[fltsim.0]
title=SF 28 A Tandemfalke
sim=SF28
model=
panel=
sound=
texture=
kb_checklists=sf28_check
kb_reference=sf28_ref
description="Scheibe SF 28 A Tandem-Falke"
ui_manufacturer="Scheibe"
ui_type="SF 28 A Tandemfalke"
ui_typerole="Motorglider"
ui_createdby"Wolfgang Piper"
ui_variation=
visual_damage=1
atc_heavy=0
atc_id=FCEYS
atc_airline=
atc_flight_number=
prop_anim_ratio=0.5
[General]
performance=Länge:8.15 m \nSpannweite: 16.3m \nGewicht: 580 kg max, 380 kg leer\nDesigner: Wolfgang Piper, 07/2006
Category=airplane
[CameraDefinition.0]
Title = "Tail"
Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description = Looking forward from behind the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .75
ShowWeather = Yes
InitialXyz = 0, 3.1, -20.0
InitialPbh = 10, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.1]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 12.5, 1.9, 0.0
InitialPbh = 9, 0, 270
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = TRUE
ClipMode=Minimum
[CameraDefinition.2]
Title = "Left Wing"
Guid = {33320004-b71a-4f9f-9105-1eb674ab7f3c}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = -12.5, 1.9, 0.0
InitialPbh = 9, 0, 90
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = TRUE
ClipMode=Minimum
[CameraDefinition.001]
Title = "Rear Seat"
Guid = {195EAB58-9E4A-4E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = .7
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=30
HeadingPanRate=75
PanAcceleratorTime=0
InitialXyz=0.0, 0.0, -1.15
InitialPbh=0, 0, 0
[WEIGHT_AND_BALANCE]
max_gross_weight=1385.000000
empty_weight=885.000000
reference_datum_position=0.0000, 0.0000, 0.0000
empty_weight_CG_position=-3.90000,0.000000,0.000000
station_load.0=170,2.00000,0.000000,0.000000 // Pilot
station_load.1=170,-1.00000,0.000000,0.000000 // Guest
station_load.2=10,-16.00000,0.000000,0.000000 // CG- Korrektur
empty_weight_roll_MOI=900.000000
empty_weight_pitch_MOI=2300.000000
empty_weight_yaw_MOI=700.000000
empty_weight_coupled_MOI=0.000000
[GeneralEngineData]
engine_type=0
Engine.0=6.5, 0.0, 0.00
fuel_flow_scalar=0.88
min_throttle_limit=0.00000
[Electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 33
[piston_engine]
power_scalar=1.00
cylinder_displacement=60.0
compression_ratio=7.5
number_of_cylinders=2
max_rated_rpm=3420
max_rated_hp=220
fuel_metering_type=1
cooling_type=0
normalized_starter_torque=0.3
turbocharged=0
max_design_mp=0
min_design_mp=0
critical_altitude=0
emergency_boost_type=0
emergency_boost_mp_offset=0
emergency_boost_gain_offset=0
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.45
idle_rpm_mechanical_efficiency_scalar=1.45
max_rpm_friction_scalar=1.10
idle_rpm_friction_scalar=1.10
[propeller]
thrust_scalar = 0.6 //Propeller thrust scalar
propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 5.0 //Propeller Diameter, (feet)
propeller_blades= 2 //Number of propeller blades
propeller_moi= 3 //Propeller moment of inertia
beta_max= 45.0 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 15.0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1100.0 //Miminum governed RPM
prop_tc= 0.1 //Prop time-constant
gear_reduction_ratio= 0.95 //Propeller gear reduction ratio
fixed_pitch_beta= 0.0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit= 80.0 //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= 1 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather= 700.0 //Minimum RPM for prop feathering
beta_feather= 50.5 //Feathering pitch angle (degrees)
power_absorbed_cf= 0.9 //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= 15.0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0.0 //Minimum pitch angle in reverse, (degrees)
