[fltsim.0]
title=Ukraine Mediterrenian Airlines  Douglas DC-9-51 UR-CBY
sim=aia_dc_9_50
model=
panel=
sound=
texture=UMAir\UR-CBY
kb_checklists=
kb_reference=
atc_id=UR-CBY
atc_airline=UM Air
atc_flight_number=
ui_manufacturer=траффик Ukraine Mediterrenian Airlines
ui_type=DC-9-50
ui_variation=UR-CBY
description=AI Aardvark DC-9-50 Repaint by Sanovich ([email protected])
atc_id_color=0000000000
visual_damage=0
 
[fltsim.1]
title=Ukraine Mediterrenian Airlines  Douglas DC-9-51 UR-CCT
sim=aia_dc_9_50
model=
panel=
sound=
texture=UMAir\UR-CCT
kb_checklists=
kb_reference=
atc_id=UR-CCT
atc_airline=UM Air
atc_flight_number=
ui_manufacturer=траффик Ukraine Mediterrenian Airlines
ui_type=DC-9-50
ui_variation=UR-CCT 
description=AI Aardvark DC-9-50 Repaint by Sanovich ([email protected])
atc_id_color=0000000000
visual_damage=0


[fltsim.2]
title=Ukraine Mediterrenian Airlines  Douglas DC-9-51 UR-CCS
sim=aia_dc_9_50
model=
panel=
sound=
texture=UMAir\UR-CCS
kb_checklists=
kb_reference=
atc_id=UR-CCS
atc_airline=UM Air
atc_flight_number=
ui_manufacturer=траффик Ukraine Mediterrenian Airlines
ui_type=DC-9-50
ui_variation=UR-CCS
description=AI Aardvark DC-9-50 Repaint by Sanovich ([email protected])
atc_id_color=0000000000
visual_damage=0

[General]
atc_type=MCDONNELDOUGLAS 
atc_model=DC9 
editable=1 
performance=Only experienced AI pilots should attempt to fly this aircraft. 
 

[weight_and_balance]

// ACM V1.0 pl4
max_gross_weight = 120000
empty_weight = 79686
reference_datum_position = 77, 0, 0
empty_weight_CG_position = -72, 0, 0
empty_weight_pitch_MOI = 951967
empty_weight_roll_MOI = 465681
empty_weight_yaw_MOI = 1447094
empty_weight_coupled_MOI = 0
max_number_of_stations = 1

station_load.0 = 33000, -69.5,  0.0, 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=1                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=-103.6, -8.5, 0.6                    //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=-103.6,  8.5, 0.6                    //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.0                   //Scalar for fuel flow efficiency
min_throttle_limit=-0.250000
 

[TurbineEngineData]
fuel_flow_gain=0.002                 //Gain on fuel flow
inlet_area=10.4                  //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920                 //RPM, second stage compressor rated value
static_thrust=19000                 //Lbs, max rated static thrust at Sea Level
afterburner_available=0                     //Afterburner available?
reverser_available=1                     //Thrust reverser available?
 

[jet_engine]
thrust_scalar=1.0
 

[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]
static_pitch = -0.5
static_cg_height = 4.1
max_number_of_points = 7

point.0 = 1, -16.1697, 0, -4.4134, 1500, 0, 1.08, 25, 1, 2.5, 0.9, 7, 5, 0, 0, 0
point.1 = 1, -83.0959, -8.3297, -5.4231, 3000, 1, 1.85, 0, 1.5, 2.5, 0.8, 7, 7, 2, 0, 0
point.2 = 1, -83.1, 8.33, -5.4231, 3000, 2, 1.85, 0, 1.5, 2.5, 0.8, 7, 7, 3, 0, 0
point.3 = 2, -92.3227, -47.3471, 3.0831, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -92.3227, 47.3471, 3.0831, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -129.6882, 0, 6.8754, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, -14.574, 0, 1.8174, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
gear_system_type=0


[Views]
eyepoint=-13.3, -1.82, 5.0    //(feet) longitudinal, lateral, vertical distance from reference datum
 

