[fltsim.0]
title=Vmax 747-200 VMAX Transexport
sim=vmax_classic_2

model=
panel=
sound=
texture=
kb_checklists=Boeing747-200_check
kb_reference=Boeing747-200_ref
atc_type=Boeing
atc_model=B742
atc_id_enable=1
atc_id=EW-445TQ
atc_id_color=0xffffffff
editable=0
atc_airline=Transexport
atc_flight_number=337	
atc_heavy=1
ui_manufacturer=Ready For Pushback
ui_type=747-200F
ui_variation=Trans Avia Export
visual_damage=1
description=Vmax Classic 747-200\Manufactured between 1970 and 1986\nPowered by 4 Pratt & Whitney JT9D Engines \ Copyright of Ralph's Panel Shop and Vmax Flight Systems
atc_parking_codes=
atc_parking_types=

//FS2004 Version 2 

[FORCEFEEDBACK]
GEAR_BUMP_NOSE_MAGNITUDE=6000
GEAR_BUMP_NOSE_DIRECTION=18000
GEAR_BUMP_NOSE_DURATION=250000
GEAR_BUMP_LEFT_MAGNITUDE=6000
GEAR_BUMP_LEFT_DIRECTION=35500
GEAR_BUMP_LEFT_DURATION=250000
GEAR_BUMP_RIGHT_MAGNITUDE=6000
GEAR_BUMP_RIGHT_DIRECTION=00500
GEAR_BUMP_RIGHT_DURATION=250000
GROUND_BUMPS_MAGNITUDE1=3250
GROUND_BUMPS_ANGLE1=8900
GROUND_BUMPS_INTERCEPT1=5.0
GROUND_BUMPS_SLOPE1=0.48
GROUND_BUMPS_MAGNITUDE2=750
GROUND_BUMPS_ANGLE2=9100
GROUND_BUMPS_INTERCEPT2=0.075
GROUND_BUMPS_SLOPE2=1.0
CRASH_MAGNITUDE1=10000
CRASH_DIRECTION1=01000
CRASH_MAGNITUDE2=10000
CRASH_DIRECTION2=9000
CRASH_PERIOD2=75000
CRASH_DURATION2=2500000

[ELECTRICAL]
;BUSTYPE, MAXAMPLOAD, MINVOLTAGE  
;BUSTYPES:0=MAINBUS,1=AVIONICSBUS,2=BATTERYBUS,3=HOTBATTERYBUS,4-7=GENERATOR/ALTERNATORBUS(1-4)

;BUS TYPES:
;0=MAIN BUS(MOST COMPONENTS CONNECTED HERE)
;1=AVIONICS BUS
;2=BATTERY BUS
;3=HOT BATTERY BUS(BYPASSESE MASTER SWITCH)
;4=GENERATOR/ALTERNATOR BUS1
;5=GENERATOR/ALTERNATOR BUS2
;6=GENERATOR/ALTERNATOR BUS3
;7=GENERATOR/ALTERNATOR BUS4 
;BUSTYPE, MAXAMPLOAD, MINVOLTAGE 

MAX_BATTERY_VOLTAGE = 30.0
GENERATOR_ALTERNATOR_VOLTAGE = 30.0
GENERATOR_ALTERNATOR_AMPS = 100.0 
FLAP_MOTOR = 0, 15, 17.0
GEAR_MOTOR = 0, 15, 17.0
AUTOPILOT = 0, 12, 0.0
AVIONICS_BUS = 0, 10, 17.0
AVIONICS = 1, 10, 10.0
PITOT_HEAT = 0, 15, 10.0
ADDITIONAL_SYSTEM = 0, 10, 4.0
MARKER_BEACON = 1, 10, 6.0
GEAR_WARNING = 0, 2, 10.0
FUEL_PUMP = 0, 15, 5.0
STARTER1 = 0, 20, 15.0
STARTER2 = 0, 20, 15.0
STARTER3 = 0, 20, 15.0
STARTER4 = 0, 20, 15.0
LIGHT_NAV = 0, 10, 5.0
LIGHT_BEACON = 0, 10, 5.0
LIGHT_LANDING = 0, 25, 15.0
LIGHT_TAXI = 0, 25, 15.0
LIGHT_STROBE = 0, 10, 10.0
LIGHT_PANEL = 0, 5, 10.0
AUTO_BRAKES = 0, 1, 5.0
HYDRAULIC_PUMP = 0, 5, 5.0
FUEL_TRANSFER_PUMP = 0, 5, 5.0
LIGHT_RECOGNITION = 0, 5, 5.0
LIGHT_WING = 0, 10, 10.0
LIGHT_LOGO = 0, 10, 10.0

