//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 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 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(Wheel Cover) sim = Savannah model = 2 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 = 3. Canadian C-DCMT Wheel Cover 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.3] title = Savannah 4(Wheel Cover) sim = Savannah model = 2 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 = 4. Italian I-5231 Wheel Cover 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 [General] [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 [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] reference_datum_position = -0.2, 0.0, 1.50 //Std FS Datum location empty_weight_CG_position = 1.3, 0.0, -1.64 //On thrust line CG_forward_limit= 0.5 // CG_aft_limit = -0.5 // empty_weight = 607.0 //Ref 2 max_gross_weight= 1232.0 //Ref 2 empty_weight_roll_MOI = 238.8 empty_weight_pitch_MOI = 307.1 empty_weight_yaw_MOI = 450.4 empty_weight_coupled_MOI= 0.0 max_number_of_stations= 2 station_load.0= 170.0, 0.0, -0.6, -2.5, L Seat //ACM station_load.1= 170.0, 0.0, 0.6, -2.5, R Seat //ACM [Fuel] fuel_type = 1 number_of_tank_selectors= 1 electric_pump = 1 LeftMain = 0.0, -3.0, 0.0, 10.5, 0.6 //ACM and Ref RightMain= 0.0, 3.0, 0.0, 10.5, 0.6 //ACM and Ref [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, 0.249, 2.5, 0.95, 0, 0, 0, 0, 0 point.1 = 1, -0.5016, -2.95, -5.5913, 1575, 1, 0.6, 0, 0.390, 1.277, 0.6, 0, 0, 2, 0, 0 point.2 = 1, -0.5215, 2.95, -5.5917, 1575, 2, 0.6, 0, 0.390, 1.277, 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 [Brakes] parking_brake = 1 toe_brakes_scale= 0.75 [Views] eyepoint= -1.0, -0.6, -0.9 [Airplane_geometry] wing_winglets_flag = 0 spoilerons_available = 0 spoiler_handle_available= 0 wing_area = 139.500 //Ref 1 wing_span = 29.620 //Ref 2 wing_root_chord = 4.724 //Ref 1 wing_dihedral = 0.000 //Ref 4 wing_incidence = 0.000 //Ref 4 wing_twist = -1.000 //Guess oswald_efficiency_factor = 0.870 //Perfect wing= 1.0 wing_sweep = 0.000 //Ref 4 wing_pos_apex_lon = 1.931 //Defined (1/4-chord fwd of Datum) wing_pos_apex_vert = 0.000 //Defined htail_area = 19.300 //ACM htail_span = 7.800 //ACM htail_pos_lon = -10.450 //ACM htail_pos_vert = -0.083 //ACM htail_incidence = 0.000 //Guess htail_sweep = 0.000 //Ref 4 vtail_area = 12.040 //ACM vtail_span = 3.500 //ACM vtail_sweep = 40.400 //ACM vtail_pos_lon = -9.690 //ACM vtail_pos_vert = -0.090 //ACM elevator_area = 8.950 //ACM aileron_area = 11.300 //ACM rudder_area = 5.870 //ACM 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 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons = 0.000 [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 [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 //ACM [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 = 6.00 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 [Electrical] engine_generator_map = 1 electric_always_available = 0 max_battery_voltage = 12.0 //Ref 3 generator_alternator_voltage = 13.5 //Ref 3 max_generator_alternator_amps= 18.5 //Ref 3 additional_system= 0, 5.0, 10.0 autopilot = 0, 5.0, 10.0 avionics_bus = 0, 5.0, 10.0 avionics = 1, 2.0, 10.0 flap_motor = 0, 5.0, 10.0 fuel_pump = 0, 5.0, 10.0 light_nav = 0, 5.0, 10.0 light_beacon = 0, 2.0, 10.0 light_landing = 0, 2.0, 10.0 light_taxi = 0, 2.0, 10.0 light_strobe = 0, 2.0, 10.0 light_panel = 0, 2.0, 10.0 marker_beacon = 1, 2.0, 10.0 pitot_heat = 0, 2.0, 10.0 starter1 = 0, 20.0, 10.0 [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 [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 [Effects] windshield_rain_effect_available= 1 wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown= fx_tchdwn_s, 1 startup = fx_engstrt_cub, 1 [Exits] number_of_exits= 2 exit_rate.0 = 0.3 exit_rate.1 = 0.3 [Stall_warning] type= 1 [Attitude_indicators] attitude_indicator.0= 1 [Turn_indicators] turn_indicator.0= 1,0 [Direction_indicators] direction_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 [Forcefeedback] stick_shaker_magnitude = 5000 //0 - 10000 stick_shaker_direction = 0 //0 - 35999 degrees stick_shaker_period = 111111 //in microseconds ground_bumps_magnitude1 = 3250 //0 - 10000 ground_bumps_angle1 = 8900 //0 - 35999 degrees ground_bumps_intercept1 = 5.00 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 = 1.000 crash_magnitude1 = 10000 //0 - 10000 crash_direction1 = 1000 //0 - 35999 degrees crash_magnitude2 = 10000 //0 - 10000 crash_direction2 = 9000 //0 - 35999 degrees crash_period2 = 75000 //in microseconds crash_duration2 =2500000 //in microseconds [Keyboard_response] elevator= 150.0, 250.0 aileron = 150.0, 250.0 rudder = 150.0, 250.0 [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
