[fltsim.0]
title=AI AN-26 Transavia Garantiya
sim=An-26
model=
panel=
sound=
texture=AN26_TAG
atc_id=
ui_manufacturer=Arkhangelsk Region
ui_type=AI An-26
ui_variation=Transavia Garantiya
atc_airline=Transavia Garantiya
atc_parking_codes=AN26,TAG
atc_parking_types=RAMP,CARGO
description=Antonov An-26 design by V-Zhyhulskiy

[General]
atc_type=Antonov
atc_model=An26
editable=0
performance=Antonov KB -1969, Crew 4 man, 2 Turboprop AI-24T 2075kW, weight 15020 starting weights 24000kg, loading 5500kg, speed 240mph, max 270, height 8100m, range 900-2250km, (C) 2002- Vladimir Zhyhulskiy: [email protected]


[WEIGHT_AND_BALANCE]
max_gross_weight=15000                        // (pounds)
empty_weight=9090                             // (pounds)

reference_datum_position=0.0, 0, 0       // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0.0, 0, 0       // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50

station_load.0=170,  5.0, -2.0, 0.0           //Pilot           Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1=170,  5.0,  2.0, 0.0           //Co-Pilot        Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2=170, -2.1, -2.0, 0.0           //Passenger       Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3=170, -2.1,  2.0, 0.0           //Passenger       Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4=170, -5.3, -2.0, 0.0           //Passenger       Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5=170, -5.3,  2.0, 0.0           //Passenger       Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI=30000
empty_weight_roll_MOI=18200
empty_weight_yaw_MOI=36500
empty_weight_coupled_MOI=0.0

[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=0.75
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.4
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=0.9
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0

[GeneralEngineData]
engine_type=5                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=-8.3, -4.8, 0.5                      //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=-8.3,  4.8, 0.5                      //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.0                   //Scalar for fuel flow efficiency
min_throttle_limit=-0.349915

[propeller]
thrust_scalar=1.0                   //Propeller thrust scalar
propeller_type=0                     //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=8.8                   //Propeller Diameter, (feet)
propeller_blades=4                     //Number of propeller blades
propeller_moi=24                    //Propeller moment of inertia
beta_max=45                    //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=15.2                  //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=25520                 //Miminum governed RPM
prop_tc=0.004                 //Prop time-constant
gear_reduction_ratio=17.6                  //Propeller gear reduction ratio
fixed_pitch_beta=0                     //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80                    //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=1                     //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=1                     //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=1                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available=1               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather=700                   //Minimum RPM for prop feathering
beta_feather=79.3                  //Feathering pitch angle (degrees)
power_absorbed_cf=0.9                   //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0          //Defeathering accumulators available? 0=FALSE, 1=TRUE 
prop_reverse_available=1                     //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta=1.0                   //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=-14.0                 //Minimum pitch angle in reverse, (degrees)

[TurbineEngineData]
fuel_flow_gain=0.011                 //Gain on fuel flow
inlet_area=1.0                   //Square Feet, engine nacelle inlet area
rated_N2_rpm=28920                 //RPM, second stage compressor rated value
static_thrust=158                   //Lbs, max rated static thrust at Sea Level

[turboprop_engine]
power_scalar=1.0                   //Scalar on Turboprop power
maximum_torque=4270                  //Maximum torque available (ft-lbs)


[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 17.0
marker_beacon=1, 2 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
starter1=0, 20, 17.0
light_nav=0, 5 , 17.0
light_beacon=0, 5 , 17.0
light_landing=0, 5 , 17.0
light_taxi=0, 5 , 17.0
light_strobe=0, 5 , 17.0
light_panel=0, 5 , 17.0

//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)

[contact_points]
point.0=1,  28.00,   0.00, -7.2, 1181, 0, 0.596, 39.9, 0.296, 2.5, 0.9516,  4.8,  4.8, 0, 0.0, 0.0
point.1=1,  -1.67,  -8.58, -7.2, 1574, 1, 0.596,  0.0, 0.642, 2.5, 0.8152,  4.5,  5.2, 2, 0.0, 0.0
point.2=1,  -1.67,   8.58, -7.2, 1574, 2, 0.596,  0.0, 0.642, 2.5, 0.8152,  4.8,  4.9, 3, 0.0, 0.0
point.3=2,  -3.33, -23.92, -6.00,  787, 0, 0.000,  0.0, 0.000, 0.0, 0.0000,  0.0,  0.0, 5, 0.0, 0.0
point.4=2,  -3.33,  23.92, -6.00,  787, 0, 0.000,  0.0, 0.000, 0.0, 0.0000,  0.0,  0.0, 6, 0.0, 0.0
point.5=2, -22.67,   0.00,  6.00,  787, 0, 0.000,  0.0, 0.000, 0.0, 0.0000,  0.0,  0.0, 9, 0.0, 0.0
point.6=2,  23.08,   0.00, -3.50,  787, 0, 0.000,  0.0, 0.000, 0.0, 0.0000,  0.0,  0.0, 4, 0.0, 0.0

static_pitch=-0
static_cg_height=6.6
gear_system_type=0

[Views]
eyepoint=4.54, -1.20, 3.25



[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
Transponder.1=1
Marker.1=1

