[fltsim.0]
title=AI Trident 2 BEA
sim=ai trident
panel=
model=
sound=
texture=BEA Red Square
kb_checklists=
kb_reference=TRI2_Ref
description=Hawker Siddeley Trident 2E G-AVFF entered service with BEA in 1968. It was was flown at the Farborough Airshow in this livery. It served with BEA & British Airways until the end of 1984 & was scrapped at Southend a few months later.\nModel by David Maltby\nwww.Maltbyd.fsnet.co.uk
ui_manufacturer=Hawker Siddeley
ui_type=Trident 2
ui_variation=BEA
atc_heavy=1
atc_id=G-AVFF
atc_airline=BEA
atc_flight_number=225

[General]
atc_type=BRITISHAEROSPACE
atc_model=TRID
editable=1
visual_damage=1
performance=\n\n

[pitot_static]
vertical_speed_time_constant=1                //Increasing this value will cause a more instantaneous reaction in the VSI

[WEIGHT_AND_BALANCE]
max_gross_weight=138500.000
empty_weight=110999.000

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=0.000000,0.000000,0.000000,0.000000

;Moments of Inertia
empty_weight_pitch_MOI=3172439.000
empty_weight_roll_MOI=2262183.000
empty_weight_yaw_MOI=3337024.000
empty_weight_coupled_MOI=0.000
CG_forward_limit=0.000
CG_aft_limit=1.000

[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=0.800
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

[GeneralEngineData]
engine_type=1
Engine.0=4.750, -16.100, -2.500
Engine.1=4.750, 16.100, -2.500
fuel_flow_scalar=1.000

[TurbineEngineData]
fuel_flow_gain=0.002
inlet_area=19.600
rated_N2_rpm=29920.000
static_thrust=15000.000
afterburner_available=0
reverser_available=1

[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)




[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

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -25.14, -52.65, 0.95, fx_navredm ,
light.1 = 3, -25.14, 52.65, 0.95, fx_navgrem ,
light.2 = 2, -86.54, 0.00, 21.92, fx_strobeh ,
light.3 = 2, -27.22, -53.65, 0.84, fx_strobeh ,
light.4 = 2, -27.22, 53.65, 0.84, fx_strobeh ,
light.5 = 1, 6.85, 0.00, -3.95, fx_beaconb ,
light.6 = 1, 28.20, 0.00, 10.25, fx_beaconh ,
light.7 = 4, 44.41, 0.00, 3.50, fx_vclight ,
light.8=3, -28.22, -53.65, 0.78, fx_navwhih ,
light.9=3, -28.22, 53.65, 0.78, fx_navwhih ,

[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

[exits]
number_of_exits=2
exit_rate.0=0.4                               ;Percent per second
exit_rate.1=0.4                               ;Percent per second

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

[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;

[fuel]
Center1=0.000, 0.000, 0.000, 2313.000, 0.000
LeftMain=-3.000, -19.000, 0.000, 1500.000, 0.000
RightMain=-3.000, 19.000, 0.000, 1500.000, 0.000
fuel_type=2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1                    

[airplane_geometry]
wing_area= 1462.000
wing_span= 98.000
wing_root_chord= 24.000
wing_dihedral= 5.000
wing_incidence= 1.500
wing_twist= -0.500
oswald_efficiency_factor= 0.750
wing_winglets_flag= 0
wing_sweep= 35.000
wing_pos_apex_lon= 12.000
wing_pos_apex_vert= -4.000
htail_area= 300.000
htail_span= 33.000
htail_pos_lon= -38.000
htail_pos_vert= 16.000
htail_incidence= 0.000
htail_sweep= 35.000
vtail_area= 250.000
vtail_span= 15.000
vtail_sweep= 25.000
vtail_pos_lon= -25.000
vtail_pos_vert= 4.000
elevator_area= 35.000
aileron_area= 50.000
rudder_area= 50.000
elevator_up_limit= 22.000
elevator_down_limit= 22.000
aileron_up_limit= 22.000
aileron_down_limit= 22.000
rudder_limit= 22.000
elevator_trim_limit= 8.000
spoiler_limit= 40.000
spoilerons_available= 0
aileron_to_spoileron_gain= 3.000
min_ailerons_for_spoilerons= 10.000
min_flaps_for_spoilerons= 0.000

[contact_points]
point.0= 1.000, 38.850, 0.000, -11.030, 1574.803, 0.000, 1.250, 67.000, 0.500, 1.340, 0.500, 8.000, 8.000, 0.000, 0.000, 0.000
point.1= 1.000, -5.010, -11.000, -10.767, 1574.803, 1.000, 1.418, 0.000, 0.500, 1.530, 0.600, 9.000, 9.000, 2.000, 0.000, 0.000
point.2= 1.000, -5.010, 11.000, -10.767, 1574.803, 2.000, 1.418, 0.000, 0.500, 1.530, 0.600, 9.000, 9.000, 3.000, 0.000, 0.000
point.3= 2.000, -21.900, -48.000, -1.300, 501.849, 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, -21.900, 48.000, -1.300, 501.849, 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, -30.000, 0.000, -4.700, 501.849, 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, 57.800, 0.000, 0.000, 501.849, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= 0.400
static_cg_height= 10.400

[Reference Speeds]
flaps_up_stall_speed= 130.000
full_flaps_stall_speed= 105.000
cruise_speed= 450.000

[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=0.800
extending-time=25.000
system_type=1
damaging-speed=250.000
blowout-speed=300.000
lift_scalar=0.70
drag_scalar=0.70
pitch_scalar=0.70
flaps-position.0=0.000, 0.000
flaps-position.1=1.000, 0.000
flaps-position.2=2.000, 0.000
flaps-position.3=5.000, 0.000
flaps-position.4=10.000, 0.000
flaps-position.5=15.000, 0.000
flaps-position.6=25.000, 0.000
flaps-position.7=30.000, 0.000
flaps-position.8=40.000, 0.000

[Flaps.1]
type=2
span-outboard=0.800
extending-time=10.000
system_type=1
damaging-speed=250.000
blowout-speed=300.000
lift_scalar=1.000
drag_scalar=1.000
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=1.000, 0.000

[Flaps.2]
type=2
span-outboard=0.800
extending-time=15.000
system_type=1
damaging-speed=250.000
blowout-speed=300.000
lift_scalar=1.000
drag_scalar=1.000
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=0.500, 0.000
flaps-position.2=1.000, 0.000