17-12-2010, 05:49 AM
Just wondering if anyone has a payload model for the Mil Viz_Cessna 310
I have tried using the default file and the files posted here for the Dream fleet model but they seem to be way off. The following is the
config file:
.//FDE v4 09-29-10
//.air file record 509 modified to x=0, y=0 on 09-08-10 by Bill Leaming
//aircraft.cfg prop_moi modified to be 2.1 on 09-08-10 by Bill Leaming
//this was done to eliminate the "backwards windmilling props" for FSX+SP2
[fltsim.0]
title=Cessna 310 N5077J
sim=Cessna 310v4
model=
panel=
sound=
texture=N5077J
kb_checklists=Cessna 310v4_checklist
kb_reference=Cessna 310v4_references
ui_manufacturer=Cessna
ui_type="310R"
ui_model="C310"
ui_variation=N5077J 3dAnalog
ui_typerole="Twin Engine Prop"
ui_createdby="Military Visualizations"
atc_id=N5077J
description=Although no longer in production, the Cessna C310, was and still is one of the most popular twin engine aircraft and the
choice of many General Aviation enthusiasts.
[fltsim.1]
title=Cessna 310 N5225J
sim=Cessna 310v4
model=G1000
panel=G1000
sound=
texture=N5225J
kb_checklists=Cessna 310v4_checklist
kb_reference=Cessna 310v4_references
ui_manufacturer=Cessna
ui_type="310R"
ui_model="C310"
ui_variation=N5225J G1000
ui_typerole="Twin Engine Prop"
ui_createdby="Military Visualizations"
atc_id=N5225J
description=Although no longer in production, the Cessna C310, was and still is one of the most popular twin engine aircraft and the
choice of many General Aviation enthusiasts.
[fltsim.2]
title=Cessna 310 YV2068
sim=Cessna 310v4
model=freeradio
panel=freeradio
sound=
texture=YV2068
kb_checklists=Cessna 310v4_checklist
kb_reference=Cessna 310v4_references
ui_manufacturer=Cessna
ui_type="310R"
ui_model="C310"
ui_variation=YV2068 FreeRadio
ui_typerole="Twin Engine Prop"
ui_createdby="Military Visualizations"
atc_id=YV2068
description=Although no longer in production, the Cessna C310, was and still is one of the most popular twin engine aircraft and the
choice of many General Aviation enthusiasts.
[fltsim.3]
title=Cessna 310 CGTER FreeRadio
sim=Cessna 310v4
model=freeradio
panel=freeradio
sound=
texture=CGTER
kb_checklists=Cessna 310v4_checklist
kb_reference=Cessna 310v4_references
ui_manufacturer=Cessna
ui_type="310R"
ui_model="C310"
ui_variation=CGTER FreeRadio
ui_typerole="Twin Engine Prop"
ui_createdby="Military Visualizations"
atc_id=CGTER
description=Although no longer in production, the Cessna C310, was and still is one of the most popular twin engine aircraft and the
choice of many General Aviation enthusiasts.
[fltsim.4]
title=Cessna 310 DIRFT 3dAnalog
sim=Cessna 310v4
model=
panel=
sound=
texture=DIRFT
kb_checklists=Cessna 310v4_checklist
kb_reference=Cessna 310v4_references
ui_manufacturer=Cessna
ui_type="310R"
ui_model="C310"
ui_variation=DIRFT 3dAnalog
ui_typerole="Twin Engine Prop"
ui_createdby="Military Visualizations"
atc_id=DERFT
description=Although no longer in production, the Cessna C310, was and still is one of the most popular twin engine aircraft and the
choice of many General Aviation enthusiasts.
[fltsim.5]
title=Cessna 310 COLIN FreeRadio
sim=Cessna 310v4
model=freeradio
panel=freeradio
sound=
texture=COLIN
kb_checklists=Cessna 310v4_checklist
kb_reference=Cessna 310v4_references
ui_manufacturer=Cessna
ui_type="310R"
ui_model="C310"
ui_variation=MILVIZ FreeRadio
ui_typerole="Twin Engine Prop"
ui_createdby="Military Visualizations"
atc_id=COLIN
description=Although no longer in production, the Cessna C310, was and still is one of the most popular twin engine aircraft and the
choice of many General Aviation enthusiasts.
