[fltsim.0] title=AI Airlift Vickers Viking BEA sim=FSDS2 Vickers Viking model= panel= sound= texture=beawt kb_checklists= description=Viking ui_manufacturer=Vickers ui_type=Viking ui_variation=BEA "Sir Bertram Ramsey" visual_damage=1 atc_heavy=0 atc_id=G-AJBQ atc_airline=Beeline atc_flight_number=VC2 atc_type=BRITISHAEROSPACE atc_model=BL18 prop_anim_ratio=0.9 atc_parking_codes=BAW [fltsim.1] title=AI Airlift Vickers Viking RAF sim=FSDS2 Vickers Viking model= panel= sound= texture=VL263 kb_checklists= description=RAF Viking ui_manufacturer=Vickers ui_type=Viking ui_variation=RAF visual_damage=1 atc_heavy=0 atc_id=R-AJBQ atc_airline=RAF atc_flight_number=VC3 atc_type=BRITISHAEROSPACE atc_model=BL19 prop_anim_ratio=0.9 atc_parking_codes=BAW [fltsim.2] title=AI Airlift Vickers Viking SASd sim=FSDS2 Vickers Viking model= panel= sound= texture=ddl kb_checklists= description=SASD Viking ui_manufacturer=Vickers ui_type=Viking ui_variation=SAS visual_damage=1 atc_heavy=0 atc_id=R-AJBQ atc_airline=SAS atc_flight_number=VC3 atc_type=BRITISHAEROSPACE atc_model=BL17 prop_anim_ratio=0.9 atc_parking_codes=SAS [General] performance=Model Designer : Rick Piper\nCrew: 3-4 \nEngines: 2 x 1690hp Bristol Hercules 634\nMax Speed: 263 mph \nTypical Cruise Speed 182 kts =210 mph@10,000 ft\nCeiling: 20,000 ft \nRange: approx 1,700 m Max. atc_type=BRITISHAEROSPACE atc_model=BL17 [WEIGHT_AND_BALANCE] max_gross_weight=34000 empty_weight=23000 reference_datum_position=0.0,0.0,0.0 empty_weight_CG_position=0.0,0.0,0.0 max_number_of_stations=50 ;Moments of Inertia empty_weight_roll_MOI=109699.03 empty_weight_pitch_MOI=201179.10 empty_weight_yaw_MOI=131797.97 empty_weight_coupled_MOI=0.0 station_load.0=170, 14.0, -1.6, 0 //Pilot station_load.1=170, 14.0, 1.6, 0 //Co-Pilot station_load.2=170, 11.5, 0.6, 0 //Nav/engineer station_load.3=170, 8.2, -2.9, 0 //pax1 station_load.4=170, 8.2, 0.7, 0 //pax2 station_load.5=170, 8.2, 2.9, 0 //pax3 station_load.6=170, 4.5, -2.9, 0 //pax4 station_load.7=170, 4.5, 0.7, 0 //pax5 station_load.8=170, 4.5, 2.9, 0 //pax6 station_load.9=170, 1.7, -2.9, 0 //pax7 station_load.10=170, 1.7, 0.7, 0 //pax8 station_load.11=170, 1.7, 2.9, 0 //pax9 station_load.12=170, -2.1, -2.9, 0 //pax10 station_load.13=170, -2.1, 0.7, 0 //pax11 station_load.14=170, -2.1, 2.9, 0 //pax12 station_load.15=170, -6.0, -2.9, 0 //pax13 station_load.16=170, -6.0, 0.7, 0 //pax14 station_load.17=170, -6.0, 2.9, 0 //pax15 station_load.18=170, -9.7, -2.9, 0 //pax16 station_load.19=170, -9.7, 0.7, 0 //pax17 station_load.20=170, -9.7, 2.9, 0 //pax18 station_load.21=170, -13.3, -2.9, 0 //pax19 station_load.22=170, -13.3, 0.7, 0 //pax20 station_load.23=170, -13.3, 2.9, 0 //pax21 station_load.24=170, -17.0, -2.9, 0 //pax22 station_load.25=170, -17.0, 0.7, 0 //pax23 station_load.26=170, -17.0, 2.9, 0 //pax24 station_load.27=250, 11.6, -4.0, 0 //Front Baggage hold station_load.28=50, -5.0, -4.5, 0 //Centre Baggage hold station_load.29=70, -15.0, -4.5, 0 //Rear Baggage hold [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 p_factor_on_yaw = 0.5 torque_on_roll = 1.0 gyro_precession_on_yaw = 1.0 gyro_precession_on_pitch = 1.0 [Flaps.0] type=1 span-outboard = 0.5 extending-time = 10 flaps-position.0 = 0.0 flaps-position.1 = 15.0 flaps-position.2 = 30.0 flaps-position.3 = 50.0 damaging-speed = 145.0 blowout-speed = 180.0 lift_scalar= 1.4 drag_scalar = 1.7 pitch_scalar = 1.0 system_type=1 [GeneralEngineData] engine_type=0 Engine.0=11.111, -11.397, -1.687 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=11.111, 11.397, -1.687 fuel_flow_scalar=0.65 min_throttle_limit = 0.0 master_ignition_switch = 1 [piston_engine] power_scalar=1.08 cylinder_displacement=155.57 compression_ratio=7.5 number_of_cylinders=14 max_rated_rpm=2900.0 max_rated_hp=1970.0 fuel_metering_type=1 cooling_type=0 normalized_starter_torque=0.015 turbocharged=1 max_design_mp=47.25 min_design_mp=0.0 critical_altitude=10000.0 emergency_boost_type=0 emergency_boost_mp_offset=0.0 emergency_boost_gain_offset=0.0 fuel_air_auto_mixture=1 auto_ignition=1 max_rpm_mechanical_efficiency_scalar=1.0 idle_rpm_mechanical_efficiency_scalar=0.9 max_rpm_friction_scalar=1.0 idle_rpm_friction_scalar=1.2 [propeller] thrust_scalar=0.86 propeller_type=0 rotation=-1,-1 propeller_diameter=13.3 propeller_blades=4 propeller_moi=99.2 beta_max=30.0 beta_min=18.0 