[fltsim.0]
title=Antonov An26 Ukrainian AF (VPS)
sim=An26zh
model=
panel=UA
sound=
texture=
kb_checklists=An26_Check
kb_reference=
ui_manufacturer=Antonov
ui_type=An26
ui_variation=UA AF (VPS)
atc_id=UA29
prop_anim_ratio=-1.53
atc_airline=UAAF
atc_flight_number=UA29
description=Antonov An-26 of Ukrainian AF (Odessa, Shkolhiy AFB)

[fltsim.1]
title=Antonov An26 Russian Navy (VMF)
sim=An26zh
model=
panel=
sound=
texture=VMF
kb_checklists=An26_Check
kb_reference=
ui_manufacturer=Antonov
ui_type=An26
ui_variation=Ru Navy (VMF)
atc_id=RA07
prop_anim_ratio=-1.53
atc_airline=Ru Navy
atc_flight_number=RA07
description=Antonov An-26 of Russian Navy - Nord fleet (Pushkin AFB)

[fltsim.2]
title=Antonov An26 UN
sim=An26zh
model=
panel=
sound=
texture=UN
kb_checklists=An26_Check
kb_reference=
ui_manufacturer=Antonov
ui_type=An26
ui_variation=UN
atc_id=UN96
prop_anim_ratio=-1.53
atc_airline=UN
atc_flight_number=UN96
description=Antonov An-26 UN RA 26664

[fltsim.3]
title=Antonov An26 AFL NORTH VARIANT
sim=An26zh
model=
panel=
sound=
texture=AFL
kb_checklists=An26_Check
kb_reference=
ui_manufacturer=Antonov
ui_type=An26
ui_variation=Aeroflot
atc_id=2651
prop_anim_ratio=-1.53
atc_airline=Aeroflot
atc_flight_number=2651
description=Antonov An-26 Aeroflot Nosern Division RA 26511

[General]
performance=An26 transport (by Vladimir Zhyhulskiy [email protected],january,2008, Kiev, Ukraine)
atc_type=An26
atc_model=An26
editable=0




\\\=====================================================================================================
///====================================================
///====================================================
///====================================================

[WEIGHT_AND_BALANCE]
empty_weight=29542	// Empty weight of aircraft DOW (lbs)
reference_datum_position=0,0,0	// (feet) distance from FS Reference: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0,0,0 	// (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50	// Payload  weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.0=379,31,0,0	// Weight Pilots (lbs)
station_load.1=190,27,0,0	// Weight stewards in front (lbs)
station_load.2=190,-19,0,0	// Weight stewards in rear (lbs)
station_load.3=331,20.5,0,0	// Weight cargo 1 (lbs)
station_load.4=776,-23,0,0	// Weight cargo 2 (lbs)


station_load.5=190,16.1,0,0	// Weight passengers row 1 (lbs)
station_load.6=758,13.6,0,0	
station_load.7=569,11,0,0	
station_load.8=569,8.4,0,0	
station_load.9=569,5.8,0,0
station_load.10=758,3.2,0,0
station_load.11=379,0.6,0,0
station_load.12=569,-1.9,0,0
station_load.13=569,-4.5,0,0
station_load.14=569,-7.1,0,0
station_load.15=569,-9.7,0,0
station_load.16=379,-12.3,0,0
station_load.17=758,-14.9,0,0
station_load.18=190,-17.4,0,0

//The Zero Fuel Weight of this aircraft is 17600 kg equal 38801 pounds

// Moment of Inertia
empty_weight_roll_MOI=287051
empty_weight_pitch_MOI=233733
empty_weight_yaw_MOI=283747
empty_weight_coupled_MOI=0
max_gross_weight=45900
CG_forward_limit=0.000
CG_aft_limit=1.000

///====================================================
///====================================================
///====================================================

[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=0.900
induced_drag_scalar=0.900
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[GeneralEngineData]
engine_type=5
Engine.0=7.620,-14.190,2.040
Engine.1=7.620,14.190,2.040
fuel_flow_scalar=0.75
min_throttle_limit=-0.250000

[TurbineEngineData]
fuel_flow_gain=0.005
inlet_area=1.100
rated_N2_rpm=29920.000
static_thrust=400.000
afterburner_available=0

