[fltsim.0]
title=Moni Motorglider Green Stripe
sim=Moni
model=
panel=
sound=
texture=
kb_checklists=
description=Moni Motorglider
ui_manufacturer=Moni
ui_type=Moni Motorglider
ui_variation=A Green Stripe
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=

[fltsim.1]
title=Moni Motorglider White
sim=Moni
model=
panel=
sound=
texture=1
kb_checklists=
description=Moni Motorglider
ui_manufacturer=Moni
ui_type=Moni Motorglider
ui_variation=White
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=

[fltsim.2]
title=Moni Motorglider Green 
sim=Moni
model=
panel=
sound=
texture=2
kb_checklists=
description=Moni Motorglider
ui_manufacturer=Moni
ui_type=Moni Motorglider
ui_variation=Green1
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=

[fltsim.3]
title=Moni Motorglider Beige Stripe 
sim=Moni
model=
panel=
sound=
texture=3
kb_checklists=
description=Moni Motorglider
ui_manufacturer=Moni
ui_type=Moni Motorglider
ui_variation=Beige Stripe
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=

[General]
performance=Performance\nCruise speed 110 MPH.\nStall speed 39 Kts.\nBest L\/D speed 59 Kts.\nTakeoff distance 738 Ft.Fuel consumption 4.5 GPHGlide ratio 31:1\nLoad limits:+5.3G \/ -2.65G\nMinimum sink rate 184 FPMF\nuel capacity 23 Gal.\n Max range 650+ NM\nMax endurance 7 Hrs.\nDimensions\nMax gross wt 1874 Lb.\nBasic empty wt 1331 Lb.\nUseful load 539 Lb.\nWingspan 57.3 Ft. (folded) 33.3 Ft.\nLength 26.4 Ft.Height 6.33 Ft.\nBy William Ortis, Lionheart Creations Ltd.
atc_type=
atc_model=

[WEIGHT_AND_BALANCE]
reference_datum_position=     0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000
max_number_of_stations=50
station_load.0=0.000, 0.000, 0.000, 0.000
empty_weight= 269.000
empty_weight_roll_MOI= 7243.000
empty_weight_pitch_MOI= 11060.000
empty_weight_yaw_MOI= 14484.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 6063.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[Views]
eyepoint= -2.0,0.00,1.35

[flight_tuning]
cruise_lift_scalar     =3.00
parasite_drag_scalar   =1.00
induced_drag_scalar    =1.00
elevator_effectiveness =2.50
aileron_effectiveness  =1.40
rudder_effectiveness   =1.20
pitch_stability        =3.0
roll_stability         =1.000
yaw_stability          =1.000
elevator_trim_effectiveness =2.0
aileron_trim_effectiveness  =1.000
rudder_trim_effectiveness   =1.000

[fuel]
Main= -0.970, 0.00, -1.610, 14.500, 0.000
fuel_type=1.000000
number_of_tank_selectors=1
LeftMain=-0.970000,-12.250000,-1.610000,24.500000,0.000000
RightMain=-0.970000,12.250000,-1.610000,24.500000,0.000000
External1=1.940000,0.000000,-3.870000,175.000000,0.000000
electric_pump=0

[airplane_geometry]
wing_area               = 180.0                 //Square feet
wing_span               = 57.0                  //Feet
wing_root_chord         = 4.6                   //Feet
wing_dihedral           = 3.5                   //Degrees
wing_incidence          = 3.0                   //Degrees
wing_twist              = -2.0                  //Degrees
oswald_efficiency_factor= 1.0                   //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 0.0                   //Degrees, wing leading edge
wing_pos_apex_lon       = -0.5                  //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              = 21.0                  //Square feet
htail_span              = 7.9                   //Feet
htail_pos_lon           = -17.3                 //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         = 0.0                   //Degrees
htail_sweep             = 0.0                   //Degrees, horizontal tail leading edge
vtail_area              = 17.0                  //Square feet
vtail_span              = 4.7                   //Feet, tip to body
vtail_sweep             = 0.0                   //Degrees, vertical tail leading edge
vtail_pos_lon           = -16.0                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 3.9                   //Feet, vertical distance from reference point, positive going up
elevator_area           = 16.0                  //Square feet
aileron_area            = 14.7                  //Square feet
rudder_area             = 6.0                   //Square feet
elevator_up_limit       = 26.0                  //Degrees
elevator_down_limit     = 26.0                  //Degrees
aileron_up_limit        = 30.0                  //Degrees
aileron_down_limit      = 30.0                  //Degrees
rudder_limit            = 30.0                  //Degrees
elevator_trim_limit     = 15.0                  //Degrees
spoiler_limit           = 70.0                  //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

