[fltsim.0]
title=Biman B777-300ER
sim=Boeing 777-300ER General Electric 90-115B1
model=
panel=
sound=
texture=BG
checklists=
atc_airline=Bangladeshi
atc_id=S2-B73
atc_flight_number=BG012
atc_heavy=1
atc_parking_types=GATE
atc_parking_codes=
ui_manufacturer=Boeing
ui_type=777-300ER
ui_variation=Biman B7773ER
visual_damage=1
description=Biman Bangladesh Airlines Boeing 777-300ER, I hope you'll enjoy the repaint as; I have spent great
amount of time to provide you with the most acurate paintalong with realistic
shadow, shine and reflective effectsFeaturing 32bit Highly Detailed graphics
with night light effects,The model includes all the usual things as a steering
nosewheel, taxi and landing lights, dynamics shine and all moving parts,
including a fully animated landing gear animation. Some special things include
three opening doors, with visible interior. Flexing wings, wing views and
trim animation for the horizontal stabilisers.
Model, dynamics by: Project Opensky, Repaint By: Aziz Palas.
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
[weight_and_balance]
max_gross_weight = 660000
empty_weight = 347800
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 41600000
empty_weight_roll_MOI = 42000000
empty_weight_yaw_MOI = 67500000
empty_weight_coupled_MOI = 1000
max_number_of_stations = 7
station_load.0 = "4200, 70, 0, 5, 1st Class - 24 pax" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "9450, 40, 0, 5, Business Class - 54 pax" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "28875, -10, 0, 5, Econ Front - 165 pax" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "20125, -55, 0, 5, Econ Rear - 115 pax" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "11250, 50, 0, 0, Fore Cargo" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = "11250, -50, 0, 0, Aft Cargo " //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = "1000, -70, 0, 0, Bulk Cargo" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 1, 28.5, 0, 12.4, Opensky_beacon
light.1 = 1, 4.75, 0, -9, Opensky_beacon
light.2 = 3, -127, 0, 4.5, Opensky_nav_yellow
light.3 = 8, 32.7, -10.1, 1.3, Opensky_nav_yellow
light.4 = 8, 32.7, 10.1, 1.3, Opensky_nav_yellow
light.5 = 4, 105, 0, 5.4, Opensky_747_vclight
light.6 = 2, -127.9, 0, 8.5, fx_strobeh
light.7 = 4, 105, -2.2, 5.328, Opensky_747_vclight
light.8 = 4, 105, 2.2, 5.328, Opensky_747_vclight
light.9 = 8, 12.5, 23, 0, Opensky_nacelle_refl
light.10 = 8, 12.5, -23, 0, Opensky_nacelle_refl
light.11 = 8, 25, 30, 0, Opensky_wing_light
light.12 = 8, 25, -30, 0, Opensky_wing_light
light.13 = 8, 0, 56, 0, Opensky_wing_light
light.14 = 8, 0, -56, 0, Opensky_wing_light
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 0.735
min_throttle_limit = -0.32
engine.0 = 10.0, -32.583, -10.500
engine.1 = 10.0, 32.583, -10.500
[smokesystem]
smoke.0 = -15, 22, 32, Opensky_revspray
smoke.1 = -15, 22, -32, Opensky_revspray
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = opensky_sparks, 1
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2
number_of_tank_selectors = 3
electric_pump = 1
Center1 = 10, 0, -4, 14220, 10
LeftMain = -5, -35, 0, 6200, 6
LeftAux = -10, -49.705, 0, 9300, 6
RightMain = -5, 35, 0, 6200, 6
RightAux = -10, 49.705, 0, 9300, 6
[contact_points]
static_pitch = 0
static_cg_height = 14.5
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 17
//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)
Point.0= 1, 92.500, 0.000, -16.750, 1881.102, 0, 2.0, 70.0, 1.200, 1.800, 1.5, 7.000, 9.000, 0.000, 240.000, 280.000
Point.1= 1, -10.900, -20.291, -18.250, 2574.803, 1, 2.6, 0.0, 1.700, 1.100, 1.5, 10.900, 11.900, 2.000, 240.000, 280.000
