[fltsim.0]
title = Ultimate N325GP
sim = Ultimate Bipe
model = 
panel = 
sound = 
texture = BLUEHAWK
kb_checklists = 
atc_id = N325GP
ui_manufacturer = ULTIMATE AIRCRAFT CORP.
ui_type = AEROBATIC
ui_variation = BLUEHAWK


[fltsim.1]
title = Ultimate OH-XSF
sim = Ultimate Bipe
model = 
panel = 
sound = 
texture = OH-XSF
kb_checklists = 
atc_id = OH-XSF
ui_manufacturer = ULTIMATE AIRCRAFT CORP.
ui_type = AEROBATIC
ui_variation = UNLIMITED F1

[fltsim.2]
title = Ultimate OH-XSF SHARK
sim = Ultimate Bipe
model = 
panel = 
sound = 
texture = OH-XSF SHARK
kb_checklists = 
atc_id = OH-XSF
ui_manufacturer = ULTIMATE AIRCRAFT CORP.
ui_type = AEROBATIC
ui_variation = SHARK

[fltsim.3]
title = Ultimate LABATT'S
sim = Ultimate Bipe
model = 
panel = 
sound = 
texture = LABATT'S
kb_checklists = 
atc_id = C_GILB
ui_manufacturer = ULTIMATE AIRCRAFT CORP.
ui_type = AEROBATIC
ui_variation = LABATT"S BLUE

[fltsim.4]
title = Ultimate N360JW
sim = Ultimate Bipe
model = 
panel = 
sound = 
texture = N360JW
kb_checklists = 
atc_id = N360JW
ui_manufacturer = ULTIMATE AIRCRAFT CORP.
ui_type = AEROBATIC
ui_variation = N360JW

[General]
atc_type = ULTIMATE
atc_model = 10-300s
prop_anim_ratio = 1.72
Category = airplane
editable = 0
performance = "Designed and  build by Gordon Price\n\nVisit http://moleski.net/ultbipe to learn more about this wonderful aerobatic aircraft\n"


[CameraDefinition.0]
Title = "Tail"
Guid = {D8D67955-2E9B-4e75-9D8B-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 = .5
ShowWeather = Yes
InitialXyz = 0, 2.0, -3.9
InitialPbh = 10, 0, 0
XyzAdjust = TRUE
Category = Aircraft
MomentumEffect = TRUE
ClipMode = Minimum

[CameraDefinition.0]
Title = "Tail"
Guid = {D8D67955-2E9B-4e75-9D8B-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 = .5
ShowWeather = Yes
InitialXyz = 0, 2.0, -3.9
InitialPbh = 10, 0, 0
XyzAdjust = TRUE
Category = Aircraft
MomentumEffect = TRUE
ClipMode = Minimum

[CameraDefinition.1]
Title = "Nose"
Guid = {8A1987D0-09B6-7E48-B4E1-62C5DBE2A720}
Description = Looking back from the nose of the engine toward the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 0, 1.1, 4.0
InitialPbh = 20, 0, 180
XyzAdjust = TRUE
Category = Aircraft
MomentumEffect = FALSE
ClipMode = Minimum

[CameraDefinition.2]
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 = 0.5
ShowWeather = Yes
InitialXyz = 5, 0.3, 0
InitialPbh = 0, 0, 270
XyzAdjust = TRUE
Category = Aircraft
MomentumEffect = FALSE
ClipMode = Minimum

[CameraDefinition.3]
Title = "Left Wing"
Guid = {7a91803e-898b-435a-8391-725be6a48203}
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 = 0.5
ShowWeather = Yes
InitialXyz = -5, 0.3, 0
InitialPbh = 0, 0, 90
XyzAdjust = TRUE
Category = Aircraft
MomentumEffect = FALSE
ClipMode = Minimum


[WEIGHT_AND_BALANCE]
max_gross_weight = 1250
empty_weight = 975

reference_datum_position = 0, 0, 0
empty_weight_CG_position = -0.0, 0, 0
CG_forward_limit = 0
CG_aft_limit = 0

max_number_of_stations = 13
station_load.0 = 140, -5.8,0, 1.0
station_load.2 = 0, 0, 0, 0


;Moments = of Inertia
empty_weight_pitch_MOI = 7400
empty_weight_roll_MOI = 500
empty_weight_yaw_MOI = 940
empty_weight_coupled_MOI = 0

[electrical]
max_battery_voltage = 12.0
generator_alternator_voltage = 13.8
max_generator_alternator_amps = 40.0

;BusType, = MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus = 0, 5 , 9.5
avionics = 1, 5 , 9.5
additional_system = 0, 2 , 9.5
marker_beacon = 1, 2 , 9.0
fuel_pump = 0, 5 , 9.0

[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 1.4
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
pitch_stability = 0.7
roll_stability = 0.95
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 = 0.5



[GeneralEngineData]
engine_type = 0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 3.5, 0.0, 0.60                       //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0                           //Fuel flow scalar
min_throttle_limit = 0.0               //Minimum percent throttle.  Generally negative for turbine reverser

[piston_engine]
power_scalar = 1.0                              //Piston power scalar
cylinder_displacement = 90                  //Cubic inches per cylinder
compression_ratio = 8.0                         //Compression ratio
number_of_cylinders = 6                           //Number of cylinders
max_rated_rpm = 2700                             //Max rated RPM
max_rated_hp = 300                               //Max rated HP
fuel_metering_type = 0                           //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type = 0                                 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque = 0.3                  //Starter torque factor
turbocharged =1                                //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp = 30                               //Max design manifold pressure, (inHg)
min_design_mp = 15                               //Min design manifold pressure, (inHg)
critical_altitude = 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                    //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset = 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 = 1.0       //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 = 1.0                   //Scalar on idle RPM friction
detonation_onset = 36

