//iss; 0808222000 v0.9, for 'vkg_v01.zip' by Ted Cook // Font=Verdana,10pt. regular: //modified for FSX by Leyland Spurr [fltsim.0] title=Viking knil sim=viking model=knil panel=knil sound=HS texture=knil kb_checklists=viking_check kb_reference=viking_ref atc_id=B5563 ui_manufacturer=Vickers ui_type=Type 55 'Viking' IV ui_variation=KNIL ui_typerole="reconnaissance amphibian" ui_createdby="Brian Farrington & Leyland Spurr from an FS9 original by Ted Cook" description=Exported to the Royal Dutch East Indies Air Force in 1922. Length: 34 ft 0 in Wingspan: 50 ft 0 in Height: 15 ft 1 in Wing area: 639 ft² Empty weight: 3,750 lb Loaded weight: 5,6000 lb Powerplant: 1× Napier 'Lion', 450 hp. atc_heavy=0 atc_airline= atc_flight_number= [General] atc_type=Vickers atc_model=Viking editable=1 performance=Range: 450 mi Service ceiling: 9,000 ft Rate of climb: 400 ft/min. category=airplane [WEIGHT_AND_BALANCE] max_gross_weight =5600.0 empty_weight =3750.0 reference_datum_position = 0.0, 0.0, 0.0 empty_weight_CG_position = -1.5, 0.0, 0.0 max_number_of_stations =0 ;Moments of Inertia empty_weight_pitch_MOI =5852.0 empty_weight_roll_MOI =5013.0 empty_weight_yaw_MOI =9427.0 empty_weight_coupled_MOI =0.0 [flight_tuning] cruise_lift_scalar =1.0 parasite_drag_scalar =1.3 induced_drag_scalar =1.0 elevator_effectiveness =0.3 aileron_effectiveness =1.2 rudder_effectiveness =1.2 pitch_stability =2.5 roll_stability =2.5 yaw_stability =2.5 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 =0.5 torque_on_roll =1.0 gyro_precession_on_roll =1.0 gyro_precession_on_yaw =1.0 [GeneralEngineData] engine_type =0 Engine.0 =-4.24, 0.00, 4.24 fuel_flow_scalar =1.55 min_throttle_limit =0.1 [piston_engine] power_scalar =1.0 cylinder_displacement =121.8 compression_ratio = 5.8 number_of_cylinders = 12 max_rated_rpm =2250.0 max_rated_hp = 450.0 fuel_metering_type =1 cooling_type =1 normalized_starter_torque =0.04332 turbocharged=0 max_design_mp=0 min_design_mp=0 critical_altitude=0 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=0.0 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 BestPowerSpecificFuelConsumption=0.5 detonation_onset=38.5 [propeller] thrust_scalar =1.0 propeller_type =1 propeller_diameter = 9.3 propeller_blades = 4 propeller_moi =27.4 gear_reduction_ratio = 1.52 fixed_pitch_beta =17.0 low_speed_theory_limit =80.0 beta_max=0 beta_min=0 min_gov_rpm=0.0 prop_tc=0.0 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.0 beta_feather=0.0 power_absorbed_cf=0.0 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.0 minimum_reverse_beta=0.0 [contact_points] max_number_of_points =20 ;Rem.....0.........1.......2......3.......4.....5....6.....7.....8.....9....10.....11..12..13 point.0= 1, -12.5, 0.0, -5.5, 3200, 0, 0.3, 50.0, 0.2, 1.7, 0.90, 0.0, 0.0, 0 // GEAR point.1= 1, 1.4, -3.4, -6.5, 3200, 1, 1.6, 0.0, 0.4, 1.7, 0.85, 4.0, 4.0, 2 point.2= 1, 1.4, 3.4, -6.5, 3200, 2, 1.6, 0.0, 0.4, 1.7, 0.85, 4.0, 4.0, 3 point.3= 2, 0.0, -25.0, 0.0, 3200, 0, 0.0, 0.0, 0.0, 0.0, 0.00, 0.0, 0.0, 5 // SCRAPES point.4= 2, 0.0, 25.0, 0.0, 3200, 0, 0.0, 0.0, 0.0, 0.0, 0.00, 0.0, 0.0, 6 point.5= 2, 12.7, 0.0, 1.3, 3200, 0, 0.0, 0.0, 0.0, 0.0, 0.00, 0.0, 0.0, 4 point.6= 4, 0.0, -20.0, -3.5, 10000, 0, 0.0, 0.0, 1.0, 1.0, 0.90, 0.0, 0.0, 1 // FLOATS point.7= 4, 0.0, 20.0, -3.5, 10000, 0, 0.0, 0.0, 1.0, 1.0, 0.90, 0.0, 0.0, 1 point.8= 4, -3.0, -20.0, -3.5, 10000, 0, 0.0, 0.0, 1.0, 1.0, 0.90, 0.0, 0.0, 1 point.9= 4, -3.0, 20.0, -3.5, 10000, 0, 0.0, 0.0, 1.0, 1.0, 0.90, 0.0, 0.0, 1 point.10= 4, 10.7, 0.0, -3.9, 10000, 0, 0.0, 0.0, 1.0, 1.0, 0.90, 0.0, 0.0, 1 // PONTOON point.11= 4, 7.8, -2.8, -3.8, 10000, 0, 0.0, 0.0, 1.0, 1.0, 0.90, 0.0, 0.0, 1 point.12= 4, 7.8, 2.8, -3.8, 10000, 0, 0.0, 0.0, 1.0, 1.0, 0.90, 0.0, 0.0, 1 point.13= 4, 0.0, -3.0, -5.0, 10000, 0, 0.0, 0.0, 1.0, 1.0, 0.90, 0.0, 0.0, 1 point.14= 4, 0.0, 3.0, -5.0, 10000, 0, 0.0, 0.0, 1.0, 1.0, 0.90, 0.0, 0.0, 2 point.15= 4, -12.7, -1.7, -4.2, 10000, 0, 0.0, 0.0, 