[GROUND_REACTION]
MAIN_GEAR_STATIC_COMPRESSION   = 1.0		// (FEET), THE DISTANCE THE MAIN GEAR STRUT IS COMPRESSED WHEN AT REST ON THE GROUND
CENTER_GEAR_STATIC_COMPRESSION = 0.8            // (FEET), THE DISTANCE THE CENTER GEAR STRUT IS COMPRESSED WHEN AT REST ON THE GROUND
MAIN_GEAR_DAMPING_RATIO	       = 0.9		// MAIN GEAR STRUT DAMPING, 0 = UNDAMPED OSCIALLATIONS, 1 = CRITICALLY DAMPED
CENTER_GEAR_DAMPING_RATIO      = 0.9		// CENTER GEAR STRUT DAMPING, 0 = UNDAMPED OSCIALLATIONS, 1 = CRITICALLY DAMPED
MAX_STEERING_ANGLE             =70.0

[PITOT_STATIC]
VERTICAL_SPEED_TIME_CONSTANT = 999.0	//INCREASING THIS VALUE WILL CAUSE A MORE INSTANTANEOUS REACTION IN THE VSI

[WEIGHT_AND_BALANCE]

// Passenger/Cargo Load Data
// Created by the RFP Aircraft Loader by Dave March
// Created for the 747-200 Classic (Ready for Pushback)

// Warning: Use with other aircraft may cause unpredictable results!