[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 20.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.5
drag_scalar=1.0
pitch_scalar= 1.0
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 2.000, 0.000
flaps-position.3= 5.000, 0.000
flaps-position.4= 10.000, 0.000
flaps-position.5= 15.000, 0.000
flaps-position.6= 25.000, 0.000
flaps-position.7= 30.000, 0.000
flaps-position.8= 40.000, 0.000

[Flaps.1]
type= 2
span-outboard= 0.800
extending-time= 2.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.00
drag_scalar= .00
pitch_scalar= 0.00
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000

[Flaps.2]
type= 2
span-outboard= 0.800
extending-time= 3.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.00
drag_scalar= 0.00
pitch_scalar= 0.00
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.500, 0.000
flaps-position.2= 1.000, 0.000
 

[lights]

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

light.0 = 3, -87.77, 46.78, 3.41, fx_navgrem
light.1 = 3, -87.77, -46.78, 3.41, fx_navredm
light.2 = 2, -87.97, -46.96, 3.34, fx_strobeh
light.3 = 2, -87.97, 46.96, 3.34, fx_strobeh
light.4 = 3, -91.41, 47.43, 3.13, fx_navwhi
light.5 = 3, -91.41, -47.43, 3.13, fx_navwhi
light.6 = 1, -71, 0, 10.29, fx_beaconb
light.7 = 1, -76.5, 0, -1.24, fx_beacon


[pitot_static]
vertical_speed_time_constant=1                //Increasing this value will cause a more instantaneous reaction in the VSI
 
 

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

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 1

Center1 = -76.2, 0, -6, 580, 3
Center2 = -78.2, 0, -6, 580, 3
LeftMain = -78.7, -12.1, -4, 2920, 3
RightMain = -78.7, 12.1, -4, 2920, 3
electric_pump=0


[airplane_geometry]
wing_area=1209.0                //Square feet
wing_span=107.8                 //Feet
wing_root_chord=23.1                  //Feet
wing_dihedral=3.0                   //Degrees
wing_incidence=1.3                   //Degrees
wing_twist=0.0                   //Degrees
oswald_efficiency_factor=0.8                   //Measure of lift effeciency of wing
wing_winglets_flag=0                     //Are winglets available?
wing_sweep=24.5                  //Degrees, wing leading edge
wing_pos_apex_lon=-61.0                 //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=341.0                 //Square feet
htail_span=40.0                  //Feet
htail_pos_lon=-134.0                //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=0.0                   //Degrees
htail_sweep=30.0                  //Degrees, horizontal tail leading edge
vtail_area=168.0                 //Square feet
vtail_span=14.8                  //Feet, tip to body
vtail_sweep=25.0                  //Degrees, vertical tail leading edge
vtail_pos_lon=-131.8                //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=10.9                  //Feet, vertical distance from reference point, positive going up
elevator_area=145.0                 //Square feet
aileron_area=38.0                  //Square feet
rudder_area=65.3                  //Square feet
elevator_up_limit=26.0                  //Degrees
elevator_down_limit=26.0                  //Degrees
aileron_up_limit=30.0                  //Degrees
aileron_down_limit=30.0                  //Degrees
rudder_limit=30.0                  //Degrees
elevator_trim_limit=20.0                  //Degrees
spoiler_limit=60.0                  //Degrees
spoilerons_available=1                     //Spoilerons Available?
aileron_to_spoileron_gain=3                   //Aileron to spoileron gain
min_ailerons_for_spoilerons=10                //Degrees
min_flaps_for_spoilerons=0                    //Minimum flap handle position when spoilerons activate
 

[Reference Speeds]
flaps_up_stall_speed=142.0                 //Knots True (KTAS)
full_flaps_stall_speed=113.6                 //Knots True (KTAS)
cruise_speed=477                //Knots True (KTAS)
max_indicated_speed=340.000000
max_mach=0.820020
 

[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=1800.0 
autothrottle_available=1 
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8 ;
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]
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
 

[direction_indicators]
direction_indicator.0=3,0 

[brakes]
toe_brakes_scale=0.885037
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[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