	
[propeller]
thrust_scalar = 1.0                             //Propeller thrust scalar
propeller_type = 0                               //0=Constant Speed, 1=Fixed Pitch
propeller_diameter = 7                        //Propeller Diameter, (feet)
propeller_blades = 3                             //Number of propeller blades
propeller_moi = 5.9                              //Propeller moment of inertia
beta_max = 34                                    //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min = 17                                    //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm = 1400                               //Miminum governed RPM
prop_tc = 0.1                                    //Prop time-constant
gear_reduction_ratio = 1.0                       //Propeller gear reduction ratio
fixed_pitch_beta = 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 = 0                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available = 0               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather = 0                          //Minimum RPM for prop feathering
beta_feather = 0                                 //Feathering pitch angle (degrees)
power_absorbed_cf = 0                            //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                       //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta = 0                         //Minimum pitch angle in reverse, (degrees)



//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

[contact_points]
max_number_of_points = 7
point.0 = 1, -14, 0, -3.45, 8000.0, 0.0, 0.238, 60.0, 0.3, 2.5, 0.6, 0.0, 0.0, 0.0, 0.0, 0.0
point.1 = 1, 0.889, -3.3 -4.7, 1600, 1, 0.709, 0, 0.323, 2.1, 0.8, 0, 0, 2, 0, 0
point.2 = 1, 0.889, 3.2, -4.7, 1600, 1, 0.709, 0, 0.323, 2.1, 0.8, 0, 0, 3, 0, 0
point.3 = 2,  -1.40, -12.45,  0.0,  787.40, 0, 0.0000,   0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0
point.4 = 2,  -1.40,  12.45,  0.0,  787.40, 0, 0.0000,   0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0
point.5 = 2, -16.10,   0.00,  5.2,  787.40, 0, 0.0000,   0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0
point.6 = 2,   4.8,    0.00,  0.6, 787.40, 0, 0.0000,   0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0


static_pitch = 10
static_cg_height = 4
gear_system_type = 4
tailwheel_lock = 1

[Views]
eyepoint = -5.8,0, 1.0



[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 0.6  //Brake scalar
differential_braking_scale = 1.0        //Delta on the amount of brake when the rudder pedals deflected
auto_brakes = 0

[hydraulic_system]
normal_pressure = 0.0    //PSI

[exits]
number_of_exits = 2
exit_rate.0 = 0.4
exit_rate.1 = 0.4

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

[SMOKESYSTEM]
smoke.0 = -10.00, -0.70, 0.0, fx_smoke_w

[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 = 0,0

[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 = 1,0

[vacuum_system]
max_pressure = 5.15   //PSI
vacuum_type = 1   //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi
engine_map = 1

[pneumatic_system]
max_pressure = 0.000000

[pitot_static]
vertical_speed_time_constant = 1                //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat = 0.0    //Scalar on heat effectiveness, 0 = not available

[LIGHTS]
//Types: = 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 4,  -6.62,   0.00, 1.00, fx_vclightwhi

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

[fuel]
Center1 = -2.6,  0.0,  0.0, 35.1, 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 = 1
electric_pump = 1

[airplane_geometry]
wing_area = 192
wing_span = 21.8
wing_root_chord = 3.0
wing_dihedral = 0
wing_incidence = 0
wing_twist = 0
oswald_efficiency_factor = 0.98
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 1.33
wing_pos_apex_vert = 0
htail_area = 12
htail_span = 7.6
htail_pos_lon = -10
htail_pos_vert = 0
htail_incidence = 0
htail_sweep = 0
vtail_area = 4
vtail_span = 5.8
vtail_sweep = 0
vtail_pos_lon = -10.5
vtail_pos_vert = 0
elevator_area = 18
aileron_area = 18
rudder_area = 7.4
elevator_up_limit = 20
elevator_down_limit = 20
aileron_up_limit = 35
aileron_down_limit = 35
rudder_limit = 30
elevator_trim_limit = 18
spoiler_limit = 0
spoilerons_available = 0
aileron_to_spoileron_gain = 0
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
auto_spoiler_available = 0
positive_g_limit_flaps_up = 9.0
negative_g_limit_flaps_up = -9.0


[Reference Speeds]
flaps_up_stall_speed = 55.0                  //Knots True (KTAS)
full_flaps_stall_speed = 55.0                  //Knots True (KTAS)
cruise_speed = 150.0                 //Knots True (KTAS)
max_indicated_speed = 300                   //Red line (KIAS)

[autopilot]
autopilot_available = 0
flight_director_available = 0

[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 = 140,  240
aileron = 200, 1000
rudder = 200, 1000

[forcefeedback]
ground_bumps_magnitude1 = 3000            ; 0 - 10000
ground_bumps_angle1 = 8900                ; 0 - 35999 degrees
ground_bumps_intercept1 = 4.0
ground_bumps_slope1 = 0.25
ground_bumps_magnitude2 = 350             ; 0 - 10000
ground_bumps_angle2 = 9100                ; 0 - 35999 degrees
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 0.7
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 = 2
stick_shaker = 0

[deice_system]
structural_deice_type = 0     //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots


[Flaps.0]
type=0
span-outboard=0.500000
extending-time=0.000000
system_type=0