[fltsim.0]
title=Boeing 727-200 cargo
sim=b727
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=S9-BAQ
atc_airline=Air GEMINI
atc_flight_number=293
ui_manufacturer=Boeing
ui_type=727-200
ui_variation=AIR GEMINI
visual_damage=1
description=Paint by Mario Coelho\n40 years old and still flying, the venerable 727 far surpassed Boeing's most optimistic sales forecasts. 1831 were built, with many still in service today. Noisy and inefficient by today's standards, it set new standards for comfort and reliability in its day.
atc_heavy=0
[General]
atc_type=BOEING AIRCRAFT
atc_model=B727
editable=1
performance=Max speed: 598 mph\nRange: 2,728 mi\nCeiling: 33,000 ft.\nEmpty weight: 99,370\nLoaded: 190,090\nPassengers: 145 typical
[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 = 209000.000
empty_weight = 100000.000
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 = 20000.000, 0.000, 0.000, 0.000
;Moments of Inertia
empty_weight_pitch_MOI = 5600000.000
empty_weight_roll_MOI = 1400000.000
empty_weight_yaw_MOI = 4000000.000
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 =1.000
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 = 1
Engine.0 = -45.000, -9.000, 4.000
Engine.1 = -45.000, 9.000, 4.000
fuel_flow_scalar = 1.000
Engine.2= -60.000, 0.000, 3.000
[TurbineEngineData]
fuel_flow_gain = 0.002
inlet_area = 18.000
rated_N2_rpm = 29920.000
static_thrust = 16000.000
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, 40.000, 0.000, -7.500, 1181.100, 0.000, 1.442, 55.920, 0.800, 2.500, 0.900, 4.000, 4.000, 0.000, 0.000, 0.000
point.1= 1.000, -7.750, -8.580, -8.900, 1574.800, 1.000, 1.442, 0.000, 1.000, 2.500, 0.900, 6.900, 6.900, 2.000, 0.000, 0.000
point.2= 1.000, -7.750, 8.580, -8.900, 1574.800, 2.000, 1.442, 0.000, 1.000, 2.500, 0.900, 7.100, 7.100, 3.000, 0.000, 0.000
point.3= 2.000, -14.170, -47.330, 0.000, 787.400, 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, -14.170, 47.330, 0.000, 787.400, 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, -54.000, 0.000, 2.830, 787.400, 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, 42.670, 0.000, -3.750, 787.400, 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= -1.000
static_cg_height= 7.500
[Views]
eyepoint=43.7, -1.31, 3.55 //(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, -22.89, -53.20, 0.85, fx_navredm ,
light.1 = 3, -22.89, 53.20, 0.85, fx_navgrem ,
light.2 = 3, -80.73, 0.00, 23.16, fx_navwhih ,
light.3 = 2, -24.00, -53.53, 0.85, fx_strobeh ,
light.4 = 2, -24.00, 53.53, 0.85, fx_strobeh ,
light.5 = 2, 3.36, 0.00, -4.21, fx_beaconb ,
light.6 = 1, 29.96, 0.00, 9.15, fx_beaconh ,
light.7 = 4, 60.87, 0.00, 6.39, fx_vclight ,
light.8 = 5, 66.0, 0.00, -7.00, newll,
[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=1800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm = 90
autothrottle_takeoff_ga=1
pitch_takeoff_ga = 8;
use_no_default_bank = 1
use_no_default_pitch = 1
[fuel]
Center1 = 0.000, 0.000, 0.000, 3800.000, 0.000
LeftMain = -3.000, -19.000, 0.000, 2500.000, 0.000
RightMain = -3.000, 19.000, 0.000, 2500.000, 0.000
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
[airplane_geometry]
wing_area = 1400.000
wing_span = 108.000
wing_root_chord = 25.000
wing_dihedral = 2.000
wing_incidence = 1.000
wing_twist = -0.500
oswald_efficiency_factor= 0.750
wing_winglets_flag = 0
wing_sweep = 35.000
wing_pos_apex_lon = 12.000
wing_pos_apex_vert = 0.000
htail_area = 350.000
htail_span = 35.000
htail_pos_lon = -60.000
htail_pos_vert = 24.000
htail_incidence = 0.000
htail_sweep = 30.000
vtail_area = 440.000
vtail_span = 20.000
vtail_sweep = 35.000
vtail_pos_lon = -45.000
vtail_pos_vert = 8.000
elevator_area = 45.000
aileron_area = 25.000
rudder_area = 59.000
elevator_up_limit = 22.500
elevator_down_limit = 19.500
aileron_up_limit = 20.000
aileron_down_limit = 20.000
rudder_limit = 26.000
elevator_trim_limit = 20.000
spoiler_limit = 60.000
spoilerons_available = 1
aileron_to_spoileron_gain = 3.000
min_ailerons_for_spoilerons = 10.000
min_flaps_for_spoilerons = 0.000
[Reference Speeds]
flaps_up_stall_speed = 140.000
full_flaps_stall_speed = 110.000
cruise_speed = 515.000
[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= 0.400
extending-time= 8.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.500
drag_scalar= 0.500
pitch_scalar= 0.250
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= 1
span-outboard= 0.400
extending-time= 8.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.500
drag_scalar= 0.500
pitch_scalar= 0.250
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.2]
type= 2
span-outboard= 0.800
extending-time= 4.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 4.000
drag_scalar= 0.400
pitch_scalar= 0.200
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.000, 0.000
flaps-position.2= 0.000, 0.000
flaps-position.3= 1.000, 0.000
[Flaps.3]
type= 2
span-outboard= 0.800
extending-time= 4.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.500
drag_scalar= 0.500
pitch_scalar= 0.250
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.000, 0.000
flaps-position.2= 0.000, 0.000
flaps-position.3= 1.000, 0.000
