[fltsim.0]
title=Piper Warrior-II_nwf_panel_4x3
sim=Piper Warrior-II_nwf
model=nwf
panel=4x3
sound=
texture=
kb_checklists=
kb_reference=
ui_manufacturer=PIPER
ui_type=Warrior-II
ui_variation=Warrior-II_nwf_panel_4x3
description=Flight dynamics derived from FS X Cessna 172, adapted by Rien Cornelissen to match Warrior flight characteristics as closely as possible.
atc_id=PH-SVG
atc_id_color=0x0xffffffff
atc_id_font=Arial,-28,1,1000,1
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.1]
title=Piper Warrior-II_wwf_panel_4x3
sim=Piper Warrior-II_wwf
model=wwf
panel=4x3
sound=
texture=
kb_checklists=
kb_reference=
ui_manufacturer=PIPER
ui_type=Warrior-II
ui_variation=Warrior-II_wwf_panel_4x3
description=Flight dynamics derived from FS X Cessna 172, adapted by Rien Cornelissen to match Warrior flight characteristics as closely as possible.
atc_id=PH-SVG
atc_id_color=0xffffffff
atc_id_font=Arial,-28,1,1000,1
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.2]
title=Piper Warrior-II_nwf_panel_16x9
sim=Piper Warrior-II_nwf
model=nwf
panel=16x9
sound=
texture=
kb_checklists=
kb_reference=
ui_manufacturer=PIPER
ui_type=Warrior-II
ui_variation=Warrior-II_nwf_panel_16x9
description=Flight dynamics derived from FS X Cessna 172, adapted by Rien Cornelissen to match Warrior flight characteristics as closely as possible.
atc_id=PH-SVG
atc_id_color=0xffffffff
atc_id_font=Arial,-28,1,1000,1
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.3]
title=Piper Warrior-II_wwf_panel_16x9
sim=Piper Warrior-II_wwf
model=wwf
panel=16x9
sound=
texture=
kb_checklists=
kb_reference=
ui_manufacturer=PIPER
ui_type=Warrior-II
ui_variation=Warrior-II_wwf_panel_16x9
description=Flight dynamics derived from FS X Cessna 172, adapted by Rien Cornelissen to match Warrior flight characteristics as closely as possible.
atc_id=PH-SVG
atc_id_color=0xffffffff
atc_id_font=Arial,-28,1,1000,1
atc_heavy=0
atc_airline=
atc_flight_number=
[CameraDefinition.0]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = 10, 0.75, 0
InitialPbh = 5, 0, 270
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum
[CameraDefinition.1]
Title = "Left Wing"
Guid = {3A09FD6C-D406-4d8f-A5CD-FA4F5E0C12ED}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = -10, 0.75, 0
InitialPbh = 5, 0, 90
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum
[CameraDefinition.2]
Title = "Tail"
Guid = {D8D67955-2E9B-4e75-A5CE-8EFFBBFAC64A}
Description = Looking forward from the tip of the vertical stabilizer
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.75
ShowWeather = Yes
InitialXyz = 0, 1.9, -10
InitialPbh = 11, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.001]
Title = "Virtual Cockpit - 2"
Guid = {195EAB58-9E4A-0E2A-B34C-A8D9D948F078}
Description = This is the description of the virtual cockpit view.
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = True
PanPbhAdjust = Swivel
PanPbhReturn = True
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = 0.90
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=30
HeadingPanRate=75
PanAcceleratorTime=0
HotKeySelect=1
InitialXyz=0.03, 0.05, -0.2
InitialPbh=8, 0, 0
//lateral-vertical-longitudinal, in meters
[CameraDefinition.002]
Title = "Flap-Trims-Fuelselector"
Guid = {195EAB58-9E4A-1E2A-C34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = True
PanPbhAdjust = Swivel
PanPbhReturn =True
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.30
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.2, 0.1, 0.5
InitialPbh=90, 0, 0
[CameraDefinition.003]
Title = "Radio Stack"
Guid = {195EAB58-9E4A-2E2A-D34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = True
PanPbhAdjust = Swivel
PanPbhReturn = True
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.2
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.5, -0.1, 0.0
InitialPbh=12, 0, 0
[CameraDefinition.004]
Title = "Right Seat"
Guid = {195EAB58-9E4A-3F3B-E34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = True
PanPbhAdjust = Swivel
PanPbhReturn = True
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = 1.00
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.5, 0.0, 0.0
InitialPbh=2.0, 0.0, 0.0
//lateral-vertical-longitudinal, in meters
[General]
atc_type=PIPER
atc_model=Warrior
editable=1
performance=Maximum Speed\t126 kts \nCruise Speed\t104 kts \nPropeller\t\t Fixed Pitch\n\t\tTwo-Bladed\nMaximum Range\t730 nm \nService Ceiling\t13,000 ft\t \nFuel Capacity\t50 gal\t \nEmpty Weight\t1,541 lb\\n\nMax. Gross Weight\t2,440 lb\t \nLength\t\t23 ft, 9.6 in\nWingspan\t35 ft \t \nHeight\t\t7 ft, 3.6 in\t \nSeating\t \t 4\n
Category=airplane
[WEIGHT_AND_BALANCE]
max_gross_weight= 2440.000
empty_weight= 1541.000
reference_datum_position= 3.6, 0.0, 0.0
empty_weight_CG_position= -3.0, 0.0, 0.0
max_number_of_stations=5
station_load.0= 170, -3, -1.5, 0.0
station_load.1= 170, -3, 1.5, 0.0
station_load.2= 0, -6.2, -1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3= 0, -6.2, 1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4= 0, -8.0, 0.0, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI= 1400.000
empty_weight_roll_MOI= 1137.000
