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 עמוד ראשי -> פלייט סימולטור -> בעיה/בקשה|c172 ב-FSX

שליחת הודעה חדשה   תגובה להודעה
צפה בנושא הקודם :: צפה בנושא הבא  
מחבר הודעה
idonadel
טיסות סדירות



הצטרף בתאריך: Dec 31, 2007
הודעות: 246
מיקום: ראש העין

הודעהנשלח: 16:57 ,9 מרץ 2008, א'    כותרת הודעה: בעיה/בקשה|c172 ב-FSX תגובה עם ציטוט

שלום לכולם.
יש לי בעיה העם הססנה הדיפולטית של FSX(לא עובדת) עצוב .
מה שרציתי לבקש זה העם מישהו יכול לעלות לי את קובץ ה-aircraft.cfg של המטוס.(זה ממש יעזור לי מזיל דמעה )

תודה מראש.

ד"א
עם עברתי על חוק כל שהוא אני מתנצל מראש נבוך
והמשחק מקורי

עידו נדל
חזור למעלה
טיסה לפרופיל הטייס שלח הודעה פרטית לטייס שלח דואר אלקטרוני לטייס אתר הבית של הטייס שלח הודעה במסנג'ר לטייס
uri_ba
טיסות סדירות



הצטרף בתאריך: Sep 17, 2007
הודעות: 4669

הודעהנשלח: 1:02 ,19 מרץ 2008, ד'    כותרת הודעה: תגובה עם ציטוט


קוד:


[fltsim.0]
title=Cessna Skyhawk 172SP Paint1
sim=Cessna172SP
model=
panel=
sound=
texture=1
kb_checklists=Cessna172SP_check
kb_reference=Cessna172SP_ref
atc_id=G-BAFM
ui_manufacturer="Cessna"
ui_type="C172SP Skyhawk"
ui_variation=" Blue, Gold"
ui_typerole="Single Engine Prop"
ui_createdby="Microsoft Corporation"
description="A stable and trustworthy plane, most pilots have logged at least a few hours in a Cessna 172, since it's the most widely available aircraft in the rental fleet, and is used by most flight schools. Since the first prototype was completed in 1955, more than 35,000 C172s have been produced, making it the world's most popular single-engine plane.  One of Cessna's first tricycle-gear airplanes, the 172 quickly became the favorite of a growing class of business pilots.  Its reliability and easy handling (along with thoughtful engineering and structural updates) have ensured its continued popularity for decades."

[fltsim.1]
title=Cessna Skyhawk 172SP Paint2
sim=Cessna172SP
model=
panel=
sound=
texture=2
kb_checklists=Cessna172SP_check
kb_reference=Cessna172SP_ref
atc_id=HB-MES
ui_manufacturer="Cessna"
ui_type="C172SP Skyhawk"
ui_variation=" White,Green"
ui_typerole="Single Engine Prop"
ui_createdby="Microsoft Corporation"
description="A stable and trustworthy plane, most pilots have logged at least a few hours in a Cessna 172, since it's the most widely available aircraft in the rental fleet, and is used by most flight schools. Since the first prototype was completed in 1955, more than 35,000 C172s have been produced, making it the world's most popular single-engine plane.  One of Cessna's first tricycle-gear airplanes, the 172 quickly became the favorite of a growing class of business pilots.  Its reliability and easy handling (along with thoughtful engineering and structural updates) have ensured its continued popularity for decades."

[fltsim.2]
title=Cessna Skyhawk 172SP Paint3
sim=Cessna172SP
model=
panel=
sound=
texture=3
kb_checklists=Cessna172SP_check
kb_reference=Cessna172SP_ref
atc_id=N176CM
atc_id_color=0xffffffff
ui_manufacturer="Cessna"
ui_type="C172SP Skyhawk"
ui_variation=" Orange, Black"
ui_typerole="Single Engine Prop"
ui_createdby="Microsoft Corporation"
description="A stable and trustworthy plane, most pilots have logged at least a few hours in a Cessna 172, since it's the most widely available aircraft in the rental fleet, and is used by most flight schools. Since the first prototype was completed in 1955, more than 35,000 C172s have been produced, making it the world's most popular single-engine plane.  One of Cessna's first tricycle-gear airplanes, the 172 quickly became the favorite of a growing class of business pilots.  Its reliability and easy handling (along with thoughtful engineering and structural updates) have ensured its continued popularity for decades."

