[fltsim.0]
title=Boeing 727-2F2 Cargo Turkish Airlines
sim=B722-J17R-173
model=
panel=
sound=
texture=THY
atc_id=TC-JCA
atc_heavy=0
atc_flight_number=722
atc_airline=Turkish Cargo
ui_manufacturer=Boeing
ui_type=727-2F2
ui_variation=Turkish Airlines Cargo
description=B727-2F2, Edirne,Complete Package\nMDL Erick Cantu, Repaint Arno Aksu\nPanel Richard Probst, Sound Erick Cantu\nFDE Charles Fox, FDE, Panel and Sound mods by FlyTHY.
visual_damage=1
[General]
atc_type=BOEING AIRCRAFT
atc_model=B722
editable=0
performance=Cruise Speed: M0.82 @ FL350-370\nMaximum Range: 2,100 nm\nService Ceiling: 37,000 ft\nEmpty Weight: 97,650 lbs\nFuel Weight: 54,197 lbs (8,090 US Gal) \nMax Takeoff Weight: 173,000 lbs\nMax Landing Weight: 150,000 lbs or\nMax Landing Weight: 31,197 lbs fuel (57% fuel)\nPayload Weight: 21,153 lbs\nMAC: 24.9%\nSimulated Passengers: 106\nVmo\/Mmo: 375kts\/M0.91\n ( FL100\/Mach)\nClimb: 250kts\/300kts\/M0.78\nMax Cruise: 250kts\/350kts\/M0.82\nDescent: 250kts\/280kts\/M0.78
[pitot_static]
vertical_speed_time_constant=50 //Increasing this value will cause a more instantaneous reaction in the VSI
[WEIGHT_AND_BALANCE]
max_gross_weight=173000
empty_weight=118803
reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=1.000, 0.000, 0.000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
;Moments of Inertia
empty_weight_pitch_MOI=3359174
empty_weight_roll_MOI=661702
empty_weight_yaw_MOI=3963643
empty_weight_coupled_MOI=0
[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.0750
induced_drag_scalar=0.9130
elevator_effectiveness=1.000
aileron_effectiveness=1.0
rudder_effectiveness=10.000
pitch_stability=2.000
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=1.700
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
[GeneralEngineData]
engine_type=1
Engine.0=-49.714, -9.000, 0.857
Engine.1=-65.143, 0.000, 0.857
Engine.2=-49.714, 9.000, 0.857
fuel_flow_scalar=1.7609
[SMOKESYSTEM]
smoke.0=0.857, -57.714, -9.000, fx_smoke_rx
smoke.1=0.857, -73.143, 0.000, fx_smoke_rx
smoke.2=0.857, -57.714, 9.000, fx_smoke_rx
[TurbineEngineData]
fuel_flow_gain=0.002
inlet_area=9.852
rated_N2_rpm=12250.000
static_thrust=16400.000
afterburner_available=0
reverser_available=1
[jet_engine]
thrust_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, 65.000, 0.000, -7.100, 1181.100, 0.000, 1.323, 55.000, 0.300, 2.300, 0.700, 4.200, 4.200, 0.000, 250.0, 280.0 //ngear
point.1=1.000, -2.250, -9.670, -8.800, 1574.803, 1.000, 2.000, 0.000, 1.450, 0.550, 0.900, 6.900, 6.900, 2.000, 250.0, 280.0 //lgear
point.2=1.000, -2.250, 9.670, -8.800, 1574.803, 2.000, 2.000, 0.000, 1.450, 0.550, 0.900, 7.200, 7.200, 3.000, 250.0, 280.0 //rgear
point.3=2.000, -23.900, -55.850, -0.583, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 //lwing
point.4=2.000, -23.900, 55.850, -0.583, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 //rwing
point.5=2.000, 81.300, 0.000, 1.900, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //nose
point.6=2.000, -81.000, 0.000, 23.800, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //tail
point.7=2.000, -35.200, 0.000, -3.150, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //thook
static_pitch= -0.900
static_cg_height= 8.700
[Views]
eyepoint= 72.50, 0.00, 6.15
[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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0= 3, -16.70, -55.50, 0.75, fx_navredm ,
