[fltsim.0]
title=AI Airlift Vickers Viking BEA 
sim=FSDS2 Vickers Viking
model=
panel=
sound=
texture=beawt
kb_checklists=
description=Viking
ui_manufacturer=Vickers
ui_type=Viking
ui_variation=BEA "Sir Bertram Ramsey"
visual_damage=1
atc_heavy=0
atc_id=G-AJBQ
atc_airline=Beeline
atc_flight_number=VC2
atc_type=BRITISHAEROSPACE
atc_model=BL18
prop_anim_ratio=0.9
atc_parking_codes=BAW

[fltsim.1]
title=AI Airlift Vickers Viking RAF 
sim=FSDS2 Vickers Viking
model=
panel=
sound=
texture=VL263
kb_checklists=
description=RAF Viking
ui_manufacturer=Vickers
ui_type=Viking
ui_variation=RAF  
visual_damage=1
atc_heavy=0
atc_id=R-AJBQ
atc_airline=RAF
atc_flight_number=VC3
atc_type=BRITISHAEROSPACE
atc_model=BL19
prop_anim_ratio=0.9
atc_parking_codes=BAW

[fltsim.2]
title=AI Airlift Vickers Viking SASd 
sim=FSDS2 Vickers Viking
model=
panel=
sound=
texture=ddl
kb_checklists=
description=SASD Viking
ui_manufacturer=Vickers
ui_type=Viking
ui_variation=SAS  
visual_damage=1
atc_heavy=0
atc_id=R-AJBQ
atc_airline=SAS
atc_flight_number=VC3
atc_type=BRITISHAEROSPACE
atc_model=BL17
prop_anim_ratio=0.9
atc_parking_codes=SAS


[General]
performance=Model Designer : Rick Piper\nCrew: 3-4 \nEngines: 2 x 1690hp Bristol Hercules 634\nMax Speed: 263 mph
\nTypical Cruise Speed 182 kts =210 mph@10,000 ft\nCeiling: 20,000 ft \nRange:  approx 1,700 m Max.
atc_type=BRITISHAEROSPACE
atc_model=BL17

[WEIGHT_AND_BALANCE]
max_gross_weight=34000
empty_weight=23000

reference_datum_position=0.0,0.0,0.0
empty_weight_CG_position=0.0,0.0,0.0

max_number_of_stations=50

;Moments of Inertia
empty_weight_roll_MOI=109699.03 
empty_weight_pitch_MOI=201179.10  
empty_weight_yaw_MOI=131797.97 
empty_weight_coupled_MOI=0.0
station_load.0=170, 14.0, -1.6, 0  //Pilot
station_load.1=170, 14.0, 1.6, 0  //Co-Pilot
station_load.2=170, 11.5, 0.6, 0  //Nav/engineer
station_load.3=170, 8.2, -2.9, 0   //pax1
station_load.4=170, 8.2, 0.7, 0    //pax2
station_load.5=170, 8.2, 2.9, 0    //pax3
station_load.6=170, 4.5, -2.9, 0   //pax4
station_load.7=170, 4.5, 0.7, 0    //pax5
station_load.8=170, 4.5, 2.9, 0    //pax6
station_load.9=170, 1.7, -2.9, 0   //pax7
station_load.10=170, 1.7, 0.7, 0   //pax8
station_load.11=170, 1.7, 2.9, 0    //pax9
station_load.12=170, -2.1, -2.9, 0   //pax10
station_load.13=170, -2.1, 0.7, 0    //pax11
station_load.14=170, -2.1, 2.9, 0    //pax12
station_load.15=170, -6.0, -2.9, 0   //pax13
station_load.16=170, -6.0, 0.7, 0    //pax14
station_load.17=170, -6.0, 2.9, 0    //pax15
station_load.18=170, -9.7, -2.9, 0   //pax16
station_load.19=170, -9.7, 0.7, 0    //pax17
station_load.20=170, -9.7, 2.9, 0    //pax18
station_load.21=170, -13.3, -2.9, 0 //pax19
station_load.22=170, -13.3, 0.7, 0  //pax20
station_load.23=170, -13.3, 2.9, 0  //pax21
station_load.24=170, -17.0, -2.9, 0 //pax22
station_load.25=170, -17.0, 0.7, 0  //pax23
station_load.26=170, -17.0, 2.9, 0  //pax24
station_load.27=250, 11.6, -4.0, 0 //Front Baggage hold
station_load.28=50, -5.0, -4.5, 0  //Centre Baggage hold
station_load.29=70, -15.0, -4.5, 0  //Rear Baggage hold

