[fltsim.0]
title=Zenair CH 801 Maroon & White
sim=Zenair CH 801
model=
panel=
sound=
texture=
kb_checklists=
ui_manufacturer=Zenair
ui_type=801
ui_variation=CH 801 Maroon & White
atc_id_color=0000000000
visual_damage=0
description=The Zenith CH 801 STOL is a larger version of the Zenith 701 two seat aircraft. \nThe 801 has four seats and a much higher payload but with almost the same short field\ntakeoff and landing preformance.\n
atc_id=N801BU

[fltsim.1]
title=Zenair CH 801 Emma Field FC
sim=Zenair CH 801
model=
panel=
sound=
texture=1
kb_checklists=
ui_manufacturer=Zenair
ui_type=801
ui_variation=CH 801 Emma Field FC
atc_id_color=0000000000
visual_damage=0
description=The Zenith CH 801 STOL is a larger version of the Zenith 701 two seat aircraft. \nThe 801 has four seats and a much higher payload but with almost the same short field\ntakeoff and landing preformance.\n
atc_id=N667EM

[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 

[Autopilot]
use_no_default_pitch=1 // 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank=1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode.
autopilot_available=1 
flight_director_available=0 
default_vertical_speed=700.000000 
autothrottle_available=0 
pitch_takeoff_ga=8.000000 
default_pitch_mode=0
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

[General]
performance=Maximum Speed\t120 kts\nCruise Speed\t90 kts\nMaximum Range\t300 nm\nService Ceiling\t15,000 ft\nMax Gross Weight\t1500 lb\nSeating\t\t4\nUseful Load\t900 lb\n\n\n 
atc_type=EXPERIMENTAL 
atc_model= 
editable=1 

[weight_and_balance]

// ACM V1.0 pl5
max_gross_weight = 2200.000
empty_weight = 1150.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.000, 0.000, 0.000
empty_weight_pitch_MOI = 895.000
empty_weight_roll_MOI = 624.000
empty_weight_yaw_MOI = 1211.000
empty_weight_coupled_MOI = 0.000
max_number_of_stations = 2

station_load.0 = 200.000, 0.740, 0.000, -0.040
station_load.1 = 150.000, -2.260, 0.000, 0.200
CG_forward_limit= 0.000
CG_aft_limit= 1.000


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, -14.39, 0, 1.78, fx_navwhi
light.1 = 3, 0.13, -15.86, 3.77, fx_navred
light.2 = 3, 0.13, 15.88, 3.78, fx_navgre
light.3 = 1, -15.72, 0, 8.02, fx_beacon_SV
light.4 = 2, -0.14, -15.88, 3.77, fx_strobe
light.5 = 2, -0.14, 15.88, 3.77, fx_strobe
light.6 = 4, -0.06, 0, 1.66, fx_vclightBB1

[smokesystem]
smoke.0 = -1.86, -3.82, -1.02, fx_smoke_w

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

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 1
number_of_tank_selectors = 1

LeftMain = 0.000, -4.130, 3.510, 15.000, 0.500
RightMain = 0.000, 4.130, 3.510, 15.000, 0.500
electric_pump=1


[contact_points]
static_pitch = 3.000
static_cg_height = 3.400
max_number_of_points = 9

point.0 = 1.000, 4.750, 0.000, -3.600, 1181.102, 0.000, 0.809, 33.420, 0.200, 2.500, 1.710, 0.000, 0.000, 0.000, 0.000, 0.000
point.1 = 1.000, -1.150, -3.167, -3.400, 1574.803, 1.000, 0.809, 0.000, 0.230, 2.500, 1.257, 0.000, 0.000, 2.000, 0.000, 0.000
point.2 = 1.000, -1.150, 3.167, -3.400, 1574.803, 2.000, 0.809, 0.000, 0.230, 2.500, 1.257, 0.000, 0.000, 3.000, 0.000, 0.000
point.3 = 2.000, 0.000, -15.740, 3.101, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4 = 2.000, 0.000, 15.740, 3.101, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5 = 2.000, -16.678, 0.000, 2.377, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6 = 2.000, 5.933, 0.000, -1.190, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.7 = 2.000, -15.667, 0.000, 8.192, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
point.8 = 2.000, -1.827, 0.000, -1.201, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000


[keyboard_response]
elevator = 100.000000, 180.000000
aileron = 200.000000, 1000.000000
rudder = 200.000000, 1000.000000


[forcefeedback]
gear_bump_nose_magnitude = 1000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 450
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1
crash_magnitude1 = 2000
crash_direction1 = 1000
crash_magnitude2 = 2000
crash_direction2 = 9000
crash_period2 = 7500
crash_duration2 = 2500000
stick_shaker_magnitude = 2000
stick_shaker_direction = 0
stick_shaker_period = 111111