[fltsim.3]
title=Cessna Skyhawk 172SP Paint4
sim=Cessna172SP
model=
panel=
sound=
texture=4
kb_checklists=Cessna172SP_check
kb_reference=Cessna172SP_ref
atc_id=N52KA
atc_id_color=0xffffffff
ui_manufacturer="Cessna"
ui_type="C172SP Skyhawk"
ui_variation=" Used Trainer"
ui_typerole="Single Engine Prop"
ui_createdby="Microsoft Corporation"
description="A stable and trustworthy plane, most pilots have logged at least a few hours in a Cessna 172, since it's the most widely available aircraft in the rental fleet, and is used by most flight schools. Since the first prototype was completed in 1955, more than 35,000 C172s have been produced, making it the world's most popular single-engine plane.  One of Cessna's first tricycle-gear airplanes, the 172 quickly became the favorite of a growing class of business pilots.  Its reliability and easy handling (along with thoughtful engineering and structural updates) have ensured its continued popularity for decades."

[fltsim.4]
title=Cessna Skyhawk 172SP G1000
sim=Cessna172SP
model=G1000
panel=G1000
sound=
texture=G1000
kb_checklists=Cessna172SP_check
kb_reference=Cessna172SP_ref
atc_id=N700MS
atc_id_color=0xffffffff
ui_manufacturer="Cessna"
ui_type="C172SP Skyhawk G1000"
ui_variation=" Glass Cockpit"
ui_typerole="Single Engine Prop"
ui_createdby="Microsoft Corporation"
description="A stable and trustworthy plane, most pilots have logged at least a few hours in a Cessna 172, since it's the most widely available aircraft in the rental fleet, and is used by most flight schools. Since the first prototype was completed in 1955, more than 35,000 C172s have been produced, making it the world's most popular single-engine plane.  One of Cessna's first tricycle-gear airplanes, the 172 quickly became the favorite of a growing class of business pilots.  Its reliability and easy handling (along with thoughtful engineering and structural updates) have ensured its continued popularity for decades."

[fltsim.5]
title=Cessna Skyhawk 172SP
sim=Cessna172SP
model=
panel=
sound=
texture=
kb_checklists=Cessna172SP_check
kb_reference=Cessna172SP_ref
atc_id=N760PL
ui_manufacturer="Cessna"
ui_type="C172SP Skyhawk"
ui_variation=" Red, Gold"
ui_typerole="Single Engine Prop"
ui_createdby="Microsoft Corporation"
description="A stable and trustworthy plane, most pilots have logged at least a few hours in a Cessna 172, since it's the most widely available aircraft in the rental fleet, and is used by most flight schools. Since the first prototype was completed in 1955, more than 35,000 C172s have been produced, making it the world's most popular single-engine plane.  One of Cessna's first tricycle-gear airplanes, the 172 quickly became the favorite of a growing class of business pilots.  Its reliability and easy handling (along with thoughtful engineering and structural updates) have ensured its continued popularity for decades."

[General]
atc_type=Cessna
atc_model=C172
editable=0
performance="Maximum Speed\n126 kts            203 km\/hr\n\nCruise Speed\n124 kts            200 km\/hr\n\nEngine\nTextron Lycoming IO-360-L2A 180 bhp\n\nPropeller\nTwo-Bladed Macauley Fixed Pitch\n\nMaximum Range\n638 nm            734 mi          1181 km\n\nService Ceiling\n14,000 ft\t         4267 m\n\nFuel Capacity\n56 gal\t          212 L\t \n\nEmpty Weight\n1,665 lb\t          1,002 kg\n\nMaximum Gross Weight\n2,550 lb\t          1,157 kg\n\nLength\n27 ft, 2 in          8.2 m\n\nWingspan\n36 ft, 1 in\t           11 m\n\nHeight\n8 ft, 11 in\t           2.72 m\n\nSeating\t           4\n\nUseful Load\n893 lb\t           405 kg\n"
Category = airplane

[CameraDefinition.0]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = 7.5, 0.75, 0
InitialPbh = 5, 0, 270
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum

[CameraDefinition.1]
Title = "Left Wing"
Guid = {3A09FD6C-D406-4d8f-A5CD-FA4F5E0C12ED}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = -7.5, 0.75, 0
InitialPbh = 5, 0, 90
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum

[CameraDefinition.2]
Title = "Tail"
Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64A}
Description = Looking forward from the tip of the vertical stabilizer
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.75
ShowWeather = Yes
InitialXyz = 0, 1.9, -5.75
InitialPbh = 11, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.001]
Title = "Right Seat"
Guid = {195EAB58-9E4A-1E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = 0.75
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.5, 0.04, -0.1
InitialPbh=0, 0, 0

[CameraDefinition.002]
Title = "Radio Stack"
Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.2
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0, -0.2, 0
InitialPbh=9, 0, 22

[CameraDefinition.003]
Title = "Light Switches"
Guid = {195EAB58-9E4A-3E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.3
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0, -0.5, 0
InitialPbh=0, 0, -5

