[fltsim.0]
title=bonhomme richard // PLEASE EDIT
sim=air // PLEASE EDIT
model=
panel=
sound=
texture=
kb_checklists=Cessna208B_Check
kb_reference=Cessna208B_ref
atc_id_color=0xff000000
atc_id=N200
atc_airline=
atc_flight_number=1123
atc_parking_types=DOCK
ui_manufacturer=Ship
ui_type=Sh_Zweidecker 2.Rang // PLEASE EDIT
ui_variation=YOUR Ship // PLEASE EDIT
atc_parking_codes=
description= Open gun scuttles and hoist flag: Shift+E - Fire the guns : I key -lift anchor and dinghy & rotate winch: G key
[General]
atc_type=Cessna
atc_model=C208
editable=0
performance=Length 43m/142ft\nCruise speed 20.0Knots\n[Shift+E] Cargo Door \n \n \n \n \n
[WEIGHT_AND_BALANCE]
max_gross_weight=3000 // (pounds)
empty_weight=3000 // (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_pitch_MOI=27241.36
empty_weight_roll_MOI=56108.57
empty_weight_yaw_MOI=10431.43
empty_weight_coupled_MOI=0.0
[Flaps.0]
type=1
span-outboard=0.5 // Percent span for flap position
extending-time=5.7 // Seconds, time to fully extend
system_type=0 // 0 = electrical
damaging-speed=175 // KIAS
blowout-speed=175 // KIAS
flaps-position.0=0 // degrees
flaps-position.1=10,175 // degrees
flaps-position.2=20,150 // degrees
flaps-position.3=30,125 // degrees
[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=5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=0.0, 0.0, 0.5 //(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
[propeller]
thrust_scalar=1.0 //Propeller thrust scalar
propeller_type=0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=8.8 //Propeller Diameter, (feet)
propeller_blades=3 //Number of propeller blades
propeller_moi=19 //Propeller moment of inertia
beta_max=45 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=15.6 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=25520 //Miminum governed RPM
prop_tc=0.004 //Prop time-constant
gear_reduction_ratio=17.4 //Propeller gear reduction ratio
fixed_pitch_beta=0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=0 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=1 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available=1 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather=700 //Minimum RPM for prop feathering
beta_feather=88.0 //Feathering pitch angle (degrees)
power_absorbed_cf=0.9 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available=1 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta=1.0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=-14.0 //Minimum pitch angle in reverse, (degrees)
[TurbineEngineData]
fuel_flow_gain=1.0 //Gain on fuel flow
inlet_area=1.0 //Square Feet, engine nacelle inlet area
rated_N2_rpm=18000 //RPM, second stage compressor rated value
static_thrust=158 //Lbs, max rated static thrust at Sea Level
[turboprop_engine]
power_scalar=1.0 //Scalar on Turboprop power
maximum_torque=1900 //Maximum torque available (ft-lbs)
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 5 , 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 2 , 17.0
marker_beacon=1, 2 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
starter1=0, 20, 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
[contact_points]
;/0 Class
;/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 / Water Rudder Effectiveness (0=Undamped, 1=Critically Damped) / 1.0 = normal
;/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, 4.00, 0.0, -3.00, 9600, 0, 0.00, 0.0, 0.85, 2.5, 0.65, 0.1, 0.1, 0, 0.0, 0.0
point.1=4, 5.00, 0.0, -3.0, 9600, 0, 0.00, 0.0, 0.85, 2.5, 0.65, 0.0, 0.0, 1, 0.0, 0.0
point.2=4, -21.35, -8.0, -3, 9600, 0, 0.00, 5.0, 0.95, 2.5, 0.65, 0.0, 0.0, 2, 0.0, 0.0
point.3=4, -21.35, 8.0, -3, 9600, 0, 0.00, 5.0, 0.95, 2.5, 0.65, 0.0, 0.0, 3, 0.0, 0.0
point.4=1, -21.35, -8.0, -3.0, 9600, 0, 0.00, 5.0, 0.95, 2.5, 0.65, 5.0, 5.0, 2, 0.0, 0.0
point.5=1, -21.35, 8.0, -3.0, 9600, 0, 0.00, 5.0, 0.95, 2.5, 0.65, 5.0, 5.0, 3, 0.0, 0.0
static_pitch=0.000000
static_cg_height=0.000000
gear_system_type=1
[Views]
//eyepoint=7.20, 0.0, 54.0
eyepoint=-59.0, 0.0, 19.0 //(feet) longitudinal, lateral, vertical distance from reference datum
max_number_of_points=21
static_pitch=0.000 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=2.8 //feet, altitude of CG when at rest on the ground
gear_system_type=1 //Hydraulic
[gear_warning_system]
gear_warning_available=2 //Amphib
pct_throttle_limit=0.1 //Percent throttle that activates warning
flap_limit_idle=20.1 //Flap angle that activates warning at idle
flap_limit_power=13.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake=1
toe_brakes_scale=0.061037
[hydraulic_system]
normal_pressure=3000.0 //PSI
electric_pumps=0 //no electric pumps
engine_map=1,0,0,0 //pump on Eng1
[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
Adf.2=1
Transponder.1=1
Marker.1=1
[LIGHTS]
;/Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
;/ First figure : 1 means "activated"
;/ 4 means activated when pressing "L" key
;/ second figure : Positive (+)=more in front * Negative (-)=more aft
;/ third figure : Positive (+)=more at right * negative (-)=more at left
;/ forth figure : positive (+)=up * negative (-)=down
light.1=4, -66.2, -7.1, 18.3, fx_navredh ,
light.2=4, -66.2, 7.6, 18.1, fx_navgre ,
light.3=4, -66.2, 0.60, 20.8, fx_navwhi ,
light.4=1, 72.00, 0.00, 0.00, fx_AI_ship_trail-of-spray
light.5=1, 72.00, 0.00, 0.00, fx_AI_ship_wake_s
light.6=4, -50.5, 0.50, 15.9, fx_navwhi ,
light.7=1, 15.5, -30.3, 8.0, fx_engsmoke_delayed 240s
light.8=1, 10 ,-300 , 0 ,fx_wtrspray_l_delayed_243s
light.9=1, 0 ,-350 , 0 ,fx_wtrspray_l_delayed_243s
light.10=1,-15,-390 , 0 ,fx_wtrspray_l_delayed_243s
[EFFECTS]
wake = fx_wake_ijt1
water =ian
wake=fx_wake_s
[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=100, 180
aileron=200, 1000
rudder=200, 1000
[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=1
[turn_indicators]
;/Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=1,0
//[airspeed_indicators]
airspeed_indicator.0=1.16, -22.0
[fuel]
LeftMain=-0.3, -1.1, 2.5, 166.0, 3.6 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-0.3, 1.1, 2.5, 166.0, 3.6 //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=1
[airplane_geometry]
wing_area=279.0 //Square feet
wing_span=52.1 //Feet
wing_root_chord=6.4 //Feet
wing_dihedral=3.9 //Degrees
wing_incidence=2.5 //Degrees
wing_twist=-1.7 //Degrees
oswald_efficiency_factor=0.7 //Measure of lift effeciency of wing
wing_winglets_flag=0 //Are winglets available?
