[fltsim.0]
title=Seawise giant full
sim=Seawise giant full
model=
panel=
sound=
texture=
kb_checklists=
atc_id=16865
atc_airline=Seawise giant full
atc_flight_number=7381155
ui_manufacturer=Sumitomo Heavy Industries, Japan
ui_type=ship
ui_variation=Seawise giant full
[fltsim.1]
title=jahre viking full
sim=Seawise giant full
model=
panel=
sound=
texture=jahre
kb_checklists=
atc_id=16865
atc_airline=Seawise giant full
atc_flight_number=7381155
ui_manufacturer=Sumitomo Heavy Industries, Japan
ui_type=ship
ui_variation=jahre viking full
[pitot_static]
vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000
[CameraDefinition.0]
Title = Bow
Guid = {69d5d7e1-b025-018a-0750-02286c0ee9d3}
Description = standing on the bow
Origin = Center
SnapPbhAdjust = swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = none
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.75
PitchPanRate = 60
HeadingPanRate = 60
ShowWeather = Yes
InitialXyz = 0.000000, 14.793587, 227.947438
InitialPbh = 0.000000, -0.000000, -0.000000
XyzAdjust = TRUE
ShowLensFlare = TRUE
Category = Aircraft
MomentumEffect = TRUE
ClipMode = Minimum
[CameraDefinition.1]
Title = Art deck
Guid = {00b2b00c-5397-0b3a-80a3-6a360671d610}
Description = aft deck near helo pad
Origin = Center
SnapPbhAdjust = swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = none
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.75
PitchPanRate = 60
HeadingPanRate = 60
ShowWeather = Yes
InitialXyz = 16.745052, 9.707459, -209.759975
InitialPbh = 0.000000, -0.000000, 180.000000
XyzAdjust = TRUE
ShowLensFlare = TRUE
Category = Aircraft
MomentumEffect = TRUE
ClipMode = Minimum
[CameraDefinition.2]
Title = Docking Bridge Port
Guid = {46008237-6633-a513-0d40-4b869d5226ab}
Description = standing on the portside docking bridge
Origin = Center
SnapPbhAdjust = swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = none
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.75
PitchPanRate = 60
HeadingPanRate = 60
ShowWeather = Yes
InitialXyz = -32.600000, 27.746413, -168.866393
InitialPbh = 0.000000, 0.000000, 0.000000
XyzAdjust = TRUE
ShowLensFlare = TRUE
Category = Aircraft
MomentumEffect = TRUE
ClipMode = Minimum
[CameraDefinition.3]
Title = Starboard Docking Bridge
Guid = {b507a7d7-5a62-5690-9890-ceaeaa093242}
Description = standing on the starbord docking bridge
Origin = Center
SnapPbhAdjust = swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = none
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.75
PitchPanRate = 60
HeadingPanRate = 60
ShowWeather = Yes
InitialXyz = 35.600000, 27.746413, -168.866393
InitialPbh = 0.000000, 0.000000, 0.000000
XyzAdjust = TRUE
ShowLensFlare = TRUE
Category = Aircraft
MomentumEffect = TRUE
ClipMode = Minimum
[CameraDefinition.4]
Title = Starboard Side Lifeboat
Guid = {846da194-b0ab-d649-a619-8a20960e8044}
Description = starboard side lifeboat deck
Origin = Center
SnapPbhAdjust = swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = none
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.75
PitchPanRate = 60
HeadingPanRate = 60
ShowWeather = Yes
InitialXyz = 23.830117, 15.979774, -185.029870
InitialPbh = 0.000000, -0.000000, -0.000000
XyzAdjust = TRUE
ShowLensFlare = TRUE
Category = Aircraft
MomentumEffect = TRUE
ClipMode = Minimum
[CameraDefinition.5]
Title = Main Deck
Guid = {2a3d29d7-3a08-0c07-d064-c86d07eb9929}
Description = a view if the main deck
Origin = Center
SnapPbhAdjust = swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = none
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.75
PitchPanRate = 60
HeadingPanRate = 60
ShowWeather = Yes
InitialXyz = 0.000000, 12.488485, 22.801783
InitialPbh = 0.000000, -0.000000, -0.000000
XyzAdjust = TRUE
ShowLensFlare = TRUE
Category = Aircraft
MomentumEffect = TRUE
ClipMode = Minimum
[WEIGHT_AND_BALANCE]
max_gross_weight=70000 // (pounds)
empty_weight=70000 // (pounds)
reference_datum_position=61.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-60.5, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50
;Moments of Inertia
empty_weight_roll_MOI=18002310
empty_weight_pitch_MOI=24223159
empty_weight_yaw_MOI=39531785
empty_weight_coupled_MOI=0
[fuel]
LeftMain=-85.0, -28.0, -4.0, 12546.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-85.0, 28.0, -4.0, 12546.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux=112.0, -36.5, -3.0, 4482.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux=112.0, 36.5, -3.0, 4482.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftTip=-130.0, -73.0, 0.0, 1322.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightTip=-130.0, 73.0, 0.0, 1322.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1=83.5, 0.0, -7.0, 17164.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center2=193.5, 0.0, 6.0, 3300.0, 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
electric_pump=0
[airplane_geometry]
wing_area=5825.0 //Square feet
wing_span=211.4 //Feet
wing_root_chord=48.8 //Feet
wing_dihedral=7.0 //Degrees
wing_incidence=2.0 //Degrees
wing_twist=-1.0 //Degrees
