[fltsim.0] title=Beriev BE-103 light amphibious aircraft sim=beriev_be103 model= panel= sound= texture= kb_checklists=be_103_Check kb_reference=be_103_ref atc_id=BE103 atc_id_color=0xff000000 ui_manufacturer=Beriev ui_type=BE 103 ui_variation=Oshkosh Blue visual_damage=1 description=The Be-103 light multipurpose amphibious aircraft is a monoplane with low-set water-displacement wing with a root strake, all-moving horizontal tail located in the propeller blow zone, and tricycle landing gear. A unique feature of the amphibious aircraft includes implementation of a water-displacement wing concept, which improves seaworthiness and stability when moving on water. Power plants are two IO-360ES4 piston engines made by Teledyne Continental Motors (USA) each rated at 210 h.p. The engines are mounted on horizontal pylons on both sides of the hull above the rear part of the center wing section, providing protection to the propellers against water spray during take-off and landing on water. The aircraft is fitted with MTV-12-D-C-F-R (M) variable-pitch three-blade reversible propellers. The low-set wing (in relation to hull) provides for wing-in-ground effect during take-off and landing. Thanks to this feature the aircraft does not need flaps and can skim on the wing trailing edges. This also makes aircraft construction simpler. The hull is wide enough to provide a comfortable cabin for passengers and sufficient space for cargo and luggage. There are a total of 6 seats (1 pilot/5 passenger) atc_heavy=0 atc_airline= atc_flight_number= [fltsim.1] title=Beriev BE-103 Red sim=beriev_be103 model= panel= sound= texture=red kb_checklists=be_103_Check kb_reference=be_103_ref atc_id=BE103 atc_id_color=0xff000000 ui_manufacturer=Beriev ui_type=BE 103 ui_variation=BFU Red visual_damage=1 description=The Be-103 light multipurpose amphibious aircraft is a monoplane with low-set water-displacement wing with a root strake, all-moving horizontal tail located in the propeller blow zone, and tricycle landing gear. A unique feature of the amphibious aircraft includes implementation of a water-displacement wing concept, which improves seaworthiness and stability when moving on water. Power plants are two IO-360ES4 piston engines made by Teledyne Continental Motors (USA) each rated at 210 h.p. The engines are mounted on horizontal pylons on both sides of the hull above the rear part of the center wing section, providing protection to the propellers against water spray during take-off and landing on water. The aircraft is fitted with MTV-12-D-C-F-R (M) variable-pitch three-blade reversible propellers. The low-set wing (in relation to hull) provides for wing-in-ground effect during take-off and landing. Thanks to this feature the aircraft does not need flaps and can skim on the wing trailing edges. This also makes aircraft construction simpler. The hull is wide enough to provide a comfortable cabin for passengers and sufficient space for cargo and luggage. There are a total of 6 seats (1 pilot/5 passenger) atc_heavy=0 atc_airline= atc_flight_number=636 [fltsim.2] title=Beriev BE-103 BFU sim=beriev_be103 model= panel= sound= texture=bfu kb_checklists=be_103_Check kb_reference=be_103_ref atc_id=BE103C atc_id_color=0xff000000 ui_manufacturer=Beriev ui_type=BE 103 ui_variation=BFU visual_damage=1 description=The Be-103 light multipurpose amphibious aircraft is a monoplane with low-set water-displacement wing with a root strake, all-moving horizontal tail located in the propeller blow zone, and tricycle landing gear. A unique feature of the amphibious aircraft includes implementation of a