// This is the flight dynamics file of the Douglas C-47 miltary version of  DC-3
// Developers: Daniel Fuernkaess, Manfred Jahn, Alexander M. Metzger, Hans-Joerg Naegele
// Release Date ???
// last change: HN
// last change: AMM Jan 12, 2013
// last change: HN, Aug 10, 2013
// last change: HN, Aug 16, 2013
// last change: HN, Sep 2, 2013
// last change: HN, Sep 11, 2013
// last change: HN, Sep 17, 2013

[fltsim.0]
title=Douglas C-47 EATS 315221 
sim=Douglas_DC3_v1.2
model=C47_1
panel=
sound=
texture=EATS_315221
kb_checklists=douglas_c47_check
kb_reference=douglas_c47_ref
atc_id=315221
ui_manufacturer="Douglas"
ui_type="C-47R Skytrain"
ui_variation="EATS 315221"
ui_typerole="Twin Engine Prop"
ui_createdby=
description="European Air Transport Service Operation Plainfare 1948"



[Cameradefinition.1]
Title=Overhead Panel
Guid = {C95EAB58-9E4A-9E2A-A34C-D8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
SmoothZoomTime = 2.0
ZoomPanScalar = 1.15
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=40
HeadingPanRate=60
PanAcceleratorTime=0
InitialXyz=0.0, 0.0, -0.15
InitialPbh=-20.0, 0.00, 25

[Cameradefinition.2]
Title=Standard
Guid = {C95EAB58-9E4A-9E2B-A34C-D8D9D948F078}
Description = 
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = 0.5
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=40
HeadingPanRate=60
PanAcceleratorTime=0
InitialXyz=0.0, 0.0, 0.0
InitialPbh=15, 0, 0

[Cameradefinition.3]
Title=Engine Controls
Guid = {C95EAB58-9E4A-9E2C-A34C-D8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=40
HeadingPanRate=60
PanAcceleratorTime=0
InitialXyz=0.0, 0.0, -0.1
InitialPbh=35, 0, 35

[Cameradefinition.3]
Title=Spot
Guid = {BCA3FDD1-FB83-4BBA-8407-4922A7F0D00C}
Description = This is the description of the spot view.
Origin = Center
SnapPbhAdjust = Ordinal
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = FlatChase
ShowAxis = No
AllowZoom = Yes
InitialZoom = 0.4
SmoothZoomTime = 2.0
ShowWeather = Yes
XyzAdjust = FALSE
Transition = Yes
ShowLensFlare=TRUE
Category = Outside
ClipMode = Spot
PitchPanRate=30
HeadingPanRate=75
PanAcceleratorTime=0

[Cameradefinition.4]
Title=Locked Spot
Guid = {BCA3FDD1-FB83-4BBA-8407-4922A7F0D00D}
Description = This is the description of the spot view.
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = FlatChaseLocked
ShowAxis = No
AllowZoom = Yes
InitialZoom = 0.4
SmoothZoomTime = 2.0
ShowWeather = Yes
XyzAdjust = FALSE
Transition = Yes
ShowLensFlare=TRUE
Category = Outside
ClipMode = Spot
PitchPanRate=30
HeadingPanRate=75
PanAcceleratorTime=0
HotKeySelect=3

[Cameradefinition.5]
Title=FlyBy
Guid = {6B79DD49-9B4A-439D-BF40-ACBF157B0BA0}
Description = This is the description of the fly by view.
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = FlyBy
ShowAxis = No
AllowZoom = Yes
InitialZoom = 0.4
SmoothZoomTime = 2.0
ShowWeather = Yes
XyzAdjust = FALSE
Transition = No
ChaseDistance = 500
ChaseHeading = 15
ChaseAltitude = 10
ChaseTime = 20
ShowLensFlare=FALSE
Category = Outside
ClipMode = Tower

[Cameradefinition.6]
Title=Top-Down
Guid = {A2849229-938A-448f-8AC6-01EF2291C171}
Description = This is the description of the map or top down view.
Origin = Center
SnapPbhAdjust = Orthogonal
PanPbhAdjust = Orthogonal
Track = None
ShowAxis = Yes
AllowZoom = Yes
InitialZoom = 256
SmoothZoomTime = 2.0
ShowWeather = No
XyzAdjust = FALSE
Transition = No
ShowLensFlare=FALSE
Category = Outside
HotKeySelect=4

