[fltsim.0]
title=B-25D Mitchell #0
sim=B25D_Mitchell
model=
panel=
sound=
texture=
description=Test B25D
ui_manufacturer=
ui_type=B-25
ui_variation=
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=
[WEIGHT_AND_BALANCE]
empty_weight = 19480.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.000, 0.000, 0.000
max_number_of_stations = 50
station_load.0 = 170.000, 12.000, -4.000, 2.000
station_load.0 = 170, 12.0, 4.0, 2.0 //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 61203.470
empty_weight_roll_MOI = 43209.890
empty_weight_yaw_MOI = 83573.240
empty_weight_coupled_MOI= 0.000
max_gross_weight= 26970.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
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
[piston_engine]
power_scalar = 1.0
cylinder_displacement= 185.930
compression_ratio= 6.850
number_of_cylinders= 14
max_rated_rpm= 2600.000
max_rated_hp= 1700.000
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque= 0.035
turbocharged= 1
max_design_mp= 44.300
min_design_mp= 1.000
critical_altitude= 17000.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 0
auto_ignition= 0
fuel_flow_scalar= 1.000
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
[propeller]
thrust_scalar = 1.0
propeller_type= 0
propeller_diameter= 12.583
propeller_blades= 3
propeller_moi= 52.300
beta_max= 49.000
beta_min= 18.000
min_gov_rpm= 1400.000
prop_tc= 0.010
gear_reduction_ratio= 1.780
fixed_pitch_beta= 0.000
low_speed_theory_limit= 80.000
prop_sync_available= 0
prop_deice_available= 0
prop_feathering_available= 0
prop_auto_feathering_available= 0
min_rpm_for_feather= 0.000
beta_feather= 0.000
power_absorbed_cf= 0.000
defeathering_accumulators_available= 0
prop_reverse_available= 0
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000
[exits]
number_of_exits = 1
exit_rate.0 = 0.4 ;Percent per second
[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0
[contact_points]
//0 Class
//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
point.0= 1.000, 15.840, 0.000, -7.900, 1400.000, 0.000, 1.500, 45.000, 1.060, 2.500, 0.700, 6.000, 7.000, 0.000, 0.000, 0.000
point.1= 1.000, -1.820, -9.230, -8.000, 2000.000, 1.000, 2.500, 0.000, 1.060, 2.500, 0.860, 7.500, 8.500, 2.000, 0.000, 0.000
point.2= 1.000, -1.820, 9.230, -8.000, 2000.000, 2.000, 2.500, 0.000, 1.060, 2.500, 0.860, 7.000, 8.000, 3.000, 0.000, 0.000
point.3= 2.000, 0.000, -55.830, 1.000, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, 0.000, 55.830, 1.000, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -39.580, 0.000, -2.830, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 17.160, 0.000, -4.830, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_cg_height = 6.880
static_pitch = 1.280
gear_system_type=0
[Views]
eyepoint= -4.56, 0.00, 3.22 //(feet) longitudinal, lateral, vertical distance from reference datum
[General]
performance=B25D AI model
atc_type=
atc_model=
[fuel]
Center1= -2.310, 0.000, 1.200, 215.000, 0.000
LeftMain= -2.310, -4.950, 0.820, 335.000, 0.000
RightMain= -2.310, 4.950, 0.820, 335.000, 0.000
External1= -2.310, 0.000, -1.200, 335.000, 0.000
fuel_type= 1.000
number_of_tank_selectors= 1
electric_pump=0
[airplane_geometry]
wing_area= 610.000
wing_span= 67.583
wing_root_chord= 9.667
wing_dihedral= 0.000
wing_incidence= 1.000
wing_twist= 0.000
oswald_efficiency_factor= 0.750
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 0.000
htail_area= 331.000
htail_span= 43.000
htail_pos_lon= -38.750
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 0.000
vtail_area= 220.000
vtail_span= 16.912
vtail_sweep= 0.000
vtail_pos_lon= -38.750
vtail_pos_vert= 7.167
elevator_area= 94.410
aileron_area= 80.250
rudder_area= 39.490
elevator_up_limit= 28.000
elevator_down_limit= 22.999
aileron_up_limit= 26.001
aileron_down_limit= 18.999
rudder_limit= 28.000
elevator_trim_limit= 19.996
spoiler_limit= 0.000
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000
[GeneralEngineData]
engine_type= 0
Engine.0= 8.167, -9.250, 0.000
Engine.1= 8.167, 9.250, 0.000
fuel_flow_scalar= 1.000
min_throttle_limit=0.000000
[Reference Speeds]
flaps_up_stall_speed= 110.000
full_flaps_stall_speed= 88.000
cruise_speed= 258.857
max_indicated_speed=760.500000
[keyboard_response]
elevator= 350.000, 500.000
aileron= 450.000, 1000.000
rudder= 200.000, 1000.000
[autopilot]
autopilot_available= 1
flight_director_available= 0
default_vertical_speed= 700.000
autothrottle_available= 0
pitch_takeoff_ga= 8.000
autoland_available= 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=0.000000
[brakes]
toe_brakes_scale=1.000000
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=6.930556
[stall_warning]
type=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[direction_indicators]
direction_indicator.0=1,0
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 15.000, 0.000
flaps-position.2= 30.000, 0.000
flaps-position.3= 45.000, 0.000