[turboprop_engine]
power_scalar=1.0
maximum_torque=11124.000
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[propeller]
thrust_scalar=1.25
propeller_type=0
propeller_diameter=13.280
propeller_blades=6
propeller_moi=80.000
beta_max=45.0
beta_min=11.500
min_gov_rpm=24994.000
prop_tc=0.002
gear_reduction_ratio=24.686400
fixed_pitch_beta=0.000
low_speed_theory_limit=80.000
prop_sync_available=1
prop_deice_available=1
prop_feathering_available=1
prop_auto_feathering_available=1
min_rpm_for_feather=350.000
beta_feather=79.300
power_absorbed_cf=0.900
defeathering_accumulators_available=0
prop_reverse_available=1
minimum_on_ground_beta=0.000
minimum_reverse_beta=-20.000

[fuel]
// Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain=-3.560000,-14.230000,4.060000,678.000000,3.000000
RightMain=-3.560000,14.230000,4.060000,678.000000,3.000000
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=0


///==========================================================================
///====================================================
///====================================================

[contact_points]
        //0  Class                        <0=none,1=wheel, 2=scrape, 3=float>
        //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)

point.0=1.00,19.00, 0.00,-7.7,1600, 0.00, 1.1, 85.0, 0.80, 1.700000, 0.95, 10.00,10.00, 0.00, 0.00,0.00
point.1=1.00,-8.00,-12.5,-7.9,1800, 1.00, 1.6, 0.00, 0.75, 1.200000, 0.43, 10.00,10.00, 2.00, 0.00,0.00
point.2=1.00,-8.00,12.50,-7.9,1800, 2.00, 1.6, 0.00, 0.75, 1.200000, 0.43, 10.00,10.00, 3.00, 0.00,0.00
point.3=2.00,-3.916667,-46.500000,4.416667,1574.803150,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,5.00,0.00,0.00
point.4=2.00,-3.916667,46.500000,4.416667,1574.803150,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,6.00,0.00,0.00
point.5=2.00,-44.750000,0.00,2.00,1574.803150,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,9.00,0.00,0.00
point.6=2.00,22.333333,0.00,-2.500000,1574.803150,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,4.00,0.00,0.00
point.7= 5, -30.9, -5.25, -7.30,1600, 0, 0.00, 50.0, 0.0,  0.0,       1.00, 8.0, 8.2, 0, 0.0, 0.0

static_pitch=-0.30
static_cg_height=7.0
gear_system_type=0

///=======================================
///====================================================
///====================================================

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=10.000000
system_type=0
flaps-position.0=0                                    
flaps-position.1=10                                   
flaps-position.2=30                                   
flaps-position.3=40    
lift_scalar=1.0
drag_scalar=1.40   //0.5
pitch_scalar=1.40 //1.000

///=========================================
///====================================================
///====================================================

[Views]
eyepoint=0.19, -1.77, 1.71 


///eyepoint=18.7, -1.77, 1.74    //(feet) longitudinal, lateral, vertical distance from reference datum

///=========================================
///====================================================
///====================================================

[exits]
number_of_exits = 2
exit_rate.0 = 0.053                             ;Percent per second
exit_rate.1 = 0.2                               ;Percent per second

[TailHook]
tailhook_length=4                               ;(feet)
tailhook_position = -15.0, 0.0, -1.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust = 1.0

[folding_wings]
wing_fold_system_type=4                       ;0=None
fold_rates=0.075,0.075	                          ;Percent per second


[EFFECTS]
wake=fx_wake
water=fx_spray
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
startup=fx_An26start
windshield_rain_effect_available = 1
dirt=fx_An26dust

///============================================================                          
[SMOKESYSTEM]
smoke.0=0,-2.0,0.0, fx_An26box.fx   

///====================================================
///====================================================

