[fltsim.0]
title=Valmet L-70 Vinka
sim=Valmet L-70 Vinka
model=one
panel=
sound=
texture=
kb_checklists=Valmet L-70 Vinka_check
kb_reference=Valmet L-70 Vinka_ref
atc_id_enable=0
atc_id=
ui_manufacturer=Valmet
ui_type=LEKO-70 Prototype
ui_variation=One pilot
visual_damage=1
description=Valmet L-70 Vinka is a Finnish three place basic training plane. It has 200 hp. Lycoming engine which gives the plane a 200 km\/h travelling speed and 3000 m max, altitude. Prototypes, Leko-70, first flight was in 1975 and first serial built Vinka flew in December 29, 1979. Finnish Air Force has used the plane since 1980.\n
atc_heavy=0
atc_airline=Valmet
atc_flight_number=F91

[fltsim.1]
title=Valmet L-70 Vinka2
sim=Valmet L-70 Vinka
model=two
panel=
sound=
texture=
kb_checklists=Valmet L-70 Vinka_check
kb_reference=Valmet L-70 Vinka_ref
atc_id_enable=0
atc_id=
ui_manufacturer=Valmet
ui_type=LEKO-70 Prototype
ui_variation=Two pilots
visual_damage=1
description=Valmet L-70 Vinka is a Finnish three place basic training plane. It has 200 hp. Lycoming engine which gives the plane a 200 km\/h travelling speed and 3000 m max, altitude. Prototypes, Leko-70, first flight was in 1975 and first serial built Vinka flew in December 29, 1979. Finnish Air Force has used the plane since 1980.\n
atc_heavy=0
atc_airline=Valmet
atc_flight_number=F92

[fltsim.2]
title=Valmet L-70 Vinka VN10
sim=Valmet L-70 Vinka
model=one
panel=
sound=
texture=1
kb_checklists=Valmet L-70 Vinka_check
kb_reference=Valmet L-70 Vinka_ref
atc_id_enable=0
atc_id=
ui_manufacturer=Valmet
ui_type=L-70 Vinka VN-10
ui_variation=One pilot
visual_damage=1
description=Valmet L-70 Vinka is a Finnish three place basic training plane. It has 200 hp. Lycoming engine which gives the plane a 200 km\/h travelling speed and 3000 m max, altitude. Prototypes, Leko-70, first flight was in 1975 and first serial built Vinka flew in December 29, 1979. Finnish Air Force has used the plane since 1980.\n
atc_heavy=0
atc_airline=Valmet
atc_flight_number=Q45

[fltsim.3]
title=Valmet L-70 Vinka2 VN10
sim=Valmet L-70 Vinka
model=two
panel=
sound=
texture=1
kb_checklists=Valmet L-70 Vinka_check
kb_reference=Valmet L-70 Vinka_ref
atc_id_enable=0
atc_id=
ui_manufacturer=Valmet
ui_type=L-70 Vinka VN-10
ui_variation=Two pilots
visual_damage=1
description=Valmet L-70 Vinka is a Finnish three place basic training plane. It has 200 hp. Lycoming engine which gives the plane a 200 km\/h travelling speed and 3000 m max, altitude. Prototypes, Leko-70, first flight was in 1975 and first serial built Vinka flew in December 29, 1979. Finnish Air Force has used the plane since 1980.\n
atc_heavy=0
atc_airline=Valmet
atc_flight_number=Q46

[General]
atc_type=Ilmavoimat
atc_model=AA1
editable=0
performance=LENGHT: 7,50 m\nWINGSPAN: 9,36 m\nMAX WEIGHT: 1250 kg\nENGINE: Lycoming AEIO-360-A1B6 200 hp.\nCOMBAT RADIUS: 680 km\nDesigner: Mikko Maliniemi\nE-mail: mmniemi@hotmail.com\nFlight Dynamics: Kari Virtanen\nE-mail: kari.virtanen@dlc.fi\nDate: June, 2003\n

[WEIGHT_AND_BALANCE]
empty_weight = 1922
max_gross_weight= 2293.000
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.026000,0.000000,0.000000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
station_load.1=0.000000,0.500000,1.500000,0.000000

;Moments of Inertia
empty_weight_pitch_MOI  = 1077
empty_weight_roll_MOI  = 748
empty_weight_yaw_MOI  = 1660
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=1.000
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

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing 6=taxi, 7=recognition, 8=wing, 9=logo
light.0=3,  0.75, -14.77, 0.52, fx_navred
light.1=3,  0.75,  14.77, 0.52, fx_navgre
light.2=3,  -14.21,   0.00, 0.60, fx_navwhi
light.3=1, -13.18,   0.00, 6.00, fx_beacon_vinka
light.4=2,  1.14,   0.00, 0.50, fx_vclight_vinka
light.5=9,  1.14,   0.00, 0.50, fx_vclight_vinka2

