[fltsim.0] title=Zodiac XL Red/White sim=Zenith Zodiac XL model= panel= sound= texture= checklists= description=Zenair's kit-built 'ZodiacXL' is the latest generationof the Zodiac line. Economical and a pleasure to fly, the 2-seat,all-metal, bubble-canopied Zodiac combines excellent performance, handling, and visibilty, with low cost and building ease, making it a favorite around the world. ui_manufacturer="Zenair" // new ui_type="601UL" // new //ui_manufacturer=Zenith Aircraft Company //ui_type=Zodiac XL ui_variation=Zodiac XL Red/White atc_heavy=0 atc_id=9601Z atc_airline= atc_flight_number= [fltsim.1] title=Zodiac XL Red/White Stripes sim=Zenith Zodiac XL model= panel= sound= texture=1 checklists= description=Zenair's kit-built 'ZodiacXL' is the latest generation of the Zodiac line. Economical and a pleasure to fly, the 2-seat,all-metal, bubble-canopied Zodiac combines excellent performance, handling, and visibilty, with low cost and building ease, making it a favorite around the world. ui_manufacturer="Zenair" // new ui_type="601UL" // new //ui_manufacturer=Zenith Aircraft Company //ui_type=Zodiac XL ui_variation=Zodiac XL Red/White Stripes atc_heavy=0 atc_id=283WP atc_airline= atc_flight_number= [fltsim.2] title=Zodiac XL red wing bar sim=Zenith Zodiac XL model= panel= sound= texture=2 checklists= description=Zenair's kit-built 'Zodiac 601UL' is the microlight model in the Zodiac line. A 2-seat,all-metal, bubble-canopied Zodiac combines excellent performance, handling, and visibilty, with low cost and building ease. The version here is modelled on G-CDLW based at EGHP (Popham). ui_manufacturer="Zenair" // new ui_type="601UL" // new //ui_manufacturer=Zenith Aircraft Company //ui_type=Zodiac XL ui_variation=Zodiac XL red wing bar atc_heavy=0 atc_id=G-CDLW atc_airline= atc_flight_number= [WEIGHT_AND_BALANCE] reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= -0.450, 0.000, 0.000 max_number_of_stations=50 station_load.0= 170.000, 0.000, 0.000, 0.000 empty_weight= 550.000 empty_weight_roll_MOI= 400.000 empty_weight_pitch_MOI= 650.000 empty_weight_yaw_MOI= 700.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 1058.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [fuel] LeftMain= 0.000, -5.000, 0.000, 8.000, 0.000 RightMain= 0.000, 5.000, 0.000, 8.000, 0.000 fuel_type=1.000 number_of_tank_selectors=1 electric_pump=0 [WEIGHT_AND_BALANCE] reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= -0.450, 0.000, 0.000 max_number_of_stations=50 station_load.0= 170.000, 1.9,-1.0,0.0 //0.000, 0.000, 0.000 station_load.1= 170.000, 1.9,1.0,0.0 // new station_name.0 = "Pilot" station_name.1 = "Passenger" empty_weight= 550.000 empty_weight_roll_MOI= 400.000 empty_weight_pitch_MOI= 650.000 empty_weight_yaw_MOI= 700.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 1058.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [fuel] LeftMain= 1.000, -4.850, 0.150, 8.000, 0.000 RightMain= 1.000, 5.150, 0.150, 8.000, 0.000 fuel_type=1.000 number_of_tank_selectors=1 [airplane_geometry] wing_area= 122.000 wing_span= 27.000 wing_root_chord= 4.500 wing_dihedral= 3.000 wing_incidence= 0.000 wing_twist= -1.000 oswald_efficiency_factor= 0.837 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 0.000 wing_pos_apex_vert= 0.000 htail_area= 18.000 htail_span= 7.250 htail_pos_lon= -11.667 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 6.000 vtail_span= 2.793 vtail_sweep= 0.000 vtail_pos_lon= -12.417 vtail_pos_vert= 1.500 elevator_area= 7.740 aileron_area= 12.200 rudder_area= 2.100 elevator_up_limit= 27.502 elevator_down_limit= 20.626 aileron_up_limit= 19.481 aileron_down_limit= 14.897 rudder_limit= 23.491 elevator_trim_limit= 19.481 spoiler_limit= 59.989 spoilerons_available= 0 aileron_to_spoileron_gain= 0.