[fltsim.0] title=YO51 sim=YO51 model= panel= sound= texture= kb_checklists= prop_anim_ratio=1.76 atc_id_color=0x00000000 atc_heavy=0 atc_id_font=Verdana,0,1,0,0 atc_type=Single atc_model=YO-51 atc_id=STOL visual_damage=0 ui_manufacturer=Ryan ui_type=Dragonfly ui_variation=USAAC description=The YO-51 Ryan Dragonfly was a prewar attempt by the USAAC to produce a STOL aircraft. [General] editable=1 performance=Weight: Empty 3000 lbs Gross 4206 lbs\n Span:52' \n Length:34' 5"\n Speed: restricted cruise, restricted\n Ceiling: restricted \n Power:420 hp Wright Whirlwind\n Designer: P. Clawson\n Date: 12/2008\n Category=airplane [pitot_static] vertical_speed_time_constant=2 pitot_heat=1.000000 [weight_and_balance] // ACM V2.5 max_gross_weight = 4206 empty_weight = 3000 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 5833 empty_weight_roll_MOI = 3944 empty_weight_yaw_MOI = 9306 empty_weight_coupled_MOI = 0 CG_forward_limit = 0 CG_aft_limit = 1 max_number_of_stations = 1 station_load.0 = 170, -2.14, 0, 0.78 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, 0.375, -25.308, 3.374, fx_navred light.1 = 3, 0.375, 25.308, 3.3374, fx_navgre light.2 = 3, -23.889, 0, 6.547, fx_navwhi light.3 = 4, -2.45, 0, 2.2, fx_vclight [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 0 fuel_flow_scalar = 1 min_throttle_limit = 0 engine.0 = 5.34, 0, 0, [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn_s, 1 windshield_rain_effect_available = 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 1 number_of_tank_selectors = 1 electric_pump = 0 LeftMain = 0, -2.5, 0, 85, 0 RightMain = 0, 2.5, 0, 85, 0 [contact_points] static_pitch = 10.5 static_cg_height = 7.3 tailwheel_lock = 0 gear_system_type = 1 max_number_of_points = 7 point.0 = 1, -24.9436, 0, -2.681, 1574.8032, 0, 0.45, 22, 0.2, 2.5, 0.8, 2.2, 2, 0, 132, 150 point.1 = 1, 3.25, -8.1031, -7.7, 1574.8032, 1, 1, 0, 0.8, 1.25, 0.8, 6, 6, 2, 132, 150 point.2 = 1, 3.25, 8.1031, -7.7, 1574.8032, 2, 1, 0, 0.8, 1.25, 0.8, 6.5, 6.5, 3, 132, 150 point.3 = 2, -26.3747, -0.035, -0.8869, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.4 = 2, -0.8319, 25.7765, 3.1802, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5 = 2, -0.9828, -25.9633, 3.0382, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.6 = 2, 7.3387, 0, -5.7836, 1250, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0 [keyboard_response] elevator = 350, 500 aileron = 450, 1000 rudder = 200, 1000 [forcefeedback] [airplane_geometry] wing_area = 363 wing_span = 52.22 wing_root_chord = 6.70 wing_dihedral = 0 wing_incidence = 1.0 wing_twist = 0 oswald_efficiency_factor = 1.0 wing_winglets_flag = 0 wing_sweep = 0 wing_pos_apex_lon = 2.25 wing_pos_apex_vert = 3.76 htail_area = 38 htail_span = 22.20 htail_pos_lon = -19.76 htail_pos_vert = 1.58 htail_incidence = 0 htail_sweep = 14 vtail_area = 23.8 vtail_span = 5.96 vtail_sweep = 25 vtail_pos_lon = -20.35 vtail_pos_vert = 0.95 elevator_area = 21.6 aileron_area = 22.4 rudder_area = 14.9 elevator_up_limit = 22 elevator_down_limit = 22 aileron_up_limit = 22 aileron_down_limit = 22 rudder_limit = 22 elevator_trim_limit = 18 spoiler_limit = 60 aileron_to_spoileron_gain = 0 spoiler_handle_available = 1 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 spoilerons_available = 0 auto_spoiler_available=0 spoiler_extension_time=0.000000 positive_g_limit_flaps_up=4.000000 positive_g_limit_flaps_down=2.000000 negative_g_limit_flaps_up=-1.500000 negative_g_limit_flaps_down=-1.500000 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 60 engine_generator_map = 1 