[General]
atc_type=Cessna
atc_model=310
editable=1
performance=Cruise Speed: 200 kts 370 km/hr; Engine: Teledyne Continental Motors IO-550-C 300 hp; Propeller: Three-bladed
McCauley constant-speed, variable pitch; Maximum Range: 1,569 nm 2,906 km; Service Ceiling: 20,688 ft 6,306 m; Fuel Capacity: 142 gal
537 L; Maximum Gross Weight: 5,524 lb 2,509 kg; Length: 29 ft, 10 in 9.09 m; Wingspan: 37 ft, 10 in 11.53 m; Height: 9 ft, 9 in 2.97 m;
Seating: Up to 6; Useful Load: 1,634 lb 741 kg.
Category=airplane
[CameraDefinition.001]
Title = "Right Seat"
Guid = {2BFAD225-486A-4284-B007-683AD63F2852}
Description = Virtual Cockpit Right Seat
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = 0.75
SmoothZoomTime = 3.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=100
HeadingPanRate=120
InitialXyz=0.60, 0.001, -0.061
InitialPbh=11.57, 0, 0
[CameraDefinition.002]
Title = "Fuel Selector"
Guid = {2BFAD223-486A-4284-B007-683AD63F2852}
Description = Virtual Cockpit Fuel Selector
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.75
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.30, -0.46, 0.23
InitialPbh=72.28, 0, 0
[CameraDefinition.003]
Title = "Lower Panel"
Guid = {D95E57AC-1EF3-442e-901D-8C7168F4DA9D}
Description = Virtual Cockpit Lower Panel
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.60
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-0.035, -0.458, 0.195
InitialPbh=6.41, 0, 0
[CameraDefinition.004]
Title = "Throttle Quadrant"
Guid = {403CC4B7-5645-4019-B413-D91878A3B772}
Description = Virtual Cockpit Throttle Quadrant
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.60
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.27, -0.305, 0.085
InitialPbh=24.96, 0, 0
[CameraDefinition.005]
Title = "Middle Left Seat"
Guid = {2EFAD225-486F-4284-B007-683AD63F2859}
Description = VC Middle Left Seat
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = 0.75
SmoothZoomTime = 3.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=60
HeadingPanRate=80
InitialXyz=-0.00, -0.09, -1.031
InitialPbh=1.57, 0, 0
[CameraDefinition.1]
Title = "Tail Cam"
Guid = {B8AB17EC-C99F-4898-912C-60DBE370B21F}
Description = Tail Lipstick Camera
Origin = Center
MomentumEffect = No
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.70
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
PitchPanRate=80
HeadingPanRate=100
InitialXyz=0, 1.589, -4.916
InitialPbh=10.017, 0, 0
Category=Aircraft
ClipMode=Minimum
[CameraDefinition.2]
Title = "Right Elevator"
Guid = {83FF08E4-A9BC-463c-A155-0B9AE5D8D5CD}
Description = Right Elevator
Origin = Center
MomentumEffect = No
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.60
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
PitchPanRate=20
HeadingPanRate=60
InitialXyz=2.83, 0.58, -4.916
InitialPbh=7.158, 0, -23.90
Category=Aircraft
ClipMode=Minimum
[CameraDefinition.3]
Title = "Landing Gear"
Guid = {EA64BF5E-55D6-46e4-8C50-E31E4177C74F}
Description = Landing Gear
Origin = Center
MomentumEffect = No
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-2.18, -0.17, -6.13
InitialPbh=2.99, 0, 20.64
Category=Aircraft
ClipMode=Minimum
[WEIGHT_AND_BALANCE]
max_gross_weight = 5500
empty_weight = 3500
reference_datum_position = 0, 0, -0.4
empty_weight_CG_position = 0.0, 0, 0
//CG_forward_limit = 0
//CG_aft_limit = 1
empty_weight_pitch_MOI = 3000
empty_weight_roll_MOI = 2500
empty_weight_yaw_MOI = 3000
empty_weight_coupled_MOI = 0
max_number_of_stations = 50
station_load.0 = 180,-0.6,-1.0, 1.00
station_load.1 = 180,-0.6, 1.0, 1.00
station_load.2 = 0, -3.2,-1.0, 1.00
station_load.3 = 0, -3.2, 1.0, 1.00
station_load.4 = 0, -6.0,-1.0, 1.00
station_load.5 = 0, -6.0, 1.0, 1.00
station_load.6 = 0, 4.5, 0.0, 0.0
station_load.7 = 0, -8.0, 0.0, 0.0
station_load.8 = 0, -1.6,-7.0, 0.5
station_load.9 = 0, -1.6, 7.0, 0.5
station_name.0 = pilot
station_name.1 = fwd pax
station_name.2 = pax row 2
station_name.3 = pax row 2
station_name.4 = pax row 3
station_name.5 = pax row 3
station_name.6 = fwd bag max 350
station_name.7 = aft bag max 160
station_name.8 = lt bag max 120