[WEIGHT_AND_BALANCE]
max_gross_weight = 2550                         // (pounds)
empty_weight = 1650                             // (pounds)

reference_datum_position     =  3.6, 0, 0       // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     = -3.0, 0, 0       // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 50

station_load.0 = 170, -3.0, -1.5, 0.0          // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170, -3.0,  1.5, 0.0          // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 =   0, -6.2, -1.5, 0.0          // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 =   0, -6.2,  1.5, 0.0          // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 =   0, -8.0,  0.0, 0.0          // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

station_name.0 = "Pilot"
station_name.1 = "Front Passenger"
station_name.2 = "Rear Passenger"
station_name.3 = "Rear Passenger"
station_name.4 = "Baggage"

;Moments of Inertia
empty_weight_pitch_MOI  = 1400.0
empty_weight_roll_MOI   = 1137.0
empty_weight_yaw_MOI    = 2360.0
empty_weight_coupled_MOI= 0.0


[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 = 0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 2.4, 0.0, 0.0                        //(feet) longitudinal, lateral, vertical distance from reference datum
ThrustAnglesPitchHeading.0 = 0,0                //Thrust pitch and heading angles in degrees (+pitch down, +heading right)
fuel_flow_scalar= 0.88                          //Fuel flow scalar
min_throttle_limit = 0.0                        //Minimum percent throttle.  Generally negative for turbine reverser

[piston_engine]
power_scalar = 1.0                              //Piston power scalar
cylinder_displacement= 90.0                     //Cubic inches per cylinder
compression_ratio= 8.5                          //Compression ratio
number_of_cylinders=4                           //Number of cylinders
max_rated_rpm= 2700                             //Max rated RPM
max_rated_hp= 180                               //Max rated HP
fuel_metering_type= 0                           //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0                                 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3                  //Starter torque factor
turbocharged= 0                                 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 0                                //Max design manifold pressure, (inHg)
min_design_mp= 0                                //Min design manifold pressure, (inHg)
critical_altitude= 0                            //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0                         //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0                    //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0                  //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0                        //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 0                                //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 1.0       //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0      //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0                    //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0                   //Scalar on idle RPM friction
BestPowerSpecificFuelConsumption=0.49           //SFC at Best Power mixture ratio

[propeller]
thrust_scalar = 1.0                             //Propeller thrust scalar
propeller_type= 1                               //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 6.3                         //Propeller Diameter, (feet)
propeller_blades= 2                             //Number of propeller blades
propeller_moi= 5.0                              //Propeller moment of inertia
beta_max= 0                                     //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 0                                     //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 0                                  //Miminum governed RPM
prop_tc= 0                                      //Prop time-constant
gear_reduction_ratio= 1.0                       //Propeller gear reduction ratio
fixed_pitch_beta= 20                            //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= 0                         //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 0                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available= 0               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather= 0                          //Minimum RPM for prop feathering
beta_feather= 0                                 //Feathering pitch angle (degrees)
power_absorbed_cf= 0                            //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available= 0          //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available= 0                       //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta= 0                       //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0                         //Minimum pitch angle in reverse, (degrees)

[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

        //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               (0=Undamped, 1=Critically Damped)
        //11 Extension Time              (seconds)
        //12 Retraction Time             (seconds)
        //13 Sound Type
[contact_points]
point.0 = 1,  0.90,  0.00, -4.09, 1500, 0, 0.5, 22.0, 0.25,2.5, 0.7, 0.0, 0.0, 0
point.1 = 1, -4.70, -4.50, -4.01, 3500, 1, 0.5,  0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 2
point.2 = 1, -4.70,  4.50, -4.01, 3500, 2, 0.5,  0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 3
point.3 = 2, -3.90, -18.0,  3.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5
point.4 = 2, -3.90   18.0,  3.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6
point.5=  2,-20.23,   0.0,  0.30, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9
point.6=  2,  1.48,   0.0, -2.17, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4
point.7=  2,-22.80,   0.0,  5.83, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7
point.8=  2, -4.90,   0.0, -2.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 8

max_number_of_points = 21

static_pitch=3.02                //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=3.765           //feet, altitude of CG when at rest on the ground

[brakes]
parking_brake = 1        //Parking brake available
toe_brakes_scale = 0.68  //Brake scalar
auto_brakes = 0

[hydraulic_system]
normal_pressure = 0.0    //PSI

[Views]
eyepoint= -3.95, -0.85, 1.9         //(feet) longitudinal, lateral, vertical distance from reference datum

[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
light.0 = 3,  -2.76, -18.11, 2.97, fx_navred
light.1 = 3,  -2.78,  18.11, 2.95, fx_navgre
light.2 = 2,  -3.13, -18.31, 2.95, fx_strobe
light.3 = 2,  -3.11,  18.31, 2.95, fx_strobe
light.4 = 1, -20.51,   0.00, 6.20, fx_beacon
//light.5 = 4,  -2.27,   0.00, 1.45, fx_vclight

