//iss;  0808222000  v0.9, for 'vkg_v01.zip' by Ted Cook
// Font=Verdana,10pt. regular:
//modified for FSX by Leyland Spurr


[fltsim.0]
title=Viking knil
sim=viking
model=knil
panel=knil
sound=HS
texture=knil
kb_checklists=viking_check
kb_reference=viking_ref
atc_id=B5563
ui_manufacturer=Vickers
ui_type=Type 55 'Viking' IV
ui_variation=KNIL
ui_typerole="reconnaissance amphibian"
ui_createdby="Brian Farrington & Leyland Spurr from an FS9 original by Ted Cook"
description=Exported to the Royal Dutch East Indies Air Force in 1922. Length: 34 ft 0 in  Wingspan: 50 ft 0 in   Height: 15 ft 1 in  Wing area: 639 ft²  Empty weight: 3,750 lb  Loaded weight: 5,6000 lb  Powerplant: 1× Napier 'Lion', 450 hp.
atc_heavy=0
atc_airline=
atc_flight_number=



[General]
atc_type=Vickers
atc_model=Viking
editable=1
performance=Range: 450 mi  Service ceiling: 9,000 ft  Rate of climb: 400 ft/min.
category=airplane


[WEIGHT_AND_BALANCE]
max_gross_weight =5600.0
empty_weight =3750.0

reference_datum_position     =   0.0, 0.0, 0.0
empty_weight_CG_position    = -1.5, 0.0, 0.0

max_number_of_stations =0

;Moments of Inertia
empty_weight_pitch_MOI  	=5852.0
empty_weight_roll_MOI   	=5013.0
empty_weight_yaw_MOI    	=9427.0
empty_weight_coupled_MOI	=0.0

[flight_tuning]
cruise_lift_scalar     	=1.0
parasite_drag_scalar   	=1.3
induced_drag_scalar    	=1.0
elevator_effectiveness 	=0.3
aileron_effectiveness  	=1.2
rudder_effectiveness   	=1.2
pitch_stability        	=2.5
roll_stability         		=2.5
yaw_stability          	=2.5
elevator_trim_effectiveness	=1.0
aileron_trim_effectiveness  	=1.0
rudder_trim_effectiveness   	=1.0
hi_alpha_on_roll		=1.0
hi_alpha_on_yaw		=1.0
p_factor_on_yaw		=0.5
torque_on_roll		=1.0
gyro_precession_on_roll	=1.0
gyro_precession_on_yaw	=1.0

[GeneralEngineData]
engine_type 	=0
Engine.0 		=-4.24, 0.00, 4.24
fuel_flow_scalar 	=1.55
min_throttle_limit	=0.1

[piston_engine]
power_scalar 		=1.0
cylinder_displacement	=121.8
compression_ratio		=   5.8
number_of_cylinders	= 12
max_rated_rpm		=2250.0
max_rated_hp		= 450.0
fuel_metering_type		=1
cooling_type		=1
normalized_starter_torque	=0.04332

turbocharged=0
max_design_mp=0
min_design_mp=0
critical_altitude=0
emergency_boost_type=0
emergency_boost_mp_offset=0
emergency_boost_gain_offset=0
fuel_air_auto_mixture=0
auto_ignition=0
emergency_boost_duration=0.0

max_rpm_mechanical_efficiency_scalar=1.0
idle_rpm_mechanical_efficiency_scalar=1.0
max_rpm_friction_scalar=1.0
idle_rpm_friction_scalar=1.0

BestPowerSpecificFuelConsumption=0.5
detonation_onset=38.5

[propeller]
thrust_scalar 		=1.0
propeller_type		=1
propeller_diameter		= 9.3
propeller_blades		= 4
propeller_moi		=27.4
gear_reduction_ratio	= 1.52
fixed_pitch_beta		=17.0
low_speed_theory_limit	=80.0

beta_max=0
beta_min=0
min_gov_rpm=0.0
prop_tc=0.0
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.0
beta_feather=0.0
power_absorbed_cf=0.0
defeathering_accumulators_available=0 
prop_reverse_available=0
minimum_on_ground_beta=0.0
minimum_reverse_beta=0.0

[contact_points]
max_number_of_points	=20

;Rem.....0.........1.......2......3.......4.....5....6.....7.....8.....9....10.....11..12..13
point.0= 1,   -12.5,    0.0, -5.5,   3200, 0, 0.3, 50.0, 0.2, 1.7, 0.90, 0.0, 0.0, 0	// GEAR
point.1= 1,      1.4,   -3.4, -6.5,   3200, 1, 1.6,  0.0, 0.4, 1.7, 0.85, 4.0, 4.0, 2
point.2= 1,      1.4,    3.4, -6.5,   3200, 2, 1.6,  0.0, 0.4, 1.7, 0.85, 4.0, 4.0, 3

point.3= 2,      0.0, -25.0,   0.0,   3200, 0, 0.0,  0.0, 0.0, 0.0, 0.00, 0.0, 0.0, 5	// SCRAPES
point.4= 2,      0.0,  25.0,   0.0,   3200, 0, 0.0,  0.0, 0.0, 0.0, 0.00, 0.0, 0.0, 6
point.5= 2,     12.7,   0.0,   1.3,   3200, 0, 0.0,  0.0, 0.0, 0.0, 0.00, 0.0, 0.0, 4