[flight_tuning]
cruise_lift_scalar     = 1.0
parasite_drag_scalar   = 1.0
induced_drag_scalar    = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness  = 1.0
rudder_effectiveness   = 1.0
pitch_stability        = 1.0
roll_stability         = 1.0
yaw_stability          = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0
p_factor_on_yaw          = 0.5
torque_on_roll           = 1.0
gyro_precession_on_yaw   = 1.0
gyro_precession_on_pitch = 1.0

[Flaps.0]
type=1
span-outboard = 0.5
extending-time = 10
flaps-position.0 = 0.0
flaps-position.1 = 15.0
flaps-position.2 = 30.0
flaps-position.3 = 50.0
damaging-speed = 145.0
blowout-speed = 180.0
lift_scalar= 1.4
drag_scalar = 1.7
pitch_scalar = 1.0
system_type=1

[GeneralEngineData]
engine_type=0                             
Engine.0=11.111, -11.397, -1.687               //(feet) longitudinal, lateral, vertical distance from reference datum     
Engine.1=11.111, 11.397, -1.687                 
fuel_flow_scalar=0.65
min_throttle_limit = 0.0 
master_ignition_switch = 1                 

[piston_engine]
power_scalar=1.08
cylinder_displacement=155.57
compression_ratio=7.5
number_of_cylinders=14
max_rated_rpm=2900.0
max_rated_hp=1970.0
fuel_metering_type=1
cooling_type=0
normalized_starter_torque=0.015
turbocharged=1
max_design_mp=47.25
min_design_mp=0.0
critical_altitude=10000.0
emergency_boost_type=0
emergency_boost_mp_offset=0.0
emergency_boost_gain_offset=0.0
fuel_air_auto_mixture=1
auto_ignition=1
max_rpm_mechanical_efficiency_scalar=1.0
idle_rpm_mechanical_efficiency_scalar=0.9
max_rpm_friction_scalar=1.0
idle_rpm_friction_scalar=1.2

[propeller]
thrust_scalar=0.86
propeller_type=0
rotation=-1,-1
propeller_diameter=13.3
propeller_blades=4
propeller_moi=99.2
beta_max=30.0
beta_min=18.0
min_gov_rpm=800
prop_tc=0.1
gear_reduction_ratio=1.8
fixed_pitch_beta=0.0
low_speed_theory_limit=80.0
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=0.5
power_absorbed_cf=0.9
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=0.0
minimum_reverse_beta=0.0
feathering_switches = 1

[contact_points]
point.0=1, -31.66, 0.0, -5.56, 1500.0, 0, 0.749, 90.0, 0.200, 1.5, 0.695, 6.0, 5.0, 0, 0.0, 0.0
point.1=1, 1.9, -11.4, -10.6, 1600.0, 1, 1.816, 0.0, 0.700, 0.8, 0.7, 12.0, 14.0, 2, 0.0, 0.0
point.2=1, 1.9, 11.4, -10.6, 1600.0, 2, 1.816, 0.0, 0.700, 0.8, 0.7, 9.0, 12.0, 3, 0.0, 0.0
point.3=2, 0.1, -44.9 ,0.0,1574.8,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,5.0,0.0,0.0
point.4=2, 0.1, 44.9 ,0.0,1574.8,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,6.0,0.0,0.0
point.5=2, -35.2 ,0.0 ,-2.0,1574.8,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,9.0,0.0,0.0
point.6=2, 20.1 ,0.0, -5.0,1574.8,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,4.0,0.0,0.0

static_pitch=8.32433
static_cg_height=9.9
gear_system_type=1
tailwheel_lock = 1 

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    =  0.0     //Flap angle that activates warning at idle
flap_limit_power   = 15.0     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 0.78  //Brake scalar
differential_braking_scale = 1.0        //Delta on the amount of brake when the rudder pedals deflected