empty_weight_yaw_MOI= 2360.000
empty_weight_coupled_MOI= 0.000
;CG_forward_limit= 1.500
;CG_aft_limit= -1.000
[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=0.5
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[GeneralEngineData]
engine_type= 0
Engine.0= 7.000, 0.800, 0.000
fuel_flow_scalar= 0.800
min_throttle_limit=0.000000
[piston_engine]
power_scalar=1.0 //Piston power scalar
cylinder_displacement= 80.000
compression_ratio= 8.500
number_of_cylinders= 4
max_rated_rpm= 2700.000
max_rated_hp= 160.000
fuel_metering_type= 1
cooling_type= 0
normalized_starter_torque= 1
turbocharged= 0
max_design_mp= 0.000
min_design_mp= 0.000
critical_altitude= 0.000
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=1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar=1.2 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar=1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar=1.0 //Scalar on idle RPM friction
[propeller]
thrust_scalar=1.0 //Propeller thrust scalar
propeller_type= 1
propeller_diameter= 5.675
propeller_blades= 2
propeller_moi= 3
beta_max= 0.000
beta_min= 0.000
min_gov_rpm= 0.000
prop_tc= 0.000
gear_reduction_ratio= 1.000
fixed_pitch_beta= 24.500
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= 0.000
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
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
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
flap_motor=0, 0 , 17.0
[contact_points]
//0 Class
//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
point.0 = 1, 0.90, 0.00, -3.15, 1500, 0, 0.5, 22.0, 0.25,2.5, 0.7, 0.0, 0.0, 0
point.1 = 1, -4.70, -4.50, -3.1, 3500, 1, 0.5, 0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 2
point.2 = 1, -4.70, 4.50, -3.1, 3500, 2, 0.5, 0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 3
point.3 = 2, -3.90, -18.0, 3.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5
point.4 = 2, -3.90 18.0, 3.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6
point.5= 2,-20.23, 0.0, 0.30, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9
point.6= 2, 1.48, 0.0, -2.17, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4
point.7= 2,-22.80, 0.0, 5.83, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7
point.8= 2, -4.90, 0.0, -2.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 8
max_number_of_points=21
static_pitch= 2.0
static_cg_height= 2.760
gear_system_type=0
[Views]
eyepoint=-4.6, -0.85, 2.0 //(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
light.0 = 1, -17.788, 0.00, 5.329, fx_beacon
light.1 = 1, -17.788, 0.00, 5.329, fx_beacon
light.2 = 2, -5.659, -17.758, 1.029, fx_strobeh
light.3 = 2, -5.659, 17.758, 1.029, fx_strobeh
light.4 = 4, -3.436, -0.925, 2.607, fx_vclight
light.5 = 3, -5.434, -17.672, 1.031, fx_navred3
light.6 = 3, -5.434, 17.672, 1.031, fx_navgre3
light.7 = 3, -5.857, -17.645, 1.009, fx_navwhi3
light.8 = 3, -5.857, 17.645, 1.009, fx_navwhi3
[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=100, 180
aileron=200, 1000
rudder=200, 1000
[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=1,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
LeftMain= -5.6,-5.100, -0.300, 25.000, 0.000
RightMain= -5.6, 5.100, -0.300, 25.000, 0.000
fuel_type=1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=1
[airplane_geometry]
wing_area= 169.000
wing_span= 35.000
wing_root_chord= 5.300
wing_dihedral= 6.000
wing_incidence= 1.5
wing_twist= -3.000
oswald_efficiency_factor= 0.75
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= -1.550
wing_pos_apex_vert= 1.000
htail_area= 39.000
htail_span= 13.000
htail_pos_lon= -14.300
htail_pos_vert= 0.000
htail_incidence=2.0
htail_sweep= 0.000
vtail_area= 18.000
vtail_span= 4.800
vtail_sweep= 40.000
vtail_pos_lon= -12.500
vtail_pos_vert= 2.500
elevator_area= 35.000
aileron_area= 18.300
rudder_area= 6.700
elevator_up_limit= 28.000
elevator_down_limit= 21.000
aileron_up_limit= 20.000
aileron_down_limit= 15.000
rudder_limit= 24.000
elevator_trim_limit= 19.500
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
auto_spoiler_available=0
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-1.500000
negative_g_limit_flaps_down=-1.500000
[Reference Speeds]
flaps_up_stall_speed= 55.000
full_flaps_stall_speed= 50.000
cruise_speed= 104.000
max_indicated_speed=160.000000
[autopilot]
default_bank_mode=1
default_pitch_mode=1
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.0
autothrottle_available=0
pitch_takeoff_ga=8.000000
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
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 1.000
system_type= 0
damaging-speed= 120.000
blowout-speed= 150.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 6.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 40.000, 0.000
[exits]
number_of_exits=2
exit_rate.0=0.2
[forcefeedback]
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
[brakes]
toe_brakes_scale=1.0
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[hydraulic_system]
normal_pressure=0.000000
[stall_warning]
type=1
stick_shaker=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[deice_system]
structural_deice_type=0
