//ICP. Savannah V.3.8 October 2010
//FD Ver 1.0, 9 Nov 05

//Ref 1: Savannah Specs from ICP (www.icp-avio.com)
//Ref 2: Savannah specs from Skykits Corp (www.skykits.com)
//Ref 3: Rotax 912ULS specs from Zenith Aircraft Co (www.zenithair.com)
//Ref 4: Savannah 3-view drawing

[fltsim.0]
title	=Savannah 1
sim	=Savannah
model	= 1
panel	=
sound	=
texture	= 1

visual_damage		=0

kb_checklists		=Savannah_check
kb_reference		=Savannah_ref

atc_heavy		=0
atc_airline		=
atc_flight_number	= CMT
atc_id_enable    	= 1
atc_id			= C-DCMT

atc_id_color		=0x00000000
atc_id_font		=Verdana,-11,1,600,0
ui_manufacturer		=ICP Italy
ui_type			=Savannah
ui_variation		=1. Canadian C-DCMT
ui_typerole    		= Ultralight
ui_createdby   		= Massimo Taccoli

Description		=The ICP Savannah is one of the top selling ultralights in Europe. It is dependable and easy to fly. It's STOL performance makes it easy to operate from any airfield. The Savannah is also a very good airplane for cross-country flights during which one can appreciate it's great stability.\n\nAircraft design:\nMassimo Taccoli\nSounds: Mike Hambly\n

[fltsim.1]
title	=Savannah 2
sim	=Savannah
model	=1
panel	=
sound	=
texture	=2

visual_damage		=0

kb_checklists		=Savannah_check
kb_reference		=Savannah_ref

atc_heavy		=0
atc_airline		=
atc_flight_number	=5231
atc_id_enable    	= 1
atc_id			=I-5231

atc_id_color		=0x00000000
atc_id_font		=Verdana,-11,1,600,0
ui_manufacturer		=ICP Italy
ui_type			=Savannah
ui_variation		= 2. Italian I-5231
ui_typerole    		= Ultralight
ui_createdby   		= Massimo Taccoli

Description		=The ICP Savannah is one of the top selling ultralights in Europe. It is dependable and easy to fly. It's STOL performance makes it easy to operate from any airfield. The Savannah is also a very good airplane for cross-country flights during which one can appreciate it's great stability.\n\nAircraft design:\nMassimo Taccoli \nSounds: Mike Hambly\n


[fltsim.2]

title  = Savannah 3
sim    = Savannah
model  = 2
panel  =
sound  =
texture= 3

visual_damage= 0

kb_checklists= Savannah_check
kb_reference = Savannah_ref

atc_heavy        = 0
atc_airline      =
atc_flight_number= CMT
atc_id_enable    = 1
atc_id           = C-DCMT
atc_id_color     = 0x00000000
atc_id_font      = Verdana,-11,1,600,0

ui_manufacturer= ICP Italy
ui_type        = Savannah
ui_variation   = 3. Canadian C-DCMT Wheel Cover
ui_typerole    = Ultralight
ui_createdby   = Massimo Taccoli

Description=The ICP Savannah is one of the top selling ultralights in Europe. It is dependable and easy to fly. It's STOL performance makes it easy to operate from any airfield. The Savannah is also a very good airplane for cross-country flights during which one can appreciate it's great stability. This FS aircraft represents a Canadian version fitted with wheel pants.\n\nAircraft design:\nMassimo Taccoli\nSounds: Mike Hambly\n

[fltsim.3]

title  = Savannah 4
sim    = Savannah
model  = 2
panel  =
sound  =
texture= 4

visual_damage  = 0

kb_checklists= Savannah_check
kb_reference = Savannah_ref

atc_heavy        = 0
atc_airline      =
atc_flight_number= 5231
atc_id_enable    = 1
atc_id           = I-5231
atc_id_color     = 0x00000000
atc_id_font      = Verdana,-11,1,600,0

ui_manufacturer= ICP Italy
ui_type        = Savannah
ui_variation   = 4. Italian I-5231 Wheel Cover
ui_typerole    = Ultralight
ui_createdby   = Massimo Taccoli

