[fltsim.0]
title=STALWART
sim=STALWART
model=
panel=
sound=
texture=
checklists=
atc_id=
atc_airline=
atc_flight_number=
ui_manufacturer=hama
ui_type=STALWART
ui_variation=
description= \nThe Globe/Temco Swift GC-1B was produced from 1946 to 1951. A total of 1498 of these sleek aircraft were produced and a high percentage of these planes are still flown today by loyal and loving owners! A real thoroughbred amongst GA planes they are mostly observed in their natural highly polished aluminum finish! This model portays serial number 1180 as it appeared circa 1970 with the STC gull wing canopy, Cessna seats and amphibeous floats.
kb_checklists=
kb_reference=
atc_id_color=
atc_heavy=
[General]
atc_type=Swift
atc_model=GC1
performance=\n SPECIFICATIONS: Engine make/model: Continental, Horsepower For Takeoff: 125,TBO hours: 2000 ,Fuel Type: 100LL ,Propeller type/diameter (in): 62" Wood,Gross weight (lbs): 1970 ,Empty weight, (lbs.): 1442 ,Useful load (lbs.): 528 ,Usable fuel - std. (gals.): 50 ,Wingspan: 29 ft. 3 in. ,Overall length: 20 ft. 9 in. ,Height: 6 ft. 1 in. \nPERFORMANCE:,Cruise speed (knots): ,80% power: 70 knots,Service ceiling (ft.): 14,000
Category=airplane
[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
[WEIGHT_AND_BALANCE]
empty_weight=2100 // (pounds)
reference_datum_position=3.6, 0, 2.1 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-5.3, 0, -5 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50
station_load.0=120, -3.0, -1.5, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1=120, -3.0, 1.5, 0.0 //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2=0, -8.0, 0.0, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI=2400.0
empty_weight_roll_MOI=2137.0
empty_weight_yaw_MOI=3360.0
CG_forward_limit=0.000000
CG_aft_limit=1.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=3160.000000
[exits]
number_of_exits = 2
exit_rate.0 = 0.17
exit_rate.1 = 0.2
[flight_tuning]
cruise_lift_scalar=0.0
parasite_drag_scalar=4.4
induced_drag_scalar=1.0
elevator_effectiveness=1.5
aileron_effectiveness=1.4
rudder_effectiveness=2.0
pitch_stability=2.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=0.7
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
stick_sensitivity_mode=0
[piston_engine]
power_scalar=1.0
cylinder_displacement=87.000000
compression_ratio=8.500000
number_of_cylinders=6
max_rated_rpm=2600.000000
max_rated_hp=125.000000
fuel_metering_type=1
cooling_type=0
normalized_starter_torque=1.100000
turbocharged=0
max_design_mp=0.000000
min_design_mp=0.000000
critical_altitude=0.000000
emergency_boost_type=0
emergency_boost_mp_offset=0.000000
emergency_boost_gain_offset=0.000000
fuel_air_auto_mixture=1
auto_ignition=0
fuel_flow_scalar=1.000000
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=0.500000
[propeller]
thrust_scalar=1.0
propeller_type=1
propeller_diameter=7.4000
propeller_blades=2
propeller_moi=1.900000
beta_max=0.000000
beta_min=0.000000
min_gov_rpm=0.000000
prop_tc=0.000000
gear_reduction_ratio=1.000000
fixed_pitch_beta=20.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_reverse_available=0
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000
[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
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
//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, -10.20, -5.020, -5.250, 2268.0, 1.000, 0.6, 0.000, 0.400, 2.500, 0.700, 3.000, 3.000, 2.000, 0.000, 0.000
point.1=1, -10.20, 5.020, -5.250, 2268.0, 1.000, 0.6, 0.000, 0.400, 2.500, 0.700, 3.000, 3.000, 2.000, 0.000, 0.000
point.2=1, 2.20, -5.020, -5.500, 2268.0, 1.000, 0.6, 33.000, 0.400, 2.500, 0.700, 3.000, 3.000, 2.000, 0.000, 0.000
point.3=1, 2.20, 5.020, -5.500, 2268.0, 2.000, 0.6, 33.000, 0.400, 2.500, 0.700, 3.000, 3.000, 3.000, 0.000, 0.000
point.4=2, -3.0, -10.5, -1.1, 1387.40, 0, 0.0000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0
point.5=2, -3.0, 10.5, -1.1, 1387.40, 0, 0.0000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0