[contact_points]
point.0= 1.000, -7.083, 0.000,  -0.750, 1574.803, 0.000, 0.549, 43.020, 0.113, 2.500, 1.371, 3.000, 3.000, 0.000, 0.000, 0.000
point.1= 1.000, 0.667, -14.917, -0.433, 2165.354, 0.000, 0.549, 0.000, 0.503, 2.500, 0.797, 7.500, 7.500, 2.000, 0.000, 0.000
point.2= 1.000, 0.667, 14.917, -0.433, 2165.354, 0.000, 0.549, 0.000, 0.503, 2.500, 0.797, 6.000, 6.000, 3.00, 0.000, 0.000
point.3= 1.000, 2.667, 0.000, -2.400, 1574.803, 1.000, 0.549, 43.020, 0.113, 2.500, 1.371, 3.000, 3.000, 0.000, 0.000, 0.000
point.4= 2.000, 0.000, -20.000,  1.250, 1181.102, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.5= 2.000, 0.000, 20.000,  1.250, 1181.102, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.6= 2.000, -8.250, 0.000, 1.667, 1181.102, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.7= 2.000, 2.417, 0.000,  1.083, 1181.102, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_pitch= 2.865
static_cg_height= 2.00
gear_system_type=1

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3,   0.60, -13.95, 0.05,  fx_navred ,
light.1 = 3,   0.60,  13.95, 0.19,  fx_navgre ,
light.2 = 4,  -0.50,    0.00, 2.00,  fx_vclight ,
light.3 = 3,  -2.75,    0.00,-0.55,  fx_navred ,
light.4 = 3,-10.40,    0.00,  0.70,fx_navwhi
light.5 = 2,   0.60, -13.95, 0.05, fx_strobe ,
light.6 = 2,   0.60,  13.95, 0.19, fx_strobe ,

[GeneralEngineData]
engine_type= 0
Engine.0= 2.000, 0.000, 0.000
fuel_flow_scalar= 1.000
min_throttle_limit=0.000000

[piston_engine]
cylinder_displacement= 130.000
compression_ratio= 6.000
number_of_cylinders= 2
max_rated_rpm= 2550.000
max_rated_hp= 70.000
fuel_metering_type= 2
cooling_type= 0
normalized_starter_torque= 0.035
turbocharged= 1
max_design_mp= 53.000
min_design_mp= 1.000
critical_altitude= 21500.000
emergency_boost_type= 1
emergency_boost_mp_offset= 10.000
emergency_boost_gain_offset= 0.660
fuel_air_auto_mixture= 0
auto_ignition= 0
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000

[propeller]
propeller_type= 0
propeller_diameter= 6.26
propeller_blades= 3
propeller_moi= 3.170
beta_max= 65.000
beta_min= 13.000
min_gov_rpm= 1800.000
prop_tc= 0.010
gear_reduction_ratio= 2.000
fixed_pitch_beta= 0.000
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

[Reference Speeds]
flaps_up_stall_speed= 52.000
full_flaps_stall_speed= 41.600
cruise_speed= 128.180
max_indicated_speed=760.500000

[keyboard_response]
elevator=350.000000,500.000000
aileron=450.000000,1000.000000
rudder=200.000000,1000.000000

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
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

[direction_indicators]
direction_indicator.0=1,0

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 1
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= 19.099, 0.000
flaps-position.2= 38.197, 0.000
flaps-position.3= 57.296, 0.000

[brakes]
toe_brakes_scale=1.000000
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[hydraulic_system]
electric_pumps=0
engine_map=1,0,0,0
normal_pressure=6.930556

[forcefeedback]
ground_bumps_magnitude1=2500            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=10.0
ground_bumps_slope1=0.300
ground_bumps_magnitude2=350             ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
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=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0