[fltsim.0] title=AN-2V_UCR sim=AN-2V model= panel= sound= texture= panel_alias = sound_alias = kb_checklists= kb_reference= atc_id= atc_id_color=0xffffffff atc_airline = atc_flight_number = 1 ui_manufacturer=WSK-PZL Mielec ui_type=AN-2V Seaplane ui_variation=USA Civil Register description=First appearing in 1947, the AN-2's was first dismissed as obsolete, due to it's biplane layout and homely looks. But the "Annushka" would prove the naysayers wrong.... and how! The biplane layout proved itself, and there wasn't much the AN-2 couldn't do, whether as a passenger, cargo, parachuting, crop spraying, or spec ops plane. Over 20,000 were produced, mostly in Poland. Not bad for an "obsolete" design! This model is the AN-2V seaplane version, origionaly designated AN-4. [fltsim.1] title=AN-2V_CCR sim=AN-2V model= panel= sound= texture=CCR panel_alias = sound_alias = kb_checklists= kb_reference= atc_id= atc_id_color=0xffffffff atc_airline = atc_flight_number = 1 ui_manufacturer=WSK-PZL Mielec ui_type=AN-2V Seaplane ui_variation=Canadian Civil Register description=First appearing in 1947, the AN-2's was first dismissed as obsolete, due to it's biplane layout and homely looks. But the "Annushka" would prove the naysayers wrong.... and how! The biplane layout proved itself, and there wasn't much the AN-2 couldn't do, whether as a passenger, cargo, parachuting, crop spraying, or spec ops plane. Over 20,000 were produced, mostly in Poland. Not bad for an "obsolete" design! This model is the AN-2V seaplane version, origionaly designated AN-4. [fltsim.2] title=AN-2V_EGCR sim=AN-2V model= panel= sound= texture=EGCR panel_alias = sound_alias = kb_checklists= kb_reference= atc_id= atc_id_color=0xffffffff atc_airline = atc_flight_number = 1 ui_manufacturer=WSK-PZL Mielec ui_type=AN-2V Seaplane ui_variation= East German Civil Register description=First appearing in 1947, the AN-2's was first dismissed as obsolete, due to it's biplane layout and homely looks. But the "Annushka" would prove the naysayers wrong.... and how! The biplane layout proved itself, and there wasn't much the AN-2 couldn't do, whether as a passenger, cargo, parachuting, crop spraying, or spec ops plane. Over 20,000 were produced, mostly in Poland. Not bad for an "obsolete" design! This model is the AN-2V seaplane version, origionaly designated AN-4. [General] atc_type = atc_model = editable = 1 performance = * Weight: 11030 lbs Max 12926 lbs * Power: 1000 hp MIL 1000 hp WEP * 4.0g Corner speed: 122 mph * Max speed @ SL: 145 mph * Max speed: 150 mph @ 5740 ft * Climb rate: 3475 ft/min @ 71 mph Flight Model By: Tim Piglet Conrad Piglet's Peculiar Planes 12/23/03 02:06 AM Flight Model Workbook V2.83.56 [pitot_static] vertical_speed_time_constant = 2 [WEIGHT_AND_BALANCE] max_gross_weight = 12926 empty_weight = 8030 reference_datum_position = 0, 0, 0 empty_weight_CG_position = -1.43, 0, 0 CG_forward_limit = 0 CG_aft_limit = 1 max_number_of_stations = 11 station_load.0 = 200, 2, 0, 0 station_load.1 = 200, 2, 0, 0 station_load.2 = 2600, -3, 0, 0 station_load.3 = 0, 0, 0, 0 station_load.4 = 0, 0, 0, 0 station_load.5 = 0, 0, 0, 0 station_load.6 = 0, 0, 0, 0 station_load.7 = 0, 0, 0, 0 station_load.8 = 0, 0, 0, 0 station_load.9 = 0, 0, 0, 0 station_load.10 = 0, 0, 0, 0 empty_weight_pitch_MOI = 35499 empty_weight_roll_MOI = 14056 empty_weight_yaw_MOI = 46167 empty_weight_coupled_MOI = 0 [flight_tuning] cruise_lift_scalar = 1 parasite_drag_scalar = 1 induced_drag_scalar = 1 elevator_effectiveness = 1 aileron_effectiveness = 1 rudder_effectiveness = 1 pitch_stability = 1 roll_stability = 1 yaw_stability = 1 elevator_trim_effectiveness = 1 aileron_trim_effectiveness = 1 rudder_trim_effectiveness = 1 [GeneralEngineData] engine_type = 0 Engine.0 = 11.2, 0, 0 fuel_flow_scalar = 1 min_throttle_limit=0.000000 [piston_engine] power_scalar = 1 cylinder_displacement = 202.555555555556 compression_ratio = 6.4 number_of_cylinders = 9 max_rated_rpm = 2200 max_rated_hp = 1000 fuel_metering_type = 1 cooling_type = 0 normalized_starter_torque = 0.035 turbocharged = 0 max_design_mp = 29 min_design_mp = 9 critical_altitude = 5740 emergency_boost_type = 3 emergency_boost_mp_offset = 3.2 emergency_boost_gain_offset = 0.134640028271713 fuel_air_auto_mixture = 0 auto_ignition = 0 max_rpm_mechanical_efficiency_scalar = 1 idle_rpm_mechanical_efficiency_scalar = 1 max_rpm_friction_scalar = 1 idle_rpm_friction_scalar = 1 fuel_flow_scalar = 1 emergency_boost_duration = 300 [propeller] thrust_scalar = 1 propeller_type = 0 propeller_diameter = 11 propeller_blades = 4 propeller_moi = 56.4 beta_max = 65 beta_min = 15 min_gov_rpm = 330 prop_tc = 0.01 gear_reduction_ratio = 1.2 fixed_pitch_beta = 30 low_speed_theory_limit = 80 prop_sync_available = 0 prop_deice_available = 1 prop_feathering_available = 0 prop_auto_feathering_available = 0 min_rpm_for_feather = 700 beta_feather = 88.5 power_absorbed_cf = 0.9 defeathering_accumulators_available = 0 prop_reverse_available = 0 minimum_on_ground_beta = 1 minimum_reverse_beta = -14 rotation = 1 [contact_points] max_number_of_points = 10 point.0 = 2, 6.2853, 0, -3.9859, 2100, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.1 = 5, -17.1074, -6.531, -7.8388, 2000, 0, 0, 30, 0, 0, 1, 1, 1.5, 2, 0, 0 point.2 = 5, -17.1039, 6.4904, -7.7602, 2000, 0, 0, 30, 0, 0, 1, 1, 1.4, 3, 0, 0 point.3 = 4, 6.7195, -6.4924, -9.6484, 2000, 0, 0, 0, 0.8, 2.5, 0.8, 0, 0, 2 point.4 = 4, 6.7241, 6.4671, -9.6357, 2000, 0, 0, 0, 0.8, 2.5, 0.8, 0, 0, 1 point.5 = 4, -12.5719, -6.5033, -7.7485, 2000, 0, 0, 0, 0.8, 2.5, 0.8, 0, 0, 2 point.6 = 4, -12.5818, 6.4673, -7.7687, 2000, 0, 0, 0, 0.8, 2.5, 0.8, 0, 0, 3 point.7 = 2, -28.5592, 0, 0.6453, 3000.102, 0, 0, 0, 0, 0, 0, 0, 0, 9 point.8 = 2, -0.61, -22.2891, -3.3146, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 5 point.9 = 2, -0.0872, 22.1145, -3.5182, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 6 static_pitch= 5.69 static_cg_height= 8.78 tailwheel_lock = 1 [Views] eyepoint= 3.233, -1.333, 3.265 [flaps.0] //Trailing Edge Flaps type = 1 span-outboard = 0.5 extending-time = 5 flaps-position.0 = 0 flaps-position.1 = 15, 121 flaps-position.2 = 25, 116 flaps-position.3 = 35, 111 flaps-position.4 = 45, 106 damaging-speed = 121 blowout-speed = 131 system_type = 0 lift_scalar = 0 drag_scalar = 0 pitch_scalar = 1 [flaps.1] //Leading Edge Flaps - Lift type = 2 span-outboard = 0.5 extending-time = 5 flaps-position.0 = 0 flaps-position.1 = 15 flaps-position.2 = 30 flaps-position.3 = 45 flaps-position.4 = 