[fltsim.0]
title=VARIG B747-306M KLM
sim=POSKY-Boeing 747-306M.air
model=
panel=
sound=
texture=
checklists=
atc_airline=KLM
atc_flight_number=160
ui_manufacturer=Boeing
ui_type=747-306M
ui_variation=KLM
visual_damage=1
atc_heavy=1
atc_id=1
description=

[General]
performance=Passengers\nFirst Class (P):  12 pax\nExec Class(C):  61 pax\nEcon Class(Y):188 pax \n\nCargo\nTotal lower hold volume:\n   5,497 ft3 (155.6 m3)\n    7 palletes at the Cabin no.5  \n\nCity Pairs:\nSAO-LAX-TYO\nSAO-NYC\nSAO-MIA\n\nEngines: GE CF6-80C2B1\nTO Thrust: 54,750 lb x 4\n\nMax Fuel Cap.: 57,065 US Gal.\nMaxTOW: 870,000 lbs\nMLW: 630,000 lbs\nZFW: 545,965 lbs\nOEW: 407,107 lbs\n\nMax Range: 7220 nm  \nTypical Cruise Speed \n   @ FL350: M.86

atc_type=BOEING
atc_model=B743
editable=1

[flight_tuning]
cruise_lift_scalar     = 1.0
parasite_drag_scalar   = 1.0
induced_drag_scalar    = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness  = 1.0
rudder_effectiveness   = 1.0
pitch_stability        = 1.0
roll_stability         = 1.0
yaw_stability          = 1.0
elevator_trim_effectiveness = 1.4
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0

[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

[pitot_static]
vertical_speed_time_constant=999                

[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000
max_number_of_stations=50
empty_weight=446847     
empty_weight_roll_MOI= 13155743.000
empty_weight_pitch_MOI= 22600873.000
empty_weight_yaw_MOI= 25151035.000
empty_weight_coupled_MOI= 1000.000
max_gross_weight=833000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
station_load.0=0.000000,0.000000,0.000000,0.000000

[fuel]
Center1   =0.000,   0.0, -4.0, 19431.0, 3.0
LeftMain  =-5.0, -35.0, -4.0, 16660.0, 3.0     
LeftAux   =-11.5, -52.0, -3.0, 500.0, 3.0     
RightMain =-5.0,  35.0, -4.0, 16660.0, 3.0     
RightAux  =-11.5,  52.0, -3.0, 500.0, 3.0     
fuel_type = 2                                     
number_of_tank_selectors = 1 
electric_pump=1

[airplane_geometry]
wing_area= 5500.000
wing_span= 196.000
wing_root_chord= 23.000
wing_dihedral= 6.998
wing_incidence= 2.000
wing_twist= -0.994
oswald_efficiency_factor= 0.830
wing_winglets_flag= 0
wing_sweep= 37.500
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 0.000
htail_area= 1470.000
htail_span= 72.750
htail_pos_lon= -17.167
htail_pos_vert= 0.000
htail_incidence= -4.000
htail_sweep= 37.500
vtail_area= 1060.000
vtail_span= 37.121
vtail_sweep= 45.000
vtail_pos_lon= -16.500
vtail_pos_vert= 6.083
elevator_area= 326.800
aileron_area= 225.200
rudder_area= 229.900
elevator_up_limit= 20.751
elevator_down_limit= 15.313
aileron_up_limit= 31.513
aileron_down_limit= 31.513
rudder_limit= 17.189
elevator_trim_limit= 19.167
spoiler_limit= 25.783
spoilerons_available= 0
aileron_to_spoileron_gain= 3.000
min_ailerons_for_spoilerons= 11.459
min_flaps_for_spoilerons= 0.000