Description=The ICP Savannah is one of the top selling ultralights in Europe. It is dependable and easy to fly. It's STOL performance makes it easy to operate from any airfield. The Savannah is also a very good airplane for cross-country flights during which one can appreciate it's great stability. This FS aircraft represents an Italian version.\n\nAircraft design:\nMassimo Taccoli\nSounds: Mike Hambly\n

[General]
Performance=Length: 20 ft 4 in.\nHeight: 9 ft 1 in.\nWing Span: 29 ft 5 in.\nWing Area: 139.50 sq ft.\nEngine: Rotax 912S UL 4-cyl air-cooled.\nMax Power: 100 hp at 5,800 RPM at sea level.\nProp: 72 in fixed pitch.\nEmpty Weight: 607 lb.\nMTO Weight: 1,232 lb.\nMax Speed: 103 mph at sea level.\nCruise Speed: 93 mph at 5,000 ft.\nApproach Speed (full flaps): 35 mph IAS.\nStall (full flaps): 28 mph IAS at 1,000 lbs.\nInitial Climb Rate: 1,320 fpm at sea level.\nService Ceiling: 1 person: 15,000+ ft, 2 persons: 12,000+ ft.\nRange: 410 mi.\nFuel consumption (cruise): 5.3 gph. 
atc_type=Experimental 
editable=0 
Category= airplane

[Flight_tuning]
cruise_lift_scalar		=1.0 
parasite_drag_scalar		=1.0 
induced_drag_scalar		=1.0 
elevator_effectiveness		=1.0 
aileron_effectiveness		=1.0 
rudder_effectiveness		=1.0 
pitch_stability			=1.0 
roll_stability			=1.0 
yaw_stability			=1.0 
elevator_trim_effectiveness	=1.0 
aileron_trim_effectiveness	=1.0 
rudder_trim_effectiveness	=1.0 
hi_alpha_on_roll           = 1.0
hi_alpha_on_yaw            = 1.0
p_factor_on_yaw            = 1.0
torque_on_roll             = 0.3
gyro_precession_on_roll    = 0.3
gyro_precession_on_yaw     = 0.3

[weight_and_balance]

// ACM V2.5
max_gross_weight 	= 1232
empty_weight 		= 607
reference_datum_position = -0.2, 0, 1.5
empty_weight_CG_position = 1.3, 0, -1.64
empty_weight_pitch_MOI 	= 307.1
empty_weight_roll_MOI 	= 238.8
empty_weight_yaw_MOI 	= 450.4
empty_weight_coupled_MOI = 0
CG_forward_limit 	= 0.5
CG_aft_limit 		= -0.5
max_number_of_stations 	= 2

station_load.0 		= 170.0,  0.0, -0.6, -2.5, L Seat
station_load.1 		= 170.0,  0.0,  0.6, -2.5, R Seat


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3,   0.6, -15.15,  0.6, fx_navred
light.1 = 3,   0.6,  15.15,  0.6, fx_navgre
light.2 = 3, -13.0,   0.00,  3.4, fx_navwhi

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type 		= 0
fuel_flow_scalar 	= 0.82
min_throttle_limit 	= 0.0
engine.0 		= 6.04, 0.0, -1.64

[smokesystem]
smoke.0 = -3.68, 3.1, 0, fx_SmokeStack

[effects]
wake 	= fx_wake
water 	= fx_spray
dirt 	= fx_tchdrt
concrete 	= fx_sparks
touchdown 	= fx_tchdwn_s, 1
startup 	= fx_engstrt_cub, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type 		= 1
number_of_tank_selectors = 1
electric_pump 		= 1