empty_weight = 361000

max_number_of_stations = 62

station_load.0 =   660.00,  102.00, 0.00, 0.00 // Flightdeck Crew
station_load.1 =  3080.00,   75.00, 0.00, 0.00 // Cabin Crew
station_load.2 =    70.00,  107.00, 0.00, 0.00 // Personal Gear
station_load.3 =   300.00,  -80.00, 0.00, 0.00 // Food
station_load.4 =  1510.00,   12.00, 0.00, 0.00 // Forward Holds
station_load.5 =  4616.00,   65.00, 0.00, 0.00 // Bulk Hold
station_load.6 =  1345.00,  100.00, 0.00, 0.00 // Aft Hold
station_load.7 =   880.00,   80.00, 0.00, 0.00 // First Class
station_load.8 =   880.00,   76.00, 0.00, 0.00 // First Class
station_load.9 =   880.00,   72.00, 0.00, 0.00 // First Class
station_load.10 =   880.00,   68.00, 0.00, 0.00 // First Class
station_load.11 =   880.00,   64.00, 0.00, 0.00 // First Class
station_load.12 =   660.00,   60.00, 0.00, 0.00 // First Class
station_load.13 =   660.00,   56.00, 0.00, 0.00 // First Class
station_load.14 =   660.00,   52.00, 0.00, 0.00 // First Class
station_load.15 =   660.00,   48.00, 0.00, 0.00 // First Class
station_load.16 =   440.00,   44.00, 0.00, 0.00 // First Class
station_load.17 =  1980.00,   40.00, 0.00, 0.00 // Economy Class
station_load.18 =  1980.00,   36.00, 0.00, 0.00 // Economy Class
station_load.19 =  2200.00,   32.00, 0.00, 0.00 // Economy Class
station_load.20 =  2200.00,   28.00, 0.00, 0.00 // Economy Class
station_load.21 =  1320.00,   24.00, 0.00, 0.00 // Economy Class
station_load.22 =  2200.00,   20.00, 0.00, 0.00 // Economy Class
station_load.23 =  2200.00,   16.00, 0.00, 0.00 // Economy Class
station_load.24 =  1980.00,   12.00, 0.00, 0.00 // Economy Class
station_load.25 =  1320.00,    8.00, 0.00, 0.00 // Economy Class
station_load.26 =  1980.00,    4.00, 0.00, 0.00 // Economy Class
station_load.27 =  1980.00,    0.00, 0.00, 0.00 // Economy Class
station_load.28 =  1980.00,   -4.00, 0.00, 0.00 // Economy Class
station_load.29 =  1980.00,   -8.00, 0.00, 0.00 // Economy Class
station_load.30 =  1980.00,  -12.00, 0.00, 0.00 // Economy Class
station_load.31 =  1980.00,  -16.00, 0.00, 0.00 // Economy Class
station_load.32 =  1980.00,  -20.00, 0.00, 0.00 // Economy Class
station_load.33 =  1980.00,  -24.00, 0.00, 0.00 // Economy Class
station_load.34 =  1980.00,  -28.00, 0.00, 0.00 // Economy Class
station_load.35 =  1980.00,  -32.00, 0.00, 0.00 // Economy Class
station_load.36 =  1980.00,  -36.00, 0.00, 0.00 // Economy Class
station_load.37 =  1980.00,  -40.00, 0.00, 0.00 // Economy Class
station_load.38 =  1980.00,  -44.00, 0.00, 0.00 // Economy Class
station_load.39 =  1980.00,  -48.00, 0.00, 0.00 // Economy Class
station_load.40 =  1980.00,  -52.00, 0.00, 0.00 // Economy Class
station_load.41 =  1320.00,  -56.00, 0.00, 0.00 // Economy Class
station_load.42 =  1320.00,  -60.00, 0.00, 0.00 // Economy Class
station_load.43 =  1320.00,  -64.00, 0.00, 0.00 // Economy Class
station_load.44 =  1320.00,  -68.00, 0.00, 0.00 // Economy Class
station_load.45 =  1980.00,  -72.00, 0.00, 0.00 // Economy Class
station_load.46 =  1320.00,  -76.00, 0.00, 0.00 // Economy Class
station_load.47 =  1320.00,  -80.00, 0.00, 0.00 // Economy Class
station_load.48 =  1980.00,  -84.00, 0.00, 0.00 // Economy Class
station_load.49 =  1980.00,  -88.00, 0.00, 0.00 // Economy Class
station_load.50 =  1980.00,  -92.00, 0.00, 0.00 // Economy Class
station_load.51 =  1980.00,  -96.00, 0.00, 0.00 // Economy Class
station_load.52 =  1980.00, -100.00, 0.00, 0.00 // Economy Class
station_load.53 =  1760.00, -104.00, 0.00, 0.00 // Economy Class
station_load.54 =  1760.00, -108.00, 0.00, 0.00 // Economy Class
station_load.55 =  1760.00, -112.00, 0.00, 0.00 // Economy Class
station_load.56 =  1760.00, -116.00, 0.00, 0.00 // Economy Class
station_load.57 =  1320.00,   68.00, 0.00, 0.00 // Upper Deck
station_load.58 =  1320.00,   64.00, 0.00, 0.00 // Upper Deck
station_load.59 =  1100.00,   60.00, 0.00, 0.00 // Upper Deck
station_load.60 =  1100.00,   56.00, 0.00, 0.00 // Upper Deck
station_load.61 =  1100.00,   52.00, 0.00, 0.00 // Upper Deck
station_load.62 =  1100.00,   48.00, 0.00, 0.00 // Upper Deck

// Total Weight (Pax + Cargo) = 95911 lbs

// END of Passenger/Cargo Load Data



empty_weight = 361000





reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=-5.000000,0.000000,0.000000
max_gross_weight=790180.000000


empty_weight_roll_MOI=19618435.000000
empty_weight_pitch_MOI=40143699.000000
empty_weight_yaw_MOI=36447449.000000
empty_weight_coupled_MOI=0.000000


