[fltsim.0]
title=Akrotech_Giles-202
sim=Giles-202
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=N711AK
ui_manufacturer=Akrotech
ui_type=Giles-202
ui_variation=Orange, Blue, and Yellow
description=This is a homebuilt, light weight, tandem, aerobatic stick of dynamite. It was created by Akrotech for people who are not millionaires but want to fly a stunt plane and possibly have someone teach them how to do it.
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.1]
title=Akrotech_Giles-202 With Ads
sim=Giles-202
model=
panel=
sound=
texture=2
kb_checklists=
kb_reference=
atc_id=N711AK
ui_manufacturer=Akrotech
ui_type=Giles-202
ui_variation=Blue and White
description=This is a homebuilt, light weight, tandem, aerobatic stick of dynamite. It was created by Akrotech for people who are not millionaires but want to fly a stunt plane and possibly have someone teach them how to do it.
atc_heavy=0
atc_airline=
atc_flight_number=
[General]
editable=1
atc_type=
atc_model=GILES202
performance=Giles-202 Specifications\nLength 20.0 ft.\nHeight 5.6 ft.\nWingspan 22.0 ft.\nEngine 240hp 4 Cylinders\nEmpty Weight 1,040 lbs.\nMax Load 560 lbs.\nMax Take-off Weight 1,600 lbs.\nMax aerobatic weight 1400 lbs\nCompetition aerobatic weight 1200 lbs\nFuel, fuselage 120.0 lbs., 20.0 gals.\nFuel, wings 252.0 lbs., 42.0 gals.\nFuel, total 372.0 lbs, 62.0 gals.\nSmoke 8.0 gals., 54 lbs.\nG limits +10 -10\nRoll rate 500° per sec.\nRate of climb 2,500 fpm\nCruise speed 172 knots\nStall speed 57 knots\nVne 220 knots\nSL maximum speed 190 knots\nVertical penetration > 2000 ft\nDon Halcom
editable=1
Category=airplane
[WEIGHT_AND_BALANCE]
max_gross_weight =1600.0
empty_weight =1040.00000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.350, 0.000, 0.000
max_number_of_stations =1
;Moments of Inertia
empty_weight_pitch_MOI =514.00000
empty_weight_roll_MOI =269.00000
empty_weight_yaw_MOI =596.00000
empty_weight_coupled_MOI =0.00000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
station_load.0= 170, 0.350, 0.000, 0.000
[pitot_static]
vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000
[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 =1.00000
parasite_drag_scalar =1.00000
induced_drag_scalar =1.00000
elevator_effectiveness =1.00000
aileron_effectiveness =1.00000
rudder_effectiveness =1.00000
pitch_stability =1.00000
roll_stability =1.00000
yaw_stability =1.00000
elevator_trim_effectiveness =1.00000
aileron_trim_effectiveness =1.00000
rudder_trim_effectiveness =1.00000
hi_alpha_on_roll=1.00000
hi_alpha_on_yaw=1.00000
p_factor_on_yaw=1.00000
torque_on_roll=1.00000
gyro_precession_on_roll=1.00000
gyro_precession_on_yaw=1.00000
[GeneralEngineData]
engine_type =0
Engine.0 =4.300, 0.000, 0.000
fuel_flow_scalar=1.00000
min_throttle_limit=0.000000
[piston_engine]
power_scalar =1.00000
cylinder_displacement=100.00000
compression_ratio=10.00000
number_of_cylinders=4
max_rated_rpm=2700.00000
max_rated_hp=240.00000
fuel_metering_type=0
cooling_type=0
normalized_starter_torque=0.31667
turbocharged=1
max_design_mp=29.92000
min_design_mp=0.00000
critical_altitude=14000.00000
emergency_boost_type=0
emergency_boost_mp_offset=0.00000
emergency_boost_gain_offset=0.00000
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.00000
idle_rpm_mechanical_efficiency_scalar=1.00000
max_rpm_friction_scalar=1.00000
idle_rpm_friction_scalar=1.00000
