[fltsim.0]
title=Bristol Britannia AFREK
sim=britannia
model=
panel=
sound=
texture=afrek
kb_checklists=Britannia_253_check
kb_reference=Britannia_253_ref
atc_id_color=0xffffffffff
atc_id=G-BDUR
ui_manufacturer=Bristol
ui_type=Britannia 253
ui_variation=Afrek
description=Bristol Britannia 253F. Afrek,a Greek cargo carrier,operated two British registered aircraft in the late 1970's. The carrier ceased operations in the early '80s and the aircraft were sold to Aero Caribbean. Model by Mike Stone.
atc_heavy=0
atc_airline=Afrek
atc_flight_number=721
[General]
atc_type=Bristol
atc_model=Britannia
editable=1
performance = 4 x Proteus 765 Turboprops 4,450shp max cruising speed 397mph range with max fuel 3,310 miles MTOW 185,000lb Dimensions Span 142'3" Length 124'3" Maximum payload 34,500lb
[WEIGHT_AND_BALANCE]
max_gross_weight = 185000.000
empty_weight = 93100.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.000, 0.000, 0.000
max_number_of_stations =50
;Moments of Inertia
empty_weight_pitch_MOI = 3000000.000
empty_weight_roll_MOI = 1800000.000
empty_weight_yaw_MOI = 3000000.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
station_load.0=22100.00,0.00,0.00,0.00
[flight_tuning]
cruise_lift_scalar =0.700
parasite_drag_scalar =0.900
induced_drag_scalar =1.000
elevator_effectiveness =1.000
aileron_effectiveness =1.000
rudder_effectiveness =1.000
pitch_stability =2.002
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =0.900
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
[GeneralEngineData]
engine_type = 5
Engine.0 = 13.000, -34.000, 0.000
Engine.1 = 16.000, -17.000, 0.000
fuel_flow_scalar = 0.670
Engine.2= 16.000, 17.000, 0.000
Engine.3= 13.000, 34.000, 0.000
min_throttle_limit=-0.749878
[TurbineEngineData]
fuel_flow_gain= 0.015
inlet_area= 1.0
rated_N2_rpm= 11700.000
static_thrust= 1285.000
[propeller]
propeller_type= 0
propeller_diameter= 18.00
propeller_blades= 4
propeller_moi= 107.0
beta_max=46.0
beta_min= 5.0
min_gov_rpm= 4500.0
prop_tc= 0.004
gear_reduction_ratio= 11.70
fixed_pitch_beta= 0
low_speed_theory_limit= 80.000
prop_sync_available= 1
prop_deice_available= 1
prop_feathering_available= 1
prop_auto_feathering_available= 0
min_rpm_for_feather= 700.0
beta_feather= 90.0
power_absorbed_cf= 0.9
defeathering_accumulators_available= 0
prop_reverse_available= 1
minimum_on_ground_beta= 1.0
minimum_reverse_beta= -35.0
thrust_scalar=2.10
[turboprop_engine]
maximum_torque= 12565.0
power_scalar=1.0
[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= 1.00, 43.00, 0.00, -9.00, 1581.00, 0.00, 1.25, 50.00, 0.500, 1.500, 0.952, 7.800, 6.800, 0.00, 0.00, 0.00
point.1= 1.00, -3.00,-17.00, -9.50, 1574.00, 1.00, 1.50, 0.00, 0.542, 1.500, 0.815, 8.500, 8.200, 2.00, 0.00, 0.00
point.2= 1.00, -3.00, 17.00, -9.50, 1574.00, 2.00, 1.50, 0.00, 0.542, 1.500, 0.815, 6.800, 8.900, 3.00, 0.00, 0.00
point.3= 2.000, -3.330, -23.920, -3.000, 787.000, 0.00, 0.00, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, -3.330, 23.920, -3.000, 787.000, 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, -22.670, 0.000, 0.000, 787.000, 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, 23.080, 0.000, -1.500, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch = 0.000
static_cg_height = 9.000
gear_system_type=0
[Views]
eyepoint = 42.35, -1.20, 4.49
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1
Com.2=1
Nav.1=1
Nav.2=1
Adf.1=1
Adf.2=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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, -7.07, -70.80, 1.63, fx_navred ,
light.1 = 3, -7.07, 70.80, 1.63, fx_navgre ,
light.2 = 3, -70.38, 0.00, 2.11, fx_navwhi ,
light.3 = 2, -6.77, -70.80, 1.63, fx_strobe ,
light.4 = 2, -6.77, 70.80, 1.63, fx_strobe ,
light.5 = 1, -57.40, 0.00, 27.83, fx_beacon ,
light.6 = 1, 2.61, 0.00, -4.82, fx_beacon ,
light.7 = 4, 42.93, 0.00, 5.66, fx_vclight,
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
LeftTip = 0.000, -35.000, 0.000, 2410.000, 0.000
LeftAux = 0.000, -10.000, 0.000, 2004.000, 0.000
Center1 = 0.000, 0.000, 0.000, 1476.000, 0.000
RightAux = 0.000, 10.000, 0.000, 2004.000, 0.000
RightTip = 0.000, 35.000, 0.000, 2410.000, 0.000
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 4
electric_pump=0
[airplane_geometry]
wing_area = 2075.000
wing_span = 142.000
wing_root_chord = 21.000
wing_dihedral = 3.000
wing_incidence = 3.000
wing_twist = -2.000
oswald_efficiency_factor= 0.800
wing_winglets_flag = 0
wing_sweep = 5.000
wing_pos_apex_lon = 1.000
wing_pos_apex_vert = 0.000
htail_area = 550.000
htail_span = 60.000
htail_pos_lon = -50.000
htail_pos_vert = 0.000
htail_incidence = 1.000
htail_sweep = 5.000
vtail_area = 490.000
vtail_span = 23.000
vtail_sweep = 10.000
vtail_pos_lon = -50.000
vtail_pos_vert = 10.000
elevator_area = 100.000
aileron_area = 80.000
rudder_area = 68.000
elevator_up_limit = 17.000
elevator_down_limit = 15.500
aileron_up_limit = 18.000
aileron_down_limit = 18.000
rudder_limit = 30.000
elevator_trim_limit = 15.000
spoiler_limit = 60.000
spoilerons_available = 0
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
[Reference Speeds]
flaps_up_stall_speed = 120.000
full_flaps_stall_speed = 100.000
cruise_speed = 475.000
max_indicated_speed=259.000000
max_mach=0.679980
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1000.0
autothrottle_available= 1
pitch_takeoff_ga=8.000000
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
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=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
[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= 0.600
extending-time= 15.000
system_type= 0
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.250
drag_scalar= 1.500
pitch_scalar= 0.500
flaps-position.0= 0.000, 0.000
flaps-position.1= 15.000, 0.000
flaps-position.2= 30.000, 0.000
flaps-position.3= 45.000, 0.000
[SMOKESYSTEM]
smoke.0=0.893, -11.469, -14.771, fx_smoke_rx
smoke.1=0.893, -11.469, 14.771, fx_smoke_rx
smoke.2=-3.80, -12.808, -28.942, fx_smoke_rx
smoke.3=-3.80, -12.808, 28.942, fx_smoke_rx
[brakes]
toe_brakes_scale=1.000000
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=15.011494
[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