[airplane_geometry]
wing_area= 167.000 
wing_span= 31.200 
wing_root_chord= 4.917 
wing_dihedral= 1.000 
wing_incidence= 1.747 
wing_twist= -2.999 
oswald_efficiency_factor= 0.785 
wing_winglets_flag= 0 
wing_sweep= 0.000 
wing_pos_apex_lon= 1.229 
wing_pos_apex_vert= 0.000 
htail_area= 25.000 
htail_span= 8.167 
htail_pos_lon= -12.500 
htail_pos_vert= 0.000 
htail_incidence= 3.246 
htail_sweep= 0.000 
vtail_area= 8.000 
vtail_span= 3.225 
vtail_sweep= 0.000 
vtail_pos_lon= -14.167 
vtail_pos_vert= 4.000 
elevator_area= 8.500 
aileron_area= 17.000 
rudder_area= 8.000 
elevator_up_limit= 28.000 
elevator_down_limit= 20.999 
aileron_up_limit= 22.000 
aileron_down_limit= 20.000 
rudder_limit= 23.995 
elevator_trim_limit= 19.498 
spoiler_limit= 57.296 
spoilerons_available= 0 
aileron_to_spoileron_gain= 0.000 
min_ailerons_for_spoilerons= 0.000 
min_flaps_for_spoilerons= 0.000 

[GeneralEngineData]
engine_type= 0 
Engine.0= 6.167, 0.000, 0.000 
fuel_flow_scalar= 1.000 
min_throttle_limit=0.000000

[piston_engine]
cylinder_displacement= 90.000 
compression_ratio= 8.500 
number_of_cylinders= 4 
max_rated_rpm= 2500.000 
max_rated_hp= 180.000 
fuel_metering_type= 1 
cooling_type= 1 
normalized_starter_torque= 0.300 
turbocharged= 0 
max_design_mp= 0.000 
min_design_mp= 0.000 
critical_altitude= 0.000 
emergency_boost_type= 0 
emergency_boost_mp_offset= 0.000 
emergency_boost_gain_offset= 0.000 
fuel_air_auto_mixture= 0 
auto_ignition= 0 
max_rpm_mechanical_efficiency_scalar=1.000 
idle_rpm_mechanical_efficiency_scalar=1.000 
max_rpm_friction_scalar=1.000 
idle_rpm_friction_scalar=1.000 
power_scalar=1.200 

[propeller]
propeller_type= 1 
propeller_diameter= 6.833 
propeller_blades= 2 
propeller_moi= 5.700 
beta_max= 31.800 
beta_min= 17.000 
min_gov_rpm= 1400.000 
prop_tc= 0.100 
gear_reduction_ratio= 1.000 
fixed_pitch_beta= 20.000 
low_speed_theory_limit= 80.000 
prop_sync_available= 0 
prop_deice_available= 0 
prop_feathering_available= 0 
prop_auto_feathering_available= 0 
min_rpm_for_feather= 0.000 
beta_feather= 0.000 
power_absorbed_cf= 0.000 
defeathering_accumulators_available= 0 
prop_reverse_available= 0 
minimum_on_ground_beta= 0.000 
minimum_reverse_beta= 0.000 
thrust_scalar=1.100 

[Reference Speeds]
flaps_up_stall_speed= 28.000 
full_flaps_stall_speed= 22.400 
cruise_speed= 117.429 
max_indicated_speed=140.000000

[Views]
eyepoint=0.21, -1.05, 2.40        //(feet) longitudinal, lateral, vertical distance from reference datum

[direction_indicators]
direction_indicator.0=1,0 


[flight_tuning]
cruise_lift_scalar=1.000 
pitch_stability=1.300 
roll_stability=1.000 
yaw_stability=1.000 
parasite_drag_scalar=0.950 
induced_drag_scalar=0.950 
elevator_effectiveness=1.200 
aileron_effectiveness=1.000 
rudder_effectiveness=1.000 
elevator_trim_effectiveness=1.200 
aileron_trim_effectiveness=1.000 
rudder_trim_effectiveness=1.000 

[exits]
number_of_exits=2
exit_rate.0=1.4                               ;Percent per second
exit_rate.1=2.4                               ;Percent per second

[fltsim.2]
title="Okipous" Zenair CH801 Land
sim=Zenair CH 801
model=
panel=
sound=
texture=2
kb_checklists=
ui_manufacturer=Zenith Aircraft Company
ui_type=Zenair CH 801 STOL
ui_variation=Okipous CH801 Landplane
atc_id_color=0000000000
visual_damage=0
description=The Zenith CH 801 STOL is a larger version of the Zenith 701 two seat aircraft. \nThe 801 has four seats and a much higher payload but with almost the same short field\ntakeoff and landing preformance. Repaint by Kostas Rossidis [email protected]\n

atc_id=4711
atc_airline=
atc_flight_number=
atc_heavy=0
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 3.000
system_type= 0
damaging-speed= 125.000
blowout-speed= 150.000
lift_scalar= 1.500
drag_scalar= 1.000
pitch_scalar= 1.350
flaps-position.0= 0.000, 0.000
flaps-position.1= 18.666, 0.000
flaps-position.2= 29.332, 0.000
flaps-position.3= 40.000, 0.000
[brakes]
toe_brakes_scale=0.671407
parking_brake=1
[hydraulic_system]
normal_pressure=0.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0