[fltsim.0]
title=Piper Seminole panel 16x9
sim=pipsem
model=
panel=16x9
sound=
texture=
kb_checklists=pipsem_check
kb_reference=pipsem_ref
atc_id=PH-VKA
ui_manufacturer=Piper
ui_type=Seminole
ui_variation=panel 16x9
description=The Seminole is widely used as a twin trainer.
[fltsim.1]
title=Piper Seminole panel 4x3
sim=pipsem
model=
panel=4x3
sound=
texture=
kb_checklists=pipsem_check
kb_reference=pipsem_ref
atc_id=PH-VKA
ui_manufacturer=Piper
ui_type=Seminole
ui_variation=panel 4x3
description=The Seminole is widely used as a twin trainer.
[fltsim.2]
title=Piper Seminole panel 4x3 IFR
sim=pipsem
model=
panel=4x3 IFR
sound=
texture=
kb_checklists=pipsem_check
kb_reference=pipsem_ref
atc_id=PH-VKA
ui_manufacturer=Piper
ui_type=Seminole
ui_variation=panel 4x3 IFR
description=The Seminole is widely used as a twin trainer.
[fltsim.3]
title=Piper Seminole panel 16x9 IFR
sim=pipsem
model=
panel=16x9 IFR
sound=
texture=
kb_checklists=pipsem_check
kb_reference=pipsem_ref
atc_id=PH-VKA
ui_manufacturer=Piper
ui_type=Seminole
ui_variation=panel 16x9 IFR
description=The Seminole is widely used as a twin trainer.
[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 =0.65
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=30
HeadingPanRate=75
PanAcceleratorTime=0
HotKeySelect=1
InitialXyz=0, 0.05, -0.2
InitialPbh=10, 0, 0
//lateral-vertical-longitudinal, in meters
[CameraDefinition.002]
Title = "Flap-Trims-Fuelselectors"
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, -0.30, 0.05
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, -0.3
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=Seminole
atc_model=
editable=1
performance=Cruise Speed: 158 kt\nCeiling: 15,000 ft\n
Category=airplane
[WEIGHT_AND_BALANCE]
max_gross_weight = 3800 // (pounds)
empty_weight = 2615 // (pounds)
reference_datum_position= 4.0, 0.0, 0.0
empty_weight_CG_position= -4.0, 0.0, 0.0
max_number_of_stations= 5
station_load.0= 170.0, -4.350, -0.800, -0.045
station_load.1= 170.0, -4.350, 0.800, -0.045
station_load.2= 0.0, -6.600, -0.800, -0.045 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3= 0.0, -6.600, 0.800, -0.045 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4= 0.0, -9.0, 0.0, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.0 = "Pilot"
station_name.1 = "Co-Pilot"
station_name.2 = "Passenger"
station_name.3 = "Passenger"
station_name.4 = "Passenger"
;Moments of Inertia
empty_weight_pitch_MOI = 3905.65
empty_weight_roll_MOI = 2718.64
empty_weight_yaw_MOI = 5291.04
empty_weight_coupled_MOI= 0.0
[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
[GeneralEngineData]
engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 2, -11.3, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 =2, 11.3, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 0.70 //Fuel flow scalar
min_throttle_limit=-0.250000
[piston_engine]
power_scalar = 1.0 //Piston power scalar
cylinder_displacement= 90.0 //Cubic inches per cylinder
compression_ratio= 8.5 //Compression ratio
number_of_cylinders= 4 //Number of cylinders
max_rated_rpm= 2700.0 //Max rated RPM
max_rated_hp= 180.0 //Max rated HP
fuel_metering_type= 1 //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter
cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 1 //Starter torque factor
turbocharged= 0 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 0.0 //Max design manifold pressure, (inHg)
min_design_mp= 0.0 //Min design manifold pressure, (inHg)
critical_altitude= 0.0 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0.0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0.0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 1.1 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.2 //Scalar on idle RPM friction
[propeller]
thrust_scalar = 0.75 //Propeller thrust scalar
propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 6.1 //Propeller Diameter, (feet)
propeller_blades= 3 //Number of propeller blades
propeller_moi= 3 //Propeller moment of inertia
beta_max= 31 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 14 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1100.0 //Miminum governed RPM
prop_tc= 0.1 //Prop time-constant
gear_reduction_ratio= 1.0 //Propeller gear reduction ratio
fixed_pitch_beta= 0.0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit= 80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available= 0 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available= 0 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 1 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available=1 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather= 700.0 //Minimum RPM for prop feathering
beta_feather= 82.5 //Feathering pitch angle (degrees)
power_absorbed_cf= 0.9 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available= 0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta= 0.0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0.0 //Minimum pitch angle in reverse, (degrees)
rotation=1,1