1.0, 1.0, 0.90, 0.0, 0.0, 3 point.16= 4, -12.7, 1.7, -4.2, 10000, 0, 0.0, 0.0, 1.0, 1.0, 0.90, 0.0, 0.0, 3 point.17= 5, -12.700, 0.0, -6.2, 10000, 0, 0.0, 50.0, 0.0, 0.0, 0.05, 0.1, 0.1, 0 // RUDDER static_pitch = 3.0 static_cg_height = 6.5 gear_system_type = 3 tailwheel_lock = 0 [brakes] toe_brakes_scale=0.500 parking_brake=1 auto_brakes=0 hydraulic_system_scalar=0.0 differential_braking_scale=0.5 [gear_warning_system] gear_warning_available=0 [hydraulic_system] normal_pressure=0.0 [stall_warning] type=1 stick_shaker=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [electrical] max_battery_voltage = 24.0 generator_alternator_voltage = 28.0 max_generator_alternator_amps = 60.0 [pitot_static] vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI pitot_heat=0.000000 [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 0 Com.1 = 1, 0 Com.2 = 0, 0 Nav.1 = 0, 0, 0 Nav.2 = 0, 0, 0 Adf.1 = 0 Transponder.1 = 0 Marker.1 = 0 [Views] eyepoint = 3.7, 0, -0.1 //Longitudinal, Lateral, Vertical (feet) [LIGHTS] //Types: 4=cockpit. light.0 = 4, 4.0, 0.00, -0.45, fx_vclight, [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator = 150, 250 aileron = 150, 250 rudder = 150, 250 [direction_indicators] //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another //2 Indicator number of slaving indicator if Type = 4 direction_indicator.0=3,0 [fuel] fuel_type =1 number_of_tank_selectors =1 electric_pump=0 LeftMain = -1.7, -7.03, 8.05, 53.0, 0.0 RightMain = -1.7, 7.03, 8.05, 53.0, 0.0 fuel_dump_rate=0.02 anemometer_pump=0 engine_driven_pump=1 manual_pump=0 [EFFECTS] wake=fx_wake_s water=fx_spray //water=fx_bobspray2 dirt=fx_tchdrt concrete=fx_dummy touchdown=fx_tchdwn_s, 1 startup=fx_engstrt_jenny [airplane_geometry] wing_area =639.0 wing_span =50.0 wing_root_chord = 6.78 wing_dihedral = 5.0 wing_incidence = 0.0 wing_twist = 0.0 oswald_efficiency_factor = 0.8 wing_winglets_flag = 0 wing_sweep = 0.0 wing_pos_apex_lon = 2.5 wing_pos_apex_vert = 2.97 htail_area = 37.84 htail_span = 11.0 htail_pos_lon =-19.02 htail_pos_vert = 1.7 htail_incidence = 0.0 htail_sweep = 0.0 vtail_area = 10.1 vtail_span = 6.08 vtail_sweep = 0.0 vtail_pos_lon =-18.0 vtail_pos_vert = 2.2 elevator_area = 22.72 aileron_area = 96.0 rudder_area = 15.42 elevator_up_limit = 20.0 elevator_down_limit= 20.0 aileron_up_limit = 18.0 aileron_down_limit = 14.0 rudder_limit = 30.0 elevator_trim_limit = 15.0 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 spoiler_extension_time=0.0 spoiler_handle_available=0 auto_spoiler_available=0 positive_g_limit_flaps_up=4.7 negative_g_limit_flaps_up=-3.76 positive_g_limit_flaps_down=3.29 negative_g_limit_flaps_down=-2.82 load_safety_factor=1.0 [Reference Speeds] flaps_up_stall_speed = 39.0 full_flaps_stall_speed = 39.0 cruise_speed = 78.0 max_indicated_speed = 150.0 [autopilot] autopilot_available=0 flight_director_available=0 [forcefeedback] stick_shaker_magnitude=5000 stick_shaker_direction=0 stick_shaker_period=111111 gear_bump_nose_magnitude=6000 gear_bump_nose_direction=18000 gear_bump_nose_duration=250000 gear_bump_left_magnitude=6000 gear_bump_left_direction=35500 gear_bump_left_duration=250000 gear_bump_right_magnitude=6000 gear_bump_right_direction=500 gear_bump_right_duration=250000 ground_bumps_magnitude1=3250 ground_bumps_angle1=8900 ground_bumps_intercept1=5 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ground_bumps_angle2=9100 ground_bumps_intercept2=0.075 ground_bumps_slope2=1 crash_magnitude1=10000 crash_direction1=1000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=2500000 [AirWrench] Aircraft_Length=33.90000 nose_position_lon=12.70000 [Flaps.0] type=1 span-outboard=0.500000 extending-time=0.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=30.000000,0.000000 [vacuum_system] max_pressure=5.150000 vacuum_type=1 electric_backup_pressure=0.000000 engine_map=1,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=0.150000 [deice_system] structural_deice_type=0