[hydraulic_system]
normal_pressure = 1200.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,0,0   //pumps on Eng1,2

[Views]
eyepoint=14.4,-1.6,1.5  

[LIGHTS]
light.1=4,   14.0, 0.0, 1.0, fx_vclight,
light.2=4,   6.33, 0.0, 0.0, fx_vclight_Viking ,
light.3=4,   1.33, 0.0, 0.0, fx_vclight_Viking ,
light.4=4,   -4.33, 0.0, 0.0, fx_vclight_Viking ,
light.5=4,   -9.33, 0.0, 0.0, fx_vclight_Viking ,
light.6=4,   -14.33, 0.0, 0.0, fx_vclight_Viking ,

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1
Adf.2=1
Transponder.1=1
Marker.1=1

[keyboard_response]
elevator =200, 1000
aileron  =200, 1000
rudder   =200, 1000

[direction_indicators]
direction_indicator.0=1,0
direction_indicator.1=2,0

[attitude_indicators]
attitude_indicator.0 = 1 
attitude_indicator.1 = 2 

[turn_indicators]
turn_indicator.0=2,0

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
startup=fx_engstrt_jenny
touchdown=fx_tchdwn_s, 1

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 70

[fuel]
LeftMain=0.0,-20.0,0.0,375.0,0.0  //total fuel capacity 740 Imp gallons (889 US Gallons) FS002 used US Gal!.
LeftAux=1.0,-11.4,1.0,69.0,0.0
RightMain=0.0,20.0,0.0,375.0,0.0
RightAux=1.0,11.4,1.0,69.0,0.0 
fuel_type=1
number_of_tank_selectors=1
electric_pump=1

[airplane_geometry]
wing_area=882.0
wing_span=89.2
wing_root_chord=14.8
wing_dihedral=3.0
wing_incidence=0.9
wing_twist=0.0
oswald_efficiency_factor=0.7433   
wing_winglets_flag=0
wing_sweep=0.8
wing_pos_apex_lon=0.0
wing_pos_apex_vert=0.0
htail_area=174.0
htail_span=36.0
htail_pos_lon=-31.3
htail_pos_vert=1.0
htail_incidence=0.9
htail_sweep=0.0
vtail_area=120.0
vtail_span=12.4
vtail_sweep=0.0
vtail_pos_lon=-31.3
vtail_pos_vert=5.5
elevator_area=69.0
aileron_area=14.4
rudder_area=66.0
elevator_up_limit=26.0
elevator_down_limit=26.0
aileron_up_limit=25.0
aileron_down_limit=25.0
rudder_limit=55.0
elevator_trim_limit=19.9
spoiler_limit=0.0
spoilerons_available=0
aileron_to_spoileron_gain=0.0
min_ailerons_for_spoilerons=0.0
min_flaps_for_spoilerons=0.0

[Reference Speeds]
flaps_up_stall_speed=85.0
full_flaps_stall_speed=75.0
cruise_speed=182.0
max_indicated_speed=232.0

[autopilot]
autopilot_available= 1
flight_director_available= 0
pitch_takeoff_ga=0.0
default_vertical_speed=600.0
autothrottle_available=1
direction_indicator=1
attitude_indicator =1
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=1.5
max_bank_velocity=3.0
max_throttle_rate=0.2
nav_proportional_control=9.0
nav_integrator_control=0.25
nav_derivative_control=0.0
nav_integrator_boundary=2.5
nav_derivative_boundary=0.0
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.0
gs_integrator_boundary=0.7
gs_derivative_boundary=0.0
yaw_damper_gain = 0.0
default_bank_mode=2     //Default to Heading Hold
autothrottle_arming_required=1
autothrottle_takeoff_ga=0
autothrottle_max_rpm=105.0

[forcefeedback]
ground_bumps_magnitude1=2600            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.6
ground_bumps_magnitude2=1200            ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.085
ground_bumps_slope2=0.65
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=3500000                 ; in microseconds

[stall_warning]
type=1

[SMOKESYSTEM]
smoke.0= -3.67, 6.4, -13, fx_smoke_rx
smoke.1= -3.67, 6.4, 13, fx_smoke_rx