[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to  1/2 and 1/8 respectively.
elevator=150, 250
aileron=150, 250
rudder=150, 250

[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



[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1

[SMOKESYSTEM]
smoke.0=-3.400,-44.00,-10.48, fx_smoke_rx
\\smoke.1=-3.200,-55.00,0.00, fx_smoke_rx
smoke.2=-3.400,-44.00,10.48, fx_smoke_rx 


[fuel]
LeftMain=0.0, -14.5, -1.0, 290.0, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux=0.0,  -6.0, -1.5,  109.5, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=0.0,  14.5, -1.0, 290.0, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux=0.0,   6.0, -1.5,  109.5, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=2                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1                    
electric_pump=0



[Reference Speeds]
flaps_up_stall_speed=96.0                  //Knots True (KTAS)
full_flaps_stall_speed=76.8                  //Knots True (KTAS)
cruise_speed=315.0                 //Knots True (KTAS)
max_indicated_speed=259.000000
max_mach=0.579980

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=0
pitch_takeoff_ga=8.000000
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

[forcefeedback]
stick_shaker_magnitude=5000             ; 0 - 10000
stick_shaker_direction=0                ; 0 - 35999 degrees
stick_shaker_period=111111              ; in microseconds
gear_bump_nose_magnitude=3000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=2700           ; 0 - 10000
gear_bump_left_direction=9000           ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=27000         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=1300            ; 0 - 10000
ground_bumps_angle1=08900               ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200             ; 0 - 10000
ground_bumps_angle2=09100               ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
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


[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=3,   4.1, -44.5,  4.6, fx_navred ,
light.1=3,   4.1,  44.5,  4.6, fx_navgre ,
light.2=2,   4.1,  44.5,  4.6, fx_strobe ,
light.3=2,   4.1, -44.5,  4.6, fx_strobe ,
light.4=1,  -26.9,   0.00,  9.5, fx_beacon ,
light.5=1,   -2.1,   0.00, -3.7, fx_beacon ,
light.6=4,  -16,   1.5, -1.5, fx_vclight
light.7=4,  -3,   -2.00, -1.3, fx_vclight
light.8=4,  -8,   2.00, -1.2, fx_vclight
light.9=4,  -10,   -2.00, -1.40, fx_vclight

light.10=4,  -16,   -1.5, -1.2, fx_vclight
light11=4,  -3,   2.00, -1.3, fx_vclight
light.12=4,  -8,   -2.00, -1.2, fx_vclight
light.13=4,  -10,   2.00, -1.20, fx_vclight

light.10=4, 16,   -1.5, -1.5, fx_vclight
light11=4,  18,   -1.00, -1.2, fx_vclight
light.12=4,  6,   -1.00, -1.4, fx_vclight
light.13=4,  20,   -1.00, -1.3, fx_vclight
light.14=4,  17,   -1.00, -0.5, fx_vclight


[exits]
number_of_exits=2
exit_rate.0=0.4                               ;Percent per second
exit_rate.1=0.4                               ;Percent per second

[airplane_geometry]
wing_area=310.000000
wing_span=57.166667
wing_root_chord=5.416667
wing_dihedral=5.998535
wing_incidence=0.999756
wing_twist=-1.499634
oswald_efficiency_factor=0.517744
wing_winglets_flag=1
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=67.000000
htail_span=17.166667
htail_pos_lon=-24.583333
htail_pos_vert=0.000000
htail_incidence=0.499878
htail_sweep=0.000000
vtail_area=42.000000
vtail_span=7.389181
vtail_sweep=0.000000
vtail_pos_lon=-20.500000
vtail_pos_vert=4.083333
elevator_area=16.985000
aileron_area=13.477000
rudder_area=7.275000
elevator_up_limit=16.999658
elevator_down_limit=15.498508
aileron_up_limit=18.002334
aileron_down_limit=18.002334
rudder_limit=30.000070
elevator_trim_limit=15.000035
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=5.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=9.998114,0.000000
flaps-position.2=19.996227,0.000000
flaps-position.3=29.994341,0.000000
flaps-position.4=39.992454,0.000000

[brakes]
toe_brakes_scale=1.000000
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=30.022988
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