[Cameradefinition.7]
Title=Nearest Tower
Guid = {60BC0819-BD04-4AF6-8954-8FC8AA3545FF}
Description = This is the description of the tower view.
Origin = Tower
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = Track
ShowAxis = No
AllowZoom = Yes
InitialZoom = 0.4
SmoothZoomTime = 2.0
ShowWeather = Yes
XyzAdjust = FALSE
Transition = No
ShowLensFlare=FALSE
Category = Tower
ClipMode = Tower
NoSortTitle = True

[Cameradefinition.8]
Title=Facilities Tower
Guid = {AA8C80C0-9EE2-4284-A1C2-B20CD3F5F3D9}
Description = This is the description of the tower view.
Origin = Fixed
InstancedBased = Yes
SnapPbhAdjust = None
PanPbhAdjust = None
Track = Track
ShowAxis = No
AllowZoom = Yes
InitialZoom = 0.4
SmoothZoomTime = 2.0
ShowWeather = Yes
XyzAdjust = FALSE
Transition = No
ShowLensFlare=FALSE
Category = Tower
CycleHideRadius = 7
ClipMode = Tower

[Cameradefinition.9]
Title=Facilities Runway
Guid = {607C4520-CA6F-4135-AE10-8BF28838068F}
Description = This is the description of the runway view.
Origin = Virtual Cockpit
InstancedBased = Yes
SnapPbhAdjust = None
PanPbhAdjust = None
TargetCategory = Fixed
Track = TrackBank
ShowAxis = Yes
AllowZoom = Yes
InitialZoom = 0.4
SmoothZoomTime = 2.0
ShowWeather = Yes
XyzAdjust = FALSE
Transition = No
ShowLensFlare=FALSE
Category = Runway
CycleHideRadius = 7
ClipMode = Tower
CycleHidden=Yes

[Cameradefinition.10]
Title=Landing Gear
Guid = {96873AAD-621B-4C45-8A58-DEF7B7FCB051}
Description = View of the landing gear and left wing inboard flaps
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.4
ShowWeather = Yes
InitialXyz = -2.2, -1.2, -7
InitialPbh = 0, 0, 13
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[Cameradefinition.11]
Title=Tail
Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description = Looking forward from behind the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.4
ShowWeather = Yes
InitialXyz = 0, 7.5, -30.0
InitialPbh = 10, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[Cameradefinition.12]
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 = 0.4
ShowWeather = Yes
InitialXyz = 15.8, 0.7, 2.7
InitialPbh = 8, 0, 270
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum

[Cameradefinition.13]
Title=Left Wing
Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
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 = 0.4
ShowWeather = Yes
InitialXyz = -15.8, 0.7, 2.7
InitialPbh = 8, 0, 90
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = No
ClipMode=Minimum


[CAMERADEFINITION.WHEELCAM_1]
Title=Engine One
Guid={87F6923F-63E8-497D-ABC9-714A506B666E}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=40
HeadingPanRate=60
PanAcceleratorTime=0
InitialXYZ=-.306002,-.089383,.41602
Initialpbh=21.445312,0,-111.671875

[CAMERADEFINITION.WHEELCAM_2]
Title=Pilot
Guid={316E9DFD-7D01-40AF-BC66-17BF2ED8FEAC}
Description = 
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = 0.5
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=40
HeadingPanRate=60
PanAcceleratorTime=0
HotKeySelect=1
InitialXyz=0.0, 0.0, 0.0
InitialPbh=15, 0, 0

[CAMERADEFINITION.WHEELCAM_3]
Title=Engine Two
Guid={FAC97E2F-DD9B-480A-9489-13181457B548}
Description = 
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = 0.5
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=40
HeadingPanRate=60
PanAcceleratorTime=0
InitialXYZ=1.11878,-.235645,.424586
Initialpbh=15.996094,0,117.703125

[general]
atc_type=Douglas
atc_model=DC3
editable=0
performance="Cruise speed\n185 mph    161 kts	298 km/hr\n\nEngines\nTwo Pratt & Whitney R-1830s\n\nMaximum range\n1,845 nm	2,125 mi	3,420 km\n\nService ceiling\n23,200 ft	7,071 m\n\nFuel capacity\n604 gal	2,286 L\n\nEmpty weight\n16,145 lb	7,323 kg\n\nMaximum gross weight\n26,200 lb	11,884 kg\n\nLength\n65.5 ft	20 m\n\nWingspan\n95 ft	29 m\n\nHeight\n17 ft	5.18 m\n\nMaximum seating\n21 to 28\n\nUseful load\n10,055 lb	4,560 kg"
Category = airplane

