[fltsim.0]
title=MBB BO105 Helicoptere-Avis
sim=BO105
model=
panel=
sound=
texture=

kb_checklists=BO105_check
kb_reference=

prop_anim_ratio=1.41

ui_manufacturer=MBB
ui_type=BO105
ui_variation=CBS

atc_heavy=0
atc_id=FG-VTM
atc_airline=Helicoptere-Avis
atc_flight_number=
description=Messerschmitt-Boelkov-Blom BO105CBS


[General]
performance=Rotor Dia: 32 ft 3.5in.\nLength: 28ft 1in.\nMaximum Gross Weight: 5,070lbs      \nEmpty weight: 2,469lbs\nMaximum Speed: 167 mph\nMaximum Cruise: 133 kts\/246 kmh\nMax Range: 408 nm             \n\n
atc_type=MM BO105
atc_model=CB4


[WEIGHT_AND_BALANCE]
max_gross_weight=5512                         // (pounds)
empty_weight=2513                             // (pounds)

reference_datum_position     =  0.0000, 0.0000, 0.0000       // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0.0, 0.0,0.0  // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50

station_load.0="190,  6.0, 1.17, 0.0, Pilot"               //     Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1="190,  6.0,  -1.17, 0.0, Co-Pilot"                  //     Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2="0,  0.0,  0.00, -0.2, PassengerArea"                //     Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3="0,  0.0,  0.00, 0.0, RearCargo"                //     Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4="0,  0.0,  25.00, 4.0, Hoist"                //     Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5="0,  0.0,  0.00, -2.0, ExtCargo-Hook"                //     Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI=8000
empty_weight_roll_MOI=5000
empty_weight_yaw_MOI=10000
empty_weight_coupled_MOI=0

[Helicopter]
low_realism_stability_scale=.3, .3, .7             //Pitch , Bank, Yaw Scalars on Stability in Low Realism Settings

[electrical]
max_battery_voltage=24
generator_alternator_voltage=26
max_generator_alternator_amps=150
electric_always_available=0
engine_generator_map = 0,1,1

;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot=0, 5 , 17.0
avionics_bus=0, 25 , 17.0
avionics=0, 5 , 17.0
pitot_heat=0, 5 , 17.0
additional_system=0, 2 , 17.0
marker_beacon=1, 2 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
starter1=0, 20, 17.0
starter2=0, 20, 17.0
starter3=0, 20, 17.0
standby_vacuum=1, 15, 17
hydraulic_pump=0, 2,  17
fuel_transfer_pump=0, 5,  17
light_recognition=0, 15,  17
light_nav=0, 15 , 17.0
light_beacon=0, 15 , 17.0
light_landing=0, 15 , 17.0
light_taxi=0, 15 , 17.0
light_strobe=0, 15 , 17.0
light_panel=0, 15 , 17.0
directional_gyro=1, 2 , 17.0
directional_gyro_slaving=1, 2 , 17.0



//0  Class                        <0=none,1=wheel, 2=scrape, 3=skid>
//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
//14 Airspeed limit for retraction     (KIAS)
//15 Airspeed that gear gets damage at (KIAS)

[contact_points]
point.0=3,   4.83,   3.33, -3.90, 1574.8, 0, 0.5187, 0.0, 0.286975, 2.5, 0.605067, 0.0, 0.0, 7.0, 0.0, 0.0
point.1=3,  -3.50,  -3.33, -3.98, 1574.8, 0, 0.5187, 0.0, 0.396299, 2.5, 0.728164, 0.0, 0.0, 7.0, 0.0, 0.0
point.2=3,  -3.50,   3.33, -3.98, 1574.8, 0, 0.5187, 0.0, 0.396299, 2.5, 0.728164, 0.0, 0.0, 7.0, 0.0, 0.0
point.3=3,   4.83,  -3.33, -3.90, 1574.8, 0, 0.5187, 0.0, 0.286975, 2.5, 0.605067, 0.0, 0.0, 7.0, 0.0, 0.0
point.4=2,   0.00, -16.67,  9.00,    0.0, 0, 0.0000, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 5.0, 0.0, 0.0
point.5=2,   0.00,  16.67,  9.00,    0.0, 0, 0.0000, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 6.0, 0.0, 0.0
point.6=2, -20.50,   0.00,  1.67,  787.4, 0, 0.0000, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 9.0, 0.0, 0.0
point.7=2,   0.00,   9.08,  2.58,  787.4, 0, 0.0000, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 4.0, 0.0, 0.0

static_pitch=0.0
//static_cg_height=4.194
static_cg_height=4.854

[brakes]
parking_brake=0       //Parking brake available
toe_brakes_scale=0.0  //Brake scalar

