[fltsim.0] title=Altair sim=Altair model= panel= sound= texture= kb_checklists= prop_anim_ratio=1.76 ui_manufacturer=Lockheed atc_id_color=0x00000000 atc_heavy=0 atc_id_font= visual_damage=0 description=This plane was procured and outfited for the London to Melbourne race. [General] atc_type= atc_model= editable=1 performance=Weight: Empty 3550 lbs Gross 5800 lbs\n Span:42' 9 1\/4"\n Length:28' 11"\n Speed: 187 mph cruise, 220 mph max\n Ceiling: 24500 ft \n Power:550 hp P&W Wasp\n Designer: P. Clawson\n Date: 11\/2004\n [pitot_static] vertical_speed_time_constant=2 [weight_and_balance] // ACM V2.5 max_gross_weight = 5800 empty_weight = 3550 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 5833 empty_weight_roll_MOI = 2944 empty_weight_yaw_MOI = 8306 empty_weight_coupled_MOI = 0 CG_forward_limit = 0 CG_aft_limit = 1 max_number_of_stations = 3 station_load.0 = 170, -3, 0, 0.0 station_load.1 = 0, 0, 0, 0, co-pilot station_load.2 = 0, 0, 0, 0 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -0.947, -20.812, -0.288, fx_navred light.1 = 3, -0.947, 20.812, -0.288, fx_navgre light.2 = 3, -16.731, 0, -0.575, fx_navwhi light.3 = 3, -0.947, -20.812, -0.748, fx_navred light.4 = 3, -0.947, 20.812, -0.748, fx_navgre light.5 = 4, -0.2, 0, 3.35, fx_vclight [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 0 fuel_flow_scalar = 1 min_throttle_limit = 0.1 engine.0 = 5.78, 0, 0, [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn_s, 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 = 0 LeftMain = 0, -2.5, 0, 85, 0 RightMain = 0, 2.5, 0, 85, 0 [contact_points] static_pitch = 13 static_cg_height = 6.5 tailwheel_lock = 0 gear_system_type = 1 max_number_of_points = 7 point.0 = 1, -14.6941, 0, -3.7726, 1574.8032, 0, 0.63, 22, 0.2, 2.5, 0.8, 2.2, 2, 0, 132, 150 point.1 = 1, 0.0247, -5.4027, -7.0778, 1574.8032, 1, 1.3, 0, 0.714684, 2.5, 0.274063, 6, 6, 2, 132, 150 point.2 = 1, 0.1377, 5.5366, -7.07, 1574.8032, 2, 1.3, 0, 0.714684, 2.5, 0.274063, 6.5, 6.5, 3, 132, 150 point.3 = 2, -25.9474, -0.035, -0.0712, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.4 = 2, -3, 21.1476, -0.9025, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5 = 2, -3, -21.3486, -0.7688, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.6 = 2, 6.8428, 0, -2.8765, 1250, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0 [keyboard_response] elevator = 350, 500 aileron = 450, 1000 rudder = 200, 1000 [airplane_geometry] wing_area = 294.1 wing_span = 42.9 wing_root_chord = 6.8 wing_dihedral = 4.5 wing_incidence = 0 wing_twist = 0 oswald_efficiency_factor = 0.8 wing_winglets_flag = 0 wing_sweep = 0 wing_pos_apex_lon = 1.51011904761905 wing_pos_apex_vert = 0 htail_area = 38 htail_span = 16 htail_pos_lon = -15.9 htail_pos_vert = 0 htail_incidence = 0 htail_sweep = 0 vtail_area = 23.8 vtail_span = 7.25 vtail_sweep = 0 vtail_pos_lon = -15.9 vtail_pos_vert = 0 elevator_area = 21.6 aileron_area = 22.4 rudder_area = 14.9 elevator_up_limit = 22 elevator_down_limit = 22 aileron_up_limit = 22 aileron_down_limit = 22 rudder_limit = 22 elevator_trim_limit = 18 spoiler_limit = 60 aileron_to_spoileron_gain = 0 spoiler_handle_available = 1 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 spoilerons_available = 0 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 60 engine_generator_map = 1 electric_always_available = 1 [flight_tuning] cruise_lift_scalar=1 parasite_drag_scalar=0.5 induced_drag_scalar=0.5 