[SMOKESYSTEM]
smoke.1=0.00, 2.70, 14.40, fx_smoke_w_s
smoke.2=0.00, 2.70, -14.40, fx_smoke_w_s

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

[fuel]
LeftMain=-0.10000,-1.100000,0.886000,22.98,0.792516
RightMain=-0.10000,1.100000,0.866000,22.98,0.792516
fuel_type=1.000000
number_of_tank_selectors=1

[GeneralEngineData]
engine_type= 0
Engine.0= 5.300, 0.000, 0.000
fuel_flow_scalar= 1.330

[piston_engine]
power_scalar=1.000
cylinder_displacement= 90.300
compression_ratio= 8.500
number_of_cylinders= 4
max_rated_rpm= 2640.000
max_rated_hp= 200.000
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque= 1.200
turbocharged= 0
max_design_mp= 0.000
min_design_mp= 0.000
critical_altitude= 12000.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 0
auto_ignition= 0
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.180
idle_rpm_friction_scalar=0.800

[propeller]
thrust_scalar=1.000
propeller_type=0
propeller_diameter=6.300
propeller_blades=2
propeller_moi=2.400
beta_max=28.000
beta_min=13.000
min_gov_rpm=800.000
prop_tc=0.100
gear_reduction_ratio=1.000
fixed_pitch_beta=20.000
low_speed_theory_limit=80.000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000
beta_feather=0.000
power_absorbed_cf=0.000
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=0.000
minimum_reverse_beta=0.000

[airplane_geometry]
wing_area= 155.000
wing_span= 31.600
wing_root_chord= 5.017
wing_dihedral= 6.000
wing_incidence= 2.000	//2
wing_twist= -0.300		//6
oswald_efficiency_factor= 0.700
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 1.254 	//0.886
wing_pos_apex_vert= 0.0
htail_area= 18.040
htail_span= 11.760
htail_pos_lon= -13.750
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 0.000
vtail_area= 8.320
vtail_span= 5.080
vtail_sweep= 30.000
vtail_pos_lon= -13.390
vtail_pos_vert= 0.390
elevator_area= 13.720
aileron_area= 14.400
rudder_area= 9.590
elevator_up_limit= 35.000
elevator_down_limit= 34.000
aileron_up_limit= 30.000
aileron_down_limit= 22.000
rudder_limit= 26.000
elevator_trim_limit= 16.500
spoiler_limit= 0.000
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000

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

[contact_points]
point.0=1.000000,4.250000,0.000000,-4.10000,1600.000000,0.000000,0.633333,34.080000,0.30,1.500000,0.912718,0.000000,0.000000,0.000000,0.000000,0.000000
point.1=1.000000,-1.270000,-4.180000,-3.940000,3500.000000,1.000000,0.800000,0.000000,0.35,1.500000,0.912718,0.000000,0.000000,2.000000,0.000000,0.000000
point.2=1.000000,-1.270000,4.180000,-3.940000,3500.000000,2.000000,0.800000,0.000000,0.35,1.500000,0.912718,0.000000,0.000000,3.000000,0.000000,0.000000
point.3=2.000000,0.000000,-16.416667,0.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,0.000000,16.416667,0.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-15.666667,0.000000,0.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,7.666667,0.000000,-1.333333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
point.7=2.000000,-15.666667,0.000000,6.833333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,7.000000,0.000000,0.000000
point.8=2.000000,1.000000,0.000000,-2.166667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,8.000000,0.000000,0.000000
static_pitch=3
static_cg_height=3.502809

max_number_of_points=21

[Views]
eyepoint=-0.7,-0.7,1.7

[Reference Speeds]
flaps_up_stall_speed= 58.000
full_flaps_stall_speed= 46.400
cruise_speed= 106.200

[keyboard_response]
elevator=100.0, 180.0
aileron=200.0, 1000.0
rudder=200.0, 1000.0

[autopilot]
autopilot_available=0
flight_director_available=0
default_vertical_speed=700.0
autothrottle_available=0
pitch_takeoff_ga=8.000000
use_no_default_bank=0
use_no_default_pitch=0

[Radios]
Audio.1=1
Com.1=1, 1
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 1
Adf.1=1
Adf.2=1
Transponder.1=1
Marker.1=1

[forcefeedback]
stick_shaker_magnitude=5000
stick_shaker_direction=0
stick_shaker_period=111111
gear_bump_nose_magnitude=6000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=6000           ; 0 - 10000
gear_bump_left_direction=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=6000          ; 0 - 10000
gear_bump_right_direction=00500         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=3250            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750             ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
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

[direction_indicators]
direction_indicator.0=1,0

[pitot_static]
vertical_speed_time_constant=2.0

[Flaps.0]
type= 1
span-outboard=0.000
extending-time=8.000
system_type=0
damaging-speed=108.000
blowout-speed=125.000
lift_scalar=1.000
drag_scalar=1.000
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=15.000, 0.000
flaps-position.2=45.000, 0.000

[folding_wings]
wing_fold_system_type = 4
fold_rates = 1.0, 1.0