//Unreleased textures on [fltsim.3] pending permission of Algonquin Outfitters, Oxtongue lake Ontario, Ca.
[fltsim.0]
title=Monocoupe 135 White
sim=Monocoupe
model=
panel=
sound=
sound_alias=
texture=
kb_checklists=Monocoupe_check
kb_reference=Monocoupe_notes
atc_id_color=0xffffcc
atc_id=C-YGBZ
ui_manufacturer=Monocoupe
ui_type=135
ui_variation=C-YGBZ White w/floats
description=The 1928 Monocoupe 135. Two person light private aircraft powered by the famous Warner Scarab 135 Hp radial engine. America's first successful light plane in production. At one time 80% of the light planes being sold were of the Monocoupe variety. Seaplane float version. Full panel with autopilot.
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.1]
title=Monocoupe 135 White with Floats and Canoe
sim=Monocoupe
model=1
panel=
sound=
sound_alias=
texture=
kb_checklists=Monocoupe_check
kb_reference=Monocoupe_notes
atc_id_color=0xffffcc
atc_id=C-YGBZ
ui_manufacturer=Monocoupe
ui_type=135
ui_variation=C-YGBZ White w/floats & Canoe
description=The 1928 Monocoupe 135. Two person light private aircraft powered by the famous Warner Scarab 135 Hp radial engine. America's first successful light plane in production. At one time 80% of the light planes being sold were of the Monocoupe variety. Seaplane float version. Full panel with autopilot.
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.2]
title=Monocoupe 135 Teal
sim=Monocoupe
model=
panel=2
sound=
sound_alias=
texture=2
kb_checklists=Monocoupe_check
kb_reference=Monocoupe_notes
atc_id_color=0xffffcc
atc_id=C-PBMZ
ui_manufacturer=Monocoupe
ui_type=135
ui_variation=C-PBMZ Teal w/floats
description=The 1928 Monocoupe 135. Two person light private aircraft powered by the Warner Scarab 135 Hp radial engine. America's first successful light plane in production. At one time 80% of the light planes being sold were of the Monocoupe variety. Seaplane float version. Full panel with autopilot.
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.3]
title=Monocoupe 135 Teal w/floats and Canoe
sim=Monocoupe
model=1
panel=2
sound=
sound_alias=
texture=2
kb_checklists=Monocoupe_check
kb_reference=Monocoupe_notes
atc_id_color=0xffffcc
atc_id=C-PBMZ
ui_manufacturer=Monocoupe
ui_type=135
ui_variation=C-PBMZ Teal w/floats and Canoe
description=The 1928 Monocoupe 135. Two person light private aircraft powered by the Warner Scarab 135 Hp radial engine. America's first successful light plane in production. At one time 80% of the light planes being sold were of the Monocoupe variety. Seaplane float version. Full panel with autopilot.
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.4]
title=Monocoupe 135 Morty's Outfitters floatplane
sim=Monocoupe
model=
panel=1
sound=
sound_alias=
texture=1
kb_checklists=Monocoupe_check
kb_reference=Monocoupe_notes
atc_id_color=0xffffcc
atc_id=C-MWOZ
ui_manufacturer=Monocoupe
ui_type=135
ui_variation=Morty's Outfitters full panel w/floats
description=The 1928 Monocoupe 135. Two person light private aircraft powered by theWarner Scarab 135 Hp radial engine. America's first successful light plane in production. At one time 80% of the light planes being sold were of the Monocoupe variety. Seaplane float version. Full panel with autopilot.
atc_heavy=0
atc_airline=
atc_flight_number=
[fltsim.5]
title=Monocoupe 135 Morty's Outfitters floatplane w/canoe
sim=Monocoupe
model=1
panel=1
sound=
sound_alias=
texture=1
kb_checklists=Monocoupe_check
kb_reference=Monocoupe_notes
atc_id_color=0xffffcc
atc_id=C-MWOZ
ui_manufacturer=Monocoupe
ui_type=135
ui_variation=Morty's Outfitters w/floats and Canoe
description=The 1928 Monocoupe 135. Two person light private aircraft powered by theWarner Scarab 135 Hp radial engine. America's first successful light plane in production. At one time 80% of the light planes being sold were of the Monocoupe variety. Seaplane float version with a canoe on board. Full panel with autopilot.
