[fltsim.0]
title=Adam A700
sim=a700
model=
panel=
sound=
texture=
atc_id=N484F
ui_manufacturer=Adam
ui_type=A700
ui_variation=White with Red
description=The Adam A700 first flew July 27, 2003. First customer deliveries are planned for late 2004 (adamaircraft.com). This one was made with Flight Sim Design Studio 2.24 (FSDS2) by ABACUS Publishing (abacuspub.com).
[General]
atc_type=Adam
atc_model=A700
editable=1
performance=Cruise Speed: 340 KTAS\nCeiling: 41,000 ft\nDesigner: Chuck Dome\nDate: September 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 = 0.7
[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 = 0.7 //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 = 2750 //Lbs, max rated static thrust at Sea Level
afterburner_available = 0 //Afterburner available?
reverser_available = 0 //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, -4.55, 1574, 0, 0.596, 39.9, 0.170, 2.5, 0.9516, 4.0, 4.0, 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, 4.0, 4.0, 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, 4.0, 4.0, 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 = 0.0
static_cg_height = 4.3
gear_system_type=1
[Views]
eyepoint = 10.5, -1.10, 2.5
[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=700.000000
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]
//Some lights controlled by MDL file
light.0 = 3, -7.90, 0.00, 1.20, fx_navwhi ,
light.1 = 4, 10.50, 0.00, 2.50, fx_vclight ,
light.2 = 5, 3.20, -4.08, -0.83, fx_landing ,
light.3 = 5, 3.20, 4.08, -0.83, fx_landing ,
[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
