// Title:	An-24RV dynamics
// Author:	Aless (thanks for the help to Curl, ALZP, UNKL, Agat, Vinni-Puh ...) 
// Version: v5.102
// Date: jan 2010

//full fuel, full equip., pass empty, Baggage 3 = 400kg (100%)
//TOW 19994, MAC=23.62% (with fuel), MAC=24.92 (without fuel)

[fltsim.0]
title=Samdim Design Antonov An-24RV UTAir
sim=Antonov An-24RV
model=
panel=
sound=
texture=utair
atc_airline=utair
atc_flight_number=46501
atc_id=46501
checklists=
ui_manufacturer=Antonov (Samdim Design)
ui_type=An-24RV
ui_variation=UTAir
description=The Legendary Russian Turboprop\nAn-24 is the most used short-range aircraft in the ex-USSR. First flight: september,1 1963. Hundreds are still in service.\n\nFSDS2 model by D.Samborski ([email protected])\nPanel by V.Bocharnikov ([email protected])\nGauges by S.Gritsevsky (c) 2003\nDynamics by A.Terentyev (2006)\nSounds from Mike Maarse with corrections of S.Teifel (2006)
visual_damage=1

[fltsim.1]
title=Samdim Design Antonov An-24RV UTAir noVC
sim=Antonov An-24RV
model=noVC
panel=noVC
sound=
texture=utair
atc_airline=utair
atc_flight_number=46501
atc_id=46501
checklists=
ui_manufacturer=Antonov (Samdim Design)
ui_type=An-24RV (no VC)
ui_variation=UTAir
description=The Legendary Russian Turboprop\nAn-24 is the most used short-range aircraft in the ex-USSR. First flight: september,1 1963. Hundreds are still in service.\n\nFSDS2 model by D.Samborski ([email protected])\nPanel by V.Bocharnikov ([email protected])\nGauges by S.Gritsevsky (c) 2003\nDynamics by A.Terentyev (2006)\nSounds from Mike Maarse with corrections of S.Teifel (2006)
visual_damage=1

// --- add custom liveries starting from here ---
// [fltsim.2]
// ...

// --- do not modify after this line ---
[General]
performance=48-52 Passenger\nTwin Turboprop\nRegional Commuter\n\nDevelopment version
atc_type=Antonov
atc_model=AN24

[GeneralEngineData]
engine_type=5
Engine.0=12.00, -12.956, 3.0 
Engine.1=12.00, 12.956, 3.0
fuel_flow_scalar=0.88 //0.95
min_throttle_limit=0.0 //-0.1 

[Propeller]
thrust_scalar=1.0 
propeller_type=0
propeller_diameter=12.795
propeller_blades=4
propeller_moi=300 
beta_max=49.99
beta_min=8.0  
min_gov_rpm=13900.00
prop_tc=0.006 
gear_reduction_ratio=12.1285 
fixed_pitch_beta=15
low_speed_theory_limit=60.0
prop_sync_available=1
prop_deice_available=1
prop_feathering_available=1
prop_auto_feathering_available=1
min_rpm_for_feather=500.000 //1245
beta_feather=93.320
power_absorbed_cf=1.000
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=8.0 
minimum_reverse_beta=0.0 
rotation=-1 -1

[Turboprop_engine]
power_scalar=1.0
maximum_torque=10614.3602 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.00 
idle_rpm_friction_scalar=1.0 

[TurbineEngineData]
fuel_flow_gain=0.003 //0.005
inlet_area=1.000
rated_N2_rpm= 15100
static_thrust=470 
afterburner_available=0

[flight_tuning]
cruise_lift_scalar=1.0  
pitch_stability=1.0 
roll_stability=1.000 
yaw_stability=1.000
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=1.00 
aileron_effectiveness=1.00
rudder_effectiveness=1.0 
elevator_trim_effectiveness=1.00 
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
hi_alpha_on_roll=1 //multiplier on the effects on roll at high angles of attack
hi_alpha_on_yaw=1 //multiplier on the effects on yaw at high angles of attack
p_factor_on_yaw=1 //multipliers on the effects induced by rotating propellers 
torque_on_roll=1
gyro_precession_on_yaw=1
gyro_precession_on_pitch=1