light.1= 3, -17.50, -55.85, 0.75, fx_navredm ,
light.2= 2, -15.60, -55.45, 0.70, fx_strobeh ,
light.3= 3, -23.90, -55.75, 0.55, MD80_INSPEC2 ,
light.4= 3, -16.70, 55.50, 0.75, fx_navgrem ,
light.5= 3, -17.50, 55.85, 0.75, fx_navgrem ,
light.6= 2, -15.58, 55.45, 0.70, fx_strobeh ,
light.7= 3, -23.90, 55.75, 0.55, MD80_INSPEC2 ,
light.8= 3, -81.00, 0.00, 23.80, fx_navwhi ,
light.9= 2, -81.00, 0.00, 23.80, fx_strobeh ,
light.10= 5, 24.75, -6.55, 3.30, MD80_INSPEC2 ,
light.11= 5, 24.75, 6.55, 3.30, MD80_INSPEC2 ,
light.12= 4, 72.60, -1.80, 6.35, fx_vclight ,
light.13= 4, 72.60, 1.80, 6.35, fx_vclight ,
light.14= 5, 4.80, -40.00, 8.40, fx_fxwing2.fx ,
light.15= 5, 4.80, 40.00, 8.40, fx_fxwing2.fx ,
light.16= 1, 12.50, 0.00, -3.85, MD80_BCNL ,
light.17= 1, 40.00, 0.00, 11.35, MD80_BCNU ,
[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
[exits]
number_of_exits=2
exit_rate.0=0.4 ;Percent per second
exit_rate.1=0.4 ;Percent per second
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
visual_damage=1
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=100.000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_max_rpm=99
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8
use_no_default_pitch=1
use_no_default_bank=1
[fuel]
Center1=-4.864, 0.000, -4.286, 4004.000, 0.000
LeftMain=-4.864, -14.571, -4.286, 2043.000, 0.000
RightMain=-4.864, 14.571, -4.286, 2043.000, 0.000
fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
[airplane_geometry]
wing_area=1650.000
wing_span=108.000
wing_root_chord=20.500
wing_dihedral=3.000
wing_incidence=2.000
wing_twist=-0.500
oswald_efficiency_factor=0.800
wing_winglets_flag=0
wing_sweep=32.000
wing_pos_apex_lon=7.500
wing_pos_apex_vert=-3.429
htail_area=376.000
htail_span=35.761
htail_pos_lon=-63.643
htail_pos_vert=19.286
htail_incidence=0.000
htail_sweep=42.000
vtail_area=290.000
vtail_span=15.092
vtail_sweep=57.000
vtail_pos_lon=-59.143
vtail_pos_vert=12.000
elevator_area=107.996
aileron_area=67.404
rudder_area=66.171
elevator_up_limit=17.000
elevator_down_limit=17.000
aileron_up_limit=27.000
aileron_down_limit=17.000
rudder_limit=25.000
elevator_trim_limit=10.000
spoiler_limit=60.000
spoilerons_available=1
aileron_to_spoileron_gain=2.000
min_ailerons_for_spoilerons=18.000
min_flaps_for_spoilerons=0.000
[Reference Speeds]
flaps_up_stall_speed=148.000
full_flaps_stall_speed=122.000
cruise_speed=488.000
[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
[Flaps.0]
type=1
span-outboard=0.602
extending-time=30.000
system_type=0
damaging-speed=250.000
blowout-speed=300.000
lift_scalar=0.000
drag_scalar=0.000
pitch_scalar=0.000
flaps-position.0=0.000
flaps-position.1=2.000
flaps-position.2=5.000
flaps-position.3=15.000
flaps-position.4=20.000
flaps-position.5=25.000
flaps-position.6=30.000
flaps-position.7=40.000
[Flaps.1]
type=1
span-outboard=0.602
extending-time=30.000
system_type=0
damaging-speed=250.000
blowout-speed=300.000
lift_scalar=1.450
drag_scalar=0.700
pitch_scalar=0.200
flaps-position.0=0.000
flaps-position.1=2.000
flaps-position.2=5.000
flaps-position.3=15.000
flaps-position.4=20.000
flaps-position.5=25.000
flaps-position.6=30.000
flaps-position.7=40.000
[Flaps.1]
type= 2
span-outboard= 0.800
extending-time= 8.000
system_type= 1
damaging-speed=230.000
blowout-speed= 250.000
lift_scalar= 5.000
drag_scalar= 0.000
pitch_scalar= 0.000
flaps-position.0= 0.000
flaps-position.1= 1.500
flaps-position.2= 2.000