[General]
performance=Length: 225'-2"'\nWingspan: 195'-8"\nMTOW: 775,000 LBS\nMLW: 564,000 LBS\nCruise: Max 523knts\/Economical 470knts\nAccomodation: 385 (Basic)\nRange: 5150 NM\n\n\n
atc_type=Boeing
atc_model=B742

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) 
[fuel]
Center1=   0.000000, 0.000000,-6.000000,16689.000000,  3.000000  //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) 
Center2=   0.0,0.0, -6.0,50.0, 3.0
LeftMain= -7.000000,-25.000000,0.000000,4421.000000, 3.000000
LeftAux=  -7.000000,-35.000000,0.000000,12240.000000,3.000000
RightMain=-7.000000, 25.000000,0.000000,4421.000000, 3.000000
RightAux= -7.000000, 35.000000,0.000000,12240.000000,3.000000
LeftTip=  -7.000000,-35.000000,0.000000,440.000000,  3.000000
RightTip= -7.000000, 35.000000,0.000000,440.000000,  3.000000

fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=1

[airplane_geometry]
wing_area=5503.000000
wing_span=195.666667
wing_root_chord=28.166667
wing_dihedral=6.998291
wing_incidence=1.320      
wing_twist=-0.999756
oswald_efficiency_factor=1.100000
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=1470.000000
htail_span=73.166667
htail_pos_lon=-180.000000
htail_pos_vert=0.000000
htail_incidence=3.000000
htail_sweep=0.000000
vtail_area=1290.000000
vtail_span=40.951190
vtail_sweep=0.000000
vtail_pos_lon=-116.000000
vtail_pos_vert=5.833333
elevator_area=352.000000
aileron_area=220.120000
rudder_area=219.300000
elevator_up_limit=27.501974
elevator_down_limit=20.626481
aileron_up_limit=19.480565
aileron_down_limit=14.896903
rudder_limit=23.491270
elevator_trim_limit=19.480565
spoiler_limit=59.988681
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

[contact_points]
point.0=1,  66.8,    0.0, -17.4, 1574.8, 0.000000, 5.826899, 70.0     ,0.800000, 2.500000, 0.900000, 14.000000, 14.000000, 0.000000, 0.000000, 0.000000
point.1=1, -20.5,  -17.3, -18.2, 1574.8, 1.000000, 5.826899, 23.0     ,1.000000, 2.500000, 0.900000, 18.000000, 18.000000, 2.000000, 0.000000, 0.000000
point.2=1, -20.5,   17.3, -18.2, 1574.8, 2.000000, 5.826899, 23.0     ,1.000000, 2.500000, 0.900000, 18.000000, 18.000000, 3.000000, 0.000000, 0.000000
point.3=2, -70.7, -102.0,   6.0, 1574.8, 0.000000, 0.000000, 0.000000 ,0.000000, 0.000000, 0.000000,  0.000000,  0.000000, 5.000000, 0.000000, 0.000000
point.4=2, -70.7,  102.0,   6.0, 1574.8, 0.000000, 0.000000, 0.000000 ,0.000000, 0.000000, 0.000000,  0.000000,  0.000000, 6.000000, 0.000000, 0.000000
point.5=2,-126.6,    0.0,   5.8, 1574.8, 0.000000, 0.000000, 0.000000 ,0.000000, 0.000000, 0.000000,  0.000000,  0.000000, 9.000000, 0.000000, 0.000000
point.6=2,  66.8,    0.0,   5.8, 1574.8, 0.000000, 0.000000, 0.000000 ,0.000000, 0.000000, 0.000000,  0.000000,  0.000000, 4.000000, 0.000000, 0.000000

static_pitch=0.00
static_cg_height=16.50000
gear_system_type=0

[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 49 // 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 = 200 // KIAS
blowout-speed = 250 // KIAS
lift_scalar = 0.23   
drag_scalar = 1.00   
pitch_scalar= 1.00
system_type = 1 //Hydraulic

