[fltsim.0]
title=BERIEV Be-12
sim=Be12
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=CF030
atc_id_color=0x00000000
atc_flight_number=CF030
prop_anim_ratio=-1.4
ui_manufacturer=BERIEV
ui_type=Be-12
ui_variation=NAVY
description="BE-12 Russian NAVY
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0

[weight_and_balance]
max_gross_weight = 79366.4
empty_weight = 52910.9
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -1.79, 0, 0
empty_weight_pitch_MOI = 995000
empty_weight_roll_MOI = 745000
empty_weight_yaw_MOI = 755000
empty_weight_coupled_MOI = 0
max_number_of_stations = 7

station_load.0 = "220.462,  22.0, -2.5,  0.0, Pilot"
station_load.1 = "220.462,  22.0,  2.5,  0.0, Co-Pilot"
station_load.2 = "220.462,  30.0,  0.0, -2.0, Navigator"
station_load.3 = "220.462, -11.5,  0.0,  2.5, Radist"
station_load.4 = "330.7,    0.0,   0.0,  4.0, Oil"
station_load.5 = "176.4,    0.0,   0.0,  0.0, Oxygen"
station_load.6 = "3306.93, -6.0,   0.0, -4.0, Combat charging"


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3,  2.9, -44.3,   5.2, fx_navredm ,
light.1 = 3,  2.9,  44.3,   5.2, fx_navgrem ,
light.2 = 5, 3.1, -28.2, 4.2, fx_landing
light.3 = 5, 3.1,  28.2, 4.2, fx_landing
light.5 = 7, -17,  -13,     2.0, zh_An12smok
light.6 = 7, -17,   13,     2.0, zh_An12smok
light.7 = 5,  3.1, -28.2,   4.2, fx_shockwave_landing_light,
light.8 = 5,  3.1,  28.2,   4.2, fx_shockwave_landing_light,

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 0.75
min_throttle_limit = -0.15
engine.0 = 14, -11.75, 8,
engine.1 = 14, 11.75, 8,

[effects]


[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -8.5, 6, 850, 0
LeftAux = 0, -24, 6, 380, 0
LeftTip = 0, -37, 6, 250, 0
RightMain = 0, 8.5, 6, 850, 0
RightAux = 0, 24, 6, 380, 0
RightTip = 0, 37, 6, 250, 0


[contact_points]
static_pitch=6.1
static_cg_height=10.536378
gear_system_type=0

//gear
point.0=1.000000,-42.666667,0.000000,-4.43,1574.803150,0.000000,0.942371,60.720000,0.339400,2.500000,0.715902,10.000000,10.000000,0.000000,0.000000,0.000000
point.1=1.000000,4.916667,-7.416667,-10.1,1574.803150,1.000000,0.942371,0.000000,0.452534,2.500000,0.715910,10.000000,10.000000,2.000000,0.000000,0.000000
point.2=1.000000,4.916667,7.416667,-10.1,1574.803150,2.000000,0.942371,0.000000,0.452534,2.500000,0.715910,10.000000,10.000000,3.000000,0.000000,0.000000
//float
point.3 = 4, 15.4378, 0, -5.1, 2500, 0, 0, 40, 0.25, 2.5, 0.9, 0, 0, 0, 0, 0
point.4 = 4, -2.6, 4, -4.4, 2500, 0, 0, 0, 0.5, 2.5, 0.9, 0, 0, 0, 0, 0
point.5 = 4, -2.6, -4, -4.4, 2500, 0, 0, 0, 0.5, 2.5, 0.9, 0, 0, 0, 0, 0
//scrape
point.6 = 2, -2.0, -39.10, -2, 2500, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.7 = 2, -2.0, 39.10, -2, 2500, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.8 = 2, -20.80, 0, -1.40, 2500, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.9 = 2, 0, -52, 8.65, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.10 = 2, 0, 52, 8.65, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.11 = 2, -43.30, 0.0, 4.60, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.12 = 2, 21.20, 0.0, 0.60, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.13 = 5, -31.049, 0, -2.7, 2500, 0, 0, 30, 0, 0, 0.7, 1, 1.2, 0, 0, 0


[keyboard_response]
elevator = 150.0, 250.0
aileron = 150.0, 250.0
rudder = 150.0, 250.0


