[fltsim.0]
title=RMS TITANIC
sim=hama_titanic
model=
panel=
sound=
texture=
kb_checklists=Cessna208B_Check
kb_reference=Cessna208B_ref
atc_id_color=0xff000000
atc_id=N208EH
atc_airline=TITANIC
atc_flight_number=1123
atc_parking_types=DOCK
ui_manufacturer=hama
ui_type=ship
ui_variation=TITANIC
description=[G]key Horn(VC)
atc_parking_codes=
[pitot_static]
vertical_speed_time_constant=1                //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000



[WEIGHT_AND_BALANCE]
max_gross_weight=125000                       // (pounds)
empty_weight=96000                           // (pounds)

reference_datum_position=0, 0, 0      // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-0, 0, 0     // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50


;Moments of Inertia
empty_weight_roll_MOI=552310
empty_weight_pitch_MOI=1923159
empty_weight_yaw_MOI=731785
empty_weight_coupled_MOI=0

[fuel]
Center1=0.0,0.0, 0.0, 950.0, 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)
                                     //Hydraulic

[flight_tuning]
cruise_lift_scalar=0.0
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, -0.0,  -0.9                 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=0.7                   //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, 10.1, 0.0, -3.0, 5000,0,1.40,10.0, 1.3, 2.5, 0.8, 1.0, 1.0, 0, 175.0, 175.0
point.1=1,-26.4,-6.2, -3.0, 5000,1,1.50, 0.0, 1.4, 2.5, 0.8, 0.0, 0.0, 1, 175.0, 175.0
point.2=1,-26.4, 6.2, -3.0, 5600,2,1.50, 0.0, 1.4, 2.5, 0.8, 0.0, 0.0, 2, 175.0, 175.0
point.3=4, 30.0,-2.0, -3.0, 9000,0, 0.0, 0.0, 1.0, 12.5, 0.8,  0.0,  0.0, 0, 220, 250
point.4=4, 30.0, 2.0, -3.0, 9000,0, 0.0, 0.0, 1.0, 12.5, 0.8,  0.0,  0.0, 0, 220, 250
point.5=4,-40.0,-15.0,-3.0, 9000,1, 0.0, 8.0, 1.0, 12.0, 0.8, 0.0,  0.0, 2, 220, 250
point.6=4,-40.0, 15.0,-3.0, 9000,2, 0.0, 8.0, 1.0, 12.0, 0.8, 0.0,  0.0, 3, 220, 250

static_pitch=-0.0
static_cg_height=2.8
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, 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


[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, -435.00,   0.00, 56.00, fx_navwhih ,
light.1=3, 247.00, -47.70, 60.00,  fx_navred ,
light.2=3, 247.00,  47.70, 60.00,  fx_navgrem ,
light.3=3, 446.00,   0.00, 55.00, fx_navwhih ,
light.4=3, 306.00,   0.00, 200.00, fx_navwhih ,
light.5=3, -276.00,   0.00, 140.00, fx_navwhih ,

[SMOKESYSTEM]
smoke.0=0, -370.0, 10.0, fx_sprayll.fx,
smoke.1=0, -370.0, -10.0, fx_sprayll.fx,
smoke.2=0, -380.0, 0.0, fx_sprayll.fx,
smoke.3=0, 3.50, 47.0, fx_Drainage.fx,
smoke.4=0, 3.50,-47.0, fx_Drainage.fx,
smoke.5=0,350.0, 28.0, fx_Drainage.fx,
smoke.6=0,350.0,-28.0, fx_Drainage.fx,
smoke.7=0, 0.0, 47.0, fx_Drainage.fx,
smoke.8=0, 0.0,-47.0, fx_Drainage.fx,
smoke.9=0,-280.0, 39.0, fx_Drainage.fx,
smoke.10=0,-280.0,-39.0, fx_Drainage.fx,


[EFFECTS]
wake=fx_wake_ll
water=fx_spray_t
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[Views]
//eyepoint=251.00, -0.0,65.0              //Bridge
eyepoint=246.00, 37.0,65.0          // right wing 
//eyepoint=231.00, -18.2,73.0            //Upper Deck
//eyepoint=-225.00, -38.0,62.0          // deck     ; Longitude, Latitude and Vertical position from Reference Point, (FEET)


[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

[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 \n \n \n \n
Category=airplane
[Flaps.0]
type=1
span-outboard=0.500000
extending-time=7.000000
system_type=0
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
[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