30 damaging-speed = 121 blowout-speed = 131 system_type = 0 lift_scalar = 1 drag_scalar = 0 pitch_scalar = 0 [flaps.2] //Leading Edge Flaps - Drag type = 2 span-outboard = 0.5 extending-time = 5 flaps-position.0 = 0 flaps-position.1 = 4 flaps-position.2 = 5 flaps-position.3 = 6 flaps-position.4 = 45 damaging-speed = 121 blowout-speed = 131 system_type = 0 lift_scalar = 0 drag_scalar = 1 pitch_scalar = 0 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 160 electric_always_available = 1 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 10, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 20, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 17 starter2 = 0, 20, 17 starter3 = 0, 20, 17 starter4 = 0, 20, 17 light_nav = 0, 5, 17 light_beacon = 0, 5, 17 light_landing = 0, 5, 17 light_taxi = 0, 5, 17 light_strobe = 0, 5, 17 light_panel = 0, 5, 17 prop_sync = 0, 15, 17 auto_feather = 0, 15, 17 auto_brakes = 0, 15, 17 standby_vacuum = 0, 15, 17 hydraulic_pump = 0, 2, 17 fuel_transfer_pump = 0, 5, 17 propeller_deice = 0, 5, 17 light_recognition = 0, 5, 17 light_wing = 0, 5, 17 light_logo = 0, 5, 17 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -1.09, -30.16, 5.66, fx_navred light.1 = 3, -1.09, 30.16, 5.66, fx_navgre light.2 = 3, 1.42, 0.00, 7.447, fx_navwhi light.3 = 4, 2.48, 0, 1.97, fx_vclight_offwhi [keyboard_response] elevator = 350, 500 aileron = 450, 1000 rudder = 200, 1000 [direction_indicators] direction_indicator.0 = 1, 0 [exits] number_of_exits = 2 exit_rate.0 = 0.8 exit_rate.1 = 0.4 [EFFECTS] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn, 1 [autopilot] autopilot_available = 1 flight_director_available = 0 default_vertical_speed = 1000 autothrottle_available = 0 autothrottle_arming_required = 0 autothrottle_max_rpm = 90 autothrottle_takeoff_ga = 1 pitch_takeoff_ga = 8 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 [fuel] LeftMain = 0, -5.1, 0, 158, 0 RightMain = 0, 5.1, 0, 158, 0 fuel_type = 1 number_of_tank_selectors = 1 electric_pump=1 [airplane_geometry] wing_area = 770 wing_span = 56.6458333333333 wing_root_chord = 6.79661640308937 wing_dihedral = 4 wing_incidence = 0 wing_twist = 0 oswald_efficiency_factor = 0.940160680926919 wing_winglets_flag = 0 wing_sweep = 0 wing_pos_apex_lon = 0.269154100772343 wing_pos_apex_vert = 0 htail_area = 132 htail_span = 13.1 htail_pos_lon = -24.83 htail_pos_vert = 0 htail_incidence = 0 htail_sweep = 0 vtail_area = 86.37 vtail_span = 6.2 vtail_sweep = 0 vtail_pos_lon = -25.85 vtail_pos_vert = 0 elevator_area = 57.56 aileron_area = 100 rudder_area = 28.93 elevator_up_limit = 30 elevator_down_limit = 20 aileron_up_limit = 15 aileron_down_limit = 15 rudder_limit = 30 elevator_trim_limit = 18 spoiler_limit = 0 spoilerons_available = 0 aileron_to_spoileron_gain = 0 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 [Reference Speeds] flaps_up_stall_speed = 53 full_flaps_stall_speed = 45.2 cruise_speed = 169 max_indicated_speed=220.000000 [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 = 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 [brakes] toe_brakes_scale=0.0 parking_brake=0 [hydraulic_system] electric_pumps=0 engine_map=1,0,0,0 normal_pressure=6.930556 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
