[fltsim.0]
title=AN-2T_FDU
sim=AN-2T
model= 
panel=
sound=
texture=
panel_alias=
sound_alias=
kb_checklists= 
kb_reference=
atc_id=
atc_id_color=0xffffffff
atc_airline=
atc_flight_number=2
ui_manufacturer=Antonov
ui_type=AN-2T
ui_variation=HA-ANP
description=Die Antonov AN-2T ist eine polnische Ausfьhrung der Mehrzweckvariante. Gebaut wurde die AN-2 von 1947 - 2004. Lдnge: 12,74m, Flьgelspannweite oben: 18,18m / unten: 14,24m, Flьgelflдche insgesamt: 71,60mІ, Hцhe: 4,00m. Hцchstgeschwindigkeit: 258km/h in 1.750m Hцhe.
Reichweite: 900 km
Dienstgipfelhцhe: 4.400 m
Leergewicht: 3.450 kg
Fluggewicht: 5.500 kg
Triebwerk(e): ein Schwezow Neunzylinder-Sternmotor
Leistung: 736 kW
Der Spitzname der An-2 bei der NVA lautete Anna, Tante Anna oder auch Kastendrachen. Die An-2 ist das einzige Flugzeug der DDR-Luftstreitkrдfte, das von deren Grьndung 1956 bis zur Auflцsung 1990 im Dienst stand.


[General]
atc_type =
atc_model =
editable = 1
visual_damage=1
performance = * Weight: 11065 lbs    Max 12961 lbs * Power: 1000 hp MIL  1000 hp WEP * 4.0g Corner speed: 123 mph * Max speed @ SL: 150 mph * Max speed: 160 mph @ 5740 ft * Climb rate: 3475 ft/min @ 72 mph Flight Model By: Tim Piglet Conrad Piglet's Peculiar Planes 12/15/03 11:22 PM 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 = 12961
empty_weight = 7665

reference_datum_position = 0, 0, 0
empty_weight_CG_position  = -1.55, 0, 0
CG_forward_limit = 0
CG_aft_limit = 1

max_number_of_stations = 5
station_load.0 = 200, 2, 0, 0
station_load.1 = 200, 2, 0, 0
station_load.2 = 3000, -3, 0, 0
station_load.3 = 0, 0, 0, 0

empty_weight_pitch_MOI = 34389
empty_weight_roll_MOI = 14005
empty_weight_yaw_MOI = 44992
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 = 0
emergency_boost_mp_offset = 0
emergency_boost_gain_offset = 0
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 = 0

[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 = 7
point.0 = 1, -23.8157, 0, -3.1131, 2165.354, 0, 0.749, 45, 0.3, 2.5, 0.8, 0, 0, 0, 0, 0
point.1 = 1, 2.2612, -5.3288, -8.633, 2165.354, 1, 1.35, 0, 0.3, 2.5, 0.8, 0, 0, 2, 0, 0
point.2 = 1, 2.2612, 5.3288, -8.633, 2165.354, 2, 1.35, 0, 0.3, 2.5, 0.8, 0, 0, 3, 0, 0
point.3 = 2, 6.2853, 0, -3.9859, 2100, 0, 0, 0, 0, 0, 0, 0, 0, 4
point.4 = 2, -28.5592, 0, 0.6453, 3000.102, 0, 0, 0, 0, 0, 0, 0, 0, 9
point.5 = 2, -0.61, -22.2891, -3.3146, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 5
point.6 = 2, -0.0872, 22.1145, -3.5182, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 6

static_pitch= 11.8
static_cg_height= 7.78
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]
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 = 0.149154100772343
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


[brakes]
toe_brakes_scale=0.740889
parking_brake=1

[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