = 2 span-outboard = 0.5 extending-time = 7 flaps-position.0 = 0 flaps-position.1 = 15 flaps-position.2 = 30 flaps-position.3 = 45 flaps-position.4 = 30 damaging-speed = 208 blowout-speed = 226 system_type = 1 lift_scalar = 1 drag_scalar = 0 pitch_scalar = 0 [flaps.2] //Leading Edge Flaps - Drag type = 2 span-outboard = 0.5 extending-time = 7 flaps-position.0 = 0 flaps-position.1 = 4 flaps-position.2 = 5 flaps-position.3 = 6 flaps-position.4 = 45 damaging-speed = 208 blowout-speed = 226 system_type = 1 lift_scalar = 0 drag_scalar = 1 pitch_scalar = 0 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 160 electric_always_available = 0 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 10, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 20, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 17 starter2 = 0, 20, 17 starter3 = 0, 20, 17 starter4 = 0, 20, 17 light_nav = 0, 5, 17 light_beacon = 0, 5, 17 light_landing = 0, 5, 17 light_taxi = 0, 5, 17 light_strobe = 0, 5, 17 light_panel = 0, 5, 17 prop_sync = 0, 15, 17 auto_feather = 0, 15, 17 auto_brakes = 0, 15, 17 standby_vacuum = 0, 15, 17 hydraulic_pump = 0, 2, 17 fuel_transfer_pump = 0, 5, 17 propeller_deice = 0, 5, 17 light_recognition = 0, 5, 17 light_wing = 0, 5, 17 light_logo = 0, 5, 17 [LIGHTS] light.0 = 3, 1.41, -25.225, 1.582, fx_navred light.1 = 3, 1.41, 25.225, 1.582, fx_navgre light.2 = 3, -19.249, -7.396, 8.837, fx_navwhi light.3 = 1, -19.249, 7.396, 8.837, fx_beacon light.4 = 1, 6.414, 0, -4.584, fx_beacon light.5 = 4, 9.306, 0, -.588, fx_vclight_yellow light.6 = 4, 3.012, 0, 1.339, fx_vclight_yellow light.7 = 4, -3.015, 0, 1.339, fx_vclight_yellow [keyboard_response] elevator = 350, 500 aileron = 450, 1000 rudder = 200, 1000 [direction_indicators] direction_indicator.0 = 1, 0 [exits] number_of_exits = 2 exit_rate.0 = 0.8 exit_rate.1 = 0.4 [EFFECTS] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn, 1 [autopilot] autopilot_available = 1 flight_director_available = 0 default_vertical_speed = 1000 autothrottle_available = 0 autothrottle_arming_required = 0 autothrottle_max_rpm = 90 autothrottle_takeoff_ga = 1 pitch_takeoff_ga = 8 [fuel] LeftMain = 0, -5.1, 0, 125, 0 RightMain = 0, 5.1, 0, 125, 0 fuel_type = 2 number_of_tank_selectors = 1 [airplane_geometry] wing_area = 340 wing_span = 50.5 wing_root_chord = 6.73267326732673 wing_dihedral = 1 wing_incidence = 0 wing_twist = 0 oswald_efficiency_factor = 0.86669478284625 wing_winglets_flag = 0 wing_sweep = 0 wing_pos_apex_lon = 2.38316831683168 wing_pos_apex_vert = 0 htail_area = 45.73 htail_span = 13.1 htail_pos_lon = -20.76 htail_pos_vert = 0 htail_incidence = 0 htail_sweep = 0 vtail_area = 43.4 vtail_span = 6.2 vtail_sweep = 0 vtail_pos_lon = -16.75 vtail_pos_vert = 0 elevator_area = 21 aileron_area = 21 rudder_area = 22.24 elevator_up_limit = 30 elevator_down_limit = 20 aileron_up_limit = 18 aileron_down_limit = 18 rudder_limit = 30 elevator_trim_limit = 18 spoiler_limit = 90 spoilerons_available = 1 aileron_to_spoileron_gain = 4 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 [Reference Speeds] flaps_up_stall_speed = 86 full_flaps_stall_speed = 72.1 cruise_speed = 169 [forcefeedback] gear_bump_nose_magnitude = 6000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 6000 gear_bump_left_direction = 35500 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 6000 gear_bump_right_direction = 500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 3250 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5 ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 750 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.075 ground_bumps_slope2 = 1 crash_magnitude1 = 10000 crash_direction1 = 1000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000