[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

[altimeters]
altimeter.0=1
altimeter.1=1

[airspeed_indicators]
airspeed_indicator.0=1
airspeed_indicator.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=1,0

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
attitude_indicator.1 = 2

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,1    //Turn AND Bank

[vacuum_system]
max_pressure=5.15   //PSI
vacuum_type=1       //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi
engine_map=1

[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000

[pitot_static]
vertical_speed_time_constant = 1                //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat = 1.0    //Scalar on heat effectiveness, 0 = not available

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

[exits]
number_of_exits = 2
exit.0 = 0.4 // (0=Main 1=Passenger)
exit.1 = 0.4 // (0=Main 1=Passenger)

[fuel]
LeftMain  = -3.9, -2.1, 2.5, 26.5, 0.0       //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -3.9,  2.1, 2.5, 26.5, 0.0       //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
engine_driven_pump=0

[airplane_geometry]
wing_area               = 174.0                 //Square feet
wing_span               = 36.1                  //Feet
wing_root_chord         = 4.9                   //Feet
wing_dihedral           = 1.7                   //Degrees
wing_incidence          = 1.5                   //Degrees
wing_twist              = -3.0                  //Degrees
oswald_efficiency_factor= 0.68                  //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 0                     //Degrees, wing leading edge
wing_pos_apex_lon       = -2.4                  //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           = -18.3                 //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         = 3.2                   //Degrees
htail_sweep             = 10.0                  //Degrees, horizontal tail leading edge
vtail_area              = 18.0                  //Square feet
vtail_span              = 4.8                   //Feet, tip to body
vtail_sweep             = 40.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -16.2                 //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             = 6.7                   //Square feet
elevator_up_limit       = 28.0                  //Degrees
elevator_down_limit     = 21.0                  //Degrees
aileron_up_limit        = 20.0                  //Degrees
aileron_down_limit      = 15.0                  //Degrees
rudder_limit            = 24.0                  //Degrees
elevator_trim_limit     = 19.5                  //Degrees
spoiler_limit           = 0.0                   //Degrees
spoilerons_available    = 0                     //Spoilerons Available?
aileron_to_spoileron_gain = 0                   //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0                 //Degrees
min_flaps_for_spoilerons = 0                    //Minimum flap handle position when spoilerons activate
auto_spoiler_available   = 0
positive_g_limit_flaps_up  =  4.0               //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down=  2.0               //Design G load tolerance (positive, flaps down)
negative_g_limit_flaps_up  = -1.5               //Design G load tolerance (negative, flaps up)
negative_g_limit_flaps_down= -1.5               //Design G load tolerance (negative, flaps down)
load_safety_factor         =  1.5               //Design G load safety factor


[flaps.0]       //Trailing Edge Flaps
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.5                                  // 0.0 .. 1.0
extending-time   = 7                                    // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 12.7                                 // degrees
flaps-position.2 = 25.3                                 // degrees
flaps-position.3 = 38                                   // degrees
damaging-speed   = 120                                  // KIAS
blowout-speed    = 150                                  // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 0                                         //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None


[Reference Speeds]
flaps_up_stall_speed    = 53.0                  //Knots True (KTAS)
full_flaps_stall_speed  = 48.0                  //Knots True (KTAS)
cruise_speed            = 115.0                 //Knots True (KTAS)
max_indicated_speed     = 163                   //Red line (KIAS)

[autopilot]
autopilot_available= 1
flight_director_available= 0
default_vertical_speed= 700.0
autothrottle_available= 0
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


[forcefeedback]
gear_bump_nose_magnitude=6000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=6000           ; 0 - 10000
gear_bump_left_direction=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=6000          ; 0 - 10000
gear_bump_right_direction=00500         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=3250            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750             ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
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=1
stick_shaker=0

[deice_system]
structural_deice_type=0     //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots




תהנה

אגב, הוא אמור להיות גם איפשהו על הדיסק.
חזור למעלה
טיסה לפרופיל הטייס שלח הודעה פרטית לטייס אתר הבית של הטייס
idonadel
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הצטרף בתאריך: Dec 31, 2007
הודעות: 246
מיקום: ראש העין

הודעהנשלח: 8:07 ,19 מרץ 2008, ד'    כותרת הודעה: תגובה עם ציטוט

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חזור למעלה
טיסה לפרופיל הטייס שלח הודעה פרטית לטייס שלח דואר אלקטרוני לטייס אתר הבית של הטייס שלח הודעה במסנג'ר לטייס
הצג הודעות קודמות:   
שליחת הודעה חדשה   תגובה להודעה    עמוד ראשי -> פלייט סימולטור כל הזמנים הם שעון ישראל (GMT + שעתיים)
עמוד 1 מתוך 1

 

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