[fltsim.0]
title=Biman 707-300
sim=biman707
model=
panel=
sound=
texture=Biman
atc_id_enable=1
atc_id_color=0xffffffff
atc_id=S2-ACK
atc_airline=Bangladeshi
atc_flight_number=BG002
atc_manufacturer=Boeing
atc_heavy=1
ui_manufacturer=Boeing
ui_type=B707-300
ui_variation=Biman Classic 707-321C
visual_damage=0
description=Biman Bangladesh Airlines began in January 1972 along with the nation it represented. Using an leased Bangladesh Air Force DC3 Biman quickly moved onto Fokker F27s and then two Boeing 707s.

[General]
atc_type=BOEING
atc_model=B703
editable=1
performance=


[pitot_static]
vertical_speed_time_constant=1

[flight_tuning]
cruise_lift_scalar=2.100
parasite_drag_scalar=2.100
induced_drag_scalar=2.100
elevator_effectiveness=0.700
aileron_effectiveness=1.000
rudder_effectiveness=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[TurbineEngineData]
fuel_flow_gain=0.002
inlet_area=30.000
rated_N2_rpm=29920.000
static_thrust=19000.000
afterburner_available=0
reverser_available=1

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -44.50, -72.90, 6.65, fx_navredm ,
light.1=3, -44.50, 72.90, 6.65, fx_navgrem ,
light.2=1, -26.65, 0.00, -6.70, fx_beaconb ,
light.3=1, -7.20, 0.00, 9.50, fx_beaconh ,
light.4=4, 47.75, 0.00, 3.50, fx_vclight ,
light.5=2, -44.50, -73.90, 6.65, fx_strobeh ,
light.6=2, -44.50, 73.90, 6.65, fx_strobeh ,

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[WEIGHT_AND_BALANCE]
max_gross_weight=333600.000
empty_weight=165000.000

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=48000.000, -10.000, 0.000, 0.000

;Moments of Inertia
empty_weight_pitch_MOI=4765824.000
empty_weight_roll_MOI=2287420.000
empty_weight_yaw_MOI=5516924.000
empty_weight_coupled_MOI=0.000
CG_forward_limit=0.000
CG_aft_limit=1.000

[GeneralEngineData]
engine_type=1
Engine.0=6.000, -19.000, -4.500
Engine.1=6.000, 19.000, -4.500
fuel_flow_scalar=1.000
Engine.2=2.000, -32.000, -2.000
Engine.3=2.000, 32.000, -2.000
min_throttle_limit=-0.250000

[jet_engine]
thrust_scalar=1.000

[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 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
light_nav=0, 5 , 17.0
light_beacon=0, 5 , 17.0
light_landing=0, 5 , 17.0
light_taxi=0, 5 , 17.0
light_strobe=0, 5 , 17.0
light_panel=0, 5 , 17.0

//0  Class                        <0=none,1=wheel, 2=scrape, 3=float>
//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=1.000, 37.935, 0.000, -12.100, 1574.803, 0.000, 2.000, 56.340, 0.750, 2.100, 0.900, 7.000, 7.000, 0.000, 0.000, 0.000
point.1=1.000, -17.500, -13.750, -12.412, 1574.803, 1.000, 2.000, 0.000, 1.300, 2.700, 0.920, 8.000, 8.000, 2.000, 0.000, 0.000
point.2=1.000, -17.500, 13.750, -12.412, 1574.803, 2.000, 2.000, 0.000, 1.300, 2.700, 0.920, 8.000, 8.000, 3.000, 0.000, 0.000
point.3=2.000, -25.000, -72.850, 4.000, 1574.803, 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, -25.000, 72.850, 4.000, 1574.803, 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, -82.000, 0.000, 4.000, 1574.803, 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, 70.000, 0.000, 3.000, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch=0.100
static_cg_height=12.400
max_number_of_points=21
gear_system_type=0

[Views]
eyepoint=43.7, -1.31, 3.55   //(feet) longitudinal, lateral, vertical distance from reference datum

[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.
elevator=150, 250

aileron=150, 250
rudder=150, 250

[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

[autopilot]
autopilot_available             = 1
flight_director_available       = 1
default_vertical_speed          = 1800.0
autothrottle_available          = 1
autothrottle_arming_required    = 1
autothrottle_max_rpm            = 90
autothrottle_takeoff_ga         = 1
pitch_takeoff_ga                = 8;
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=3.00
max_throttle_rate=0.10
nav_proportional_control=16.00
nav_integrator_control=0.17
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control  = 18.0 
gs_integrator_control    = 0.33
gs_derivative_control    = 0.00
gs_integrator_boundary   = 0.70
gs_derivative_boundary   = 0.00
yaw_damper_gain = 1.0

[fuel]
Center1=0.000, 0.000, 0.000, 9100.000, 0.000
LeftMain=-8.000, -20.000, 0.000, 7400.000, 0.000
RightMain=-8.000, 20.000, 0.000, 7400.000, 0.000
fuel_type=2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=0

[airplane_geometry]
wing_area=3050.000
wing_span=145.750
wing_root_chord=22.000
wing_dihedral=6.500
wing_incidence=-0.500
wing_twist=-0.500
oswald_efficiency_factor=0.700
wing_winglets_flag=0
wing_sweep=31.500
wing_pos_apex_lon=18.000
wing_pos_apex_vert=0.000
htail_area=730.000
htail_span=55.000
htail_pos_lon=-73.000
htail_pos_vert=0.000
htail_incidence=0.000
htail_sweep=40.000
vtail_area=320.000
vtail_span=28.000
vtail_sweep=38.000
vtail_pos_lon=-65.000
vtail_pos_vert=5.800
elevator_area=105.000
aileron_area=50.000
rudder_area=80.000
elevator_up_limit=24.000
elevator_down_limit=19.000
aileron_up_limit=24.000
aileron_down_limit=24.000
rudder_limit=35.000
elevator_trim_limit=18.000
spoiler_limit=40.000
spoilerons_available=1
aileron_to_spoileron_gain=3.000
min_ailerons_for_spoilerons=10.000
min_flaps_for_spoilerons=0.000

[Reference Speeds]
flaps_up_stall_speed=155.000
full_flaps_stall_speed=125.000
cruise_speed=280
max_indicated_speed=430.000000
max_mach=0.900000

[forcefeedback]
gear_bump_nose_magnitude=3000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=2700           ; 0 - 10000
gear_bump_left_direction=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=00500         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=1300            ; 0 - 10000
ground_bumps_angle1=08900               ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200             ; 0 - 10000
ground_bumps_angle2=09100               ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000                  ; 0 - 10000
crash_direction1=01000                  ; 0 - 35999 degrees
crash_magnitude2=10000                  ; 0 - 10000
crash_direction2=9000                   ; 0 - 35999 degrees
crash_period2=75000                     ; in microseconds
crash_duration2=2500000                 ; in microseconds

[Flaps.0]
type=1
span-outboard=0.700
extending-time=15.000
system_type=1
damaging-speed=250.000
blowout-speed=280.000
lift_scalar=0.850
drag_scalar=1.400
pitch_scalar=1.300
flaps-position.0=0.000, 0.000
flaps-position.1=1.000, 0.000
flaps-position.2=5.000, 0.000
flaps-position.3=10.000, 0.000
flaps-position.4=20.000, 0.000
flaps-position.5=30.000, 0.000

[brakes]
toe_brakes_scale=0.427259
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,1
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0