[fltsim.0]
title=Biman DC8-55
sim=paidc855v5
model=
panel=
sound=
texture=Biman
atc_id_enable=1
atc_id_color=0xffffffff
atc_id=S2-WP
atc_airline=Bangladeshi
atc_flight_number=BG001
atc_manufacturer=McDonnell Douglas
atc_heavy=1
ui_manufacturer=McDonnell Douglas
ui_type=DC8-55
ui_variation=Bangladesh Airlines Classic Colors
visual_damage=0
description=1972 A year Which Everyone Looked Up At The Sky After the First Flight Of The DC3 A Leased Aircract From The Bangladesh Airforce. Bangladesh Airlines Quickly Added Several Aircraft From Boeing,McDonnell Douglas, BAe Aerospace.

[General]
atc_type=MCDONNELL DOUGLAS
atc_model=DC85
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]
//Position Order: Z, X, Y
//Types: 1=beacon, 2=strobe, 3=navigation, 5=landing                   
light.0=3, -32.0,  -72.7,  5.0, fx_navredh ,
light.1=3, -32.0,  72.7,  5.0, fx_navgreh ,
light.2=3, -33.0, -72.7,  5.0, fx_strobeh ,
light.3=3, -33.0,  72.7,  5.0, fx_strobeh ,
light.4=3, -84.97,  0.00,   6.3, fx_navwhih ,
light.5=5, 12.98,  -6.2,   -1.75, fx_landing ,
light.6=5, 12.98,  6.2,   -1.75, fx_landing ,
light.7=1,  -16.66,    0.00,  8.8, fx_beacon ,
light.8=1,  -16.66,    0.00,  -5.3, fx_beaconb ,

[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=126000.000

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, -24.000, -4.500
Engine.1=6.000, 24.000, -4.500
fuel_flow_scalar=1.000
Engine.2=2.000, -45.000, -2.000
Engine.3=2.000, 45.000, -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, -11.000, 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
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;
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

[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