[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

[Weight_and_balance]
MTW=47398.6 //21500 kg
MLW=47398.6 //21500 kg
empty_weight=31261.02 //14180kg
empty_weight_cg_position=0.485, 0.000, 0.0
reference_datum_position=-3.7, 0.000, 0.000
empty_weight_roll_MOI=250000.00 //500000
empty_weight_pitch_MOI=400000.00 //700000 
empty_weight_yaw_MOI=500000.00 
empty_weight_coupled_MOI=0.000
max_gross_weight=47398.6
CG_forward_limit=0.88
CG_aft_limit=-0.7

max_number_of_stations=50
//station_load.0=2270.73,0.0,0.000000,0.000000 // 20% CAX
station_load.0=2289,-6.51716,0,0,Weight // 23.63%  cax
//station_load.0=2270.73,-18.4,0.000000,0.000000 // 33% CAX
//station_load.0=2270.73,-28.6,0.000000,0.000000 // 41% CAX
//station_load.0=2270.73,-41.8,0.000000,0.000000 // 50% CAX

[electrical]
max_battery_voltage=27
generator_alternator_voltate=28.5
max_generator_alternator_amps=600.0
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, 15, 17.0
additional_system=0, 2 , 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
starter2=0, 20, 17.0
light_nav=0, 5 , 10.0
light_beacon=0, 5 , 10.0
light_landing=0, 5 , 17.0
light_taxi=0, 5 , 17.0
light_strobe=0, 5 , 10.0
light_panel=0, 5 , 10.0

[fuel]
LeftMain=0.485, -17.400, 4.300, 483.41, 0.000 //1469kg 
LeftAux=0.485, -10.000, 4.3, 304.73, 0.000 //926kg
RightMain=0.485, 17.400, 4.3, 483.41, 0.000 //1469kg
RightAux=0.485, 10.000, 4.3, 304.73, 0.000 //926kg
fuel_type=2.000000
number_of_tank_selectors=2
electric_pump=0

[airplane_geometry]
wing_area= 780 
wing_span= 95.8 
wing_root_chord=8.8 
wing_dihedral=0.000
wing_incidence=0.0   
wing_twist=0.00
oswald_efficiency_factor=0.705
wing_winglets_flag=0
wing_sweep=0.0
wing_pos_apex_lon=2.20 
wing_pos_apex_vert=4.3
htail_area=185.461 
htail_span=29.823
htail_pos_lon=-36.5
htail_pos_vert=3.000
htail_incidence=-3.00 
htail_sweep=21.000
vtail_area=192.4
vtail_span=16.076
vtail_sweep=25.000
vtail_pos_lon=-33.4
vtail_pos_vert=3.0
elevator_area=55.54
aileron_area=65.87 //32.9375
rudder_area=53.819
elevator_up_limit=30.0 
elevator_down_limit=15.0 
aileron_up_limit=24.0  
aileron_down_limit=16.0 
rudder_limit=25.000 
elevator_trim_limit=20.0 
spoiler_limit=57.3 //1 rad test
spoilerons_available=0
aileron_to_spoileron_gain=0.000
min_ailerons_for_spoilerons=0.000
min_flaps_for_spoilerons=0.000

//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]
static_pitch=-0.002
static_cg_height=7.0
gear_system_type=0
point.0 =1.00, 22.70,     0.00, -7.30,  800, 0, 1.147, 60.0, 0.26, 2.5, 0.6, 4.50, 4.50, 0, 0, 0
point.1 =1.00, -2.20319,-12.40, -7.54, 1400, 1, 1.475,  0.0, 0.30, 2.0, 0.55, 4.50, 4.50, 2, 0, 0
point.2 =1.00, -2.20319, 12.40, -7.54, 1400, 2, 1.475,  0.0, 0.30, 2.0, 0.55, 4.50, 4.50, 3, 0, 0
point.3 =2.00, 28.03,    -0.00, -4.90, 9000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 4, 0, 0
point.4 =2.00, -2.26,     0.00, -5.24, 6000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 4, 0, 0
point.5 =2.00,-41.05,     0.00, -1.00, 6000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 9, 0, 0
point.6 =2.00, -5.22,   -47.50,  3.42, 3000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 5, 0, 0
point.7 =2.00, -5.22,    47.50,  3.43, 3000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 6, 0, 0
point.8 =2.00, -1.22,   -47.50,  3.42, 3000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 5, 0, 0
point.9 =2.00, -1.22,    47.50,  3.42, 3000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 6, 0, 0
point.10=2.00,  2.70,   -12.50, -1.30, 6000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 5, 0, 0
point.11=2.00,  2.70,    12.50, -1.30, 6000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 6, 0, 0
point.12=2.00,-38.05,     0.00, 20.00, 3000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 8, 0, 0
point.13=2.00,-32.80,     0.00,  9.00, 3000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 8, 0, 0
point.14=2.00,  4.45,     0.00,  5.50, 3000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 7, 0, 0
point.15=2.00, 24.20,     0.00,  3.75, 3000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 8, 0, 0