station_name.9 = rt bag max 120
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.2
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
hi_alpha_on_yaw = 1.0
p_factor_on_yaw = -0.3
torque_on_roll = 0.3
gyro_precession_on_yaw = 0.3
gyro_precession_on_pitch = 0.3
gyro_precession_on_roll = 0.3
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
Engine.0 = 6.5, -5.8, 0.0
Engine.1 = 6.5, 6.2, 0.0
fuel_flow_scalar= 1.0
min_throttle_limit=0.00
[piston_engine]
power_scalar = 1.0 //Piston power scalar
cylinder_displacement= 91.7 //Cubic inches per cylinder
compression_ratio= 8.0 //Compression ratio
number_of_cylinders= 6 //Number of cylinders
max_rated_rpm= 2700.0 //Max rated RPM
max_rated_hp= 300.0 //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= 0.27 //Starter torque factor
turbocharged= 0 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 0.0 //Max design manifold pressure, (inHg)
min_design_mp= 1.0 //Min design manifold pressure, (inHg)
critical_altitude= 0.0 //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= 0.0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0.0 //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
[propeller]
thrust_scalar = 1.0 //Propeller thrust scalar
propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 6.4 //Propeller Diameter, (feet) 6.4
propeller_blades= 3 //Number of propeller blades
propeller_moi= 2.1 //Propeller moment of inertia 7
beta_max= 45.0 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 15.2 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1100.0 //Miminum governed RPM
prop_tc= 0.1 //Prop time-constant
gear_reduction_ratio= 1.0 //Propeller gear reduction ratio
fixed_pitch_beta= 0.0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit= 80.0 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available= 1 //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= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather= 700.0 //Minimum RPM for prop feathering
beta_feather= 82.5 //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= 0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta= 0.0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0.0 //Minimum pitch angle in reverse, (degrees)
[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 (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)
//GEAR 40 8
point.0 = 1, 7.616, 0.00, -4.275, 1600, 0, 0.716, 32, 0.35, 1.5, 0.45, 3.0, 5.0, 0, 152, 180
point.1 = 1, -1.802, -5.98, -3.509, 1600, 1, 0.937, 0, 0.20, 3.0, 0.95, 4.1, 4.3, 2, 152, 200
point.2 = 1, -1.802, 5.98, -3.509, 1600, 2, 0.937, 0, 0.20, 3.0, 0.95, 4.3, 4.1, 3, 152, 200
//SCRAPES
point.3= 2, 0.00, -17.7, 1.2, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4= 2, 0.00, 17.7, 1.2, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5= 2,-16.6, 0.00, 0.2, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6= 2, 8.5, 0.00, 0.1,1500, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
static_pitch = 4 //Degrees
static_cg_height = 4 //Feet
gear_system_type=0
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.7 // 0.0 .. 1.0
extending-time = 4 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 15 // degrees
flaps-position.2 = 35 // degrees
damaging-speed = 160 // KIAS
blowout-speed = 190 // KIAS
[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0
[pitot_static]
vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000
[exits]
number_of_exits = 4
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
exit_rate.2 = 0.6 ;Percent per second
exit_rate.3 = 0.6 ;Percent per second
[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, 1
Adf.1 = 1
Transponder.1 = 1
Marker.1 = 1
[Views]
eyepoint = -0.95, -1.05, 3.51p //Longitudinal, Lateral, Vertical (feet)
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//Types: 6=taxi, 7=recognition, 8=wing, 9=logo 10=cabin
//NONE! ALL LIGHTS ARE PLACED IN THE .MDL FILE!!! /////////////////////
[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, 250
aileron = 100, 250
rudder = 100, 250
[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
[fuel]
//normal fuel capacity is 163 gals.
