[fltsim.0]
title=AI Xian Y7 Air Guinee
sim=an-24
model=
sound=
texture=gip
atc_flight_number=Y7
atc_airline=Phnom-Penh Air
atc_parking_codes=PPW
atc_parking_types=ramp
ui_manufacturer=Active Korea FS Traffic
ui_type=Xian Yunshuji Y7-100C
ui_variation=Royal Phnom Penh
description=AI model by Samdim, repaint by tanj
[General]
atc_type=aNtoNov
atc_model=
editable=1
performance=
[WEIGHT_AND_BALANCE]
max_gross_weight= 34500.000
empty_weight= 22941.000
reference_datum_position= 31.000, 0.000, 0.000
empty_weight_CG_position= -26.000, 0.000, 0.000
max_number_of_stations=50
station_load.0= 170.000, -9.800, -1.750, 0.000
station_load.1= 170.000, -9.800, 1.750, 0.000
station_load.2= 5660.000, -27.000, 0.000, 0.000
;Moments of Inertia
empty_weight_pitch_MOI= 268930.385
empty_weight_roll_MOI= 64343.449
empty_weight_yaw_MOI= 333273.834
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
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= -28.400, -13.300, 2.700
Engine.1= -28.400, 13.300, 2.700
fuel_flow_scalar= 1.000
min_throttle_limit=-0.250000
[propeller]
thrust_scalar=1.000
propeller_type= 0
propeller_diameter= 13.000
propeller_blades= 4
propeller_moi= 77.000
beta_max= 45.000
beta_min= 12.000
min_gov_rpm= 25520.000
prop_tc= 0.004
gear_reduction_ratio= 17.000
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= 700.000
beta_feather= 79.300
power_absorbed_cf= 0.900
defeathering_accumulators_available= 0
prop_reverse_available= 1
minimum_on_ground_beta= 1.000
minimum_reverse_beta= -14.000
[TurbineEngineData]
fuel_flow_gain= 0.011
inlet_area= 0.400
rated_N2_rpm= 29920.000
static_thrust= 200.000
afterburner_available= 0
[turboprop_engine]
power_scalar=1.000
maximum_torque= 7878.000
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
[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 = 1.000, -5.000, 0.000, -8.850, 1500.000, 0.000, 1.617, 10.000, 0.800, 2.500, 0.900, 5.000, 6.000, 0.000, 0.000, 0.000
point.1 = 1.000, -32.000, -12.990, -8.950, 3000.000, 1.000, 1.633, 0.000, 1.275, 2.500, 0.800, 6.000, 7.000, 2.000, 0.000, 0.000
point.2 = 1.000, -32.000, 12.990, -8.950, 3000.000, 2.000, 1.633, 0.000, 1.275, 2.500, 0.800, 6.000, 7.000, 3.000, 0.000, 0.000
point.3 = 2.000, -33.600, -42.500, 5.390, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4 = 2.000, -33.600, 42.500, 5.390, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5 = 2.000, -68.600, 0.000, 1.220, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6 = 2.000, 0.000, 0.000, -3.920, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 
 max_number_of_points=21
static_pitch= -0.400
static_cg_height= 7.100
gear_system_type=0
[Views]
eyepoint=-8.8, -1.45, 2.1      //(feet) longitudinal, lateral, vertical distance from reference datum
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[fuel]
LeftMain= -31.100, -9.100, 3.900, 417.500, 0.000
RightMain= -31.100, 9.100, 3.900, 417.500, 0.000
fuel_type=2                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=0
[airplane_geometry]
wing_area= 585.000
wing_span= 85.000
wing_root_chord= 7.000
wing_dihedral= 2.500
wing_incidence= 1.000
wing_twist= -3.000
oswald_efficiency_factor= 0.920
wing_winglets_flag= 0
wing_sweep= 3.000
wing_pos_apex_lon= -25.000
wing_pos_apex_vert= 0.000
htail_area= 97.000
htail_span= 26.000
htail_pos_lon= -58.900
htail_pos_vert= 0.000
htail_incidence= 1.000
htail_sweep= 8.000
vtail_area= 106.000
vtail_span= 11.700
vtail_sweep= 30.000
vtail_pos_lon= -54.900
vtail_pos_vert= 3.400
elevator_area= 53.500
aileron_area= 12.100
rudder_area= 46.400
elevator_up_limit= 10.000
elevator_down_limit= 15.500
aileron_up_limit= 18.000
aileron_down_limit= 18.000
rudder_limit= 30.000
elevator_trim_limit= 10.000
spoiler_limit= 60.000
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000
[Reference Speeds]
flaps_up_stall_speed= 92.000
full_flaps_stall_speed= 72.000
cruise_speed=270
max_indicated_speed=465.000000
max_mach=0.579980
[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=150.0, 250.0
aileron=150.0, 250.0
rudder=150.0, 250.0
[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 
use_no_default_pitch=1
default_pitch_mode=0
default_bank_mode=0
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, 5=landing
light.0 = 3, 7.04,-47.97, 3.82, fx_navredh ,
light.1 = 3, 7.04, 47.97, 3.82, fx_navgreh ,
light.2 = 3, -28.19,  0.00, 10.08, fx_navredh ,
light.3 = 2, 7.1,  48.0,  3.82, fx_strobe ,
light.4 = 2, 7.1, -48.0,  3.82, fx_strobe ,
[direction_indicators]
direction_indicator.0=3,0
[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 5.000
system_type= 0
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 30.000, 0.000
flaps-position.3= 40.000, 0.000
[brakes]
toe_brakes_scale=0.751976
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
[FSHS_AIBLAST]
OldName=Antonov
NewName=aNtoNov
