[fltsim.0]
title=Eastern Airlines B727-225 Adv.
sim=722FS2002
model=
panel=
sound=
texture=
panel_alias=
sound_alias=
kb_checklists=
kb_reference=
atc_id=N530EA
atc_id_color=0xffffffff
atc_airline=EASTERN
atc_flight_number=891
ui_manufacturer=Boeing
ui_type=B72S
ui_variation=Eastern Airlines
description=The Boeing 727 is the second most successful commercial jet airliner ever built. A total of 1,831 were built between 1963 and 1984.\nJT8D-15's at 15,500 lbs thrust\nFS2002 FDE Copyright 2001 Charles Fox
atc_heavy=0

[General]
atc_type=BOEING AIRCRAFT
atc_model=B722
performance=Cruise Speed: M0.80 @ FL350-370\nMaximum Range: 2,600 nm\nService Ceiling: 37,000 ft\nMax Takeoff Weight: 191,000 lb\nPassengers: 189\nVmo\/Mmo: 350kts\/M0.88\n                  ( FL100\/Mach)\nClimb:           250kts\/300kts\/M0.78\nMax Cruise:  250kts\/340kts\/M0.82\nDescent:       250kts\/280kts\/M0.78

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


[WEIGHT_AND_BALANCE]
max_gross_weight=191000.000
empty_weight=136161.000

reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=0.000, 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=5531932.000
empty_weight_roll_MOI=1191350.000
empty_weight_yaw_MOI=4229784.000
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=1.500
rudder_effectiveness=1.000
pitch_stability=1.404
roll_stability=2.000
yaw_stability=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[GeneralEngineData]
engine_type=1
Engine.0=-52.090, -8.600, 3.580
Engine.1=-71.680, 0.000, 2.870
fuel_flow_scalar=1.087
Engine.2=-52.090, 8.600, 3.580

[TurbineEngineData]
fuel_flow_gain=0.002
inlet_area=15.890
rated_N2_rpm=29920.000
static_thrust=15500.000
afterburner_available=0
reverser_available=1
fuel_flow_scalar=1.087

[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, 45.880, 0.000, -8.300, 800.000, 0.000, 1.442, 60.000, 0.800, 2.500, 0.900, 7.200, 5.900, 0.000, 0.000, 0.000
point.1=1.000, -14.340, -10.510, -9.000, 900.000, 1.000, 1.442, 0.000, 1.000, 2.500, 0.600, 7.900, 6.300, 2.000, 0.000, 0.000
point.2=1.000, -14.340, 10.510, -9.000, 900.000, 2.000, 1.442, 0.000, 1.000, 2.500, 0.600, 8.200, 6.600, 3.000, 0.000, 0.000

point.3=2.000, -34.410, -54.000, 0.000, 1.000, 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, -34.410, 54.000, 0.000, 1.000, 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, -41.100, 0.000, -3.820, 1.000, 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, 49.220, 0.000, -3.350, 1.000, 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=0.000
static_cg_height=7.660

[Views]
eyepoint=52.09, -1.43, 5.26   //(feet) longitudinal, lateral, vertical distance from reference datum

[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]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -25.26, -55.50, -0.25, fx_navredm ,
light.1=3, -25.26,  55.50, -0.25, fx_navgrem ,
light.2=2, -29.00, -55.50, -0.50, fx_strobeh ,
light.3=2, -29.00,  55.50, -0.50, fx_strobeh ,
light.4=2,  -2.65,   0.00, -4.60, fx_beaconb ,
light.5=1,  12.00,   0.00, 10.03, fx_beaconh ,
light.6=4,  44.41,   0.00,  3.50, fx_vclight ,
light.7=5,  13.60,   6.30, -0.50, fx_landing ,
light.8=5,  13.60,  -6.30, -0.50, fx_landing ,

[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

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=100
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=94
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;
autoland_available=1

[fuel]
Center1=-2.870, 0.000, 0.000, 4542.000, 0.000
LeftMain=-11.470, -20.550, 0.000, 1822.000, 0.000
RightMain=-11.470, 20.550, 0.000, 1822.000, 0.000
fuel_type=2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
                   

[airplane_geometry]
wing_area=1700.000
wing_span=108.000
wing_root_chord=24.370
wing_dihedral=3.000
wing_incidence=1.000
wing_twist=-0.500
oswald_efficiency_factor=0.800
wing_winglets_flag=0
wing_sweep=32.000
wing_pos_apex_lon=6.210
wing_pos_apex_vert=0.000
htail_area=375.650
htail_span=35.360
htail_pos_lon=-65.000
htail_pos_vert=21.500
htail_incidence=0.000
htail_sweep=39.000
vtail_area=302.230
vtail_span=16.250
vtail_sweep=57.000
vtail_pos_lon=-52.570
vtail_pos_vert=23.420
elevator_area=95.000
aileron_area=50.240
rudder_area=67.820
elevator_up_limit=20.000
elevator_down_limit=20.000
aileron_up_limit=20.000
aileron_down_limit=20.000
rudder_limit=30.000
elevator_trim_limit=20.000
spoiler_limit=60.000
spoilerons_available=0
aileron_to_spoileron_gain=3.000
min_ailerons_for_spoilerons=10.000
min_flaps_for_spoilerons=0.000

[Reference Speeds]
flaps_up_stall_speed=148.000
full_flaps_stall_speed=104.000
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=0.629
extending-time=20.000
system_type=1
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=2.000, 0.000
flaps-position.2=5.000, 0.000
flaps-position.3=15.000, 0.000
flaps-position.4=20.000, 0.000
flaps-position.5=25.000, 0.000
flaps-position.6=30.000, 0.000
flaps-position.7=40.000, 0.000

[Flaps.1]
type=2
span-outboard=0.950
extending-time=3.000
system_type=1
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=1.000, 0.000

[Flaps.2]
type=2
span-outboard=0.950
extending-time=3.000
system_type=1
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=0.500, 0.000
flaps-position.2=1.000, 0.000