water-displacement wing concept, which improves seaworthiness and stability when moving on water. Power plants are two IO-360ES4 piston engines made by Teledyne Continental Motors (USA) each rated at 210 h.p. The engines are mounted on horizontal pylons on both sides of the hull above the rear part of the center wing section, providing protection to the propellers against water spray during take-off and landing on water. The aircraft is fitted with MTV-12-D-C-F-R (M) variable-pitch three-blade reversible propellers. The low-set wing (in relation to hull) provides for wing-in-ground effect during take-off and landing. Thanks to this feature the aircraft does not need flaps and can skim on the wing trailing edges. This also makes aircraft construction simpler. The hull is wide enough to provide a comfortable cabin for passengers and sufficient space for cargo and luggage. There are a total of 6 seats (1 pilot/5 passenger) atc_heavy=0 atc_airline= atc_flight_number= [fltsim.3] title=Beriev BE-103 Flames sim=beriev_be103 model= panel= sound= texture=flame kb_checklists=be_103_Check kb_reference=be_103_ref atc_id=BE103 atc_id_color=0xff000000 ui_manufacturer=Beriev ui_type=BE 103 ui_variation=Flames visual_damage=1 description=The Be-103 light multipurpose amphibious aircraft is a monoplane with low-set water-displacement wing with a root strake, all-moving horizontal tail located in the propeller blow zone, and tricycle landing gear. A unique feature of the amphibious aircraft includes implementation of a water-displacement wing concept, which improves seaworthiness and stability when moving on water. Power plants are two IO-360ES4 piston engines made by Teledyne Continental Motors (USA) each rated at 210 h.p. The engines are mounted on horizontal pylons on both sides of the hull above the rear part of the center wing section, providing protection to the propellers against water spray during take-off and landing on water. The aircraft is fitted with MTV-12-D-C-F-R (M) variable-pitch three-blade reversible propellers. The low-set wing (in relation to hull) provides for wing-in-ground effect during take-off and landing. Thanks to this feature the aircraft does not need flaps and can skim on the wing trailing edges. This also makes aircraft construction simpler. The hull is wide enough to provide a comfortable cabin for passengers and sufficient space for cargo and luggage. There are a total of 6 seats (1 pilot/5 passenger) [General] atc_type=Beriev atc_model=be103 editable=1 performance=Service ceiling 17000 ft (5200 m) Maximum cruising speed at H=3000m 135 kts/h (250 km/h) Economy speed at H=9800ft (3000m) 120 kts/h (220 km/h) Maximum range (H=9800ft (3000m), 0.5 hour fuel reserve) 600 kts (1100 km) Flight endurance (H=9800ft (3000 m), 0.5 hour fuel reserve) 6 h Category=airplane Fuel consumption 14-16 g/h (38-43 kg/h) Take-off run (SL, ISA) (water/ground) 1804/1017 ft (550/310 m) Landing roll (SL, ISA) (water/ground) 984/1280 ft (300/390 m) Seaworthiness, sea state 2 (1.64 ft (0.5 m) wave height) [forcefeedback] 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=00500 gear_bump_right_duration=250000 ground_bumps_magnitude1=3250 ground_bumps_angle1=8900 ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ground_bumps_angle2=9100 ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 crash_direction1=01000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=2500000 [contact_points] //0 Class //1 Longitudinal Position (feet) //2 Lateral Position (feet) //3 Vertical Position (feet) //4 Impact Damage Threshold (Feet Per Minute) //5 Brake Map (0=None, 1=Left, 