[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3,  1.7,-47.07, 3.94, fx_navredm ,
light.1 = 3, 1.7, 47.07, 3.94, fx_navgrem ,
light.2 = 1, -1.00,  0.00, -4.21, fx_beaconh,
light.3 = 3, -42.30,   0.00,  4.00, fx_navwhi ,
light.4 = 4, 24, -1, 0, fx_vclight,
light.5 = 4, 27, 1, 0, fx_vclight,
light.6 = 4, 24,1, 0,  fx_vclight,
light.7 = 4, -3, -2, -1, fx_vclight ,
light.8 = 4, -3, 2, -1, fx_vclight,
light.9 = 4, 1.0, 0, -0.5, fx_vclight,
light.10 = 3, 14.30,   0.00,  3.20, fx_navwhi ,
light.11 = 3, 7.30,   0.00,  3.20, fx_navwhi ,
light.12 = 3, 0.30,   0.00,  3.20, fx_navwhi ,
light.13 = 3, -7.30,   0.00,  3.20, fx_navwhi ,
light.14 = 3, 19.00,   0.00,  3.20, fx_navwhi ,
\\\light.15 = 3,-30.00,  0.00, 8.90, fx_navredm ,


///====================================================
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=500
use_no_default_pitch=0		// 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank=0		// 0 = Default to Wing Leveler mode, 1 = No default bank mode.
autothrottle_available=1
autothrottle_arming_required=-256
autothrottle_takeoff_ga=-256
autothrottle_max_rpm=90.000
pitch_takeoff_ga=8.000
autoland_available=1
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

///====================================================
[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
Adf.2         = 1
Transponder.1 = 0
Marker.1      = 1

///====================================================
[brakes]
toe_brakes_scale=1.000
parking_brake=1

///====================================================

[airplane_geometry]
wing_area=753.000
wing_span=95.120
wing_root_chord=11.200
wing_dihedral=2.500
wing_incidence=2.500
wing_twist=-0.967
oswald_efficiency_factor=0.750
wing_winglets_flag=0
wing_sweep=6.000
wing_pos_apex_lon=1.000
wing_pos_apex_vert=5.100
htail_area=149.000
htail_span=32.520
htail_pos_lon=-37.600
htail_pos_vert=4.100
htail_incidence=0.000
htail_sweep=10.000
vtail_area=186.000
vtail_span=14.103
vtail_sweep=25.000
vtail_pos_lon=-33.030
vtail_pos_vert=5.100
elevator_area=35.600
aileron_area=59.400
rudder_area=56.000
elevator_up_limit=30.000
elevator_down_limit=20.000
aileron_up_limit=25.000
aileron_down_limit=25.000
rudder_limit=30.00
elevator_trim_limit=15.000
spoiler_limit=90.000
spoilerons_available=0
aileron_to_spoileron_gain=0.000
min_ailerons_for_spoilerons=0.000
min_flaps_for_spoilerons=0.000

///===========================================MISK===============
///==============================================================
///==============================================================

[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=3,0

[Reference Speeds]
flaps_up_stall_speed=98.000000
full_flaps_stall_speed=78.000000
cruise_speed=240.000
max_indicated_speed=324.000000
max_mach=0.656982

[pitot_static]
vertical_speed_time_constant=2.0	// Increasing this value will cause a faster reaction in the VSI

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=25.783101
flap_limit_idle=15.011494
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[forcefeedback]
stick_shaker_magnitude=8000		; 0 - 10000
stick_shaker_direction=18000		; 0 - 35999 degrees
stick_shaker_period=111111		; in microseconds
gear_bump_nose_magnitude=6000		; 0 - 10000
gear_bump_nose_direction=18000		; 0 - 35999 degrees
gear_bump_nose_duration=250000		; in microseconds
gear_bump_left_magnitude=5700		; 0 - 10000
gear_bump_left_direction=355000		; 0 - 35999 degrees
gear_bump_left_duration=250000		; in microseconds
gear_bump_right_magnitude=5700		; 0 - 10000
gear_bump_right_direction=79000		; 0 - 35999 degrees
gear_bump_right_duration=250000		; in microseconds
ground_bumps_magnitude1=3300		; 0 - 10000
ground_bumps_angle1=08900		; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=720		; 0 - 10000
ground_bumps_angle2=09100		; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.035
crash_magnitude1=10000			; 0 - 10000
crash_direction1=01000			; 0 - 35999 degrees
crash_magnitude2=10000			; 0 - 10000
crash_direction2=9000			; 0 - 35999 degrees
crash_period2=75000			; in microseconds
crash_duration2=2500000			; in microseconds
///====================================================END!!!==============================