[Flaps.0]
type=1
span-outboard=0.600
extending-time=16.000
system_type=1
damaging-speed=0.0 //162.000
blowout-speed=0.0 //170.000
lift_scalar=1.0 
drag_scalar=1.0
pitch_scalar=1.0
flaps-position.0= 0.000,  0.0
flaps-position.1= 5.000,  0.0
flaps-position.2=10.000,  0.0
flaps-position.3=15.000,  0.0
flaps-position.4=20.000,  0.0
flaps-position.5=25.000,  0.0
flaps-position.6=30.000,  0.0
flaps-position.7=38.000,  0.0

[Flaps.1]
type=1
span-outboard=0.600
extending-time=6.300
system_type=1
damaging-speed=0.0 //162.000
blowout-speed=0.0 //170.000
lift_scalar=0.2 
drag_scalar=0.1
pitch_scalar=0.05
flaps-position.0= 0.000, 0.0
flaps-position.1= 5.000, 0.0
flaps-position.2=10.000, 0.0
flaps-position.3=15.000, 0.0

[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
fold_rates=0.075,0.075

[exits]
number_of_exits = 2
exit_rate.0 = 0.09                             ;Percent per second
exit_rate.1 = 0.2                              ;Percent per second

[Reference Speeds]
flaps_up_stall_speed=102.000
full_flaps_stall_speed=82.800
cruise_speed=215.000
max_indicated_speed=292.000000
max_mach=0.650000

[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, 1
Adf.1=1
Transponder.1=1
Marker.1=1

[autopilot]
autopilot_available=0
flight_director_available=0
default_vertical_speed=1000.000000
autothrottle_available=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
use_no_default_bank=0	//For no wing leveler when AP On
use_no_default_pitch=0	//For no pitch holding when AP On
autoland_available=0

[Lights]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -2.26,-47.67, 3.24, fx_navredm ,
light.1 = 3, -2.26, 47.67, 3.24, fx_navgrem ,
light.2 = 2,-33.83,  0.00, 9.21, fx_beaconb ,
light.3 = 2, -4.80,  0.00,-4.21, fx_beaconh ,
light.4 = 3,-45.80,  0.00, 4.00, fx_navwhi  ,
light.5 = 4, 24.00,  2.00, 2.00, fx_vclight ,
light.6 = 4, 24.00, -2.00, 2.00, fx_vclight ,
light.7 = 5,  1.70, 26.42, 3.70, fx_landing ,
light.8 = 5,  1.70,-26.42, 3.70, fx_landing ,

[brakes]
toe_brakes_scale=0.518815
parking_brake=1

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=55.011494

[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000

[stall_warning]
type=1

[pitot_static]
vertical_speed_time_constant=0.5

[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

[Views]
eyepoint=22.2, -1.70, 2.1

[direction_indicators]
direction_indicator.0=3,0

[Effects]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[main]
Pilot=1,80
CoPilot=1,80
Navigator=1,80
RadioOperator=1,80
FrontBaggage=1,250
FrontBaggageA=1,250
Dress=1,50
BackBaggage=1,50
Stewardess=1,80
Food=1,40
Rows.4=1,75,1,75
Rows.5=1,75,1,75
Rows.6=1,75,1,75
Rows.7=1,75,1,75
Rows.8=1,75,1,75
Rows.9=1,75,1,75
Rows.10=1,75,1,75
Rows.11=1,75,1,75
Rows.12=1,75,1,75
Rows.13=1,75,1,75
Rows.14=1,75,1,75
Rows.15=1,75,0,75
Rows.16=0,75,0,75
Rows.17=1,75,1,75
Rows.18=1,75,1,75
Rows.19=1,75,1,75
Rows.20=1,75,1,75
Rows.21=1,75,1,75
Rows.22=1,75,1,75
Rows.23=1,75,1,75
Rows.24=1,75,1,75
Rows.25=1,75,1,75
Rows.26=1,75,1,75
Rows.27=1,75,1,75
Rows.28=0,75,1,75
Rows.29=0,75,0,75