2=Right) //6 Wheel Radius (feet) //7 Steer Angle (degrees) //8 Static Compression (feet) (0 if rigid) //9 Max/Static Compression Ratio //10 Damping Ratio (0=Undamped, 1=Critically Damped) //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) //gear point.0=1,14.00,0.00,-5.55,7574, 0, 0.5, 82.0, 0.25,2.5, 0.7, 5.0, 5.0, 0 point.1=1,-1.00,-4.00,-5.55,3574.803200,1.000000,0.693234,0.000000,0.206050,2.500000,0.780962,5.000000,5.000000,2.000000,0.000000,0.000000 point.2=1,-1.00,4.00,-5.55,3574.803200,2.000000,0.693234,0.000000,0.206050,2.500000,0.780962,5.000000,5.000000,3.000000,0.000000,0.000000 point.3=4.000000,16.083333,0.000000,-3.766667,2200.00000,0.000000,0.693234,0.000000,0.24050,2.500000,0.50962,0.000000,0.000000,2.000000,0.000000,0.000000 point.4=4.000000,16.083333,0.000000,-3.766667,2200.00000,0.000000,0.693234,0.000000,0.24050,2.500000,0.50962,0.000000,0.000000,3.000000,0.000000,0.000000 point.5=4.000000,16.083333,0.000000,-3.766667,2200.00000,0.000000,0.693234,0.000000,0.24050,2.500000,0.50962,0.000000,0.000000,3.000000,0.000000,0.000000 point.6=4.000000,-5.916667,0.000000,-3.266667,2200.000000,0.000000,0.693234,0.000000,0.24050,2.500000,0.50962,0.000000,0.000000,2.000000,0.000000,0.000000 point.7=4.000000,-5.916667,0.000000,-3.266667,2200.000000,0.000000,0.693234,0.000000,0.24050,2.500000,0.50962,0.000000,0.000000,2.000000,0.000000,0.000000 point.8=4.000000,-5.916667,0.000000,-3.266667,2200.000000,0.000000,0.693234,0.000000,0.24050,2.500000,0.50962,0.000000,0.000000,3.000000,0.000000,0.000000 //wingtips point.9=4.000000,1.00000,4.000000,-3.00,2200.000000,0.000000,0.693234,0.000000,0.206050,4.000000,0.980962,0.000000,0.000000,2.000000,0.000000,0.000000 point.10=4.000000,1.000000,-4.000000,-3.00,2200.000000,0.000000,0.693234,0.00000,0.206050,2.500000,0.980962,0.000000,0.000000,3.000000,0.000000,0.000000 //water rudder point.11=5.0, -5.9, 0.0,-4.0,2200, 0.0, 0.5, 20.0, 0.25, .2, 0.7, 5.0,5.0, 0 //scrapes point.12 = 2.000, -3.500, -20.000, 0.000, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.13 = 2.000, -3.500, 20.000, 0.000, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.14= 2.000, -13.810, 0.000, 1.530, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.15= 2.000, 4.357, 0.000, 0.000, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch=0 static_cg_height=5 gear_system_type=0 [Views] eyepoint=8.0,-0.8,0.2 [General] performance= [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 Transponder.1=1 Marker.1=1 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1000.000000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 use_no_default_pitch=1 use_no_default_bank=1 default_pitch_mode=0 default_bank_mode=0 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 [direction_indicators] direction_indicator.0=3,0 [SMOKESYSTEM] smoke.0=0.0, -6.0, -5.0, fx_Swordwaterfall smoke.1=0.0, -6.0, 5.0, fx_Swordwaterfall [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=0.50000,0.000000,0.000000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight=8000 empty_weight_roll_MOI=93258.000000 empty_weight_pitch_MOI=98469.000000 empty_weight_yaw_MOI=147467.000000 empty_weight_coupled_MOI=0.000000 max_gross_weight=15000 [fuel] LeftMain=0.000000,0.000000,0.000000,68.000000,0.000000 RightMain=0.000000,0.000000,0.000000,68.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=0 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.25 induced_drag_scalar = 1.25 elevator_effectiveness = .7 aileron_effectiveness = 1.3 rudder_effectiveness = 1.0 pitch_stability = 2.0 roll_stability = 1.0 yaw_stability = 1.0 elevator_trim_effectiveness = 5.