LeftMain 	= 0, -3, 0, 10.5, 0.6
RightMain 	= 0, 3, 0, 10.5, 0.6


[contact_points]
static_pitch 		= -0.85
static_cg_height 	= 3.95
tailwheel_lock 		= 0
gear_system_type 	= 0
max_number_of_points 	= 7

point.0 = 1, 	 4.1673,  0,    -5.5087, 1575, 0, 0.6, 33,   0.1744, 2.5,   0.95, 0,   0,   0, 0,   0
point.1 = 1, 	-0.5016, -2.95, -5.5913, 1575, 1, 0.65, 0,   0.3912, 1.275, 0.6,  0,   0,   2, 0,   0
point.2 = 1, 	-0.5215,  2.95, -5.5917, 1575, 2, 0.65, 0,   0.3912, 1.275, 0.6,  0,   0,   3, 0,   0
point.3 = 2,   	 1.200, -15.10,  0.60,   1575, 0, 0.0,  0.0, 0.0,    0.0,   0.0,  0.0, 0.0, 5, 0.0, 0.0
point.4 = 2,     1.200,  15.10,  0.60,   1575, 0, 0.0,  0.0, 0.0,    0.0,   0.0,  0.0, 0.0, 6, 0.0, 0.0
point.5 = 2,   -14.000,   0.00, -0.46,   1575, 0, 0.0,  0.0, 0.0,    0.0,   0.0,  0.0, 0.0, 9, 0.0, 0.0
point.6 = 2,     5.600,   0.00, -2.90,   1575, 0, 0.0,  0.0, 0.0,    0.0,   0.0,  0.0, 0.0, 4, 0.0, 0.0


[keyboard_response]
elevator = 150.0, 250.0
aileron  = 150.0, 250.0
rudder   = 150.0, 250.0


[forcefeedback]
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.00
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1.000
crash_magnitude1 = 10000
crash_direction1 = 1000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]

wing_area 		= 139.500
wing_span 		= 29.620
wing_root_chord 	= 4.724
wing_dihedral 		= 0.000
wing_incidence 		= 0.000
wing_twist 		= -1.000
oswald_efficiency_factor = 0.870
wing_winglets_flag 	= 0
wing_sweep 		= 0.000
wing_pos_apex_lon 	= 1.931
wing_pos_apex_vert 	= 0.000
htail_area 		= 19.300
htail_span 		= 7.800
htail_pos_lon 		= -10.450
htail_pos_vert 		= -0.083
htail_incidence 	= 0.000
htail_sweep 		= 0.000
vtail_area 		= 12.040
vtail_span 		= 3.500
vtail_sweep 		= 40.400
vtail_pos_lon 		= -9.690
vtail_pos_vert 		= -0.090
elevator_area 		= 8.950
aileron_area 		= 11.300
rudder_area 		= 5.870
elevator_up_limit 	= 23.000
elevator_down_limit 	= 18.000
aileron_up_limit 	= 19.500
aileron_down_limit 	= 15.000
rudder_limit 		= 23.500
elevator_trim_limit 	= 30.000
spoiler_limit 		= 0.000
aileron_to_spoileron_gain 	= 0.000
spoiler_handle_available 	= 0
min_ailerons_for_spoilerons 	= 0.000
min_flaps_for_spoilerons 	= 0.000
spoilerons_available 		= 0
auto_spoiler_available		=0
positive_g_limit_flaps_up	=4.000000
positive_g_limit_flaps_down	=2.000000
negative_g_limit_flaps_up	=-2.000000
negative_g_limit_flaps_down	=-1.000000

[electrical]
max_battery_voltage 		= 12
generator_alternator_voltage 	= 13.5
max_generator_alternator_amps 	= 18.5
engine_generator_map 		= 1
electric_always_available 	= 0
flap_motor 			= 0, 5, 10
autopilot 			= 0, 5, 10
avionics_bus 			= 0, 5, 10
avionics 			= 1, 2, 10
pitot_heat 			= 0, 2, 10
additional_system 		= 0, 5, 10
marker_beacon 			= 1, 2, 10
fuel_pump 			= 0, 5, 10
starter1 			= 0, 20, 10
light_nav 			= 0, 5, 10
light_beacon 			= 0, 2, 10
light_landing 			= 0, 2, 10
light_taxi 			= 0, 2, 10
light_strobe 			= 0, 2, 10
light_panel 			= 0, 2, 10

