[fltsim.0]
title=Boeing 747-400 MR MKIII Alitalia GE
sim=Boeing747-400-MR-MKIII
model=
panel=
sound=
texture=alitalia
ui_manufacturer=MelJet Boeing
ui_type=Boeing 747-400
ui_variation=Alitalia
atc_id=I-DEMO
atc_airline=Alitalia
atc_flight_number=AZ648
atc_heavy=1
description=MelJet Boeing 747-400 for FS2002\nVersion 3.0, Release 7 (October 23, 2002)\n\nVisual model and FDE by Melvin Rafi\nhttp:\/\/www.meljet.com
[General]
atc_type=BOEING
atc_model=B744
editable=0
performance=Flight Dynamic file Version 1.0 for FS2002\nEngine Type: General Electric CF6-80C2\n\nThis Aircraft and the Flight Dynamic File are freeware and are not to be sold or transfered in any form for which a fee is charged. Free distribution is allowed only after approval from MelJet.
[WEIGHT_AND_BALANCE]
max_gross_weight = 875000 // (pounds)
empty_weight = 450000 // (pounds)
reference_datum_position = 83.5, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -90.5, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 40000, -80.0, 0.0, 0.0 //Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_roll_MOI = 15352310
empty_weight_pitch_MOI = 24223159
empty_weight_yaw_MOI = 39531785
empty_weight_coupled_MOI = 0
[airplane_geometry]
wing_area = 5700.0 //Square feet
wing_span = 211.4 //Feet
wing_root_chord = 50.0 //Feet
wing_dihedral = 7.0 //Degrees
wing_incidence = 2.0 //Degrees
wing_twist = -1.0 //Degrees
oswald_efficiency_factor= 0.57 //Measure of lift effeciency of wing
wing_winglets_flag = 1 //Are winglets available?
wing_sweep = 37.5 //Degrees, wing leading edge
wing_pos_apex_lon = -68.2 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0 //Feet, vertical distance from reference point, positive going up
htail_area = 1450 //Square feet
htail_span = 72.8 //Feet
htail_pos_lon = -210.0 //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 = 37.5 //Degrees, horizontal tail leading edge
vtail_area = 1050 //Square feet
vtail_span = 37.1 //Feet, tip to body
vtail_sweep = 45.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -198.5 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 26.1 //Feet, vertical distance from reference point, positive going up
elevator_area = 325 //Square feet
aileron_area = 225 //Square feet
rudder_area = 230 //Square feet
elevator_up_limit = 25 //Degrees
elevator_down_limit = 15 //Degrees
aileron_up_limit = 25 //Degrees
aileron_down_limit = 15 //Degrees
rudder_limit = 31.5 //Degrees
elevator_trim_limit = 20 //Degrees
spoiler_limit = 45 //Degrees
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 3 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 15 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
[Reference Speeds]
flaps_up_stall_speed = 140.0 //Knots True (KTAS)
full_flaps_stall_speed = 112.0 //Knots True (KTAS)
cruise_speed = 505.0 //Knots True (KTAS)
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 25 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 5 // degrees
flaps-position.2 = 8 // degrees
flaps-position.3 = 15 // degrees
flaps-position.4 = 20 // degrees
flaps-position.5 = 25 // degrees
flaps-position.6 = 30 // degrees
damaging-speed = 280 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.55
drag_scalar = 1.0
pitch_scalar= 0.6
system_type = 1 //Hydraulic
[flaps.1]
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 5 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 1.0 // degrees
damaging-speed = 280 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.25
drag_scalar = 0.15
pitch_scalar= 0.1
system_type = 1 //Hydraulic
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 0.9
aileron_effectiveness = 0.9
rudder_effectiveness = 0.8
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
[fuel]
Center1 = -83.5, 0.0, -7.0, 18000.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -112.0, -35.0, -4.0, 12600.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux = -118.5, -52.0, -3.0, 5000.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -112.0, 35.0, -4.0, 12600.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux = -118.5, 52.0, -3.0, 5000.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center2 = -193.5, 0.0, 6.0, 4000.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
[autopilot]
autopilot_available = 1
flight_director_available = 1
default_vertical_speed = 1500.0
autothrottle_available = 1
autothrottle_arming_required = 1
autothrottle_max_rpm = 90
autothrottle_takeoff_ga = 1
pitch_takeoff_ga = 8;
[GeneralEngineData]
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -107.5, -69.5, -6.9 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -76.0, -38.9, -10.4 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.2 = -76.0, 38.9, -10.4 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.3 = -107.5, 69.5, -6.9 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency
[TurbineEngineData]
fuel_flow_gain = 0.002 //Gain on fuel flow
inlet_area = 48.0 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 62100 //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
[Views]
eyepoint = -20.00, -1.97, 9.4 ; Longitude, Latitude and Vertical position from Reference Point, (FEET)
[contact_points]
//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)
point.0 = 1, -25.0, 0.0, -18.0, 1000.0, 0, 2.0, 70.0, 0.5, 3.5, 0.900, 9.0, 8.0, 0, 220, 250
point.1 = 1, -114.0, -18.0, -18.5, 2000.0, 1, 2.0, 13.0, 0.5, 2.5, 0.900, 11.0, 9.0, 2, 220, 250
point.2 = 1, -114.0, 18.0, -18.5, 2000.0, 2, 2.0, 13.0, 0.5, 2.5, 0.900, 11.0, 9.0, 3, 220, 250
point.3 = 2, -152.6, -103.5, 3.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 5, 0, 0
point.4 = 2, -152.6, 103.5, 3.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 6, 0, 0
point.5 = 2, 3.0, 0.0, 0.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 9, 0, 0
point.6 = 2, -222.7, 0.0, 4.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0
static_pitch = -1.5
static_cg_height = 18.6
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot = 0, 5 , 17.0
avionics_bus = 0, 10, 17.0
avionics = 1, 5 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 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
[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
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
[exits]
number_of_exits = 2
exit_rate.0 = 0.15 ;Percent per second
exit_rate.1 = 0.15 ;Percent per second
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -196.50, 0.00, 6.40, fx_navwhih ,
light.1 = 1, -10.30, 0.00, 16.75, fx_beaconh ,
light.2 = 1, -58.70, 0.00, -11.25, fx_beaconb ,
[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
[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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[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
