[fltsim.0] title=North American OV-10A Bronco sim=ov10a model= panel= sound= texture= kb_checklists=ov10a_chk description=DIMENSIONS: \t\nWingspan:40 feet (12.2 meters)\nLength:41 feet, 7 inches (12.7 meters)\nHeight:15 feet, 1 inch (4.6 meters) \nWEIGHT:\t\nEmpty: 7,190 pounds (3,261 kilograms)\nMaximum take-off gross weight: 14,444 pounds (6,552 kilograms) \n\n ui_manufacturer=North American ui_type=OV-10A Bronco ui_variation=USAF visual_damage=1 atc_id=USAF14650 [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] empty_weight=6950 // (pounds) reference_datum_position=0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=0.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=200, 5.0, 0.0, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=200, 8.0, 0.0, 0.0 //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2=0, 0.0,0.0, 0.0, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3=0, 0.0,0.0, 0.0, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4=0, 0.0,0.0, 0.0, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5=0, 0.0,0.0, 0.0, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6=0, 0.0,0.0, 0.0, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) empty_weight_roll_MOI=10378.000000 empty_weight_pitch_MOI=9208.000000 empty_weight_yaw_MOI=19803.000000 empty_weight_coupled_MOI=0.000000 [electrical] max_battery_voltage=28.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=40.0 avionics_bus=0, 0, 1 avionics=1, 0, 1 starter1=0, 0, 1 starter2=0, 0, 1 fuel_transfer_pump=0, 0, 1 flap_motor=0, 0, 1 gear_motor=0, 0, 1 autopilot=0, 0, 1 pitot_heat=0, 0, 1 additional_system=0, 0, 1 marker_beacon=1, 0, 1 gear_warning=0, 0, 1 fuel_pump=0, 0, 1 light_nav=0, 0, 1 light_beacon=0, 1, 1 light_landing=0, 0, 1 light_taxi=0, 0, 1 light_strobe=0, 1, 1 light_panel=0, 0, 1 auto_brake=0, 0, 1 standby_vacuum=0, 0, 1 hydraulic_pump=0, 0, 1 light_recognition=0, 0, 1 light_wing=0, 0, 1 light_logo=0, 0, 1 [turboprop_engine] power_scalar=1.00 maximum_torque=1900.000000 [propeller] thrust_scalar=1.000 propeller_type=0 propeller_diameter=8.500000 propeller_blades=2 propeller_moi=11.000000 beta_max=60.000000 beta_min=10.000000 min_gov_rpm=2000.000000 prop_tc=0.004000 gear_reduction_ratio=20.865000 fixed_pitch_beta=0.000000 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=1 prop_auto_feathering_available=1 min_rpm_for_feather=700.000000 beta_feather=79.800000 power_absorbed_cf=0.900000 defeathering_accumulators_available=0 prop_reverse_available=1 minimum_on_ground_beta=-0.000000 minimum_reverse_beta=-16.300000 [flight_tuning] cruise_lift_scalar=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.00 aileron_effectiveness=2.002 rudder_effectiveness=1.000 [General] performance=Max Cruise Speed\t245 kts\nMaximum Range\t700 nm w\/internal fuel\nService Ceiling\t24,000 ft\nMax Gross Weight\t14,400 lb\nCrew\t\t2\n\nFUEL: Five self-sealing fuel tanks in wing: 252-gallon capacity (954 liters)\n150-, 230-, or 300-gallon (568-, 871-, or 1,136-liter) external tank \n\nRANGE: 700 nautical miles (1,297 kilometers) with internal fuel\n1200 nautical miles (2224 kilometers) with 150-gallon (568-liter) drop tank \n\nMISSION PERFORMANCE: 5.5 hours loiter time with 150-gallon (568-liter) drop tank\n50 [fuel] LeftMain=0.000000,-14.500000,-1.000000,126.000000,0.000000 RightMain=0.000000,14.500000,-1.000000,126.000000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=291.000000 wing_span=40.000000 wing_root_chord=7.250000 wing_dihedral=0.000000 wing_incidence=2.999268 wing_twist=0.000000 oswald_efficiency_factor=1.000013 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=70.000000 htail_span=14.583333 htail_pos_lon=-20.833333 htail_pos_vert=0.000000 htail_incidence=0.999756 htail_sweep=0.000000 vtail_area=32.000000 vtail_span=6.449806 vtail_sweep=0.000000 vtail_pos_lon=-20.833333 vtail_pos_vert=3.000000 elevator_area=18.900000 aileron_area=14.420000 rudder_area=11.160000 elevator_up_limit=34.950426 elevator_down_limit=25.210143 aileron_up_limit=25.000001 aileron_down_limit=25.000001 rudder_limit=25.000001 elevator_trim_limit=18.907607 spoiler_limit=0.000000 spoilerons_available=1 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [contact_points] point.0=1.000000,10.833333,0.000000,-3.500000,1574.803150,0.000000,0.562658,37.800000,0.173493,2.500000,0.850886,7.000000,7.000000,0.000000,0.000000,0.000000 point.1=1.000000,-1.000000,-7.333333,-3.750000,1968.503937,1.000000,0.562658,0.000000,0.206226,2.500000,0.780610,9.000000,9.000000,2.000000,0.000000,0.000000 point.2=1.000000,-1.000000,7.333333,-3.750000,1968.503937,2.000000,0.562658,0.000000,0.206226,2.500000,0.780610,10.000000,10.000000,3.000000,0.000000,0.000000 point.3=2.000000,-0.083333,-19.250000,3.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.000000,-0.083333,19.250000,3.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.000000,-20.250000,0.000000,1.500000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,13.750000,0.000000,-0.916667,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 static_pitch=-2.252197 static_cg_height=3.750926 [Flaps.0] type=1 span-outboard=0.500000 extending-time=5.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=13.333339,0.000000 flaps-position.2=26.666678,0.000000 flaps-position.3=40.000017,0.000000 [GeneralEngineData] engine_type=5 Engine.0=4.000000,-7.166667,2.000000 Engine.1=4.000000,7.166667,2.000000 fuel_flow_scalar=1.000000 [TurbineEngineData] fuel_flow_gain=0.050000 inlet_area=0.625000 rated_N2_rpm=29920.000000 static_thrust=155.000000 afterburner_available=0 [Reference Speeds] flaps_up_stall_speed=70.000000 full_flaps_stall_speed=56.000000 cruise_speed=272.911333 [keyboard_response] elevator=100.000000,180.000000 aileron=200.000000,1000.000000 rudder=200.000000,1000.000000 [Views] eyepoint=7.830442,0.000000,3.062972 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1000.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 [direction_indicators] direction_indicator.0=3,0