[fltsim.0]
title=RyanSC United States
sim=RyanSC
model=
panel=
sound=
texture=
kb_checklists=
ui_manufacturer=Ryan
ui_type="SC-W"
ui_variation="A: NC18914, United States"
atc_heavy=0
atc_id=NC18914
atc_id_color=0xFF0000
atc_airline=
atc_flight_number=
description="The Sport Cabin ( or Cruising ) was an attempt by T. Claude Ryan to capitalize on the success of his 2-place, open cockpit ST trainer by issuing an enclosed airplane for the GA pilot. The new SC would embody even more of the metal construction technology that the earlier ST had become famous for. Like the ST, the SC seemed destined for greatness until WWII interupted production after only 12 units. One more was built, from inventory, after the war. Several still exist today, including NC18914."
[fltsim.1]
title=RyanSC Canada
sim=RyanSC
model=
panel=
sound=
texture=1
kb_checklists=
ui_manufacturer=Ryan
ui_type="SC-W"
ui_variation="B: CF-TAM, Canada"
atc_heavy=0
atc_id=CF-TAM
atc_id_color=0xFF0000
atc_airline=
atc_flight_number=
description="The Sport Cabin ( or Cruising ) was an attempt by T. Claude Ryan to capitalize on the success of his 2-place, open cockpit ST trainer by issuing an enclosed airplane for the GA pilot. The new SC would embody even more of the metal construction technology that the earlier ST had become famous for. Like the ST, the SC seemed destined for greatness until WWII interupted production after only 12 units. One more was built, from inventory, after the war. Several still exist today, including NC18914."
[General]
atc_type=RYAN
atc_model=SCW
editable=1
performance=Maximum Speed...140 mph \nCruising Speed...120mph @ 1800RPM\nStalling Speed...60mph\nLanding Speed...55mph\nService Ceiling...14,500 ft\nMaximum Range...450 mi @ 75%\nEngine...Warner 145-hp air cooled 7-cyl. radial\nFuel Capacity...37 gal\nEmpty Weight...1395 lb\nGross Weight...2150lb \nUseful Load...755 lb\nPayload...390lb\nLength...25 ft \nWingspan...37.5 ft\nSeating...2-3
[WEIGHT_AND_BALANCE]
max_gross_weight = 2220.000
empty_weight = 1680.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.250, 0.000, 0.000
max_number_of_stations =50
station_load.0 =170.000000, -0.50000, 0.000000, 0.000000, Pilot //W
station_load.1 =0.000000, -0.750000, 0.000000, 0.000000, Passenger //W
station_load.2 =20.000000, -4.400000, 0.000000, 0.000000, Baggage //W
;Moments of Inertia
empty_weight_pitch_MOI= 1718.000
empty_weight_roll_MOI= 1313.000
empty_weight_yaw_MOI= 3642.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =1.056
induced_drag_scalar =1.066
elevator_effectiveness =0.900
aileron_effectiveness =1.175
rudder_effectiveness =1.000
pitch_stability =1.250
roll_stability =1.250
yaw_stability =1.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
[GeneralEngineData]
engine_type = 0
Engine.0 = 5.800, 0.000, 0.000
fuel_flow_scalar= 1.000
min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser
[piston_engine]
power_scalar =1.000
cylinder_displacement= 72.000
compression_ratio= 5.500
number_of_cylinders= 7
max_rated_rpm= 2100.000
max_rated_hp= 144.278
fuel_metering_type= 1
cooling_type= 0
normalized_starter_torque= 0.300
turbocharged= 1
max_design_mp= 34.000
min_design_mp= 0.000
critical_altitude= 10000.000
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=0.9000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.121
idle_rpm_friction_scalar=1.3
[propeller]
thrust_scalar =0.966
propeller_type= 1
propeller_diameter= 9.000
propeller_blades= 2
propeller_moi= 3.780
beta_max= 0.000
beta_min= 0.000
min_gov_rpm= 0.000
prop_tc= 0.100
gear_reduction_ratio= 1.000
fixed_pitch_beta= 13.750
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= 0.000
