[fltsim.0]
title=AN-2V Aeroflot
sim=AN-2V
model=
panel=P
sound=
texture=afl
panel_alias =
sound_alias =
kb_checklists=
kb_reference=
atc_id=
atc_id_color=0xffffffff
atc_airline =
atc_flight_number =09266
ui_manufacturer=Antonov
ui_type=AN-  2 (6)Seaplane (Tim Piglet Conrad)
ui_variation=Aeroflot
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_UCR
sim=AN-2V
model=
panel=P
sound=
texture=
panel_alias =
sound_alias =
kb_checklists=
kb_reference=
atc_id=
atc_id_color=0xffffffff
atc_airline =
atc_flight_number = 1
ui_manufacturer=Antonov
ui_type=AN-  2 (6)Seaplane (Tim Piglet Conrad)
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.2]
title=AN-2V_CCR
sim=AN-2V
model=
panel=P
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=Antonov
ui_type=AN-  2 (6)Seaplane (Tim Piglet Conrad)
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.3]
title=AN-2V_EGCR
sim=AN-2V
model=
panel=P
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=Antonov
ui_type=AN-  2 (6)Seaplane (Tim Piglet Conrad)
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
Category=airplane

[pitot_static]
vertical_speed_time_constant = 2
pitot_heat=1.000000

[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 = 220.1
compression_ratio = 4.7
number_of_cylinders = 10
max_rated_rpm = 2100
max_rated_hp = 800
fuel_metering_type = 1
cooling_type = 0
normalized_starter_torque = 0.158
turbocharged = 1
max_design_mp = 36.5
min_design_mp = 9
critical_altitude = 14750
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
max_rpm_mechanical_efficiency_scalar = 1.2
idle_rpm_mechanical_efficiency_scalar = 1
max_rpm_friction_scalar = 1
idle_rpm_friction_scalar = 1

[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, -10.2484, 2000, 0, 0, 0, 0.8, 2.5, 0.8, 0, 0, 2
point.4 = 4, 6.7241, 6.4671, -10.2357, 2000, 0, 0, 0, 0.8, 2.5, 0.8, 0, 0, 1
point.5 = 4, -12.5719, -6.5033, -9.0485, 2000, 0, 0, 0, 0.8, 2.5, 0.8, 0, 0, 2
point.6 = 4, -12.5818, 6.4673, -9.0687, 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
gear_system_type=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= 700.0
autothrottle_available= 0
pitch_takeoff_ga=8.0
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=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 0.0

[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
auto_spoiler_available=0
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=4.000000
negative_g_limit_flaps_up=-2.000000
negative_g_limit_flaps_down=-2.000000

[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
stick_shaker=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=4.900000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=0.150000
[deice_system]
structural_deice_type=0