wing_sweep=2.96 //Degrees, wing leading edge
wing_pos_apex_lon=-12.3 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=0.0 //Feet, vertical distance from reference point, positive going up
htail_area=39.0 //Square feet
htail_span=11.7 //Feet
htail_pos_lon=-27.8 //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=2.0 //Degrees
htail_sweep=5.0 //Degrees, horizontal tail leading edge
vtail_area=18.0 //Square feet
vtail_span=4.8 //Feet, tip to body
vtail_sweep=45.0 //Degrees, vertical tail leading edge
vtail_pos_lon=-25.7 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=1.5 //Feet, vertical distance from reference point, positive going up
elevator_area=16.6 //Square feet
aileron_area=18.3 //Square feet
rudder_area=50.0 //Square feet
elevator_up_limit=28.0 //Degrees
elevator_down_limit=21.0 //Degrees
aileron_up_limit=30.0 //Degrees
aileron_down_limit=25.0 //Degrees
rudder_limit=20.0 //Degrees
elevator_trim_limit=19.5 //Degrees
spoiler_limit=20.0 //Degrees
spoilerons_available=1 //Spoilerons Available?
aileron_to_spoileron_gain=1 //Aileron to spoileron gain
min_ailerons_for_spoilerons=0 //Degrees
min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate
spoiler_handle_available=0 //Defaults to True if spoiler limit > 0, else False. Should be False for spoilerons only
[Reference Speeds]
flaps_up_stall_speed=72.0 //Knots True (KCAS)
full_flaps_stall_speed=58.0 //Knots True (KCAS)
cruise_speed=140.0 //Knots True (KTAS)
max_mach=0.60
max_indicated_speed=175 //Red line (KIAS)
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000.0
autothrottle_available=1
pitch_takeoff_ga=8.0
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=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain=0.0
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
[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
[SMOKESYSTEM]
smoke.0=0, -70, 0.0, fx_smoke_ship,
;Press "I" to activate Y-not work, Z, X
//1°chiffre = Altitude (non fonctionnel?)
//2° chiffre = positif : vers l'avant:front , négatif : Vers l'arrière/back
// 3° chiffre = A droite/right(+) ou à gauche/left (-) de la ligne médiane
smoke.1= 10.00,-0.00,-20.00, fx_AI_Smokeyfire_240s
smoke.2= -0.00,-00.00,-200.00, fx_wtrspray_l.fx,fx_AI_gun_water_1s
smoke.3= 85.00,-10.00,-250.00, fx_wtrspray_l.fx,fx_AI_gun_water_3s
smoke.4= 85.00,20.00,-300.00, fx_wtrspray_l.fx,fx_AI_gun_water_3s
smoke.5= 0, 56., 12.3, fx_spray_ss.fx,
smoke.6= 0, 56., -12.8, fx_spray_ss.fx,
smoke.7= 0, -67, 0.0, fx_spray_ss.fx,
smoke.8= 0, 68, 3.0, fx_spray_ss.fx,
smoke.9= 0, 68, -3.0, fx_spray_ss.fx,
smoke.10= 1, 71.00, 0.00, -2.00, fx_AI_ship_wake_s
smoke.11=15.5, 10.3, -30.0, fx_engsmoke_10s
smoke.12=0, 132.0, 0.400, fx_ConstEXTRAeffects.fx,
smoke.13=0, 40.0, -10.400, cannonfire.fx
smoke.14=0.00,0.0, 999.00, fx_ShellHit
smoke.15=0.00,0.0,-999.00, fx_ShellHit
smoke.16=0.00,0.0, 1150.00, fx_ShellHit
smoke.17=0.00,0.0,-1150.00, fx_ShellHit
smoke.18=0.00,20.0,20.00, fx_16inch
smoke.19=0.00, 132.0,-5.00, fx_spray1.fx ;bow
smoke.20=0.00, 132.0, 5.00, fx_spray1.fx ;bow
smoke.21=0.00, 132.0, 0.00, fx_spray1.fx ;bow