emergency_boost_duration=0.00000
[propeller]
thrust_scalar =1.00000
propeller_type=0
propeller_diameter=5.75000
propeller_blades=3
propeller_moi=4.33175
beta_max=40.00000
beta_min=15.00000
min_gov_rpm=800.00000
prop_tc=0.10000
gear_reduction_ratio=1.00000
fixed_pitch_beta=0.00000
low_speed_theory_limit=80.00000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.00000
beta_feather=0.00000
power_absorbed_cf=0.00000
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=0.00000
minimum_reverse_beta=0.00000
//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
static_pitch = 9.700
static_cg_height = 4.000
gear_system_type=4
tailwheel_lock=0
point.0= 1, -11.450, 0.000, -2.500, 1181, 0, 0.300, 30.000, 0.296, 2.500, 1.000, 0.000, 0.000, 0
point.1= 1, 2.260, -2.800, -4.800, 1575, 1, 0.523, 0.000, 0.400, 4.000, 1.000, 0.000, 0.000, 2
point.2= 1, 2.260, 2.800, -4.800, 1575, 2, 0.523, 0.000, 0.400, 4.000, 1.000, 0.000, 0.000, 3
point.3= 2, 0.000, -11.000, -0.600, 1575, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5
point.4= 2, 0.000, 11.000, -0.600, 1575, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6
point.5= 2, -12.700, 0.000, 0.000, 1575, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9
point.6= 2, 7.500, 0.000, 0.000, 1575, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
[Views]
eyepoint = -3.5, 0.0, 1.25
[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=1.00, 0.00, -1.30, fx_smoke_w
[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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, -1.62, -13.28,-0.15, fx_navred
light.1 = 3, -1.62, 13.28,-0.15, fx_navgre
light.2 = 2, -2.02, -13.28,-0.15, fx_strobe
light.3 = 2, -2.02, 13.28,-0.15, fx_strobe
light.4 = 4, -6.62, 0.00, 1.50, fx_vclight
[EFFECTS]
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
fuel_type =1
number_of_tank_selectors =1
electric_pump=1
Center1= 1.000, 0.000, -1.000, 20.000, 0.500
LeftMain= 0.000, -3.000, -0.600, 0.000, 0.000
RightMain= 0.000, 3.000, -0.600, 0.000, 0.000
[airplane_geometry]
wing_area =90.00000
wing_span =22.00000
wing_root_chord =5.00000
wing_dihedral =0.00000
wing_incidence =0.00000
wing_twist =0.00000
oswald_efficiency_factor=0.80000
wing_winglets_flag =0
wing_sweep =0.00000
wing_pos_apex_lon =1.39000
wing_pos_apex_vert =-0.20000
htail_area =9.70000
htail_span =7.00000
htail_pos_lon =-8.90000
htail_pos_vert =0.80000
htail_incidence =0.00000
htail_sweep =0.00000
vtail_area =2.30000
vtail_span =4.40000
vtail_sweep =0.00000
vtail_pos_lon =-9.40000
vtail_pos_vert =1.90000
elevator_area =7.90000
aileron_area =21.20000
rudder_area =7.60000
elevator_up_limit =20.00000
elevator_down_limit =20.00000
aileron_up_limit =30.00000
aileron_down_limit =30.00000
rudder_limit =12.00000
elevator_trim_limit =12.00000
spoiler_limit =0.00000
spoilerons_available =0
aileron_to_spoileron_gain =0.00000
min_ailerons_for_spoilerons =0.00000
min_flaps_for_spoilerons =0.00000
auto_spoiler_available=0
spoiler_extension_time=0.000000
positive_g_limit_flaps_up=10.00000
positive_g_limit_flaps_down=7.00000
negative_g_limit_flaps_up=-8.00000
negative_g_limit_flaps_down=-6.00000
load_safety_factor=1.00000
spoiler_handle_available=0
[Reference Speeds]
flaps_up_stall_speed =56.99998
full_flaps_stall_speed =56.99998
cruise_speed =172.00000
max_indicated_speed=220.00000
max_mach=1.00000
[autopilot]
autopilot_available=0
flight_director_available=0
autothrottle_available=0