atc_heavy=0
atc_airline=
atc_flight_number=
[General]
atc_type=SPORTAIRCRAFT
atc_model=135
performance=Maximum Speed 140 mph, Cruise Speed 125 mph, Maximum Range 500 nm, Service Ceiling 13,000 ft, Fuel Capacity 38 U.S gal, Max Gross Weight, 1450 lb, Seating 2, Useful Load, 555 lbs
[WEIGHT_AND_BALANCE]
max_gross_weight=1450.000
empty_weight=990.000
reference_datum_position=3.600, 0.000, 0.000
empty_weight_CG_position=-3.000, 0.000, 0.000
max_number_of_stations=50
//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.0=195.000, -3.000, -1.800, 0.000 //Pilot
station_load.1=173.000, -3.000, 1.800, 0.000 //Passenger
station_load.2=42, -6.2, 0.0, 0.0 //Baggage
;Moments of Inertia
empty_weight_pitch_MOI=2300.000
empty_weight_roll_MOI=1837.000
empty_weight_yaw_MOI=1860.000
empty_weight_coupled_MOI=0.000
CG_forward_limit=0.000
CG_aft_limit=1.000
[flight_tuning]
cruise_lift_scalar=1.55
parasite_drag_scalar=1.270
induced_drag_scalar=1.050
elevator_effectiveness=0.650
aileron_effectiveness=1.00
rudder_effectiveness=0.8500
pitch_stability=1.100
roll_stability=0.900
yaw_stability=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=0.750
rudder_trim_effectiveness=0.750
[GeneralEngineData]
engine_type=0
Engine.0=2.400, 0.000, 0.000 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=0.480 //0.88
min_throttle_limit=0.000000
[piston_engine]
power_scalar=1.00 //1.00
cylinder_displacement=110.2500 //422 TOTAL
compression_ratio=5.200
number_of_cylinders=7
max_rated_rpm=2950.000 //2050.00
max_rated_hp=135.000
fuel_metering_type=1
cooling_type=0
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
[propeller]
thrust_scalar=0.354 //0.454 Propeller thrust scalar
propeller_type=0 //1, 0=Constant Speed, 1=Fixed Pitch
propeller_diameter=6.6 //Propeller Diameter, (feet)
propeller_blades=2 //Number of propeller blades
propeller_moi=5.0 //Propeller moment of inertia
beta_max=31.8 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=17.0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=1400 //0, Miminum governed RPM
prop_tc=0.1 //0, Prop time-constant
gear_reduction_ratio=1.0 //Propeller gear reduction ratio
fixed_pitch_beta=20 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=0 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=0 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=0 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available=0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather=0 //Minimum RPM for prop feathering
beta_feather=0 //Feathering pitch angle (degrees)
power_absorbed_cf=0 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available=0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta=0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=0 //Minimum pitch angle in reverse, (degrees)
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 17.0
marker_beacon=1, 2 , 17.0
fuel_pump=0, 5 , 17.0
starter1=0, 20, 17.0
light_nav=0, 5 , 17.0
light_beacon=0, 5 , 17.0
light_landing=0, 5 , 17.0
light_taxi=0, 5 , 17.0
light_strobe=0, 5 , 17.0
light_panel=0, 5 , 17.0
//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 (water rudder effectiveness:0=Undamped, 1=Critically Damped)
//11 Extension Time (seconds)
//12 Retraction Time (seconds)
//13 Sound Type
[contact_points]
point.0=4, -0.75, -3.050, -4.35, 1600.00, 0.00, 0.00, 0.0, 0.45, 2.50, 0.65, 0.00, 0.00, 0.00, 0.00, 0.00
point.1=4, -0.75, 3.050, -4.35, 1600.00, 0.00, 0.00, 0.0, 0.45, 2.50, 0.65, 0.00, 0.00, 1.00, 0.00, 0.00
point.2=4, -12.50, -3.050, -4.00, 1600.00, 0.00, 0.00, 0.0, 0.45, 2.50, 0.65, 0.00, 0.00, 2.00, 0.00, 0.00