oswald_efficiency_factor=0.68 //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=-58.2 //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=1470 //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=1060 //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=327 //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=10 //Degrees
min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate
auto_spoiler_available=1
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000
[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)
max_mach=0.92
max_indicated_speed=365.0 //Red line (KIAS)
[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=0.7
drag_scalar=0.9
pitch_scalar=0.9
system_type=1 //Hydraulic
[flaps.1]
type=2 // 1 - tail, 2 - lead
span-outboard=0.8 // 0.0 .. 1.0
extending-time=2 // seconds
flaps-position.0=0 // degrees
flaps-position.1=1.0 // degrees
damaging-speed=250 // KIAS
blowout-speed=300 // KIAS
lift_scalar=0.3
drag_scalar=0.1
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=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=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[GeneralEngineData]
engine_type=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=-107.5, -69.5, -0.9 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=-107.5, 69.5, -0.9 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.0 //Scalar for fuel flow efficiency
min_throttle_limit=-0.25; //Minimum percent throttle. Generally negative for turbine reverser
[TurbineEngineData]
fuel_flow_gain=0.002 //Gain on fuel flow
inlet_area=60.0 //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920 //RPM, second stage compressor rated value
static_thrust=56750 //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
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;
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
[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, 10.15, 0.00, -3.600, 5000, 0, 1.40, 10.0, 0.3, 2.5, 0.3, 1.0, 1.0, 0, 175.0, 175.0
point.1=1, -86.40, -6.250, -3.600, 5000, 1, 1.50, 0.0, 0.4, 2.5, 0.3, 0.0, 0.0, 1, 175.0, 175.0
point.2=1, -86.40, 6.250, -3.600, 5600, 2, 1.50, 0.0, 0.4, 2.5, 0.3, 0.0, 0.0, 2, 175.0, 175.0
point.3=4, 552.0, -8.0, -3.4, 5000.0, 0, 2.0, 0.0, 0.5, 2.5, 0.3, 0.0, 0.0, 0, 220, 250
point.4=4, 552.0, 8.0, -3.4, 5000.0, 0, 2.0, 0.0, 0.5, 2.5, 0.3, 0.0, 0.0, 0, 220, 250
point.5=4, -552.0, -8.0, -3.2, 5000.0, 1, 2.0, 10.0, 1.0, 2.0, 0.3, 0.0, 0.0, 2, 220, 250
point.6=4, -552.0, 8.0, -3.2, 5000.0, 2, 2.0, 10.0, 1.0, 2.0, 0.3, 0.0, 0.0, 3, 220, 250
static_pitch=-0.0
static_cg_height=1.5
gear_system_type=1 //Hydraulic
[gear_warning_system]
gear_warning_available=1 //Normal
pct_throttle_limit=0.1 //Percent throttle that activates warning
flap_limit_idle=5.0 //Flap angle that activates warning at idle
flap_limit_power=25.5 //Flap angle that activates warning at above idle
[brakes]
parking_brake=1 //Parking brake available
toe_brakes_scale=1.24 //Brake scalar
auto_brakes=4
[hydraulic_system]
normal_pressure=3000.0 //PSI
electric_pumps=0 //no electric pumps
engine_map=1,1,1,1 //pumps on Eng1,2,3,4
[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, 5 , 17.0
avionics=1, 5 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
light_nav=0, 10 , 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
[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, 610.00, 0.00, 103.00, fx_decklight ,
light.1=3, -610.00, -116.00, 80.00, fx_navredm ,
light.2=3, -610.00, 116.00, 80.00, fx_navgre_3c ,
light.3=3, -619, 0.0, 152.0, fx_decklight,
light.4=3, -723.00, -34.60, 124.50, fx_navwhih ,
light.5=3, -723.00, 34.60, 124.50, fx_navwhih,
light.6=3, -770.0, 1.0, 45.0, fx_navblue ,
light.7=3, -770.0, -33.0, 45.0, fx_navblue,
light.8=3, -810.0, 1.0, 45.0, fx_navblue,
light.9=3, -810.0, -33.0, 45.0, fx_navblue ,
[SMOKESYSTEM]
smoke.0= 700, 0.0, 0.0, fx_wakeBow_xl.fx,
smoke.1= 500, 0.0, 0.0, fx_wakeBow_xl.fx,
smoke.2= 300, 0.0, 0.0, fx_wakeBow_xl.fx,
smoke.3= 100, 0.0, 0.0, fx_wakeBow_xl.fx,
smoke.4= -100, 0.0, 0.0, fx_wakeBow_xl.fx,
smoke.5= -300, 0.0, 0.0, fx_wakeBow_xl.fx,
smoke.6= -500, 0.0, 0.0, fx_wakeBow_xl.fx,
smoke.7= 600, 0.0, 0.0, fx_wakeBow_shiplength1.fx
smoke.8= 100, 0.0, 0.0, fx_wakeBow_shiplength1.fx
smoke.9= -718, 0.0, 60.0, fx_Ship_smokel.fx
smoke.10= -716, 0.0, 60.0, fx_Ship_smokel.fx
[Views]
eyepoint= -618.0, 0.00, 92.0 //bridge
[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
[attitude_indicators]
;/Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0=2
attitude_indicator.1=1
[turn_indicators]
;/Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[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
[EFFECTS]
wake=fx_wake_ll
wake=fx_wakeBow_xl
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[exits]
number_of_exits = 4
exit_rate.0 = 0.1
exit_rate.1 = 0.1
exit_rate.2 = 0.1
exit_rate.3 = 0.1
[folding_wings]
wing_fold_system_type=4 ;0=None
fold_rates=0.2,0.2 ;Percent per second
[TailHook]
tailhook_length=1 ;(feet)
[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
[stall_warning]
type=2
stick_shaker=1
[General]
performance= \n \n[G]Key horn (VC)\n \n \n \n
Category=airplane
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=1