[hydraulic_system]
normal_pressure=95.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map=1,1,1,0

[Views]
eyepoint=4.646,1.248,2.278

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

[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to  1/2 and 1/8 respectively.
//NOTE: These map to cyclic (fore/aft), cyclic (left/right), and anti-torque
elevator=100,  180
aileron=200, 1000
rudder=200, 1000

[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=3,0

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0=1 

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, -15.188, -3.598, 2.796,  fx_navred ,
light.1 = 3, -15.188,  3.598, 2.796,  fx_navgre ,
light.2 = 3, -19.890,  0.000, 5.752,  fx_navwhi ,
light.3 = 1, -19.546,  0.000, 6.593,  fx_beacon ,
light.4 = 1,   4.500,  0.000,-2.543,  fx_beacon ,
light.5 = 2,  -3.217, -2.566, 0.520,  fx_strobe ,
light.6 = 2,  -3.217,  2.566, 0.520,  fx_strobe ,
light.7 = 4,   5.000,  0.00,  0.877,  fx_vclightgk ,

[SMOKESYSTEM]
//?,long,lat from ref datum
//smoke.0=-12.00, -6.00, 6.0, fx_smoke_w

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks

[exits]
number_of_exits=2
exit_rate.0=0.4
exit_rate.1=0.4

[fuel]
//Tanks Position and capacity: 
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = 0.00, 0.00, -2.00, 25.000, 4.80
RightMain = 0.000, 0.000, 0.000, 129.000, 0.000

//Fuel type: 1 = Avgas, 2 = JetA
fuel_type=2
number_of_tank_selectors = 2                    
electric_pump=1

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 0.7
engine.0 = -6.870, 0.000, 0.000
engine.1 = -6.870, 0.000, 0.000
engine.2 = -6.870, 0.000, 0.000
min_throttle_limit=0.00000

[TurbineEngineData]
fuel_flow_gain          =0.02
inlet_area              =0.000000
rated_N2_rpm            =33000
static_thrust=150.00                    

[turboprop_engine]
power_scalar            = 1.0                   //Scalar on Turboprop power
maximum_torque          = 3270                  //Maximum torque available (ft-lbs)

[Reference Speeds]
flaps_up_stall_speed=0.0                   //Knots True (KTAS)
full_flaps_stall_speed=0.0                   //Knots True (KTAS)
cruise_speed=135.0                 //Knots True (KTAS)
max_indicated_speed=140                   //Red line (KIAS)

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=0.001
autothrottle_available=1
pitch_takeoff_ga=0.000000
autothrottle_arming_required=1
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
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

[yaw_string]
yaw_string_available=1

[TailHook]
tailhook_length=4                               ;(feet)
tailhook_position=9.3.0, 0.0, 1.3            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1.0
tailhook_rate=2.0
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000

[folding_wings]
wing_fold_system_type=4
fold_rates=1.00, 1.00

[propeller]
thrust_scalar           = 1.0                   //Propeller thrust scalar
propeller_type          = 0                     //0=Constant Speed, 1=Fixed Pitch
propeller_diameter      = 8.8                   //Propeller Diameter, (feet)
propeller_blades        = 4                     //Number of propeller blades
propeller_moi           = 24                    //Propeller moment of inertia
beta_max                = 45                    //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min                = 15.2                  //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm             = 25520                 //Miminum governed RPM
prop_tc                 = 0.004                 //Prop time-constant
gear_reduction_ratio    = 17.6                  //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    = 1                     //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     = 700                   //Minimum RPM for prop feathering
beta_feather            = 79.3                  //Feathering pitch angle (degrees)
power_absorbed_cf       = 0.9                   //Coefficient of friction for power absorbed by propeller
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  = 0.0                   //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta    = -14.0                 //Minimum pitch angle in reverse, (degrees)
engine_map=0,1,2