LeftMain = -0.5, -15.00, 0.0, 51.0, 1.5
RightMain = -0.5, 15.00, 0.0, 51.0, 1.5
External1= -1.4, -3.45, 0.0, 32.0, 0.0
External2= -1.4, 3.45, 0.0, 32.0, 0.0
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 2
electric_pump=1
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[airplane_geometry]
wing_area = 179.0 //Square feet
wing_span = 36.1 //Feet
wing_root_chord = 5.9 //Feet
wing_dihedral = 5.0 //Degrees
wing_incidence = 0.0 //Degrees
wing_twist = 0.0 //Degrees
oswald_efficiency_factor= 1.0 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 0.0 //Degrees, wing leading edge
wing_pos_apex_lon = 2.0 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = -0.20 //Feet, vertical distance from reference point, positive going up
htail_area = 32.1 //Square feet
htail_span = 17.0 //Feet
htail_pos_lon =-17.0 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 1.40 //Feet, vertical distance from reference point, positive going up
htail_incidence = 0.0 //Degrees
htail_sweep = 5.0 //Degrees, horizontal tail leading edge
vtail_area = 15.0 //Square feet
vtail_span = 10.0 //Feet, tip to body
vtail_sweep = 40.0 //Degrees, vertical tail leading edge
vtail_pos_lon =-18.0 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 2.40 //Feet, vertical distance from reference point, positive going up
elevator_area = 22.1 //Square feet
aileron_area = 11.4 //Square feet
rudder_area = 11.8 //Square feet
elevator_up_limit = 16.5 //Degrees
elevator_down_limit = 15.0 //Degrees
aileron_up_limit = 20.0 //18 Degrees
aileron_down_limit = 20.0 //18 Degrees
rudder_limit = 25.0 //Degrees
elevator_trim_limit = 8.0 //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=3.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-2.000000
negative_g_limit_flaps_down=-2.000000
[Reference Speeds]
flaps_up_stall_speed = 79.0 //Knots True (KTAS)
full_flaps_stall_speed = 72.0 //Knots True (KTAS)
cruise_speed = 160.0 //Knots True (KTAS) [172 indicated]
max_indicated_speed=281.00
max_level_speed=260 //knots over the ground at 10,000 ft.