Point.2= 1, -10.900, 20.291, -18.250, 2574.803, 2, 2.6, 0.0, 1.700, 1.100, 1.5, 8.100, 13.100, 3.000, 240.000, 280.000
point.3 = 2, -44.167, -99.916, 10.000, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -44.167, 99.916, 10.000, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -108, 0, -0.6, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 88.417, 0, -7.5, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 10.000, -32.583, -8.500, 787.401, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7.0, 0.0, 0.0
point.8 = 2, 10.000, 32.583, -8.500, 787.401, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 8.0, 0.0, 0.0
point.9 = 2, 14, -32.583, -13.3, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0
point.10 = 2, 14, 32.583, -13.3, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 8, 0, 0
point.11 = 2, 105, 0, -4.5, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.12 = 2, 100, 0, 8.9, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.13 = 2, -127, 0, 41.3, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.14 = 2, -128.5, 35, 9, 787.401, 0, 0, 0, 0, 0, 0, 0, 5, 9, 0, 0
point.15 = 2, -128.5, -35, 9, 787.401, 0, 0, 0, 0, 0, 0, 0, 6, 9, 0, 0
point.16 = 2, -81.5, 0, -6, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
//[contact_points]
//static_pitch = 0
//static_cg_height = 16.4
//tailwheel_lock = 0
//gear_system_type = 1
//max_number_of_points = 28
//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)
//point.0 = 1, 91.243, -1.5, -16.5, 1881.102, 0, 1.6, 70, 1, 1.8, 2.4, 7, 9, 0, 240, 280
//point.1 = 1, 91.243, 1.5, -16.5, 1881.102, 0, 1.6, 70, 1, 1.8, 2.4, 7, 9, 0, 240, 280
//point.2 = 1, -14.800, -20.291, -17.800, 2574.803, 1, 2, 0, 1.245, 3.0, 2.2, 10.9, 11.9, 2, 240, 280
//point.3 = 1, -14.800, -15.291, -17.800, 2574.803, 1, 2, 0, 1.245, 3.0, 2.2, 8.1, 13.1, 3, 240, 280
//point.4 = 1, -9.800, -20.291, -17.800, 2574.803, 1, 2, 0, 1.245, 3.0, 2.2, 10.9, 11.9, 2, 240, 280
//point.5 = 1, -9.800, -15.291, -17.800, 2574.803, 1, 2, 0, 1.245, 3.0, 2.2, 8.1, 13.1, 3, 240, 280
//point.6 = 1, -5.000, -20.291, -17.800, 2574.803, 1, 2, 0, 1.245, 3.0, 2.2, 10.9, 11.9, 2, 240, 280
//point.7 = 1, -5.000, -15.291, -17.800, 2574.803, 1, 2, 0, 1.245, 3.0, 2.2, 8.1, 13.1, 3, 240, 280
//point.8 = 1, -14.800, 20.291, -17.800, 2574.803, 2, 2, 0, 1.245, 3.0, 2.2, 10.9, 11.9, 2, 240, 280
//point.9 = 1, -14.800, 15.291, -17.800, 2574.803, 2, 2, 0, 1.245, 3.0, 2.2, 8.1, 13.1, 3, 240, 280
//point.10 = 1, -9.800, 20.291, -17.800, 2574.803, 2, 2, 0, 1.245, 3.0, 2.2, 10.9, 11.9, 2, 240, 280
//point.11 = 1, -9.800, 15.291, -17.800, 2574.803, 2, 2, 0, 1.245, 3.0, 2.2, 8.1, 13.1, 3, 240, 280
//point.12 = 1, -5.000, 20.291, -17.800, 2574.803, 2, 2, 0, 1.245, 3.0, 2.2, 10.9, 11.9, 2, 240, 280
//point.13 = 1, -5.000, 15.291, -17.800, 2574.803, 2, 2, 0, 1.245, 3.0, 2.2, 8.1, 13.1, 3, 240, 280
//point.14 = 2, -44.167, -99.916, 10.000, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
//point.15 = 2, -44.167, 99.916, 10.000, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
//point.16 = 2, -108, 0, -0.6, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
//point.17 = 2, 88.417, 0, -7.5, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
//point.18 = 2, 10.000, -32.583, -8.500, 787.401, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7.0, 0.0, 0.0
//point.19 = 2, 10.000, 32.583, -8.500, 787.401, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 8.0, 0.0, 0.0
//point.20 = 2, 14, -32.583, -13.3, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0
//point.21 = 2, 14, 32.583, -13.3, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 8, 0, 0