[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 = 1.000,  67.333,   0.000, -13.850, 2181.102, 0.000, 5.812, 78.480, 0.859, 0.500, 0.518, 9.000, 8.000, 0.000, 0.000, 0.000
point.1 = 1.000, -12.583, -18.000, -13.833, 2574.803, 1.000, 5.812,  0.000, 0.602, 0.500, 0.551, 9.500, 8.000, 2.000, 0.000, 0.000
point.2 = 1.000, -12.583,  18.000, -13.833, 2574.803, 2.000, 5.812,  0.000, 0.602, 0.500, 0.551, 9.500, 8.000, 3.000, 0.000, 0.000
point.3 = 2.000, -49.000, -102.900,  7.000,  787.402, 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, -49.000,  102.900,  7.000,  787.402, 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, -92.667,   0.000,  -2.000,  787.402, 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,  88.167,   0.000,  -5.750,  787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 4.000, 0.000, 0.000
point.7 = 2.000,-132.667,   0.000,  55.500,  787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 8.000, 0.000, 0.000
point.8 = 2.000, -14.917, -69.500,  -7.000,  787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 9.000, 0.000, 0.000
point.9 = 2.000,  14.917, -39.167, -11.000,  787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 9.000, 0.000, 0.000
point.10= 2.000,  14.917,  39.167, -11.000,  787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 9.000, 0.000, 0.000
point.11= 2.000, -14.917,  69.500,  -7.000,  787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 9.000, 0.000, 0.000
static_pitch= -1.000
static_cg_height= 13.125
gear_system_type=0


[SMOKESYSTEM]
smoke.0=7, -44.967, -69.467, fx_posky743_vortex.fx
smoke.1=7, -44.967,  69.467, fx_posky743_vortex.fx

[GeneralEngineData]
engine_type=1
Engine.0=-14.916667,-69.500000,0.000000
Engine.1=14.916667,-39.166667,-7.000000
Engine.2=14.916667,39.166667,-7.000000
Engine.3=-14.916667,69.500000,0.000000
fuel_flow_scalar=1.15
min_throttle_limit=-0.379944

[TurbineEngineData]
bypass_ratio=4.970000
fuel_flow_gain=0.002000
inlet_area=37.558941
rated_N2_rpm=26928.000000
static_thrust=52500.000000
afterburner_available=0
reverser_available=1

[Reference Speeds]
flaps_up_stall_speed= 150.000
full_flaps_stall_speed= 126.000
cruise_speed= 524.337
max_indicated_speed=350.000000
max_mach=0.900000

[keyboard_response]
elevator= 100.000, 200.000
aileron= 100.000, 200.000
rudder= 150.000, 250.000



[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.000
autothrottle_available= 1
autothrottle_arming_required= 1
autothrottle_takeoff_ga= 1
autothrottle_max_rpm= 105.000
pitch_takeoff_ga= 14.000
use_no_default_pitch = 1 
use_no_default_bank = 1 
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000


[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 = 1                                    // degrees
flaps-position.2 = 5                                    // degrees
flaps-position.3 = 10                                   // degrees
flaps-position.4 = 20                                   // degrees
flaps-position.5 = 25                                   // degrees
flaps-position.6 = 30                                   // degrees
damaging-speed   = 200                                  // KIAS
blowout-speed    = 250                                  // KIAS
lift_scalar = 0.28
drag_scalar = 0.40
pitch_scalar= 0.40
system_type = 1                                         //Hydraulic

[flaps.1]
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.2                                  // 0.0 .. 1.0
extending-time   = 25                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 1                                    // degrees
flaps-position.2 = 5                                    // degrees
flaps-position.3 = 10                                   // degrees
flaps-position.4 = 20                                   // degrees
flaps-position.5 = 25                                   // degrees
flaps-position.6 = 30                                   // degrees
damaging-speed   = 200                                  // KIAS
blowout-speed    = 250                                  // KIAS
lift_scalar = 0.28
drag_scalar = 0.40
pitch_scalar= 0.40
system_type = 1                                         //Hydraulic

[flaps.2]
type             = 2                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 12                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 5                                    // degrees
flaps-position.2 = 10                                   // degrees  
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 0.28
drag_scalar = 0.40
pitch_scalar= 0.40
system_type = 1                                       

[stored information]
cargo_config=auto
cargo_container_type=
cargo1=0
cargo2=0
cargo3=0
cargo4=0
cargo5=0
cargo6=0
cargo7=0
cargo8=0
cargo9=0
cargo10=0
cargo11=0
cargo12=0
cargo13=0
cargo14=0
cargo15=0
cargo16=0
cargo17=0
cargo18=0
cargo19=0
cargo20=0
cargo21=0
cargo22=0
cargo23=0
cargo24=0
cargo25=0
cargo26=0
cargo27=0
cargo28=0
cargo29=0
cargo30=0
cargo_bulk=0
main_deck_cargo=0
main_deck_cargo_type=
per_pax_weight=42
forward_cargo=0
aft_cargo=0
total_passengers=301
pax_config=simple
pax_upper=0
pax1=0
pax2=0
pax3=0
pax4=0
pax5=0
pax6=0
aircraft_type=747-200
seating_type=Basic Mixed-Class
[default information]
empty_weight=439520
max_gross_weight=820000
Center1=0.000,   0.0, -4.0, 17153.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain=-5.0, -35.0, -4.0, 12538.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux=-11.5, -52.0, -3.0, 5761.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-5.0,  35.0, -4.0, 12538.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux=-11.5,  52.0, -3.0, 5761.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
station_load.0=0.000000,0.000000,0.000000,0.000000