[Brakes]
parking_brake             = 1
auto_brakes               = 0
toe_brakes_scale          = 0.75
differential_braking_scale= 1.00

[Views]
eyepoint=-1.0, -0.6, -0.9 

[Flaps.0]
type          = 1
system_type   = 0
span-outboard = 0.5
extending-time= 2.0
flaps-position.0=  0.0						//Ref 1
flaps-position.1= 20.0, 52.0					//Ref 1
flaps-position.2= 40.0, 52.0					//Ref 1

[Piston_engine]
power_scalar=1.0 
max_rpm_mechanical_efficiency_scalar	=1.0 
idle_rpm_mechanical_efficiency_scalar	=1.0 
max_rpm_friction_scalar			=1.0 
idle_rpm_friction_scalar		=1.0 
fuel_metering_type			=1 		//Ref 3
cooling_type				=0   	//Ref 3
turbocharged				=0 
emergency_boost_type			=0 
fuel_air_auto_mixture			=0 
auto_ignition				=0 
number_of_cylinders			=4 		//Ref 3
cylinder_displacement			=20.65 	//Ref 3
compression_ratio			=10.50 	//Ref 3 
max_rated_rpm				=5800.00 	//Ref 3 
max_rated_hp				=100.00 	//Ref 3 
normalized_starter_torque		=0.30 
max_design_mp				=0.00 
min_design_mp				=0.00 
critical_altitude			=0.00 
emergency_boost_mp_offset		=0.00 
emergency_boost_gain_offset		=0.00 

[Propeller]
thrust_scalar				=1.0 
rotation                           	= 1
propeller_type				=1 
prop_sync_available			=0 
prop_deice_available			=0 
prop_feathering_available		=0 
prop_auto_feathering_available		=0 
defeathering_accumulators_available	=0 
prop_reverse_available			=0 
propeller_blades			=2 
propeller_diameter			=6 
propeller_moi				=5.00 
beta_max				=0.00 
beta_min				=0.00 
fixed_pitch_beta			=23.00 
beta_feather				=0.00 
minimum_on_ground_beta			=0.00 
minimum_reverse_beta			=0.00 
min_gov_rpm				=0.00 
prop_tc					=0.10 
gear_reduction_ratio			=2.43 	//Ref 3
low_speed_theory_limit			=80.00 
min_rpm_for_feather			=0.00 
power_absorbed_cf			=0.00 

[Radios]
Audio.1	=0 
Com.1	=1, 0 
Com.2	=0, 0 
Nav.1	=0, 0, 0 
Nav.2	=0, 0, 0 
Adf.1	=0, 0 
Transponder.1=0 
Marker.1=0 

[Hydraulic_system]
normal_pressure	= 0.0

[Deice_system]
structural_deice_type= 0

[Pneumatic_system]
max_pressure    = 0.0
bleed_air_scalar= 0.0

[Vacuum_system]
vacuum_type             = 1
engine_map              = 1,0,0,0
max_pressure            = 5.15
electric_backup_pressure= 0.00

[Exits]
number_of_exits= 2
exit_rate.0    = 0.3
exit_rate.1    = 0.3

[Stall_warning]
type        = 1
stick_shaker= 1

[Pitot_static]
vertical_speed_time_constant= 2.0
pitot_heat                  = 1.0