autothrottle_arming_required=0
default_pitch_mode=0
default_bank_mode=0
use_no_default_bank=1
use_no_default_pitch=1
default_vertical_speed=1000.00000
autothrottle_takeoff_ga=1.00000
autothrottle_max_rpm=90.00000
pitch_takeoff_ga=8.00000
max_pitch=10.00000
max_pitch_acceleration=1.00000
max_pitch_velocity_lo_alt=2.00000
max_pitch_velocity_hi_alt=1.50000
max_pitch_velocity_lo_alt_breakpoint=20000.00000
max_pitch_velocity_hi_alt_breakpoint=28000.00000
max_bank=25.00000
max_bank_acceleration=1.80000
max_bank_velocity=3.00000
max_throttle_rate=0.10000
nav_proportional_control=9.00000
nav_integrator_control=0.25000
nav_derivative_control=0.00000
nav_integrator_boundary=2.50000
nav_derivative_boundary=0.00000
gs_proportional_control=9.52000
gs_integrator_control=0.26000
gs_derivative_control=0.00000
gs_integrator_boundary=0.70000
gs_derivative_boundary=0.00000
yaw_damper_gain=0.00000
[forcefeedback]
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1
crash_magnitude1=10000
crash_direction1=1000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=500
gear_bump_right_duration=250000
stick_shaker_magnitude=5000
stick_shaker_direction=0
stick_shaker_period=111111
[brakes]
toe_brakes_scale=0.79348
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.00000
flap_limit_idle=0.00000
flap_limit_power=0.00000
[hydraulic_system]
normal_pressure=0.00000
[AirWrench]
Aircraft_Length=20.00000
Vmax_sl=218.64801
Vmax_ca=241.66359
V_rc=115.07790
Climb_Rate=2100.00000
Climb_Weight=1600.00000
Max_gforce=10.00000
Emergency_hp=400.00000
WingConfig=0
Wing_Vert_Pos=0.00000
ActualSweep=5.00000
Aircraft_Type=3
FlowCorrection=1.00000
JetAltitude=0.00000
turboprop_critical_altitude=0.00000
target_roll_Vopt=310.71033
target_roll_rate=279.70000
pitch_damping=1.00000
yaw_damping=1.00000
elevator_scalar=1.00000
rudder_scalar=1.00000
Elevator_FF=60.00000
Aileron_FF=-60.00000
Control_Response=40.00000
V_Max_Control=281.94086
V_Zero_Control=563.88171
Spin_Stability=100.00000
Stall_Stability=100.00000
Elevator_Propwash=1.00000
Rudder_Propwash=1.00000
spoiler_time=0.00000
spoiler_cd=0.00000
spoiler_cl=0.00000
spoiler_cm=0.00000
flaps_cd_scalar=0.00000
flaps_cm_scalar=0.00000
gear_cd_scalar=0.00000
gear_cm_scalar=0.00000
cylinder_head_temperature=501.00000
exhaust_gas_temperature=1201.00000
fuel_pressure=30.00000
oil_pressure=60.00000
oil_temperature=241.00000
radiator_temperature=211.00000
exhaust_pressure_ratio=0.00000
interstage_turbine_temperature=-459.00000
knots_flag=1
cfs1_flag=0
tab_edit=0
AirWrenchVersion=1.01.38
nose_position_lon=5.00000
ActualIncidence=0.00000
ActualTwist=0.00000
ActualTailIncidence=0.00000
dihedral_scalar=1.00000
Roll_Response=30.00000
Adverse_Yaw=100.00000
afterburner_thrust=0.00000
mach_scale=1.00000
spoiler_type=0
flaps_type=0
vfe_enabled=0
cfs2_ai_flag=0
fs8_flag=1
laminar_flow=0
direct_edit_mach=0
fixed_wing_pos=0
VSI_Weight=1210.00000
Power_Calibration=1.11628
ClAoA_S0=1.00000
ClAoA_S1=1.00000
ClAoA_S2=1.00000
prop_design_altitude=5000.00000
protect_airfile=0
cfs2_flag=0
ai_flag=0
edit_tp_torque=0
[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=0.150000
[stall_warning]
type=1
stick_shaker=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[deice_system]
structural_deice_type=0
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 0.100
system_type= 4
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.000, 0.000