[exits]
number_of_exits = 2
exit_rate.0 = 0.15                               ;Percent per second
exit_rate.1 = 0.15                               ;Percent per second

[TailHook]    // shift+C For opening cargo door.
tailhook_length=4                               ;(feet)
tailhook_position = -15.0, 0.0, -1.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust = 1.0

[folding_wings] // CapsLock For opening main cabin cargo door
wing_fold_system_type = 4                       ;0=None
fold_rates = 0.12,0.11                          ;Percent per second

[Views]
eyepoint=83.000, -2.000, 14.800    // Longitude, Latitude and Vertical position from Reference Point, (FEET)


[electrical]
//                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor         = 1, 0 ,  1.0
gear_motor         = 0, 5 , 17.0
avionics_bus       = 0, 0 ,  1.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 0 ,  1.0
additional_system  = 0, 0 ,  1.0
marker_beacon      = 1, 2 , 17.0
gear_warning       = 7, 0 , 99.0
gear_motor         = 4, 0 ,  1.0
fuel_pump          = 0, 0 ,  1.0
fuel_transfer_pump = 0, 0 ,  1.0
starter1           = 0, 20, 17.0
starter2           = 0, 0 ,  1.0
light_nav          = 0, 0 ,  1.0
light_beacon       = 0, 0 ,  1.0
light_landing      = 0, 0 ,  1.0
light_taxi         = 0, 0 ,  1.0
light_strobe       = 0, 0 ,  1.0
light_panel        = 0, 7 , 99.0
light_recognition  = 0, 0 ,  1.0
light_wing         = 0, 0 ,  1.0
marker_beacon      = 0, 0 ,  1.0
standby_vacuum     = 0, 0 ,  1.0
auto_brakes        = 0, 0 ,  1.0
hydraulic_pump     = 0, 0 ,  1.0
propeller_device   = 0, 0 ,  1.0

[Radios]
// Radio Type = available, 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

[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

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

[SMOKESYSTEM]
//Aileron tip vortecies
smoke.0=0, -30.167, -86.167, Opensky_vortex
smoke.1=0, -30.167,  86.167, Opensky_vortex
//Wing condensation
smoke.2=0, -08.917, -39.167, Opensky_conden
smoke.3=0, -08.917,  39.167, Opensky_conden


[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing                   
light.0 = 1,   65.000,    0.600,  19.210,  Opensky_beacon ,
light.1 = 1,   13.600,    0.000,  -7.380,  Opensky_beacon ,
//light.2 = 2,  -49.000, -102.900,  13.150,  fx_strobeh ,
//light.3 = 2,  -49.000,  102.900,  13.150,  fx_strobeh ,
light.4 = 3, -122.300,   -0.250,   12.300, fx_navwhi ,
light.5 = 3, -122.300,    0.250,   12.300, fx_navwhi ,
light.6 = 2, -121.900,    0.000,   11.450, fx_strobeh ,
light.7 = 4,  85.330,     0.000,   19.005, Opensky_747_vclight ,
light.8 = 5, -117.500,   -3.500,   40.750, Opensky_logo_light ,
light.9 = 5, -117.500,    3.500,   40.750, Opensky_logo_light ,
light.10= 5,   18.700,  -29.200,   -2.000, Opensky_nacelle_refl ,
light.11= 5,   18.700,   29.200,   -2.000, Opensky_nacelle_refl ,
light.12= 5,   44.500,  -11.700,    0.000, Opensky_wing_light ,
light.13= 5,   44.500,   11.700,    0.000, Opensky_wing_light ,
light.14= 5,   57.500,  -13.700,    1.900, Opensky_wing_light ,
light.15= 5,   57.500,   13.700,    1.900, Opensky_wing_light ,
light.16= 5,   83.333,    0.000,   -2.000, Opensky_wing_light ,
[brakes]
toe_brakes_scale=0.756859
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,1
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0