point.6=2, -10.300, 0.00, -0.9, 1787.40, 0, 0.0000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0
point.7=2, 1.300, 0.00, -0.2, 1787.40, 0, 0.0000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0
point.8=4, -8.000, -5.250, -4.000, 1068.000, 0.000, 0.512, 0.000, 0.800, 2.500, 0.700, 0.000, 0.000, 1.000, 0.000, 0.0
point.9=4, -8.000, 5.250, -4.000, 1068.000, 0.000, 0.512, 0.000, 0.800, 2.500, 0.700, 0.000, 0.000, 2.000, 0.000, 0.0
point.10=4, 2.000, -5.250, -4.700, 1068.000, 0.000, 0.512, 20.000, 0.800, 2.500, 0.700, 0.000, 0.000, 3.000, 0.000, 0.0
point.11=4, 2.000, 5.250, -4.700, 1068.000, 0.000, 0.512, 20.000, 0.800, 2.500, 0.700, 0.000, 0.000, 2.000, 0.000, 0.0
point.12=5, 0.000, 5.250, -5.800, 1068.000, 0.000, 0.512, 20.000, 0.800, 2.500, 0.700, 0.000, 0.000, 2.000, 0.000, 0.0
//point.13=1, 0.000, -5.250, -5.800, 1068.000, 0.000, 0.512, 20.000, 0.800, 2.500, 0.700, 0.000, 0.000, 3.000, 0.000, 0.0
//point.14=1, -10.000, 5.250, -5.550, 1068.000, 0.000, 0.512, 20.000, 0.800, 2.500, 0.700, 0.000, 0.000, 2.000, 0.000, 0.0
//point.15=1, -10.000, -5.250, -5.550, 1068.000, 0.000, 0.512, 20.000, 0.800, 2.500, 0.700, 0.000, 0.000, 3.000, 0.000, 0.0
static_pitch=0.0
static_cg_height=5.240
gear_system_type=0
[ground_reaction]
main_gear_damping_ratio=1.4
[Views]
eyepoint=6,0.0,3.7
//[Views]
eyepoint=-7.4,-1.00,1.65 //(feet) longitudinal, lateral, vertical distance from reference datum
//eyepoint=-7.4,-0.70,1.2, pan
[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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//light.0=5, 9.7, 2.30, 0.5, fx_landing ,
//light.1=5, 9.7, -2.30, 0.5, fx_landing ,
light.2=4, 6.6 ,0.0 ,3.8, fx_vclighth,
[SMOKESYSTEM]
smoke.0=0, -11.0, 3.5,fx_smoke_engin_STALWART.fx ,
[EFFECTS]
wake=fx_wake
water = fx_spray
dirt=fx_tchdrt
concrete = fx_sparks
touchdown=fx_tchdwn, 1
[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
[fuel]
LeftMain = 0.000, -2.000, 2.000, 25.000, 0.000
RightMain = 0.000, 2.000, 2.000, 25.000, 0.000
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
[airplane_geometry]
wing_area=174.000000
wing_span=36.083333
wing_root_chord=4.916670
wing_tip_chord=4.916670
wing_dihedral=1.735840
wing_incidence=1.499634
wing_twist=-2.999268
oswald_efficiency_factor=0.708470
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=-2.371000
wing_pos_apex_vert=0.000000
htail_area=39.000000
htail_span=11.666667
htail_pos_lon=-18.266667
htail_pos_vert=0.000000
htail_incidence=3.246460
htail_sweep=0.000000
vtail_area=18.000000
vtail_pos_lon=-16.183333
vtail_pos_vert=1.500000
elevator_area=16.610000
aileron_area=18.300000
rudder_area=6.650000
elevator_up_limit=28.000447
elevator_down_limit=20.998903
aileron_up_limit=19.996227
aileron_down_limit=15.000035
rudder_limit=23.995472
elevator_trim_limit=19.497754
spoiler_limit=45.000000
vtail_span=4.837355
vtail_sweep=0.000000
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000
auto_spoiler_available=0
spoiler_extension_time=0.000000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-1.500000
negative_g_limit_flaps_down=-1.500000
[Flaps.0]
type=1
span-outboard=0.500000
extending-time=2.100000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=7.999280,0.000000
flaps-position.2=15.998561,0.000000
[Reference Speeds]
flaps_up_stall_speed=1.000000
full_flaps_stall_speed=1.200000
cruise_speed=55.000000
never_exceed_speed=300.00000
max_indicated_speed=250.000000
[GeneralEngineData]
engine_type=0
Engine.0=6.400000,0.000000,-1.300000
fuel_flow_scalar=1.000000
min_throttle_limit=0.000000
[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
autoland_available=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=\n\n
[brakes]
toe_brakes_scale=0.915555
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]
normal_pressure=0.000000
[stall_warning]
type=1
stick_shaker=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.000000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,1,1,1
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[deice_system]
structural_deice_type=0