[weight_and_balance]
// (feet) distance from FlightSim Reference position: (datum, centerline, waterline)

max_gross_weight = 26200                                          // (pounds)
empty_weight     = 17860  //=18200-340 16145   //(excl crew and incl utilities)   // (pounds)

reference_datum_position     =   20.00, 0, 0    //front of nose from mid CoG range at 19.5% MAC 251.3" = 20.94ft
empty_weight_CG_position     =  -21.00, 0, 0    //252" typical value from handbook of DC-3

max_number_of_stations =7

// 28 pax (165 lbs) 50% luggage and cargo max 40% fuel
//station_load.0  =  170,   -3.7,  -2.0,   0.0   //Weight, Lat, Lon, Vert Position
//station_load.1  =  170,   -3.7,   2.0,   0.0   //Weight, Lat, Lon, Vert Position
//station_load.2  = 1050,  -11.6,   0.0,   0.0   //Weight, Lat, Lon, Vert Position
//station_load.3  = 1320,  -18.9,   0.0,   0.0   //Weight, Lat, Lon, Vert Position
//station_load.4  = 1980,  -26.1,   0.0,   0.0   //Weight, Lat, Lon, Vert Position
//station_load.5  = 1320,  -33.5,   0.0,   0.0   //Weight, Lat, Lon, Vert Position
//station_load.6  =  450,  -48.4,   0.0,   0.0   //Weight, Lat, Lon, Vert Position

// 14 pax (165 lbs) 25% luggage and 30% cargo
station_load.0  =  170,   -3.7,  -2.0,   0.0   //Weight, Lat, Lon, Vert Position
station_load.1  =  170,   -3.7,   2.0,   0.0   //Weight, Lat, Lon, Vert Position
station_load.2  =  850,  -11.6,   0.0,   0.0   //Weight, Lat, Lon, Vert Position
station_load.3  =  660,  -18.9,   0.0,   0.0   //Weight, Lat, Lon, Vert Position
station_load.4  =  990,  -26.1,   0.0,   0.0   //Weight, Lat, Lon, Vert Position
station_load.5  =  660,  -33.5,   0.0,   0.0   //Weight, Lat, Lon, Vert Position
station_load.6  =  170,  -48.4,   0.0,   0.0   //Weight, Lat, Lon, Vert Position

station_name.0  = "Pilot"
station_name.1  = "Co-Pilot"
station_name.2  = "Forward Luggage"
station_name.3  = "Pax Row 1-2"
station_name.4  = "Pax Row 3-4-5"
station_name.5  = "Pax Row 6-7"
station_name.6  = "Rear Cargo"

CG_forward_limit=0.11
CG_aft_limit=0.28

empty_weight_pitch_MOI   =  90000
empty_weight_roll_MOI    = 160000
empty_weight_yaw_MOI     = 130000
empty_weight_coupled_MOI = 0.0

[Reference Speeds]
flaps_up_stall_speed    = 67.5                  //Knots Ind. (KIAS)
full_flaps_stall_speed  = 61.5                  //Knots Ind. (KIAS)
cruise_speed            = 140                   //Knots True (KTAS)
max_indicated_speed     = 224                   //Red line (KIAS)

[flight_tuning]
cruise_lift_scalar     = 1.0
parasite_drag_scalar   = 1.2 //compensation for higher prop efficienzy
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
p_factor_on_yaw          = 0.5
torque_on_roll           = 1.0
gyro_precession_on_yaw   = 1.0
gyro_precession_on_pitch = 1.0

[GeneralEngineData]
engine_type = 0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
//Engine.0 = -9.50, -9.1, -2.3                   //(feet) longitudinal, lateral, vertical distance from reference datum
//Engine.1 = -9.50,  9.1, -2.3                   //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.0 = -9.50, -11.3, -2.3                   //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -9.50,  11.3, -2.3                   //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 0.778 //adj. to 625 HP @5000 ft 80 USG/hr     //Fuel flow scalar
min_throttle_limit = 0.0                        //Minimum percent throttle.  Generally negative for turbine reverser
master_ignition_switch = 1                      //Master Ignition Switch

[piston_engine]
power_scalar = 0.946  /adjustment to 1200 HP    //Piston power scalar
cylinder_displacement= 130.71                   //Cubic inches per cylinder
compression_ratio= 6.7                          //Compression ratio
number_of_cylinders=14                          //Number of cylinders
max_rated_rpm= 2700                             //Max rated RPM
max_rated_hp= 1200                              //Max rated HP
fuel_metering_type= 1                           //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0                                 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.50                 //Starter torque factor
turbocharged= 1                                 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 48                               //Max design manifold pressure, (inHg)
min_design_mp= 10.0                             //Min design manifold pressure, (inHg)
critical_altitude= 7000                         //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
magneto_order_left_right_both = 1		//sets the order of the magneto switch direction

