[fltsim.0]
title=O46
sim=O46
model=
panel=
sound=
texture=
prop_anim_ratio=-1.76
kb_checklists=
kb_reference=
atc_id=NC5524N
atc_id_color=0x00000000
ui_manufacturer=Douglas
ui_type=O-46
ui_variation=USAAC
description= The Douglas O-46 was the last of a long line of Douglas Observation planes made for the USAAC. It entered service in 1937.
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
atc_heavy=0
[General]
atc_type=Douglas
atc_model=Doug O-46
editable=0
performance=
Category=airplane
[weight_and_balance]
// ACM V2.5
max_gross_weight = 6100
empty_weight = 4725
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 4007
empty_weight_roll_MOI = 3028
empty_weight_yaw_MOI = 5677
empty_weight_coupled_MOI = 0
max_number_of_stations = 1
station_load.0 = 170, -6.40, 0, 0
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -1.200, 21.002, 4.4.132, fx_navgre //bot rd
light.1 = 3, -1.200, 21.002, 4.590, fx_navgre //top rd
light.2 = 3, -1.200, -21.002, 4.132, fx_navred //bot grn
light.3 = 3, -1.200, -21.002, 4.590, fx_navred //top grn
light.4 = 3, -21.143, -0.222, 5.011, fx_navwhi
light.5 = 3, -21.143, 0.222, 5.011, fx_navwhi
light.6 = 4, -6.0, 0.0, 2.97 , fx_vclight.fx
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 1.0
min_throttle_limit = 0.0
engine.0 = 7.02, 0, 0,
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_dustrun
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
startup = fx_engstrt
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, -4.2, 2.7, 41, 0
RightMain = 0, 4.2, 2.7, 41, 0
[contact_points]
static_pitch = 14.5
static_cg_height = 6.8
tailwheel_lock = 0
gear_system_type = 0
max_number_of_points = 7
point.0 = 1, -22.9938, 0, -1.2124, 1200, 0, 0.5, 22, 0.3, 1.5, 0.595, 0, 0, 0, 0, 0
point.1 = 1, 0.3097, -4.3192, -7.1, 1600, 1, 1.45, 0, 0.4, 1.25, 0.756, 0, 0, 2, 0, 0
point.2 = 1, 0.3097, 4.3192, -7.1, 1600, 2, 1.45, 0, 0.4, 1.25, 0.752, 0, 0, 3, 0, 0
point.3 = 2, -0.5156, -22.6038, 3.0729, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -0.526, 22.6982, 3.0781, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -31.044, 0, 0.5, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 7.1111, 0, -2.9535, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
[keyboard_response]
elevator = 200, 1000
aileron = 200, 1000
rudder = 200, 1000
[forcefeedback]
ground_bumps_magnitude1 = 2600
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.6
ground_bumps_magnitude2 = 1200
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.085
ground_bumps_slope2 = 0.65
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 3500000
[airplane_geometry]
wing_area = 332.0
wing_span = 45.45
wing_root_chord = 6.19
wing_dihedral = 2
wing_incidence = 2.0
wing_twist = 0.0
oswald_efficiency_factor = 0.6
wing_winglets_flag = 0
wing_sweep = 4
wing_pos_apex_lon = 1.70
wing_pos_apex_vert = 3.60
htail_area = 51.0
htail_span = 14.11
htail_pos_lon = -18.04
htail_pos_vert = 2.54
htail_incidence = 0
htail_sweep = 22
vtail_area = 18.0
vtail_span = 6.35
vtail_sweep = 45
vtail_pos_lon = -15.71
vtail_pos_vert = 1.74
elevator_area = 16.3
aileron_area = 25.6
rudder_area = 7.8
elevator_up_limit = 30.0
elevator_down_limit = 30.0
aileron_up_limit = 25.0
aileron_down_limit = 25.0
rudder_limit = 30.0
elevator_trim_limit = 20.0
spoiler_limit = 1.0
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=4.000000
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 = 25
max_generator_alternator_amps = 60
engine_generator_map = 1
electric_always_available = 0
fuel_pump = 0, 0.60, 17
starter1 = 0, 35, 17
light_nav = 0, 2, 17
light_panel = 0, 0.30, 17
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=0.8
induced_drag_scalar=0.8
elevator_effectiveness=1.3
aileron_effectiveness=1.0
rudder_effectiveness=2.0
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
p_factor_on_yaw = 0.5
torque_on_roll = 1.8
gyro_precession_on_yaw = 0.4
gyro_precession_on_pitch = 0.0
[piston_engine]
power_scalar=1.0 //Piston power scalar
cylinder_displacement=109 //Cubic inches per cylinder
compression_ratio=6.5 //Compression ratio
number_of_cylinders=14 //Number of cylinders
max_rated_rpm=2200 //Max rated RPM
max_rated_hp=750 //Max rated HP
fuel_metering_type=1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type=0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=0.20 //Starter torque factor
turbocharged=1 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=34 //Max design manifold pressure, (inHg)
min_design_mp=10 //Min design manifold pressure, (inHg)
critical_altitude=9000 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type=0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset=0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset=0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture=0 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition=0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar=1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar=1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar=1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar=0.5 //Scalar on idle RPM friction
[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=3 //Number of propeller blades
propeller_moi=8.77 //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)
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.7 //Brake scalar
differential_braking_scale = 2.5 //Delta on the amount of brake when the rudder pedals deflected
[hydraulic_system]
normal_pressure = 0.0 //PSI
[Views]
eyepoint=-6.0, 0.0, 2.97
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Nav.1=0, 0, 0
Adf.1=1
Transponder.1=0
Marker.1=0
[flaps.1] //Trailing Edge Flaps
type =1 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.19
extending-time = 2.0 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 35 // degrees
damaging-speed = 140 // KIAS
blowout-speed = 175 // KIAS
lift_scalar = 0.5
drag_scalar = 1.5
pitch_scalar= 1.0
system_type = 0 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None
[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=1,0
direction_indicator.1=2,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=2,0
[Reference Speeds]
flaps_up_stall_speed=53.0 //Knots True (KTAS)
full_flaps_stall_speed=45.5 //Knots True (KTAS)
cruise_speed=105.0 //Knots True (KTAS)
max_indicated_speed = 200 //Red line (KIAS)
[autopilot]
autopilot_available=1
flight_director_available=0
pitch_takeoff_ga=0.0
default_vertical_speed=700.000000
autothrottle_available=0
direction_indicator=1
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 = 0.0
default_bank_mode=2 //Default to Heading Hold
[stall_warning]
type=1
stick_shaker=0
[exits]
number_of_exits = 2
exit_rate.0 = 0.6 ;Percent per second
exit_rate.1 = 0.8 ;Percent per second
[pitot_static]
pitot_heat=1.000000
[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