[altimeters]
altimeter.0=1
altimeter.1=1
[airspeed_indicators]
airspeed_indicator.0=1
airspeed_indicator.1=1
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 000.0
autothrottle_available= 1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=110.00
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
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 6000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 6000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5#
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1#
crash_magnitude1 = 10000
crash_direction1 = 1000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
[brakes]
toe_brakes_scale=0.5
parking_brake=1
differential_braking_scale = 0.5
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=31.512679
flap_limit_idle=31.512679
[hydraulic_system]
normal_pressure=0.00
[stall_warning]
type=1
stick_shaker=1
[attitude_indicators]
attitude_indicator.0=2 // 1 = vacuum gyro, 2 = electric gyro
[turn_indicators]
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15
vacuum_type=1
electric_backup_pressure=4.90
engine_map=1,1,0,0
[pneumatic_system]
max_pressure=0.00
bleed_air_scalar=0.00
[deice_system]
structural_deice_type=2
I have tried using the default file and the files posted here for the Dream fleet model but they seem to be way off. The following is the
config file:
.//FDE v4 09-29-10
//.air file record 509 modified to x=0, y=0 on 09-08-10 by Bill Leaming
//aircraft.cfg prop_moi modified to be 2.1 on 09-08-10 by Bill Leaming
//this was done to eliminate the "backwards windmilling props" for FSX+SP2
[fltsim.0]
title=Cessna 310 N5077J
sim=Cessna 310v4
model=
panel=
sound=
texture=N5077J
kb_checklists=Cessna 310v4_checklist
kb_reference=Cessna 310v4_references
ui_manufacturer=Cessna
ui_type="310R"
ui_model="C310"
ui_variation=N5077J 3dAnalog
ui_typerole="Twin Engine Prop"
ui_createdby="Military Visualizations"
atc_id=N5077J
description=Although no longer in production, the Cessna C310, was and still is one of the most popular twin engine aircraft and the
choice of many General Aviation enthusiasts.
[fltsim.1]
title=Cessna 310 N5225J
sim=Cessna 310v4
model=G1000
panel=G1000
sound=
texture=N5225J
kb_checklists=Cessna 310v4_checklist
kb_reference=Cessna 310v4_references
ui_manufacturer=Cessna
ui_type="310R"
ui_model="C310"
ui_variation=N5225J G1000
ui_typerole="Twin Engine Prop"
ui_createdby="Military Visualizations"
atc_id=N5225J
description=Although no longer in production, the Cessna C310, was and still is one of the most popular twin engine aircraft and the
choice of many General Aviation enthusiasts.
[fltsim.2]
title=Cessna 310 YV2068
sim=Cessna 310v4
model=freeradio
panel=freeradio
sound=
texture=YV2068
kb_checklists=Cessna 310v4_checklist
kb_reference=Cessna 310v4_references
ui_manufacturer=Cessna
ui_type="310R"
ui_model="C310"
ui_variation=YV2068 FreeRadio
ui_typerole="Twin Engine Prop"
ui_createdby="Military Visualizations"
atc_id=YV2068
description=Although no longer in production, the Cessna C310, was and still is one of the most popular twin engine aircraft and the
choice of many General Aviation enthusiasts.
[fltsim.3]
title=Cessna 310 CGTER FreeRadio
sim=Cessna 310v4
model=freeradio
panel=freeradio
sound=
texture=CGTER
kb_checklists=Cessna 310v4_checklist
kb_reference=Cessna 310v4_references
ui_manufacturer=Cessna
ui_type="310R"
ui_model="C310"
ui_variation=CGTER FreeRadio
ui_typerole="Twin Engine Prop"
ui_createdby="Military Visualizations"
atc_id=CGTER
description=Although no longer in production, the Cessna C310, was and still is one of the most popular twin engine aircraft and the
choice of many General Aviation enthusiasts.
[fltsim.4]
title=Cessna 310 DIRFT 3dAnalog
sim=Cessna 310v4
model=
panel=
sound=
texture=DIRFT
kb_checklists=Cessna 310v4_checklist
kb_reference=Cessna 310v4_references
ui_manufacturer=Cessna
ui_type="310R"
ui_model="C310"
ui_variation=DIRFT 3dAnalog
ui_typerole="Twin Engine Prop"
ui_createdby="Military Visualizations"
atc_id=DERFT
description=Although no longer in production, the Cessna C310, was and still is one of the most popular twin engine aircraft and the
choice of many General Aviation enthusiasts.
[fltsim.5]
title=Cessna 310 COLIN FreeRadio
sim=Cessna 310v4
model=freeradio
panel=freeradio
sound=
texture=COLIN
kb_checklists=Cessna 310v4_checklist
kb_reference=Cessna 310v4_references
ui_manufacturer=Cessna
ui_type="310R"
ui_model="C310"
ui_variation=MILVIZ FreeRadio
ui_typerole="Twin Engine Prop"
ui_createdby="Military Visualizations"
atc_id=COLIN
description=Although no longer in production, the Cessna C310, was and still is one of the most popular twin engine aircraft and the
choice of many General Aviation enthusiasts.
[General]
atc_type=Cessna
atc_model=310
editable=1
performance=Cruise Speed: 200 kts 370 km/hr; Engine: Teledyne Continental Motors IO-550-C 300 hp; Propeller: Three-bladed
McCauley constant-speed, variable pitch; Maximum Range: 1,569 nm 2,906 km; Service Ceiling: 20,688 ft 6,306 m; Fuel Capacity: 142 gal
537 L; Maximum Gross Weight: 5,524 lb 2,509 kg; Length: 29 ft, 10 in 9.09 m; Wingspan: 37 ft, 10 in 11.53 m; Height: 9 ft, 9 in 2.97 m;
Seating: Up to 6; Useful Load: 1,634 lb 741 kg.
Category=airplane
[CameraDefinition.001]
Title = "Right Seat"
Guid = {2BFAD225-486A-4284-B007-683AD63F2852}
Description = Virtual Cockpit Right Seat
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = 0.75
SmoothZoomTime = 3.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=100
HeadingPanRate=120
InitialXyz=0.60, 0.001, -0.061
InitialPbh=11.57, 0, 0
[CameraDefinition.002]
Title = "Fuel Selector"
Guid = {2BFAD223-486A-4284-B007-683AD63F2852}
Description = Virtual Cockpit Fuel Selector
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.75
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.30, -0.46, 0.23
InitialPbh=72.28, 0, 0
[CameraDefinition.003]
Title = "Lower Panel"
Guid = {D95E57AC-1EF3-442e-901D-8C7168F4DA9D}
Description = Virtual Cockpit Lower Panel
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.60
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-0.035, -0.458, 0.195
InitialPbh=6.41, 0, 0
[CameraDefinition.004]
Title = "Throttle Quadrant"
Guid = {403CC4B7-5645-4019-B413-D91878A3B772}
Description = Virtual Cockpit Throttle Quadrant
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.60
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.27, -0.305, 0.085
InitialPbh=24.96, 0, 0
[CameraDefinition.005]
Title = "Middle Left Seat"
Guid = {2EFAD225-486F-4284-B007-683AD63F2859}
Description = VC Middle Left Seat
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = 0.75
SmoothZoomTime = 3.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=60
HeadingPanRate=80
InitialXyz=-0.00, -0.09, -1.031
InitialPbh=1.57, 0, 0
[CameraDefinition.1]
Title = "Tail Cam"
Guid = {B8AB17EC-C99F-4898-912C-60DBE370B21F}
Description = Tail Lipstick Camera
Origin = Center
MomentumEffect = No
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.70
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
PitchPanRate=80
HeadingPanRate=100
InitialXyz=0, 1.589, -4.916
InitialPbh=10.017, 0, 0
Category=Aircraft
ClipMode=Minimum
[CameraDefinition.2]
Title = "Right Elevator"
Guid = {83FF08E4-A9BC-463c-A155-0B9AE5D8D5CD}
Description = Right Elevator
Origin = Center
MomentumEffect = No
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.60
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
PitchPanRate=20
HeadingPanRate=60
InitialXyz=2.83, 0.58, -4.916
InitialPbh=7.158, 0, -23.90
Category=Aircraft
ClipMode=Minimum
[CameraDefinition.3]
Title = "Landing Gear"
Guid = {EA64BF5E-55D6-46e4-8C50-E31E4177C74F}
Description = Landing Gear
Origin = Center
MomentumEffect = No
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-2.18, -0.17, -6.13
InitialPbh=2.99, 0, 20.64
Category=Aircraft
ClipMode=Minimum
[WEIGHT_AND_BALANCE]
max_gross_weight = 5500
empty_weight = 3500
reference_datum_position = 0, 0, -0.4
empty_weight_CG_position = 0.0, 0, 0
//CG_forward_limit = 0
//CG_aft_limit = 1
empty_weight_pitch_MOI = 3000
empty_weight_roll_MOI = 2500
empty_weight_yaw_MOI = 3000
empty_weight_coupled_MOI = 0
max_number_of_stations = 50
station_load.0 = 180,-0.6,-1.0, 1.00
station_load.1 = 180,-0.6, 1.0, 1.00
station_load.2 = 0, -3.2,-1.0, 1.00
station_load.3 = 0, -3.2, 1.0, 1.00
station_load.4 = 0, -6.0,-1.0, 1.00
station_load.5 = 0, -6.0, 1.0, 1.00
station_load.6 = 0, 4.5, 0.0, 0.0
station_load.7 = 0, -8.0, 0.0, 0.0
station_load.8 = 0, -1.6,-7.0, 0.5
station_load.9 = 0, -1.6, 7.0, 0.5
station_name.0 = pilot
station_name.1 = fwd pax
station_name.2 = pax row 2
station_name.3 = pax row 2
station_name.4 = pax row 3
station_name.5 = pax row 3
station_name.6 = fwd bag max 350
station_name.7 = aft bag max 160
station_name.8 = lt bag max 120