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [airplane_geometry] wing_area=637.000000 wing_span=54.166667 wing_root_chord=11.750000 wing_dihedral=10.997314 wing_incidence=0.000000 wing_twist=-0.999756 oswald_efficiency_factor=.80 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=56.000000 htail_span=13.666667 htail_pos_lon=-30.000000 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=100.000000 vtail_span=11.401754 vtail_sweep=0.000000 vtail_pos_lon=-26.666667 vtail_pos_vert=1.500000 elevator_area=20.00000 aileron_area=63.700000 rudder_area=35.000000 elevator_up_limit=25.0 elevator_down_limit=25.0 aileron_up_limit=25.0 aileron_down_limit=25.0 rudder_limit=25.0 elevator_trim_limit=19.480565 spoiler_limit=59.988681 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 auto_spoiler_available=0 spoiler_extension_time=2.000000 positive_g_limit_flaps_up=3.000000 positive_g_limit_flaps_down=2.000000 negative_g_limit_flaps_up=-2.000000 negative_g_limit_flaps_down=-2.000000 [GeneralEngineData] engine_type=0 Engine.0=4.000000,-7.000000,0.000000 Engine.1=4.000000,7.000000,0.000000 fuel_flow_scalar=.520000 min_throttle_limit=0.000000 [piston_engine] power_scalar=1.1 max_rpm_mechanical_efficiency_scalar=1.05000 idle_rpm_mechanical_efficiency_scalar=1.000000 max_rpm_friction_scalar=.950000 idle_rpm_friction_scalar=1.000000 cylinder_displacement=115.700000 compression_ratio=8.000000 number_of_cylinders=12 max_rated_rpm=3000.000000 max_rated_hp=420.000000 fuel_metering_type=1 cooling_type=0 normalized_starter_torque=0.300000 turbocharged=0 max_design_mp=0.000000 min_design_mp=0.000000 critical_altitude=0.000000 emergency_boost_type=0 emergency_boost_mp_offset=0.000000 emergency_boost_gain_offset=0.000000 fuel_air_auto_mixture=0 auto_ignition=0 [propeller] thrust scalar=1.1 propeller_type=0 propeller_diameter=6.4 propeller_blades=3 propeller_moi=6.9 beta_max=44.600000 beta_min=15.000000 min_gov_rpm=1100.000000 prop_tc=0.100000 gear_reduction_ratio=1.000000 fixed_pitch_beta=82.500000 low_speed_theory_limit=80.000000 prop_sync_available=1 prop_deice_available=1 prop_feathering_available=1 prop_auto_feathering_available=1 min_rpm_for_feather=0.000000 beta_feather=0.000000 power_absorbed_cf=0.000000 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000 [Reference Speeds] flaps_up_stall_speed=64.000000 full_flaps_stall_speed=56.000000 cruise_speed=135 max_indicated_speed=180 [keyboard_response] elevator=150.000000,200.000000 aileron=100.000000,200.000000 rudder=100.000000,200.000000 [brakes] toe_brakes_scale=.8 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [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 [exits] number_of_exits = 2 exit_rate.0 = 0.3 ;Percent per second exit_rate.1 = 0.3 ;Percent per second [Flaps.0] type=1 span-outboard=0.500000 extending-time=5.000000 system_type=1 flaps-position.0=0.000000,0.000000 flaps-position.1=45.000000,0.000000 lift_scalar=1.1 drag_scalar=1.3 pitch_scalar=1.0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0 = 3, -2.531, -20.731, -1.284, fx_navred , light.1 = 3, -2.531, 20.531, -1.284, fx_navgre , light.2 = 3, -12.00, 0.00, -2, fx_navwhi , light.3 = 2, -1.3, -19.48, -1.3, fx_strobe , light.4 = 2, -1.3, 19.48, -1.3, fx_strobe , light.5 = 1, -15.49, 0.00, 7.79, fx_beacon , light.6 = 2, -3.55, 0.00, -3.35, fx_strobe , light.7 = 4, 6.00, 0.00, 0.64, fx_vclight, [pitot_static] pitot_heat=1.000000 [vacuum_system] max_pressure=5.150000 vacuum_type=1 electric_backup_pressure=4.900000 engine_map=1,1,0,0 [pneumatic_system] max_pressure=0.000000 bleed_air_scalar=0.000000 [deice_system] structural_deice_type=2