[fltsim.0]
title=AN-28
sim=an28
model=
panel=
sound=
texture=
kb_checklists=an28_Check
kb_reference=an28_ref
atc_id=N8482A
ui_manufacturer=AHTOHOB
ui_type=28
ui_variation=White with red and blue
description=Derived from the AN14, the AN-28 served on short haul routes for the Former Soviet Union's Aeroflot airline. The Polish version is known as the Mielec M-28. This one was made with FSDS by ABACUS.

[fltsim.1]
title=AN-28 BFU
sim=an28
model=
panel=
sound=
texture=bfu
kb_checklists=an28_Check
kb_reference=an28_ref
atc_id=N8482BF
ui_manufacturer=AHTOHOB
ui_type=28
ui_variation=Bush Flying Unlimited
description=Derived from the AN14, the AN-28 served on short haul routes for the Former Soviet Union's Aeroflot airline. The Polish version is known as the Mielec M-28. This one was made with FSDS by ABACUS. Visit BFU at bfu.avsim.net

[General]
atc_type=Antonov
atc_model=28
editable=1
performance=Cruise Speed:  181 kt\nFull Load Range:  736 nm\nEngines:  TVD10B Turboprops\nDesigner:  Chuck Dome\nDate:  February 2002

[WEIGHT_AND_BALANCE]
max_gross_weight=8785                         // (pounds)
empty_weight=7000 //originally 4575           // (pounds)

reference_datum_position=16.2, 0, 0           // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-15.4, 0, 0          // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50

station_load.0=170, -11.3, -1.5, 0.0          //Pilot           Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1=170, -11.3,  1.5, 0.0          //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2=170, -13.9, -1.5, 0.0          //Rear Passenger  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3=170, -13.9,  1.5, 0.0          //Rear Passenger  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4=170, -17.2, -1.5, 0.0          //Rear Passenger  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5=170, -17.2,  1.5, 0.0          //Rear Passenger  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6=170, -20.2, -1.5, 0.0          //Rear Passenger  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7=170, -20.2,  1.5, 0.0          //Rear Passenger  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8=170, -23.2, -1.5, 0.0          //Rear Passenger  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.9=170, -23.2,  1.5, 0.0          //Rear Passenger  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.10=200, -16.2, 0.0, -5.0         //Cargo Pod (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI=8874.87
empty_weight_roll_MOI=6026.96
empty_weight_yaw_MOI=11858.54
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=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
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=-4.4, -6.0, 0.0               //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=-4.4,  6.0, 0.0               //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.12                  //Scalar for fuel flow efficiency

[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=3                     //Number of propeller blades
propeller_moi=19                       //Propeller moment of inertia
beta_max=45                            //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=5.6 //originally 15.6         //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=17.4              //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=0                  //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=5.0 //originally 88.0     //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=33000                     //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=1865                    //Maximum torque available (ft-lbs)

[Flaps.0]
type=1
span-outboard=0.5       // Percent span for flap position
extending-time=5.7      // Seconds, time to fully extend
system_type=0           // 0 = electrical
flaps-position.0=0      // degrees
flaps-position.1=10     // degrees
flaps-position.2=20     // degrees
flaps-position.3=30     // degrees

[pitot_static]
vertical_speed_time_constant=1.0    //Increasing this value will cause a more instantaneous reaction in the VSI

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 1
Com.2=1, 1
Nav.1=1, 1, 1
Nav.2=1, 1, 0
Adf.1=1
Transponder.1=1
Marker.1=1

[LIGHTS] // FS2002 FX lights
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=3,  -10.8, -35.61, 3.85, fx_navred
light.1=3,  -10.8,  35.61, 3.85, fx_navgre
light.2=2,  -10.8, -35.81, 3.85, fx_strobe
light.3=2,  -10.8,  35.81, 3.85, fx_strobe
light.4=1, -33.50,  -9.30, 10.6, fx_beacon

[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=100,  180
aileron=200, 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=3,0

[contact_points]
//0  Class
//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
point.0=1,  -4.70,  0.00, -5.25, 1500, 0, 0.5, 22.0, 0.18, 2.5, 0.7, 0.0, 0.0, 0
point.1=1, -18.00, -6.00, -5.40, 2500, 1, 0.5,  0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 2
point.2=1, -18.00,  6.00, -5.40, 2500, 2, 0.5,  0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 3
point.3=2, -15.90, -26.0,  3.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5
point.4=2, -15.90   26.0,  3.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6
point.5=2, -39.23,   0.0,  0.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9
point.6=2,  -2.50,   0.0, -2.17, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4
point.7=2, -42.00,   0.0, 10.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7
max_number_of_points=21

static_pitch=0.24           //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=5.11       //feet, altitude of CG when at rest on the ground

[Views]
eyepoint=-2.0, -1.5, 2.1    //(feet) longitudinal, lateral, vertical distance from reference datum

[fuel]
LeftMain=-18.4, -1.1, 2.5, 166.0, 3.6      //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-18.4,  1.1, 2.5, 166.0, 3.6     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=2                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1

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

[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=279.0                 //Square feet
wing_span=52.1                  //Feet
wing_root_chord=6.4             //Feet
wing_dihedral=3.9               //Degrees
wing_incidence=2.5              //Degrees
wing_twist=-1.7                 //Degrees
oswald_efficiency_factor=3.5 //originally 0.7    //Measure of lift effeciency of wing
wing_winglets_flag=0            //Are winglets available?
wing_sweep=0.0                  //Degrees, wing leading edge
wing_pos_apex_lon=-16.0         //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=0.0          //Feet, vertical distance from reference point, positive going up
htail_area=39.0                 //Square feet
htail_span=11.7                 //Feet
htail_pos_lon=-30.9             //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=0.0              //Feet, vertical distance from reference point, positive going up
htail_incidence=2.0             //Degrees
htail_sweep=5.0                 //Degrees, horizontal tail leading edge
vtail_area=18.0                 //Square feet
vtail_span=4.8                  //Feet, tip to body
vtail_sweep=45.0                //Degrees, vertical tail leading edge
vtail_pos_lon=-28.8             //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=1.5              //Feet, vertical distance from reference point, positive going up
elevator_area=16.6              //Square feet
aileron_area=18.3               //Square feet
rudder_area=6.7                 //Square feet
elevator_up_limit=28.0          //Degrees
elevator_down_limit=21.0        //Degrees
aileron_up_limit=20.0           //Degrees
aileron_down_limit=15.0         //Degrees
rudder_limit=24.0               //Degrees
elevator_trim_limit=19.5        //Degrees
spoiler_limit=20.0              //Degrees
spoilerons_available=1          //Spoilerons Available?
aileron_to_spoileron_gain=1     //Aileron to spoileron gain
min_ailerons_for_spoilerons=0   //Degrees
min_flaps_for_spoilerons=0      //Minimum flap handle position when spoilerons activate

[Reference Speeds]
flaps_up_stall_speed=66.0       //Knots True (KTAS)
full_flaps_stall_speed=52.8     //Knots True (KTAS)
cruise_speed=175.0              //Knots True (KTAS)

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000.0
autothrottle_available=0
pitch_takeoff_ga=8.000000
use_no_default_bank=1

[forcefeedback]
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=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=00500         ; 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