elevator_effectiveness=1 aileron_effectiveness=1 rudder_effectiveness=1 pitch_stability=1 roll_stability=1 yaw_stability=1 elevator_trim_effectiveness=1 aileron_trim_effectiveness=1 rudder_trim_effectiveness=1 hi_alpha_on_roll=1 hi_alpha_on_yaw=1 p_factor_on_yaw=1 torque_on_roll=1 gyro_precession_on_roll=1 gyro_precession_on_yaw=1 [piston_engine] power_scalar=1 cylinder_displacement=161.0 compression_ratio=6.5 number_of_cylinders=9 max_rated_rpm=2250 max_rated_hp=550 fuel_metering_type=1 cooling_type=1 normalized_starter_torque=0.07 turbocharged=1 max_design_mp=44 min_design_mp=9 critical_altitude=5100 emergency_boost_type=0 emergency_boost_mp_offset=0 emergency_boost_gain_offset=0 fuel_air_auto_mixture=0 auto_ignition=0 emergency_boost_duration=300 max_rpm_mechanical_efficiency_scalar=1 idle_rpm_mechanical_efficiency_scalar=1 max_rpm_friction_scalar=1 idle_rpm_friction_scalar=2.0 [propeller] thrust_scalar = 1.0 //Propeller thrust scalar propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter= 9.0 //Propeller Diameter, (feet) propeller_blades= 2 //Number of propeller blades propeller_moi= 12.76 //Propeller moment of inertia beta_max= 24.0 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min= 14.0 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm= 1400 //Miminum governed RPM prop_tc= 0.1 //Prop time-constant gear_reduction_ratio= 1.0 //Propeller gear reduction ratio fixed_pitch_beta= 0 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit= 80 //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= 0 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather= 0 //Minimum RPM for prop feathering beta_feather= 0 //Feathering pitch angle (degrees) power_absorbed_cf= 0 //Coefficient of friction for power absorbed by propeller in feather 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= 0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta= 0 //Minimum pitch angle in reverse, (degrees) [TailHook] tailhook_length=4 tailhook_position=-15, 0, -1 cable_force_adjust=1 [Views] eyepoint=-0.2, 0, 3.55 [Flaps.0] type=1 span-outboard=0.500000 extending-time=4.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=35.000000,0.000000 [direction_indicators] direction_indicator.0=1, 0 [exits] number_of_exits=1 exit_rate.0=0.4 [autopilot] autopilot_available=0 flight_director_available=0 default_vertical_speed=1000 autothrottle_available=0 autothrottle_arming_required=0 autothrottle_max_rpm=90 autothrottle_takeoff_ga=1 pitch_takeoff_ga=8 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000 max_pitch_velocity_hi_alt_breakpoint=28000 max_pitch=10 max_pitch_acceleration=1 max_pitch_velocity_lo_alt=2 max_bank=25 max_bank_acceleration=1.8 max_bank_velocity=3 max_throttle_rate=0.1 nav_proportional_control=9 nav_integrator_control=0.25 nav_derivative_control=0 nav_integrator_boundary=2.5 nav_derivative_boundary=0 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0 gs_integrator_boundary=0.7 gs_derivative_boundary=0 yaw_damper_gain=0 [Reference Speeds] flaps_up_stall_speed=59.1 full_flaps_stall_speed=48.7 cruise_speed=97 max_indicated_speed=304 max_mach=0.46 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.1 flap_limit_idle=33.75 flap_limit_power=16.875 [brakes] toe_brakes_scale=0.20 parking_brake=1 [stall_warning] type=1 [hydraulic_system] electric_pumps=0 engine_map=1, 0, 0, 0 normal_pressure=1000 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