[airplane_geometry]
wing_area = 1170
wing_span = 91.0
wing_root_chord = 13.0
wing_dihedral = -0.99
wing_incidence = 0.247192
wing_twist = 0.999756
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 5
wing_pos_apex_lon = 7
wing_pos_apex_vert = 6.79
htail_area = 300
htail_span = 33
htail_pos_lon = -35
htail_pos_vert = 5.5
htail_incidence = 0.0
htail_sweep = 3
vtail_area = 290
vtail_span = 12
vtail_sweep = 3
vtail_pos_lon = -35
vtail_pos_vert = 3
elevator_area = 65.75
aileron_area = 75.0
rudder_area = 65.0
elevator_up_limit = 35.5
elevator_down_limit = 30.0
aileron_up_limit = 20.0
aileron_down_limit = 15.0
rudder_limit = 35.0
elevator_trim_limit = 25.5
spoiler_limit = 59.9
aileron_to_spoileron_gain = 0.0
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.0
min_flaps_for_spoilerons = 0.0
spoilerons_available = 0

[electrical]
max_battery_voltage = 28
generator_alternator_voltage = 28
max_generator_alternator_amps = 40
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 1, 5, 17
avionics_bus = 0, 12, 17
avionics = 1, 2, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 5, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
starter2 = 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
hydraulic_pump = 0, 3, 17

[Flaps.0]
type=1
span-outboard=0.6
extending-time=15.0
system_type=0
damaging-speed=162.0
blowout-speed=170.0
lift_scalar=1.2								
drag_scalar=1.4							
pitch_scalar=1.2
flaps-position.0=0.0, 0
flaps-position.1=10.0, 0
flaps-position.2=25.0, 0
flaps-position.3=38.0, 0

[TurbineEngineData]
fuel_flow_gain=0.03 
inlet_area=1.0 
rated_N2_rpm=12300 
static_thrust=500.0 
afterburner_available=0 
reverser_available=0 

[turboprop_engine]
power_scalar=1.0 
maximum_torque=25300 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=15   
propeller_blades=4 
propeller_moi=300.0 
beta_max=49.0 
beta_min=3 
min_gov_rpm=10350 
prop_tc=0.1 
gear_reduction_ratio=9.87 
fixed_pitch_beta=0 
low_speed_theory_limit=55.0 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=0 
min_rpm_for_feather=500. 
beta_feather=91 
power_absorbed_cf=0.95 
defeathering_accumulators_available=0 
prop_reverse_available=0 
minimum_on_ground_beta=0.0 
minimum_reverse_beta=-0.0002 
rotation=-1, -1
feathering_switches = 1 

[Reference Speeds]
flaps_up_stall_speed=156.0 
full_flaps_stall_speed=135.0 
cruise_speed=189.0 
max_indicated_speed=243.0
max_mach=0.6

[flight_tuning]
cruise_lift_scalar=1.2 
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0 
elevator_effectiveness=0.7 
aileron_effectiveness=1.5 
rudder_effectiveness=0.6 
pitch_stability=1.0 
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=0.5 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 
hi_alpha_on_roll=0 
hi_alpha_on_yaw=0 
p_factor_on_yaw=0  
torque_on_roll=0


[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=1800.0 
autothrottle_available=1 
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90.0
pitch_takeoff_ga=8.0 
autoland_available=1
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.0
max_throttle_rate=0.1
nav_proportional_control=9.0
nav_integrator_control=0.25
nav_derivative_control=0.0
nav_integrator_boundary=2.5
nav_derivative_boundary=0.0
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.0
gs_integrator_boundary=0.7
gs_derivative_boundary=0.0
yaw_damper_gain=0.0

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1 
Com.1=1, 0 
Com.2=1, 0 
Nav.1=1, 0, 1 
Nav.2=1, 0, 0 
Adf.1=1 
Adf.2=1
Transponder.1=1 
Marker.1=1 

[direction_indicators]
direction_indicator.0=3,0 

[exits]
number_of_exits = 2
exit_rate.0 = 0.053                             ;Percent per second
exit_rate.1 = 0.2                               ;Percent per second

[TailHook]
tailhook_length=4                               ;(feet)
tailhook_position = -15.0, 0.0, -1.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust = 1.0
[folding_wings]
wing_fold_system_type=4                       ;0=None
fold_rates=0.075,0.075	
                          ;Percent per second
[Views]
eyepoint=18.13, -1.36, 2.04    //(feet) longitudinal, lateral, vertical distance from reference datum
 

[brakes]
toe_brakes_scale=0.5
parking_brake=1
differential_braking_scale = 5.0

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.1
flap_limit_power=25.5
flap_limit_idle=5.0

[hydraulic_system]
normal_pressure=3000.0
engine_map=1,1,0,0

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[airspeed_indicators]
airspeed_indicator.0 = 1.183, -24.750