[airplane_geometry]
wing_area=285.000000
wing_span=53.500000
wing_root_chord=5.3
wing_dihedral=3
wing_incidence=1.5
wing_twist=-0.999756
oswald_efficiency_factor=0.7
wing_winglets_flag=0
wing_sweep=3.000000
wing_pos_apex_lon=0.80000000
wing_pos_apex_vert=-1.000000
htail_area=24.000000
htail_span=9.3
htail_pos_lon=-14
htail_pos_vert=1.2
htail_incidence=0
htail_sweep=0.000000
vtail_area=16.000000
vtail_span=4.6
vtail_sweep=0.000000
vtail_pos_lon=-16.000000
vtail_pos_vert=2.5
elevator_area=12.4
aileron_area=11.900000
rudder_area=10.5
elevator_up_limit=20
elevator_down_limit=30
aileron_up_limit=18
aileron_down_limit=15
rudder_limit=25
elevator_trim_limit=20
spoiler_limit=40
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=0.800000
positive_g_limit_flaps_up=5.500000
positive_g_limit_flaps_down=5.500000
negative_g_limit_flaps_up=-3.500000
negative_g_limit_flaps_down=-3.500000
load_safety_factor=1.5
[flight_tuning]
cruise_lift_scalar=1.34
parasite_drag_scalar=0.8
induced_drag_scalar=0.84
elevator_effectiveness=0.6
aileron_effectiveness=0.6
rudder_effectiveness=0.8
pitch_stability=1.0
roll_stability=1.1
yaw_stability=0.8
elevator_trim_effectiveness=1.3
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=0.8
p_factor_on_yaw=-1.0 //dreht nach rechts
torque_on_roll=-1.0 //dreht nach rechts
[fuel]
Center1 = 4.5, 0.000, 1.000, 10.600, 0.000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=1
[contact_points]
//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
// Lang. Breit. Vert.
// Pos. Pos. Pos.
// 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15
//--------------------------------------------------------------------------------------------------------------------------------
point.0=1, -14.76, 0, -0.8, 1800, 0, 0.5, 20, 0.25, 2.5, 0.7, 0, 0, 0, 0, 0 // Gear Tail
point.1=1, 1.0, -0.1, -3.1, 2500, 1, 0.5, 0, 0.3, 2.5, 0.7, 0, 0, 2, 0, 0 // Gear Main
point.2=1, 1.0, 0.1, -3.1, 2500, 2, 0.5, 0, 0.3, 2.5, 0.7, 0, 0, 3, 0, 0 // Gear Main
point.3=1, -0.9, -8.6, -2.6, 2500, 0, 0.4, 0, 0.3, 2.5, 0.7, 0, 0, 2, 0, 0 // Gear Left
point.4=1, -0.9, 8.60, -2.6, 2500, 0, 0.4, 0, 0.3, 2.5, 0.7, 0, 0, 3, 0, 0 // Gear Right
point.5=2, 0, -21.0, 1.1, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 // Wing Tip
point.6=2, 0, 21.0, 1.1, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 // Wing Tip
point.7=2, -14.76, 0, -0.2, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 // Tail(?)
point.8=2, 6.5, 0, -2.6, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 // Nose
static_pitch=7 //degrees (pitch when loaded on ground)
static_cg_height=3.0 //feet, altitude of CG when at rest on the ground
gear_system_type=0
[Views]
eyepoint=1.30, 0, 1.55 //(feet) longitudinal, lateral, vertical distance from reference datum
[Reference Speeds]
flaps_up_stall_speed=35.000000
full_flaps_stall_speed=33.500000
cruise_speed=45
max_indicated_speed=150
[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000
[autopilot]
autopilot_available=0
flight_director_available=1
default_vertical_speed=700.000000
autothrottle_available=0
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_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=2,0
[exits]
number_of_exits=4
exit_rate.0=0.5
exit_rate.1=1
exit_rate.2=1
exit_rate.3=1
[Flaps.0]
type=0
[brakes]
toe_brakes_scale=1.000031
parking_brake=1
[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=0
[vacuum_system]
max_pressure=0
vacuum_type=1
[pneumatic_system]
max_pressure=0
[deice_system]
structural_deice_type=0
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