//point.22 = 2, 105, 0, -4.5, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
//point.23 = 2, 100, 0, 8.9, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
//point.24 = 2, -127, 0, 41.3, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
//point.25 = 2, -128.5, 35, 9, 787.401, 0, 0, 0, 0, 0, 0, 0, 5, 9, 0, 0
//point.26 = 2, -128.5, -35, 9, 787.401, 0, 0, 0, 0, 0, 0, 0, 6, 9, 0, 0
//point.27 = 2, -81.5, 0, -6, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
[keyboard_response]
elevator = 100.000, 200.000
aileron = 100.000, 200.000
rudder = 100.000, 200.000
[forcefeedback]
gear_bump_nose_magnitude = 6000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 6000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 6000
gear_bump_right_direction = 00500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1.0
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
[airplane_geometry]
wing_area = 4605.000
wing_span = 205
wing_root_chord = 50.000
wing_dihedral = 6.218
wing_incidence = 1.000
wing_twist = -0.500
oswald_efficiency_factor = 0.600
wing_winglets_flag = 1
wing_sweep = 35
wing_pos_apex_lon = 30.000
wing_pos_apex_vert = 0.000
htail_area = 1291
htail_span = 70
htail_pos_lon = -96.5
htail_pos_vert = 5
htail_incidence = 0.000
htail_sweep = 40.000
vtail_area = 573.000
vtail_span = 35
vtail_sweep = 45
vtail_pos_lon = -85
vtail_pos_vert = 8.800
elevator_area = 137.000
aileron_area = 68.000
rudder_area = 232.000
elevator_up_limit = 24.000
elevator_down_limit = 18.000
aileron_up_limit = 24.000
aileron_down_limit = 18.000
rudder_limit = 32.000
elevator_trim_limit = 16.000
spoiler_limit = 45.000
aileron_to_spoileron_gain = 1.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 12.000
min_flaps_for_spoilerons = 0
spoilerons_available = 1
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 2, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 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
[flight_tuning]
cruise_lift_scalar=1.00
parasite_drag_scalar=0.55
induced_drag_scalar=0.88
elevator_effectiveness=1.00
aileron_effectiveness=1.60
rudder_effectiveness=1.00
pitch_stability=1.00
roll_stability=1.00
yaw_stability=1.00
elevator_trim_effectiveness=0.40
aileron_trim_effectiveness=0.50
rudder_trim_effectiveness=0.50
[General]
performance=Passengers\n3-class conf: 301 \n2-class conf: N/A \n1-class conf: N/A\n\nCargo\n14 LD-3 containers aft \n600 cubic Ft (17 cubic m)\nTotal lower hold volume: 7,120 cu ft \n\nDimensions\nSpan 212 ft 7 in\nLength 242 ft 4 in\nHeight 61 ft 5 in \n (--max 58 ft 8 in--min)\n\nEngines: General Electric 90-115B1\nTO Thrust Rating: 115,100 lb\n\nMax Fuel Cap.: 47,890 gal\nMaxTOW: 775,000 lb\nZFW: 524,000 lb\n\nMax Range: 7,930 nautical miles (14,685 km)\nTypical Cruise Speed \n @ FL350: M.84
atc_type=BOEING
atc_model=B773
editable=0
[pitot_static]
vertical_speed_time_constant=999 //Increasing this value will cause a more instantaneous reaction in the VSI
[jet_engine]
thrust_scalar=1.000
[TurbineEngineData]
bypass_ratio=6.400000
fuel_flow_gain=0.001
inlet_area=65.962
rated_N2_rpm=29920.000
static_thrust=115100.000
afterburner_available=0
reverser_available=1
[Reference Speeds]
flaps_up_stall_speed=174.000
full_flaps_stall_speed=158.000
cruise_speed=485.00
max_indicated_speed=330.000000
max_mach=0.890020
[Views]
eyepoint=103.002, -1.756, 5.20
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=800.000
autothrottle_available=1
autothrottle_arming_required= 1
autothrottle_takeoff_ga= 1
autothrottle_max_rpm= 110.000
pitch_takeoff_ga=8.00 //0.000
use_no_default_pitch = 1 // 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank = 1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode.