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000
//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= 1.000, -15.000, 0.000, -1.70, 1200.000, 0.000, 0.538, 20.000, 0.400, 2.500, 0.520, 0.000, 0.000, 7.000, 0.000, 0.000
point.1= 1.000, 1.240, -3.984, -4.95, 1600.000, 1.000, 0.728, 0.000, 0.540, 2.500, 0.650, 0.000, 0.000, 2.000, 0.000, 0.000
point.2= 1.000, 1.240, 3.984, -4.95, 1600.000, 2.000, 0.728, 0.000, 0.540, 2.500, 0.650, 0.000, 0.000, 3.000, 0.000, 0.000
point.3= 2.000, -1.000, -17.700, 1.800, 800.000, 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, -1.000, 17.700, 1.800, 800.000, 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, -14.400, 0.000, 4.500, 800.000, 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, 5.400, 0.000, -2.200, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch = 12.000
static_cg_height = 4.300
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.5 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
[hydraulic_system]
normal_pressure = 0.0 //PSI
[Views]
eyepoint = -1.574, -0.748, 2.151
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, .021, -18.00, .732, fx_navred ,
light.1 = 3, .021, 18.00, .732, fx_navgre ,
light.3 = 4, -1.70, 0.00, 2.25, fx_vclight,
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 0
Com.1 = 1, 0
Nav.1 = 0, 0, 0
Adf.1 = 0
Transponder.1 = 0
Marker.1 = 0
[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 =200, 1000
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=2
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
startup=fx_engstrt_cub
touchdown=fx_tchdwn_s, 1
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor = 0, 5 , 17.0
gear_motor = 0, 5 , 17.0
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
gear_warning = 0, 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
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
[fuel]
Center1 = 2.800, 0.000, 0.000, 37.000, 0.000
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=0
[airplane_geometry]
wing_area = 178.500
wing_span = 35.200
wing_root_chord = 5.250
wing_dihedral = 1.100
wing_incidence = 2.500
wing_twist = -1.000
oswald_efficiency_factor= 0.600
wing_winglets_flag = 0
wing_sweep = 0.000
wing_pos_apex_lon = 1.3125
wing_pos_apex_vert = 2.100
htail_area = 18.200
htail_span = 9.600
htail_pos_lon = -13.400
htail_pos_vert = 1.300
htail_incidence = 1.130
htail_sweep = 30.000
vtail_area = 13.000
vtail_span = 4.440
vtail_sweep = 38.000
vtail_pos_lon = -13.500
vtail_pos_vert = 1.600
elevator_area = 10.640
aileron_area = 9.600
rudder_area = 6.550
elevator_up_limit = 30.000
elevator_down_limit = 20.000
aileron_up_limit = 20.000
aileron_down_limit = 20.000
rudder_limit = 28.000
elevator_trim_limit = 10.000
spoiler_limit = 0.600
spoilerons_available = 1
aileron_to_spoileron_gain = 3.000
min_ailerons_for_spoilerons = 10.000
min_flaps_for_spoilerons = 0.000
[Reference Speeds]
flaps_up_stall_speed = 33.000
full_flaps_stall_speed = 33.000
cruise_speed = 120.000
max_indicated_speed = 200 //Red line (KIAS)
[autopilot]
autopilot_available= 0
flight_director_available= 0
[forcefeedback]
ground_bumps_magnitude1=2600 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.6
ground_bumps_magnitude2=1200 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
ground_bumps_intercept2=0.085
ground_bumps_slope2=0.65
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=3500000 ; in microseconds
[stall_warning]
type=1
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 0
damaging-speed= 120.000
blowout-speed= 150.000
lift_scalar= 1.250
drag_scalar= 1.350
pitch_scalar= 0.010
flaps-position.0= 0.000, 0.000
flaps-position.1= 15.500, 0.000
flaps-position.2= 25.500, 0.000
flaps-position.3= 35.500, 0.000