point.6= 4,      0.0, -20.0, -3.5, 10000, 0, 0.0,  0.0, 1.0, 1.0, 0.90, 0.0, 0.0, 1	// FLOATS
point.7= 4,      0.0,   20.0, -3.5, 10000, 0, 0.0,  0.0, 1.0, 1.0, 0.90, 0.0, 0.0, 1
point.8= 4,     -3.0, -20.0, -3.5, 10000, 0, 0.0,  0.0, 1.0, 1.0, 0.90, 0.0, 0.0, 1
point.9= 4,     -3.0,  20.0, -3.5, 10000, 0, 0.0,  0.0, 1.0, 1.0, 0.90, 0.0, 0.0, 1

point.10= 4,   10.7,    0.0, -3.9, 10000, 0, 0.0,  0.0, 1.0, 1.0, 0.90, 0.0, 0.0, 1	// PONTOON
point.11= 4,    7.8,   -2.8, -3.8, 10000, 0, 0.0,  0.0, 1.0, 1.0, 0.90, 0.0, 0.0, 1
point.12= 4,    7.8,    2.8, -3.8, 10000, 0, 0.0,  0.0, 1.0, 1.0, 0.90, 0.0, 0.0, 1
point.13= 4,    0.0,   -3.0, -5.0, 10000, 0, 0.0,  0.0, 1.0, 1.0, 0.90, 0.0, 0.0, 1
point.14= 4,    0.0,    3.0, -5.0, 10000, 0, 0.0,  0.0, 1.0, 1.0, 0.90, 0.0, 0.0, 2
point.15= 4, -12.7,   -1.7, -4.2, 10000, 0, 0.0,  0.0, 1.0, 1.0, 0.90, 0.0, 0.0, 3
point.16= 4, -12.7,    1.7, -4.2, 10000, 0, 0.0,  0.0, 1.0, 1.0, 0.90, 0.0, 0.0, 3

point.17= 5, -12.700, 0.0, -6.2, 10000, 0, 0.0, 50.0, 0.0, 0.0, 0.05, 0.1, 0.1, 0	// RUDDER

static_pitch 	= 3.0
static_cg_height	= 6.5
gear_system_type	= 3
tailwheel_lock	= 0

[brakes]
toe_brakes_scale=0.500
parking_brake=1
auto_brakes=0
hydraulic_system_scalar=0.0
differential_braking_scale=0.5

[gear_warning_system]
gear_warning_available=0

[hydraulic_system]
normal_pressure=0.0

[stall_warning]
type=1
stick_shaker=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[electrical]
max_battery_voltage 		= 24.0
generator_alternator_voltage 	= 28.0
max_generator_alternator_amps 	= 60.0

[pitot_static]
vertical_speed_time_constant = 1.0              //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=0.000000

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

[Views]
eyepoint = 3.7, 0, -0.1   //Longitudinal, Lateral, Vertical (feet)

[LIGHTS]
//Types:  4=cockpit.
light.0 = 4,  4.0,   0.00, -0.45, fx_vclight,

[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

[fuel]
fuel_type =1
number_of_tank_selectors =1                    
electric_pump=0
LeftMain  = -1.7, -7.03, 8.05, 53.0, 0.0
RightMain = -1.7,  7.03, 8.05, 53.0, 0.0
fuel_dump_rate=0.02
anemometer_pump=0
engine_driven_pump=1
manual_pump=0

[EFFECTS]
wake=fx_wake_s
water=fx_spray
//water=fx_bobspray2
dirt=fx_tchdrt
concrete=fx_dummy
touchdown=fx_tchdwn_s, 1
startup=fx_engstrt_jenny

[airplane_geometry]
wing_area               	=639.0
wing_span               	=50.0
wing_root_chord         	= 6.78
wing_dihedral           	= 5.0
wing_incidence          	= 0.0
wing_twist              	= 0.0
oswald_efficiency_factor	= 0.8
wing_winglets_flag      	= 0
wing_sweep              	= 0.0
wing_pos_apex_lon       	= 2.5
wing_pos_apex_vert      	= 2.97

htail_area            	=  37.84
htail_span           	=  11.0
htail_pos_lon        	=-19.02
htail_pos_vert      	=   1.7
htail_incidence     	=   0.0
htail_sweep         	=   0.0

vtail_area           	=  10.1
vtail_span           	=   6.08
vtail_sweep          =   0.0
vtail_pos_lon        	=-18.0
vtail_pos_vert      	=   2.2

elevator_area      	= 22.72
aileron_area         	= 96.0
rudder_area         	= 15.42

elevator_up_limit  	= 20.0
elevator_down_limit= 20.0
aileron_up_limit     	= 18.0
aileron_down_limit 	= 14.0
rudder_limit          = 30.0
elevator_trim_limit = 15.0

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
spoiler_extension_time=0.0
spoiler_handle_available=0
auto_spoiler_available=0
positive_g_limit_flaps_up=4.7
negative_g_limit_flaps_up=-3.76
positive_g_limit_flaps_down=3.29
negative_g_limit_flaps_down=-2.82
load_safety_factor=1.0

[Reference Speeds]
flaps_up_stall_speed  =  39.0
full_flaps_stall_speed =  39.0
cruise_speed            =  78.0
max_indicated_speed = 150.0

[autopilot]
autopilot_available=0
flight_director_available=0

[forcefeedback]
stick_shaker_magnitude=5000
stick_shaker_direction=0
stick_shaker_period=111111
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=500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1
crash_magnitude1=10000
crash_direction1=1000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000

[AirWrench]
Aircraft_Length=33.90000
nose_position_lon=12.70000
[Flaps.0]
type=1
span-outboard=0.500000
extending-time=0.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=30.000000,0.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=0.150000
[deice_system]
structural_deice_type=0