electric_always_available = 1 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 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 hi_alpha_on_roll=1 hi_alpha_on_yaw=1 p_factor_on_yaw=1 torque_on_roll=1 gyro_precession_on_roll=1 gyro_precession_on_yaw=1 [piston_engine] power_scalar=1 cylinder_displacement=215 compression_ratio=6.5 number_of_cylinders=7 max_rated_rpm=2250 max_rated_hp=700 fuel_metering_type=1 cooling_type=1 normalized_starter_torque=0.07 turbocharged=1 max_design_mp=44 min_design_mp=9 critical_altitude=5100 emergency_boost_type=0 emergency_boost_mp_offset=0 emergency_boost_gain_offset=0 fuel_air_auto_mixture=0 auto_ignition=0 emergency_boost_duration=300 max_rpm_mechanical_efficiency_scalar=1 idle_rpm_mechanical_efficiency_scalar=1.0 max_rpm_friction_scalar=1 idle_rpm_friction_scalar=1.0 [propeller] thrust_scalar=1.0 //Propeller thrust scalar propeller_type=0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=10 //Propeller Diameter, (feet) propeller_blades=2 //Number of propeller blades propeller_moi=6.0 //Propeller moment of inertia beta_max=24.0 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min=14.0 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm=1400 //Miminum governed RPM prop_tc=0.1 //Prop time-constant gear_reduction_ratio=1.0 //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=0 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available=0 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available=0 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available=0 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather=0 //Minimum RPM for prop feathering beta_feather=0 //Feathering pitch angle (degrees) power_absorbed_cf=0 //Coefficient of friction for power absorbed by propeller in feather defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available=0 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta=0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta=0 //Minimum pitch angle in reverse, (degrees) [Views] eyepoint=-2.45, 0, 2.2 [Flaps.0] type=1 span-outboard=0.500000 extending-time=4.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=25.000000,0.000000 [direction_indicators] direction_indicator.0=1, 0 [exits] number_of_exits=1 exit_rate.0=0.4 //[autopilot] autopilot_available=0 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 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000 max_pitch_velocity_hi_alt_breakpoint=28000 max_pitch=10 max_pitch_acceleration=1 max_pitch_velocity_lo_alt=2 max_bank=25 max_bank_acceleration=1.8 max_bank_velocity=3 max_throttle_rate=0.1 nav_proportional_control=9 nav_integrator_control=0.25 nav_derivative_control=0 nav_integrator_boundary=2.5 nav_derivative_boundary=0 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0 gs_integrator_boundary=0.7 gs_derivative_boundary=0 yaw_damper_gain=0 [Reference Speeds] flaps_up_stall_speed=59.1 full_flaps_stall_speed=48.7 cruise_speed=200 max_indicated_speed=304 max_mach=0.46 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.1 flap_limit_idle=33.75 flap_limit_power=16.875 [brakes] toe_brakes_scale=1.5 parking_brake=1 [stall_warning] type=1 stick_shaker=0 [hydraulic_system] electric_pumps=0 engine_map=1, 0, 0, 0 normal_pressure=1000 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [vacuum_system] max_pressure=5.000000 vacuum_type=1 electric_backup_pressure=0.000000 engine_map=1,0,0,0 [pneumatic_system] max_pressure=0.000000 bleed_air_scalar=1.000000 [deice_system] structural_deice_type=0 [autopilot] autopilot_available=0 flight_director_available=0
