[fltsim.0]
title=Boeing 777-200ER United Airlines
sim=Boeing777-200-MR-MKIII //pss-777 airfile is recommended
model=pw
panel=
sound=
texture=ua
ui_manufacturer=MelJet
ui_type=B777-200ER
ui_variation=United Airlines
atc_id=
atc_airline=UNITED
atc_flight_number=777
atc_heavy=1
description=MelJet Boeing 777-200ER for FS2002\nVersion 1.0, Release 1 (January 4, 2003)\n\nVisual model and FDE by Melvin Rafi\nhttp:\/\/www.meljet.com
[fltsim.1]
title=Boeing 777-200ER Delta Airlines
sim=Boeing777-200-MR-MKIII //pss-777 airfile is recommended
model=rr
panel=
sound=
texture=dal2
ui_manufacturer=MelJet
ui_type=B777-200ER
ui_variation=Delta Airlines
atc_id=
atc_airline=Delta
atc_flight_number=777
atc_heavy=1
description=MelJet Boeing 777-200ER for FS2002\nVersion 1.0, Release 1 (January 4, 2003)\n\nVisual model and FDE by Melvin Rafi\nhttp:\/\/www.meljet.com
[General]
atc_type=BOEING
atc_model=B772
editable=0
performance=Flight Dynamic file Version 1.0 for FS2002\nEngine Thrust: 84000lbs each\nPowerplants: PW4090, Trent 895, GE90-94B\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.
[GROUND_REACTION]
MAX_STEERING_ANGLE=70
main_gear_static_compression=0.3 // (feet), The distance the main gear strut is compressed when at rest on the ground
center_gear_static_compression=0.25 // (feet), The distance the center gear strut is compressed when at rest on the ground
main_gear_damping_ratio=1.0 // Main gear strut damping, 0 = undamped osciallations, 1 = critically damped
center_gear_damping_ratio=1.0 // Center gear strut damping, 0 = undamped osciallations, 1 = critically damped
[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
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.2
induced_drag_scalar = 1.2
elevator_effectiveness = 1.0
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
pitch_stability = 1.1
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[jet_engine]
thrust_scalar = 1.0
[WEIGHT_AND_BALANCE]
//WHEN RECONFIGURING WEIGHT WITH PSS LOAD EDIT, MANUALLY RE-ENTER THE POSITIONS AS SHOWN BELOW!
//THIS WEIGHT CONFIG REPRESENTS A REASONABLY FULL LOAD OF 270 PASS (FC=18, BC=46, EC=206) WITH BAGGAGE (16239 LBS) AND CARGO (20398 LBS)
//MAX FUEL IS 225219 LBS AT TAKE OFF (96% WING TANKS-9195 GALS EACH,59% MAIN-15228 GALS, 33618 GALS TOTAL)
//IT IS RECOMMENDED THAT YOU USE A DIFFERENT CONFIG FILE WHEN USING PSS LOADEDIT AND MANUALLY ENTER THE WEIGHT VALUES HERE
empty_weight = 303864
reference_datum_position = 0.0, 0, 0 //DO NOT CHANGE THIS POSITION
empty_weight_CG_position = 0.0, 0, 0 //DO NOT CHANGE THIS POSITION
//WEIGHT, POSITION FORE-AFT, PORT-STARBORD, ABOVE-BELOW REFERENCE DATUM
station_load.0 = 0450, 98.00, 0.0, 2.0 //Weight Crew (lbs)
station_load.1 = 3000, 29.00, 0.0, -5.0 //Weight Galleys (lbs)
station_load.2 = 16239, -31.00, 0.0, -5.0 //Weight Baggage (lbs) Baggage
station_load.3 = 20398, 55.00, 0.0, -5.0 //Weight Cargo (lbs) Cargo
station_load.4 = 4320, 65.00, 0.0, 2.0 //Weight Psgr Sect OA (lbs) First
station_load.5 = 11040, 15.00, 0.0, 2.0 //Weight Psgr Sect OB (lbs) Business
station_load.6 = 49440, -35.00, 0.0, 2.0 //Weight Psgr Sect OC (lbs) Economy
//TOTAL ZFW = 405301
empty_weight_roll_MOI=18250000.000000
empty_weight_pitch_MOI=29000000.000000
empty_weight_yaw_MOI=10500000.000000
empty_weight_coupled_MOI=100.000000
[GeneralEngineData]
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 24.00, -31.55, -9.5 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 24.00, 31.55, -9.5 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 0.95 //Scalar for fuel flow efficiency
[TurbineEngineData]
fuel_flow_gain = 0.001900 //Gain on fuel flow
inlet_area = 120.0 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 84000 //Lbs, max rated static thrust at Sea Level
afterburner_available = 0 //Afterburner available?
reverser_available = 1 //Thrust reverser available?