[Airspeed_indicators]
airspeed_indicator.0= 1,0

[Altimeters]
altimeter.0= 1

[Attitude_indicators]
attitude_indicator.0= 1

[Direction_indicators]
direction_indicator.0=1,0 

[Turn_indicators]
turn_indicator.0= 1,0

[Autopilot]
autopilot_available=1 
flight_director_available=1 
default_pitch_mode          =  0
default_bank_mode           =  0
autothrottle_available=1 
autothrottle_arming_required=  0
autothrottle_takeoff_ga             =     1.0
autothrottle_max_rpm                =  5600.0 
max_throttle_rate                   =     0.1
default_vertical_speed=700.0 
pitch_takeoff_ga=8.0 
max_pitch                           =    10.0
max_pitch_acceleration              =     1.0
max_pitch_velocity_lo_alt           =     2.0
max_pitch_velocity_hi_alt           =     1.5
max_pitch_velocity_lo_alt_breakpoint= 20000.0
max_pitch_velocity_hi_alt_breakpoint= 28000.0
max_bank                            =    25.0
max_bank_acceleration               =     1.8
max_bank_velocity                   =     3.0
nav_proportional_control            =     9.0
nav_integrator_control              =     0.25
nav_derivative_control              =     0.0
nav_integrator_boundary             =     2.5
nav_derivative_boundary             =     0.0
gs_proportional_control             =     9.52
gs_integrator_control               =     0.26
gs_derivative_control               =     0.0
gs_integrator_boundary              =     0.7
gs_derivative_boundary              =     0.0
yaw_damper_gain                     =     0.0

[Reference Speeds]
full_flaps_stall_speed	=28.0 
flaps_up_stall_speed	=35.0 
cruise_speed		=89.9 
max_indicated_speed   	=108.6		//Ref 1

[CameraDefinition.0]
Title          = "Tail"
Guid           = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64A}
Description    = Looking forward from the tip of the vertical stabilizer
Origin         = Center
SnapPbhAdjust  = Swivel
SnapPbhReturn  = FALSE
PanPbhAdjust  = Swivel
PanPbhReturn  = FALSE
Track         = None
ShowAxis      = FALSE
AllowZoom     = TRUE
InitialZoom   = .5
ShowWeather   = Yes
InitialXyz    = 0, 0.5, -10.0
InitialPbh    = 10, 0, 0
XyzAdjust     = TRUE
Category      = Aircraft
MomentumEffect= TRUE
ClipMode      = Minimum
[CameraDefinition.1]
Title         = "Nose"
Guid          = {8A1987D0-09B6-7E48-B4E1-62C5DBE2A720}
Description   = Looking back from the nose of the engine toward the cockpit
Origin        = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust  = Swivel
PanPbhReturn  = FALSE
Track         = None
ShowAxis      = FALSE
AllowZoom     = TRUE
InitialZoom   = .5
ShowWeather   = Yes
InitialXyz    = 0.0, 0.5, 8.0
InitialPbh    = 20, 0, 180
XyzAdjust     = TRUE
Category      = Aircraft
MomentumEffect= FALSE
ClipMode      = Minimum
[CameraDefinition.2]
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    = 8.0, 0.5, 0.0
InitialPbh    = 0, 0, 270
XyzAdjust     = TRUE
Category      = Aircraft
MomentumEffect= FALSE
ClipMode      = Minimum
[CameraDefinition.3]
Title         = "Left Wing"
Guid          = {7a91803e-898b-435a-8391-725be6a48203}
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    = -8.0, 0.5, 0.0
InitialPbh    = 0, 0, 90
XyzAdjust     = TRUE
Category      = Aircraft
MomentumEffect= FALSE
ClipMode      = Minimum
[CameraDefinition.001]
Title         = "Right Seat"
Guid          = {8ff6c134-098d-409f-baec-caba3f683f98}
Origin        = Virtual Cockpit
MomentumEffect= YES
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust  = Swivel
PanPbhReturn  = False
Track         = None
ShowAxis      = YES
AllowZoom     = TRUE
InitialZoom   = .6
SmoothZoomTime= 2.0
ZoomPanScalar = 1.0
ShowWeather   = Yes
XyzAdjust     = TRUE
ShowLensFlare = FALSE
Category      = Cockpit
PitchPanRate  = 20
HeadingPanRate= 60
InitialXyz    = 0.4, 0.0, 0.0
InitialPbh    = 0, 0, 0