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=0.300000
max_pitch_velocity_lo_alt_breakpoint= 7000.000000
max_pitch_velocity_hi_alt_breakpoint=24000.000000
max_bank=30.000000
max_bank_acceleration=1.200000
max_bank_velocity=2.000000
max_throttle_rate=0.024
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=1.000000
[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
[flaps.0] //Inboard Trailing Edge
type = 1 // 1 - tail, 2 - lead
span-outboard = 4.2 // 0.0 .. 1.0
extending-time = 35 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 0 // degrees
flaps-position.2 = 5 // degrees
flaps-position.3 = 15 // degrees
flaps-position.4 = 20 // degrees
flaps-position.5 = 25 // degrees
flaps-position.6 = 30 // degrees
damaging-speed = 260 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.82
drag_scalar = 0.95
pitch_scalar= 0.60
system_type = 1 //Hydraulic
[flaps.1] //Outboard Trailing Edge
type = 1 // 1 - tail, 2 - lead
span-outboard = 4.8 // 0.0 .. 1.0
extending-time = 35 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 5 // degrees
flaps-position.2 = 10 // degrees
flaps-position.3 = 15 // degrees
flaps-position.4 = 20 // degrees
flaps-position.5 = 25 // degrees
flaps-position.6 = 30 // degrees
damaging-speed = 260 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.40
drag_scalar = 0.50
pitch_scalar= 0.30
system_type = 1 //Hydraulic
[flaps.2] //Inboard Leading Edge Slats
type = 2 // 1 - tail, 2 - lead
span-outboard = 4.5 // 0.0 .. 1.0
extending-time = 18 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 5 // degrees
flaps-position.2 = 5 // degrees
flaps-position.3 = 5 // degrees
flaps-position.4 = 5 // degrees
flaps-position.5 = 20 // degrees
flaps-position.6 = 20 // degrees
damaging-speed = 260 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.30
drag_scalar = 0.30
pitch_scalar= 0.30
system_type = 1 //Hydraulic
[direction_indicators]
direction_indicator.0=3,0
[brakes]
toe_brakes_scale=0.580
parking_brake=1
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[TailHook] // For opening cargo door.
tailhook_length=1 ;(feet)
tailhook_position = 0.0, 0.0, 0.0 ;(feet) longitudinal, lateral, vertical positions from datum
[folding_wings] // For opening main deck cargo door.
wing_fold_system_type = 4 ;0=None
fold_rates = 0.05,1.00 ;Percent per second
[exits]
number_of_exits = 4
exit_rate.0 = 0.10 ;Percent per second
exit_rate.1 = 0.08 ;Percent per second
exit_rate.2 = 0.10 ;Percent per second
exit_rate.3 = 0.08 ;Percent per second