prop_anim_ratio=-1.76
[airplane_geometry]
wing_area = 4605.0 //Square feet
wing_span = 198.250000 //Feet
wing_root_chord = 28.666667 //Feet
wing_dihedral = 5.998535 //Degrees
wing_incidence = 0.999756 //Degrees
wing_twist = -0.494385 //Degrees
oswald_efficiency_factor= 0.611045 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 0.0 //Degrees, wing leading edge
wing_pos_apex_lon = 32.5 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = -3.5 //Feet, vertical distance from reference point, positive going up
htail_area = 1089.0 //Square feet
htail_span = 70.0 //Feet
htail_pos_lon = -90.5 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 4.6 //Feet, vertical distance from reference point, positive going up
htail_incidence = 0.0 //Degrees
htail_sweep = 0.0 //Degrees, horizontal tail leading edge
vtail_area = 572.0 //Square feet
vtail_span = 27.269030 //Feet, tip to body
vtail_sweep = 0.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -80.3 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 10.8 //Feet, vertical distance from reference point, positive going up
elevator_area = 70.0 //Square feet
aileron_area = 26.8 //Square feet
rudder_area = 56.2 //Square feet
elevator_up_limit = 26.000825 //Degrees
elevator_down_limit = 26.000825 //Degrees
aileron_up_limit = 30.000070 //Degrees
aileron_down_limit = 30.000070 //Degrees
rudder_limit = 30.000070 //Degrees
elevator_trim_limit = 30.000013 //Degrees
spoiler_limit = 59.988681 //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 = 180.0 //Knots True (KTAS)
full_flaps_stall_speed = 120.0 //Knots True (KTAS)
cruise_speed = 560.0 //Knots True (KTAS)
[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, 85.42, 0.00, -17.50, 1181.1, 0, 3.500, 70.0, 1.0, 2.5, 0.7200, 15.0, 15.0, 0, 220.0, 280.0
point.1=1, -5.50, -18.00, -19.00, 1574.8, 1, 4.167, 20.0, 1.0, 2.5, 0.7500, 15.0, 15.0, 2, 220.0, 280.0
point.2=1, -5.50, 18.00, -19.00, 1574.8, 2, 4.167, 20.0, 1.0, 2.5, 0.7500, 15.0, 15.0, 3, 220.0, 280.0
point.3=2, -31.17, -99.33, 5.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -31.17, 99.33, 5.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -101.28, 0.00, 2.35, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, 104.00, 0.00, -3.75, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
static_pitch =0.00000
static_cg_height =17.56
[flaps.0] //Inboard Trailing Edge
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 28 // seconds
flaps-position.0=0.000000,0.000000
flaps-position.1=6.665409,0.000000
flaps-position.2=13.330818,0.000000
flaps-position.3=19.996227,0.000000
flaps-position.4=26.661636,0.000000
flaps-position.5=33.327045,0.000000
flaps-position.6=39.992454,0.000000
damaging-speed = 260 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 0.5
system_type = 1 //Hydraulic
[flaps.1] //Outboard Trailing Edge
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 28 // seconds
flaps-position.0=0.000000,0.000000
flaps-position.1=6.665409,0.000000
flaps-position.2=13.330818,0.000000
flaps-position.3=19.996227,0.000000
flaps-position.4=26.661636,0.000000
flaps-position.5=33.327045,0.000000
flaps-position.6=39.992454,0.000000
damaging-speed = 260 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 0.5
system_type = 1 //Hydraulic
[flaps.2] //Inboard Leading Edge Slats
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 5 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 1.0 // degrees
damaging-speed = 260 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 0.2
system_type = 1 //Hydraulic
[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
pitot_heat = 0, 15, 17.0
additional_system = 0, 20, 17.0
marker_beacon = 1, 2, 17.0
starter1 = 0, 20, 17.0
starter2 = 0, 20, 17.0
starter3 = 0, 20, 17.0
starter4 = 0, 20, 17.0
auto_brakes = 0, 15, 17.0
hydraulic_pump = 0, 2, 17.0
fuel_transfer_pump = 0, 5, 17.0
max_battery_voltage = 28.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps= 60.0
electric_always_available = 0
[pitot_static]
vertical_speed_time_constant=99
[exits]
number_of_exits = 1
exit_rate.0 = 0.1 ;Percent per second
[TailHook]
tailhook_length=1 ;(feet)
tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1.0
[folding_wings]
wing_fold_system_type=4 ;0=None
fold_rates=0.075,0.075 ;Percent per second
[Views]
eyepoint =97.5, -2.00, 2.25
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3,-102.70, 0.00, 6.50, fx_navwhih , //aft fuselage nav light
light.1 = 2,-102.70, 0.00, 6.50, fx_strobeh , //aft fuselage strobe
light.2 = 1, 39.00, 0.00, 10.50, fx_beaconh , //upper beacon
light.3 = 1, 20.25, 0.00, -11.50, fx_beaconb , //lower beacon
light.4 = 4, 96.30, 0.00, 3.00, fx_vclighth , //cockpit light splash
light.5 = 5, 53.25, -9.65, -3.55, fx_navwhih , //wing-engine light located on fuselage ls
light.6 = 5, 53.25, 9.65, -3.55, fx_navwhih , //wing-engine light located on fuselage rs
light.7 = 5, 40.55, 23.60, -7.50, fx_fxwing.fx, //wing and engine light splash effect rs
light.8 = 5, 40.50, -23.50, -7.50, fx_fxwing.fx, //wing and engine light splash effect ls
light.9 = 3, -88.00, -15.00, 5.40, fx_navwhi , //simulated tail light mounted on left horizontal stabilizer
light.10 = 3, -88.00, 15.00, 5.40, fx_navwhi , //simulated tail light mounted on right horizontal stabilizer
light.11 = 6, 97.0, 0.00, -10.0, MJ772TL , //nose gear light splash
[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
[fuel]
Center1 = 0.0, 0.0, -3.0, 26100.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = 2.0, -35.0, 0.0, 9580.0, 2.4 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = 2.0, 35.0, 0.0, 9580.0, 2.4 //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=1200.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=99
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8.0
use_no_default_pitch=1
use_no_default_bank=1
[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, 1
Adf.1=1
Transponder.1=1
Marker.1=1
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