[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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
//GEAR
point.0 = 1, 1.86, 0.00, -3.30, 1600, 0, 0.633, 40, 0.17, 2.5, 0.90, 4.0, 4.0, 0, 152, 180
point.1 = 1, -5.73, -5.14, -3.40, 3500, 1, 0.886, 0, 0.50, 2.5, 0.85, 4.0, 4.0, 2, 152, 200
point.2 = 1, -5.73, 5.14, -3.40, 3500, 2, 0.886, 0, 0.50, 2.5, 0.85, 4.0, 4.0, 3, 152, 200
static_pitch = 0.5 //Degrees
static_cg_height = 2.95 //Feet
gear_system_type=0
[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 = 31.5 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.0 //Brake scalar
auto_brakes = 0
[hydraulic_system]
normal_pressure = 0.0 //PSI
[flaps.0]
type = 1 // 1 - trail, 2 - lead
span-outboard = 0.41 // 0.0 .. 1.0
extending-time = 0.1 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 15 // degrees
flaps-position.2 = 30 // degrees
flaps-position.2 = 40
damaging-speed = 110 // KIAS
blowout-speed = 170 // KIAS
[electrical]
max_battery_voltage = 12.0
generator_alternator_voltage = 14.0
max_generator_alternator_amps = 80.0
;BusType, MaxAmpLoad, MinVoltage ;BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
gear_motor = 0, 10, 9.0
autopilot = 0, 10 , 9.0
avionics_bus = 0, 10 , 9.0
avionics = 1, 10 , 9.0
pitot_heat = 0, 4 , 9.0
additional_system = 0, 4 , 9.0
marker_beacon = 1, 4 , 9.0
gear_warning = 0, 4 , 9.0
fuel_pump =4, 10 , 9.0
light_nav = 4, 10 , 9.0
light_landing = 4, 10 , 9.0
light_strobe = 4, 10 , 9.0
light_panel = 4, 10 , 9.0
[pitot_static]
vertical_speed_time_constant = 0.3 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000
[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
[Views]
eyepoint= -4.408, -0.815, 2.189 //(feet) longitudinal, lateral, vertical distance from reference datum
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 2, -5.894, -19.728, 1.109, fx_strobeh
light.1 = 2, -5.894, 19.728, 1.109, fx_strobeh
light.2 = 4, -4.428, -0.421, 2.802, fx_vclight
light.3 = 3, -5.651, -19.605, 1.112, fx_navred3
light.4 = 3, -5.651, 19.605, 1.112, fx_navgre3
light.5 = 3, -22.517, 0.000, 5.696, 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 = 150, 250
aileron = 150, 250
rudder = 150, 250
[altimeters]
altimeter.0=1
[airspeed_indicators]
airspeed_indicator.0=1
[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
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,1 //Turn and Bank
[vacuum_system]
max_pressure=5.15
vacuum_type=1
electric_backup_pressure=4.9
engine_map=1,1
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.00000
[fuel]
LeftMain = -5.2, 6.500, 0.850, 54.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -5.2, -6.500, 0.850, 54.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 2
electric_pump=1
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
[airplane_geometry]
wing_area = 183.8 //Square feet
wing_span = 38.6 //Feet
wing_root_chord = 5.3 //Feet
wing_dihedral = 6.9 //Degrees
wing_incidence = 2.5 //Degrees (2.5)
wing_twist = -1.5 //Degrees
oswald_efficiency_factor= 0.6 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 0.0 //Degrees, wing leading edge
wing_pos_apex_lon = -5.6 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_area = 60.0 //Square feet
htail_span = 15.9 //Feet
htail_pos_lon = -20.1 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence = 2.0 //Degrees
htail_sweep = 0.0 //Degrees, horizontal tail leading edge
vtail_area = 88.0 //Square feet
vtail_span = 10.7 //Feet, tip to body
vtail_sweep = 0.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -22.9 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 3.1 //Feet, vertical distance from reference point, positive going up
elevator_area = 20.0 //Square feet
aileron_area = 11.3 //Square feet
rudder_area = 10.5 //Square feet
elevator_up_limit = 17.0 //Degrees
elevator_down_limit = 15.5 //Degrees
aileron_up_limit = 18.0 //Degrees
aileron_down_limit = 18.0 //Degrees
rudder_limit = 20.0 //Degrees
elevator_trim_limit = 15.0 //Degrees
spoiler_limit = 0.0 //Degrees
spoilerons_available = 0 //Spoilerons Available?
aileron_to_spoileron_gain = 0 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
auto_spoiler_available=0
positive_g_limit_flaps_up=3.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-2.000000
negative_g_limit_flaps_down=-2.000000
[Reference Speeds]
flaps_up_stall_speed = 58.0 //Knots True (KTAS)
full_flaps_stall_speed =55.0 //Knots True (KTAS)
cruise_speed = 140.0 //Knots True (KTAS)
max_indicated_speed=200.0
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 700.0
autothrottle_available= 0
pitch_takeoff_ga=8.000000
use_no_default_bank=1
default_bank_mode=0
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
[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
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=9000 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=27000 ; 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
[stall_warning]
type=1
stick_shaker=0
[attitude_indicators]
[deice_system]
structural_deice_type=0 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots
