[fltsim.0]
title =  An-14A
sim = an14a
model = a
panel =
sound =
texture = sarmy
panel_alias =
sound_alias =
kb_checklists =
kb_reference =
atc_id =
atc_id_color = 0xffffffff
atc_parking_types =
atc_parking_code =
ui_manufacturer = Antonov
ui_type = An-14A Little Bee
ui_variation = AN-14A (Soviet Army, Grey)
description =  Antonov 14 "Clod". Antonov OKB light STOL twin-prop aircraft.

[General]
atc_type = Antonov
atc_model = atc_model
editable = 1
performance=Flight model v.1.0\nCruise speed - 170-180 km/h at 2000 m, max. distance - 800km.\nTake off roll distance - less than 100m with take off speed 70-80 km/h at 15-degree flaps setting.\nLanding with full flaps down, rollout distance - 100m\n\nMany of parameteres were calculated with FDE workbook by Jerry Beckwith.

[pitot_static]
vertical_speed_time_constant = 2

[WEIGHT_AND_BALANCE]
max_gross_weight = 8000
empty_weight = 5500

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

max_number_of_stations = 3
station_load.0 = 150, 0, 0, 0, Pilot
station_load.1 = 1400, 0, 0, 0, Load
station_load.2 = 0, 0, 0, 0, Passengers


empty_weight_pitch_MOI = 15609
empty_weight_roll_MOI = 18132
empty_weight_yaw_MOI = 24096
empty_weight_coupled_MOI = 0

[flight_tuning]
cruise_lift_scalar = 1
parasite_drag_scalar = 2.2
induced_drag_scalar = 1.0
elevator_effectiveness = 1.7
aileron_effectiveness = 1
rudder_effectiveness = 1.7
pitch_stability = 1
roll_stability = 1
yaw_stability = 1
elevator_trim_effectiveness = 1
aileron_trim_effectiveness = 1
rudder_trim_effectiveness = 1
hi_alpha_on_roll = 1
hi_alpha_on_yaw = 1
p_factor_on_yaw = 1
torque_on_roll = 1
gyro_precession_on_roll = 1
gyro_precession_on_yaw = 1

[GeneralEngineData]
engine_type = 0
Engine.0 = 2.0, -8.5, 2.0
Engine.1 = 2.0, 8.5, 2.0
fuel_flow_scalar = 0.6
min_throttle_limit = 0.1

[piston_engine]
power_scalar=1.0                              //Piston power scalar
cylinder_displacement=95.75          //???     //Cubic inches per cylinder
compression_ratio=6.4                 //???     //Compression ratio
number_of_cylinders=9                           //Number of cylinders
max_rated_rpm=2918                              //Max rated RPM
max_rated_hp=360                                //Max rated HP
fuel_metering_type=2                            //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter
cooling_type=0                                  //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=0.35                  //Starter torque factor
turbocharged=1                                  //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=34.8                              //Max design manifold pressure, (inHg)
min_design_mp=0.0                               //Min design manifold pressure, (inHg)
critical_altitude=9800.0              //???     //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type=0                          //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_gain_offset=0.0                 //Multiplier on manifold pressure due to emergency boost
emergency_boost_mp_offset=0.0                   //Additional manifold pressure supplied by emergency boost
fuel_air_auto_mixture=0                         //Automixture available? 0=FALSE, 1=TRUE
auto_ignition=0                                 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar=1.0        //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar=1.0       //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar=1.0                     //Scalar on maximum RPM friction
idle_rpm_friction_scalar=0.5 //1.0                    //Scalar on idle RPM friction

[propeller]
thrust_scalar=0.7
propeller_type=0
propeller_diameter=7.874
propeller_blades=3
propeller_moi=3.7                                                         //???
beta_max=34.5
beta_min=14.5
min_gov_rpm=1200.0
prop_tc=0.1
gear_reduction_ratio=1.0
fixed_pitch_beta=0.0
low_speed_theory_limit=80.0
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=14.5
minimum_reverse_beta=14.5
rotation = 1, 1

[contact_points]
max_number_of_points=4
point.0=1,  10.167,  0.00,  -5.333, 1500, 0, 1.5, 60, 0.239, 2.5, 0.6, 0, 0, 0, 0, 0

point.1=1,  -2.583, -5.85, -5.333, 1500, 1, 1.5,  0, 0.239, 2.5, 0.7, 0, 0, 2, 0, 0
point.2=1,  -2.583,  5.85, -5.333, 1500, 2, 1.5,  0, 0.239, 2.5, 0.7, 0, 0, 3, 0, 0


point.3=5, -22.417,  0.00,   0.75,  3000, 0,   0,  0,     0,   0,   0, 1, 3, 9, 0, 0


static_pitch=0
static_cg_height=5
gear_system_type=4


[Views]
eyepoint=5.25, -1.33, 2.4 //5.0, -1.2, 2.3//<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<,

[flaps.0]       //Trailing Edge Flaps
type = 1
span-outboard = 0.5
extending-time = 5
flaps-position.0 = 0
flaps-position.1 = 5, 150
flaps-position.2 = 10, 150
flaps-position.3 = 15, 150
flaps-position.4 = 20, 150
flaps-position.5 = 25, 150
flaps-position.6 = 30, 100
flaps-position.7 = 35, 80
flaps-position.8 = 40, 80
damaging-speed = 250
blowout-speed = 350
system_type = 0
lift_scalar = 0.1
drag_scalar = 0.1
pitch_scalar = 0.1

[flaps.1]       //Leading Edge Flaps - Lift	
type = 2
span-outboard = 0.5
extending-time = 5
flaps-position.0 = 0
flaps-position.1 = 6.428571429
flaps-position.2 = 12.85714286
flaps-position.3 = 19.28571429
flaps-position.4 = 25.71428571
flaps-position.5 = 32.14285714
flaps-position.6 = 38.57142857
flaps-position.7 = 45
flaps-position.8 = 38.57142857
damaging-speed = 173
blowout-speed = 217
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 = 7
flaps-position.5 = 8
flaps-position.6 = 9
flaps-position.7 = 10
flaps-position.8 = 45
damaging-speed = 173
blowout-speed = 217
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 = 0
engine_generator_map= 1,1

flap_motor = 0, 15, 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
light.0=4,  5.5, 0.0, 1.0,  fx_vclight//<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<
//light.1=4,  5.5,  1.0, 2.0,  fx_vclight

//Nick Needham's FX:
//light.1 = 8, -15.300, -4.800, -5.500, fx_nickspropdust_dirt_s
//light.2 = 8, -15.300,  4.800, -5.500, fx_nickspropdust_dirt_s
//light.3 = 9, -15.300, -4.800, -5.500, fx_nickspropdust_gravsnd_s
//light.4 = 9, -15.300,  4.800, -5.500, fx_nickspropdust_gravsnd_s
//light.5 = 6, -15.300, -4.800, -5.500,  fx_nickspropdust_watrsno_s
//light.6 = 6, -15.300,  4.800, -5.500,  fx_nickspropdust_watrsno_s


[keyboard_response]
elevator = 350, 500
aileron  = 450, 1000
rudder   = 200, 1000

[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=2,2

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2,2

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=1,1

[exits]
number_of_exits = 1
exit_rate.0 = 0.4

//<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<