station_name.9 = rt bag max 120
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.2
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
hi_alpha_on_yaw = 1.0
p_factor_on_yaw = -0.3
torque_on_roll = 0.3
gyro_precession_on_yaw = 0.3
gyro_precession_on_pitch = 0.3
gyro_precession_on_roll = 0.3
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
Engine.0 = 6.5, -5.8, 0.0
Engine.1 = 6.5, 6.2, 0.0
fuel_flow_scalar= 1.0
min_throttle_limit=0.00
[piston_engine]
power_scalar = 1.0 //Piston power scalar
cylinder_displacement= 91.7 //Cubic inches per cylinder
compression_ratio= 8.0 //Compression ratio
number_of_cylinders= 6 //Number of cylinders
max_rated_rpm= 2700.0 //Max rated RPM
max_rated_hp= 300.0 //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= 0.27 //Starter torque factor
turbocharged= 0 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 0.0 //Max design manifold pressure, (inHg)
min_design_mp= 1.0 //Min design manifold pressure, (inHg)
critical_altitude= 0.0 //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= 0.0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0.0 //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
[propeller]
thrust_scalar = 1.0 //Propeller thrust scalar
propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 6.4 //Propeller Diameter, (feet) 6.4
propeller_blades= 3 //Number of propeller blades
propeller_moi= 2.1 //Propeller moment of inertia 7
beta_max= 45.0 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 15.2 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1100.0 //Miminum governed RPM
prop_tc= 0.1 //Prop time-constant
gear_reduction_ratio= 1.0 //Propeller gear reduction ratio
fixed_pitch_beta= 0.0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit= 80.0 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available= 1 //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= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather= 700.0 //Minimum RPM for prop feathering
beta_feather= 82.5 //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= 0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta= 0.0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0.0 //Minimum pitch angle in reverse, (degrees)
[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 (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)
//GEAR 40 8
point.0 = 1, 7.616, 0.00, -4.275, 1600, 0, 0.716, 32, 0.35, 1.5, 0.45, 3.0, 5.0, 0, 152, 180
point.1 = 1, -1.802, -5.98, -3.509, 1600, 1, 0.937, 0, 0.20, 3.0, 0.95, 4.1, 4.3, 2, 152, 200
point.2 = 1, -1.802, 5.98, -3.509, 1600, 2, 0.937, 0, 0.20, 3.0, 0.95, 4.3, 4.1, 3, 152, 200
//SCRAPES
point.3= 2, 0.00, -17.7, 1.2, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4= 2, 0.00, 17.7, 1.2, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5= 2,-16.6, 0.00, 0.2, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6= 2, 8.5, 0.00, 0.1,1500, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
static_pitch = 4 //Degrees
static_cg_height = 4 //Feet
gear_system_type=0
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.7 // 0.0 .. 1.0
extending-time = 4 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 15 // degrees
flaps-position.2 = 35 // degrees
damaging-speed = 160 // KIAS
blowout-speed = 190 // KIAS
[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0
[pitot_static]
vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000
[exits]
number_of_exits = 4
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
exit_rate.2 = 0.6 ;Percent per second
exit_rate.3 = 0.6 ;Percent per second
[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, 1
Adf.1 = 1
Transponder.1 = 1
Marker.1 = 1
[Views]
eyepoint = -0.95, -1.05, 3.51p //Longitudinal, Lateral, Vertical (feet)
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//Types: 6=taxi, 7=recognition, 8=wing, 9=logo 10=cabin
//NONE! ALL LIGHTS ARE PLACED IN THE .MDL FILE!!! /////////////////////
[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, 250
aileron = 100, 250
rudder = 100, 250
[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
[fuel]
//normal fuel capacity is 163 gals.