[Flaps.1]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.2
extending-time = 49 // 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 = 200 // KIAS
blowout-speed = 250 // KIAS
lift_scalar = 0.23   
drag_scalar = 1.000
pitch_scalar=-15.00
system_type = 1 //Hydraulic

[Flaps.2]
type= 2
span-outboard= 0.800     
extending-time= 3.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar=-1.00    
drag_scalar= 0.000
pitch_scalar=-15.25
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 1.000, 0.000

[Flaps.3]
type= 2
span-outboard= 0.800      
extending-time= 3.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar=-1.00     
drag_scalar= 0.000
pitch_scalar=0.00
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.000, 0.000
flaps-position.2= 1.000, 0.000

[GeneralEngineData]
engine_type=1
Engine.0=  5.333333,-70.083333,-7.233333
Engine.1= 25.833333,-40.916667,-7.000000
Engine.2= 25.833333, 40.916667,-7.000000
Engine.3= -5.333333, 70.083333,-7.233333
fuel_flow_scalar=0.988000                
min_throttle_limit=-0.349915

[TurbineEngineData]
fuel_flow_gain=0.002170
inlet_area=54.843840        
rated_N2_rpm=29920.000000
static_thrust=44703.200000 
afterburner_available=0
reverser_available=1

[Reference Speeds]
flaps_up_stall_speed=173.000000
full_flaps_stall_speed=138.400000
cruise_speed=527.744626
max_indicated_speed=385.734375
max_mach=0.860010

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
eyepoint=95.678662,-1.499446,12.816150


[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=00.10000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=1
autothrottle_max_rpm=94.000000
pitch_takeoff_ga=13.000000       
autoland_available=0
use_no_default_bank=1
use_no_default_pitch=1
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=16.00
nav_integrator_control=0.17
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control  = 18.0
gs_integrator_control    = 0.33
gs_derivative_control    = 0.00
gs_integrator_boundary   = 0.70
gs_derivative_boundary   = 0.00
yaw_damper_gain = 1.0
default_pitch_mode=0
default_bank_mode=0

[flight_tuning]
cruise_lift_scalar     = 1.0
parasite_drag_scalar   = 1.2        
induced_drag_scalar    = 1.2        
elevator_effectiveness = 0.85
aileron_effectiveness  = 1.0
rudder_effectiveness   = 1.0
pitch_stability        = 1.27
roll_stability         = 1.0
yaw_stability          = 1.2
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0

[direction_indicators]
direction_indicator.0=3,0

[turn_indicators]
turn_indicator.0=1,0

[airspeed_indicators]
airspeed_indicator.0=0.9827, -3.0

[attitude_indicators]
attitude_indicator.0=1

[Radios]
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]
light.0 = 1, 78.50, 0.00, 16.25, VM742_beacon ,
light.1 = 1, 35.00, 0.00, -11.30, VM742_beacon ,
light.2 = 2, -111.00, 0.00, 7.25, VM742_strobes ,
light.3 = 8, -10.00, -50.827, 10.90, VM742_wing_l,
light.4 = 8, -10.00, 50.827, 10.90, VM742_wing_r,
light.5 = 4,  93.55,  0.00,  10.00, VM742_vclight_1,


[SMOKESYSTEM]
smoke.0=0.00, 0.00,-96.50, fx_contrail_l.fx
smoke.1=0.00, 0.00, 96.50, fx_contrail_l.fx

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[exits]
number_of_exits = 2
exit_rate.0 = 0.2                               ;Percent per second
exit_rate.1 = 0.2

[folding_wings]
wing_fold_system_type = 4                       ;0=None
fold_rates = 0.12,0.11                          ;Percent per second

[TailHook]
tailhook_length=4                               ;(feet)
tailhook_position = -15.0, 0.0, -1.0            ;(feet) longitudinal,
lateral, vertical positions from datum
cable_force_adjust = 0.0

[brakes]
toe_brakes_scale=0.694815
parking_brake=1

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=1145.915590
flap_limit_idle=572.957795

[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,1
normal_pressure=3000.000000

[stall_warning]
type=1