[fltsim.0] title=Zivko Edge 540 Kirby Chambliss sim=Zivko Edge 540 Kirby Chambliss model= panel= sound= texture= checklists= description=\n\n ui_variation=red bull [General] performance=By Mikko Maliniemi\ne-mail: mmniemi@hotmail.com\n\nM.M.Niemi's FS Planes\nhttp:\/\/gamma.nic.fi\/~mmniemi\/fsplanes\n\nDesigned with FS Design Studio\n\nPanel textures:\nAlex Wolski\ne-mail: N45328@aol.com\n\nAlexAerobatics\nhttp:\/\/www.alexaerobatics.homestead.com [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=0.000000,0.000000,0.000000 empty_weight=1500.000000 empty_weight_roll_MOI=1600.000000 empty_weight_pitch_MOI=3200.000000 empty_weight_yaw_MOI=3093.000000 empty_weight_coupled_MOI=0.000000 max_gross_weight=2250.000000 [fuel] Center1 = -2.6, 0.0, 0.0, 11.1, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center2 = -0.6, 0.0, 0.0, 2.3, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain = -1.8, -2.1, -0.8, 15.9, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = -1.8, 2.1, -0.8, 15.9, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 electric_pump=1 [airplane_geometry] wing_area=112.000000 wing_span=24.583333 wing_root_chord=4.583333 wing_dihedral=2.598267 wing_incidence=0.000000 wing_twist=0.000000 oswald_efficiency_factor=0.745333 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=28.000000 htail_span=10.500000 htail_pos_lon=-11.250000 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=15.000000 vtail_span=4.415880 vtail_sweep=0.000000 vtail_pos_lon=-12.500000 vtail_pos_vert=1.500000 elevator_area=10.000000 aileron_area=18.400000 rudder_area=7.000000 elevator_up_limit=26.000825 elevator_down_limit=26.000825 aileron_up_limit=30.000070 aileron_down_limit=30.000070 rudder_limit=30.000070 elevator_trim_limit=15.000035 spoiler_limit=0.000000 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [contact_points] point.0=1.000000,-21.666667,0.000000,-1.000000,1377.952756,0.000000,0.512270,45.600000,0.793601,2.500000,1.010076,0.000000,0.000000,0.000000,0.000000,0.000000 point.1=1.000000,3.833333,-3.166667,-5.166667,1968.503937,1.000000,0.512270,0.000000,0.448557,2.500000,0.515853,0.000000,0.000000,2.000000,0.000000,0.000000 point.2=1.000000,3.833333,3.166667,-5.166667,1968.503937,2.000000,0.512270,0.000000,0.448557,2.500000,0.515853,0.000000,0.000000,3.000000,0.000000,0.000000 point.3=2.000000,0.000000,-12.250000,-1.166667,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.000000,0.000000,12.250000,-1.166667,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.000000,-14.000000,0.000000,4.333333,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,3.416667,0.000000,-1.833333,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 static_pitch=9.041748 static_cg_height=3.844793 [brakes] toe_brakes_scale=1.000031 parking_brake=1 [Flaps.0] type=0 span-outboard=0.500000 extending-time=0.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=0.000000,0.000000 flaps-position.2=0.000000,0.000000 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 2.0 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 p_factor_on_yaw = 0.5 torque_on_roll = 0.5 [GeneralEngineData] engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = 3.5, 0.0, 0.60 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar= 1.0 //Fuel flow scalar min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser [piston_engine] power_scalar = 1.5 //Piston power scalar cylinder_displacement= 90.3 //Cubic inches per cylinder compression_ratio= 8.7 //Compression ratio number_of_cylinders=6 //Number of cylinders max_rated_rpm= 2700 //Max rated RPM max_rated_hp= 300 //Max rated HP fuel_metering_type= 0 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid normalized_starter_torque= 0.3 //Starter torque factor turbocharged= 0 //Is it turbocharged? 0=FALSE, 1=TRUE max_design_mp= 0 //Max design manifold pressure, (inHg) min_design_mp= 0 //Min design manifold pressure, (inHg) critical_altitude= 0 //Altitude to which the turbocharger will provide max design manifold pressure (feet) emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power emergency_boost_mp_offset= 0 //Additional manifold pressure supplied by emergency boost emergency_boost_gain_offset= 0 //Multiplier on manifold pressure due to emergency boost fuel_air_auto_mixture= 0 //Automixture available? 0=FALSE, 1=TRUE auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE max_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on maximum RPM mechanical efficiency idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction [propeller] thrust_scalar = 1.5 //Propeller thrust scalar propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter= 6.2 //Propeller Diameter, (feet) propeller_blades= 3 //Number of propeller blades propeller_moi= 5.9 //Propeller moment of inertia beta_max= 34 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min= 17 //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 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) [SMOKESYSTEM] smoke.0=0.00, -0.70, 1.40, fx_smoke_r [Reference Speeds] flaps_up_stall_speed=60.000000 full_flaps_stall_speed=48.000000 cruise_speed=177.673281 max_indicated_speed=245.000000 [keyboard_response] elevator=140.000000,240.000000 aileron=200.000000,1000.000000 rudder=200.000000,1000.000000 [Views] eyepoint=-2.921998,0.000000,1.589157 [autopilot] autopilot_available=0 flight_director_available=0 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [direction_indicators] direction_indicator.0=1,0