point.3=4, -12.50, 3.050, -4.00, 1600.00, 0.00, 0.00, 0.0, 0.45, 2.50, 0.65, 0.00, 0.00, 3.00, 0.00, 0.00
point.4=2.000, -3.900, -16.000, 3.000, 1000.000, 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, -3.900, 16.000, 3.000, 1000.000, 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, -18.230, 0.000, 0.000, 1000.000, 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, 1.480, 0.000, -1.170, 1000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.8=2.000, -18.800, 0.000, 3.830, 1000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
point.9=2.000, -4.900, 0.000, -1.000, 1000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000
point.10= 5, -30.90, -5.250, -7.300, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 2.0, 1.5, 0, 0.0, 0.0
point.11= 5, -30.90, 5.250, -7.300, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 2.1, 1.5, 0, 0.0, 0.0
max_number_of_points=21
static_pitch=4.010
static_cg_height=3.350
[Views]
eyepoint=-5.80, -0.55, 0.10 //(feet) longitudinal, lateral, vertical distance from reference datum -5.80, -0.55, -0.05
[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, 1
Adf.1=1
Transponder.1=1
Marker.1=1
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=3, -4.00, -16.01, 2.61, fx_navred
light.1=3, -4.00, 16.01, 2.61, fx_navgre
light.2=2, -4.00, -16.01, 2.61, fx_strobe
light.3=2, -4.00, 16.01, 2.61, fx_strobe
light.4=1, -18.60, 0.00, 0.60, fx_beacon
light.5=1, -9.00, 0.00, -1.25, fx_navwhi
light.6=4, -3.9, 0.00, -0.00, fx_vclight
[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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
LeftMain=-3.900, -3.100, 2.500, 16.00, 0.000
RightMain=-3.900, 3.100, 2.500, 16.00, 0.000
fuel_type=1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=1
[airplane_geometry]
wing_area=156.880
wing_span=32.000
wing_root_chord=5.00
wing_dihedral=4.200
wing_incidence=1.500
wing_twist=-3.000
oswald_efficiency_factor=0.680
wing_winglets_flag=0
wing_sweep=0.000
wing_pos_apex_lon=-2.400
wing_pos_apex_vert=2.500
htail_area=12.000
htail_span=5.700
htail_pos_lon=-17.300
htail_pos_vert=0.500
htail_incidence=-1.2
htail_sweep=10.000
vtail_area=3.500
vtail_span=3.100
vtail_sweep=20.000
vtail_pos_lon=-17.200
vtail_pos_vert=1.500
elevator_area=4.300
aileron_area=13.300
rudder_area=4.200
elevator_up_limit=35.000
elevator_down_limit=35.000
aileron_up_limit=22.000
aileron_down_limit=22.000
rudder_limit=30.000
elevator_trim_limit=19.500
spoiler_limit=0.000
spoilerons_available=0
aileron_to_spoileron_gain=0.000
min_ailerons_for_spoilerons=0.000
min_flaps_for_spoilerons=0.000
[stall_warning]
type=0
[SMOKESYSTEM]
smoke.0=0.00, 0.00, 0.00, fx_smoke_w //X(no effect??),long, Lateral
[Reference Speeds]
flaps_up_stall_speed=33.200
full_flaps_stall_speed=33.200
cruise_speed=80.000 ///85MPH
max_indicated_speed=163.000000
[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.0
autothrottle_available=0
pitch_takeoff_ga=8.000
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
[forcefeedback]
gear_bump_nose_magnitude=6000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=6000 ; 0 - 10000
gear_bump_left_direction=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=6000 ; 0 - 10000
gear_bump_right_direction=00500 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=3250 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750 ; 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
[flaps.0] //Trailing Edge Flaps
type=0 // 1 - tail, 2 - lead
system_type=4 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None
[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
