[fltsim.0]
title=Maverick
sim=mavjet
model=
panel=
sound=
texture=
atc_id=N7473F
ui_manufacturer=Maverick Jets
ui_type=Maverick
ui_variation=White with Red
description=Maverick Jets is the first company to be delivering custom light-weight personal executive jets to the general public. This one was made with Flight Sim Design Studio 2.20 (FSDS2) by ABACUS Publishing (abacuspub.com).
[General]
atc_type=Maverick
atc_model=Maverick
editable=1
performance=Cruise Speed: 300 kt\nRange: 1600 nm\nCeiling: 31,000 ft\nDesigner: Chuck Dome\nDate: August 2003
[WEIGHT_AND_BALANCE]
max_gross_weight = 10000 // (pounds)
empty_weight = 7000 // (pounds)
reference_datum_position = -0.5, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 170, 5.0, -2.0, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170, 5.0, 2.0, 0.0 //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 30000
empty_weight_roll_MOI = 18200
empty_weight_yaw_MOI = 36500
empty_weight_coupled_MOI= 0.0
[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, 10, 9.5
avionics = 1, 5 , 9.5
additional_system = 0, 20, 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 = 1.0
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 = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -8.3, -4.8, 0.5 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -8.3, 4.8, 0.5 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 0.3 //Scalar for fuel flow efficiency
min_throttle_limit=0.000000
[TurbineEngineData]
fuel_flow_gain = 0.0025 //Gain on fuel flow
inlet_area = 4.2895 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 2500 //Lbs, max rated static thrust at Sea Level
afterburner_available = 0 //Afterburner available?
reverser_available = 1 //Thrust reverser available?
[jet_engine]
thrust_scalar = 1.0
//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]
point.0=1, 11.00, 0.00, -4.50, 1181, 0, 0.596, 39.9, 0.170, 2.5, 0.9516, 4.8, 4.8, 0, 0.0, 0.0
point.1=1, -2.90, -8.58, -4.79, 1574, 1, 0.596, 0.0, 0.642, 2.5, 0.8152, 4.5, 5.2, 2, 0.0, 0.0
point.2=1, -2.90, 8.58, -4.79, 1574, 2, 0.596, 0.0, 0.642, 2.5, 0.8152, 4.8, 4.9, 3, 0.0, 0.0
point.3=2, -3.33, -23.92, -3.00, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -3.33, 23.92, -3.00, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -22.67, 0.00, 0.00, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, 23.08, 0.00, -1.50, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
static_pitch = -1.0
static_cg_height = 4.3
gear_system_type=1
[Views]
eyepoint = 5.0, -1.3, 1.175
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 5 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 15 // degrees
flaps-position.2 = 25 // degrees
flaps-position.3 = 40 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 0
Com.2 = 1, 0
Nav.1 = 1, 0, 1
Nav.2 = 1, 0, 0
Adf.1 = 1
Transponder.1 = 1
Marker.1 = 1
[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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[fuel]
LeftMain = 0.0, -9.5, -1.0, 115.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux = 0.0, -6.0, -1.5, 50.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = 0.0, 9.5, -1.0, 115.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux = 0.0, 6.0, -1.5, 50.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=0
[airplane_geometry]
wing_area = 310.0 //Square feet
wing_span = 45.0 //Feet
wing_root_chord = 6.9 //Feet
wing_dihedral = 6.0 //Degrees
wing_incidence = 1.0 //Degrees
wing_twist = -1.5 //Degrees
oswald_efficiency_factor= 0.7 //Measure of lift effeciency of wing
wing_winglets_flag = 1 //Are winglets available?
wing_sweep = 1.0 //Degrees, wing leading edge
wing_pos_apex_lon = 2.1 //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 = 67.0 //Square feet
htail_span = 17.2 //Feet
htail_pos_lon = -22.6 //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 = 0.5 //Degrees
htail_sweep = 20.0 //Degrees, horizontal tail leading edge
vtail_area = 42.0 //Square feet
vtail_span = 7.4 //Feet, tip to body
vtail_sweep = 40.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -20.5 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 4.1 //Feet, vertical distance from reference point, positive going up
elevator_area = 17.0 //Square feet
aileron_area = 13.5 //Square feet
rudder_area = 7.3 //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 = 30.0 //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
[Reference Speeds]
flaps_up_stall_speed = 96.0 //Knots True (KTAS)
full_flaps_stall_speed = 76.8 //Knots True (KTAS)
cruise_speed = 315.0 //Knots True (KTAS)
max_indicated_speed=2010.000000
max_mach=3.000000
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 1
autothrottle_arming_required= 0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga= 0
pitch_takeoff_ga = 8;
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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation
light.0 = 3, -1.15, -17.65, -0.33, fx_navred ,
light.1 = 3, -1.15, 17.65, -0.33, fx_navgre ,
light.2 = 3, -13.85, 0.00, 6.10, fx_navwhi ,
light.3 = 2, -1.05, -17.65, -0.33, fx_strobe ,
light.4 = 2, -1.05, 17.65, -0.33, fx_strobe ,
light.5 = 1, -12.85, 0.00, 6.10, fx_beacon ,
light.6 = 4, 7.00, 0.00, 0.50, fx_vclight,
[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
[brakes]
toe_brakes_scale=1.525925
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=15.011494
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