min_gov_rpm=800 prop_tc=0.1 gear_reduction_ratio=1.8 fixed_pitch_beta=0.0 low_speed_theory_limit=80.0 prop_sync_available=1 prop_deice_available=1 prop_feathering_available=1 prop_auto_feathering_available=0 min_rpm_for_feather=700.0 beta_feather=0.5 power_absorbed_cf=0.9 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.0 minimum_reverse_beta=0.0 feathering_switches = 1 [contact_points] point.0=1, -31.66, 0.0, -5.56, 1500.0, 0, 0.749, 90.0, 0.200, 1.5, 0.695, 6.0, 5.0, 0, 0.0, 0.0 point.1=1, 1.9, -11.4, -10.6, 1600.0, 1, 1.816, 0.0, 0.700, 0.8, 0.7, 12.0, 14.0, 2, 0.0, 0.0 point.2=1, 1.9, 11.4, -10.6, 1600.0, 2, 1.816, 0.0, 0.700, 0.8, 0.7, 9.0, 12.0, 3, 0.0, 0.0 point.3=2, 0.1, -44.9 ,0.0,1574.8,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,5.0,0.0,0.0 point.4=2, 0.1, 44.9 ,0.0,1574.8,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,6.0,0.0,0.0 point.5=2, -35.2 ,0.0 ,-2.0,1574.8,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,9.0,0.0,0.0 point.6=2, 20.1 ,0.0, -5.0,1574.8,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,4.0,0.0,0.0 static_pitch=8.32433 static_cg_height=9.9 gear_system_type=1 tailwheel_lock = 1 [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 0.0 //Flap angle that activates warning at idle flap_limit_power = 15.0 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.78 //Brake scalar differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected [hydraulic_system] normal_pressure = 1200.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [Views] eyepoint=14.4,-1.6,1.5 [LIGHTS] light.1=4, 14.0, 0.0, 1.0, fx_vclight, light.2=4, 6.33, 0.0, 0.0, fx_vclight_Viking , light.3=4, 1.33, 0.0, 0.0, fx_vclight_Viking , light.4=4, -4.33, 0.0, 0.0, fx_vclight_Viking , light.5=4, -9.33, 0.0, 0.0, fx_vclight_Viking , light.6=4, -14.33, 0.0, 0.0, fx_vclight_Viking , [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1 Adf.2=1 Transponder.1=1 Marker.1=1 [keyboard_response] elevator =200, 1000 aileron =200, 1000 rudder =200, 1000 [direction_indicators] direction_indicator.0=1,0 direction_indicator.1=2,0 [attitude_indicators] attitude_indicator.0 = 1 attitude_indicator.1 = 2 [turn_indicators] turn_indicator.0=2,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks startup=fx_engstrt_jenny touchdown=fx_tchdwn_s, 1 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 70 [fuel] LeftMain=0.0,-20.0,0.0,375.0,0.0 //total fuel capacity 740 Imp gallons (889 US Gallons) FS002 used US Gal!. LeftAux=1.0,-11.4,1.0,69.0,0.0 RightMain=0.0,20.0,0.0,375.0,0.0 RightAux=1.0,11.4,1.0,69.0,0.0 fuel_type=1 number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area=882.0 wing_span=89.2 wing_root_chord=14.8 wing_dihedral=3.0 wing_incidence=0.9 wing_twist=0.0 oswald_efficiency_factor=0.7433 wing_winglets_flag=0 wing_sweep=0.8 wing_pos_apex_lon=0.0 wing_pos_apex_vert=0.0 htail_area=174.0 htail_span=36.0 htail_pos_lon=-31.3 htail_pos_vert=1.0 htail_incidence=0.9 htail_sweep=0.0 vtail_area=120.0 vtail_span=12.4 vtail_sweep=0.0 vtail_pos_lon=-31.3 vtail_pos_vert=5.5 elevator_area=69.0 aileron_area=14.4 rudder_area=66.0 elevator_up_limit=26.0 elevator_down_limit=26.0 aileron_up_limit=25.0 aileron_down_limit=25.0 rudder_limit=55.0 elevator_trim_limit=19.9 spoiler_limit=0.0 spoilerons_available=0 aileron_to_spoileron_gain=0.0 min_ailerons_for_spoilerons=0.0 min_flaps_for_spoilerons=0.0 [Reference Speeds] flaps_up_stall_speed=85.0 full_flaps_stall_speed=75.0 cruise_speed=182.0 max_indicated_speed=232.0 [autopilot] autopilot_available= 1 flight_director_available= 0 pitch_takeoff_ga=0.0 default_vertical_speed=600.0 autothrottle_available=1 direction_indicator=1 attitude_indicator =1 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=1.5 max_bank_velocity=3.0 max_throttle_rate=0.2 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 default_bank_mode=2 //Default to Heading Hold autothrottle_arming_required=1 autothrottle_takeoff_ga=0 autothrottle_max_rpm=105.0 [forcefeedback] ground_bumps_magnitude1=2600 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.6 ground_bumps_magnitude2=1200 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.085 ground_bumps_slope2=0.65 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=3500000 ; in microseconds [stall_warning] type=1 [SMOKESYSTEM] smoke.0= -3.67, 6.4, -13, fx_smoke_rx smoke.1= -3.67, 6.4, 13, fx_smoke_rx