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 auto_spoiler_available=0 spoiler_extension_time=5.000000 positive_g_limit_flaps_up=4.000000 positive_g_limit_flaps_down=2.000000 negative_g_limit_flaps_up=-1.500000 negative_g_limit_flaps_down=-1.500000 [contact_points] point.0= 1.000, 5.333, 0.000, -3.550, 2000.000, 0.000, 0.507, 33.120, 0.070, 50.000, 0.850, 0.000, 0.000, 0.000, 0.000, 0.000 point.1= 1.000, -1.000, -4.500, -3.600, 1574.803, 1.000, 0.507, 0.000, 0.300, 2.000, 0.850, 0.000, 0.000, 2.000, 0.000, 0.000 point.2= 1.000, -1.000, 4.500, -3.600, 1574.803, 2.000, 0.507, 0.000, 0.300, 2.000, 0.850, 0.000, 0.000, 3.000, 0.000, 0.000 point.3= 2.000, -0.583, -13.917, 0.000, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4= 2.000, -0.583, 13.917, 0.000, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5= 2.000, 6.000, 0.000, -2.900, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6= 2.000, -16.333, 0.000, 0.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= 1.791 static_cg_height= 3.418 [GeneralEngineData] engine_type= 0 Engine.0= 9.333, 0.000, 0.567 fuel_flow_scalar= 1.000 min_throttle_limit=0.00 //0.000000 [piston_engine] max_rpm_mechanical_efficiency_scalar=0.85 //1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=0.500 //1.000 cylinder_displacement=82.6 //78.000 (82.6 = ref for rotax engine) compression_ratio= 10.5 //8.500 number_of_cylinders= 4 //6 max_rated_rpm=5800 //2386 //2800.000 max_rated_hp= 100.00 //105.000 fuel_metering_type= 1 cooling_type= 0 normalized_starter_torque= 0.300 turbocharged= 1 max_design_mp= 23.000 min_design_mp= 1.000 critical_altitude= 12000.000 emergency_boost_type= 0 emergency_boost_mp_offset= 0.000 emergency_boost_gain_offset= 0.000 fuel_air_auto_mixture= 0 auto_ignition= 0 power_scalar=1.000 [propeller] propeller_type= 1 propeller_diameter= 6.000 propeller_blades= 3 propeller_moi= 6.000 beta_max= 14.609 beta_min= 15.000 min_gov_rpm= 1400.000 prop_tc= 0.100 gear_reduction_ratio= 2.430 //1.000 fixed_pitch_beta=20.000 //20.000 low_speed_theory_limit= 80.000 prop_sync_available= 0 prop_deice_available= 0 prop_feathering_available= 0 prop_auto_feathering_available= 0 min_rpm_for_feather= 0.000 beta_feather= 0.000 power_absorbed_cf= 0.000 defeathering_accumulators_available= 0 prop_reverse_available= 0 minimum_on_ground_beta= 0.000 minimum_reverse_beta= 0.000 thrust_scalar=1.000 [Reference Speeds] flaps_up_stall_speed= 33.9.000 full_flaps_stall_speed= 28.600 cruise_speed= 100.0 max_indicated_speed=130.3 [keyboard_response] elevator=150.000, 250.000 aileron=150.000, 250.000 rudder=150.000, 250.000 [Views] eyepoint=1.9,-1.0,2.0 //1.9,-0.5,1.6 [General] performance=Length: 19'\s Span: 27'\s Height: 6'6''\nSeating: 2\s Range: 480 miles\nWeight: 650\/1300 lbs. empty\/max\nEngine: 105 hp Jabiru 3300A\nZodiac details: see www.zenithair.com\nreal Zodiac designed by Chris Heintz\nvirtual: Paul Hartl, Copyright 2004\npdhartl@cox-internet.com FS2002\/4 version\nmade with Abacus's "Design Studio 2"\n atc_type="Zenair" atc_model="601UL" Category=airplane [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000 autothrottle_available=0 pitch_takeoff_ga=8.000 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=25.000000 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 [flight_tuning] cruise_lift_scalar=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 parasite_drag_scalar=0.70 induced_drag_scalar=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [direction_indicators] direction_indicator.0=1,0 [Folding_wings] wing_fold_system_type=4 fold_rates=0.040,0.039 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 5.000 system_type= 3 damaging-speed= 0.000 blowout-speed= 0.000 lift_scalar= 1.000 drag_scalar= 1.0 //0.150 pitch_scalar=0.5 // 1.0 0.050 flaps-position.0= 0.000, 0.000 flaps-position.1= 13.331, 0.000 //13.331, 0.000 flaps-position.2= 13.331, 0.000 //26.662, 0.000 flaps-position.3= 13.331, 0.000 //39.992, 0.000 [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=1.000000 [vacuum_system] max_pressure=5.000000 vacuum_type=1 electric_backup_pressure=0.000000 engine_map=1,1,1,1 [pneumatic_system] max_pressure=0.000000 bleed_air_scalar=0.000000 [deice_system] structural_deice_type=0