LeftMain = -0.5, -15.00, 0.0, 51.0, 1.5
RightMain = -0.5, 15.00, 0.0, 51.0, 1.5
External1= -1.4, -3.45, 0.0, 32.0, 0.0
External2= -1.4, 3.45, 0.0, 32.0, 0.0
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 2
electric_pump=1
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[airplane_geometry]
wing_area = 179.0 //Square feet
wing_span = 36.1 //Feet
wing_root_chord = 5.9 //Feet
wing_dihedral = 5.0 //Degrees
wing_incidence = 0.0 //Degrees
wing_twist = 0.0 //Degrees
oswald_efficiency_factor= 1.0 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 0.0 //Degrees, wing leading edge
wing_pos_apex_lon = 2.0 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = -0.20 //Feet, vertical distance from reference point, positive going up
htail_area = 32.1 //Square feet
htail_span = 17.0 //Feet
htail_pos_lon =-17.0 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 1.40 //Feet, vertical distance from reference point, positive going up
htail_incidence = 0.0 //Degrees
htail_sweep = 5.0 //Degrees, horizontal tail leading edge
vtail_area = 15.0 //Square feet
vtail_span = 10.0 //Feet, tip to body
vtail_sweep = 40.0 //Degrees, vertical tail leading edge
vtail_pos_lon =-18.0 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 2.40 //Feet, vertical distance from reference point, positive going up
elevator_area = 22.1 //Square feet
aileron_area = 11.4 //Square feet
rudder_area = 11.8 //Square feet
elevator_up_limit = 16.5 //Degrees
elevator_down_limit = 15.0 //Degrees
aileron_up_limit = 20.0 //18 Degrees
aileron_down_limit = 20.0 //18 Degrees
rudder_limit = 25.0 //Degrees
elevator_trim_limit = 8.0 //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=3.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-2.000000
negative_g_limit_flaps_down=-2.000000
[Reference Speeds]
flaps_up_stall_speed = 79.0 //Knots True (KTAS)
full_flaps_stall_speed = 72.0 //Knots True (KTAS)
cruise_speed = 160.0 //Knots True (KTAS) [172 indicated]
max_indicated_speed=281.00
max_level_speed=260 //knots over the ground at 10,000 ft.
[altimeters]
altimeter.0=1
altimeter.1=1
[airspeed_indicators]
airspeed_indicator.0=1
airspeed_indicator.1=1
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 000.0
autothrottle_available= 1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=110.00
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
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 6000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 6000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5#
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1#
crash_magnitude1 = 10000
crash_direction1 = 1000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
[brakes]
toe_brakes_scale=0.5
parking_brake=1
differential_braking_scale = 0.5
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=31.512679
flap_limit_idle=31.512679
[hydraulic_system]
normal_pressure=0.00
[stall_warning]
type=1
stick_shaker=1
[attitude_indicators]
attitude_indicator.0=2 // 1 = vacuum gyro, 2 = electric gyro
[turn_indicators]
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15
vacuum_type=1
electric_backup_pressure=4.90
engine_map=1,1,0,0
[pneumatic_system]
max_pressure=0.00
bleed_air_scalar=0.00
[deice_system]
structural_deice_type=2
Robin