[propeller]
thrust_scalar = 1.5 // adjusted for SE perfomance   //Propeller thrust scalar
rotation=1,1 //Engine 1,2,3,... Rotation direction. 1 = CW, -1 = CCW
propeller_type= 0                               //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 11.53                       //Propeller Diameter, (feet)
propeller_blades= 3                             //Number of propeller blades
propeller_moi= 80 //40.2                        //Propeller moment of inertia
beta_max= 40.0                                  //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 17.4 //18.0 adjusted to 2100 RMP at 25" MAP                          //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1200                               //Miminum governed RPM
prop_tc= 0.002 //0.01                           //Prop time-constant
gear_reduction_ratio= 1.778                     //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= 89.5                              //Feathering pitch angle (degrees)
power_absorbed_cf= 0.9                          //Coefficient of friction for power absorbed by propeller in feather
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)
feathering_switches = 1                         //Switches which invoke feathering


[fuel]		// AMM TCDS 6a2
// standard fuel tank config: 804 gal
LeftMain =  -20.04,  -4.0, -2.5, 202.0,  4.0	// left fwd center
RightMain=  -20.04,   4.0, -2.5, 202.0,  4.0	// right fwd center
LeftAux=    -22.99,  -4.0, -2.5, 200.0,  9.0	// left aft center (aux)
RightAux=   -22.99,   4.0, -2.5, 200.0,  9.0	// right aft center (aux)
//tanks set with same distance fwd/bwd at main spar

// additional R4D8 wing tanks: 822 gal
// LeftTip=    -22.68,  -17.0, -2.1, 411.0,  2.0	// left outer wing
// RightTip=   -22.68,   17.0, -2.1, 411.0,  2.0	// right outer wing

fuel_type = 1                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 2                    
electric_pump=1
manual_pump=1					// simulates auxiliary fuel pumps

[airplane_geometry]
wing_area               = 987.0                 //Square feet
wing_span               = 95.0                  //Feet
wing_root_chord         = 11.50                  //Feet
wing_dihedral           = 5.0                   //Degrees
wing_incidence          = 2.0                   //Degrees
wing_twist              = -1.0                  //Degrees
oswald_efficiency_factor= 0.60                  //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 14.5 //14.5                  //Degrees, wing leading edge
wing_pos_apex_lon       = -13.30 //13.0         //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = -2.7                  //Feet, vertical distance from reference point, positive going up

htail_area              = 95.8                  //Square feet
htail_span              = 28.25                 //Feet
htail_pos_lon           = -52.7                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = -52.7                 //Feet, vertical distance from reference point, positive going up
htail_incidence         =  2.0                   //Degrees
htail_sweep             = 27.0                  //Degrees, horizontal tail leading edge

vtail_area              = 37.9                  //Square feet
vtail_span              = 11.49                 //Feet, tip to body
vtail_sweep             = 37.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -51.4                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 6.7                   //Feet, vertical distance from reference point, positive going up

elevator_area           = 83.4                  //Square feet
aileron_area            = 102.8                 //Square feet
rudder_area             = 46.7                  //Square feet
elevator_up_limit       = 20.0                  //Degrees
elevator_down_limit     = 20.0                  //Degrees
aileron_up_limit        = 20.0                  //Degrees
aileron_down_limit      = 14.0                  //Degrees
rudder_limit            = 15.0                  //Degrees
elevator_trim_limit     = 12.0                  //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  =  2.5               //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  = -1.0               //Design G load tolerance (negative, flaps up) 
negative_g_limit_flaps_down= -1.0               //Design G load tolerance (negative, flaps down) 
load_safety_factor         =  1.5               //Design G load safety factor 

[flaps.0]       //Trailing Edge Flaps system
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.5                                  // 0.0 .. 1.0
extending-time   = 10                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 11                                   // degrees
flaps-position.2 = 22                                   // degrees
flaps-position.3 = 33                                   // degrees
flaps-position.4 = 44                                   // degrees
damaging-speed   = 140                                  // KIAS
blowout-speed    = 175                                  // KIAS
lift_scalar = 1.0
drag_scalar = 0.0
pitch_scalar= 0.0
system_type = 1                                         //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None

[flaps.1]       //Trailing Edge Flaps lift
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.5                                  // 0.0 .. 1.0
extending-time   = 10                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 15                                   // degrees
flaps-position.2 = 30                                   // degrees
flaps-position.3 = 40                                   // degrees
flaps-position.4 = 45                                   // degrees
damaging-speed   = 130                                  // KIAS
blowout-speed    = 175                                  // KIAS
lift_scalar = 1.0
drag_scalar = 0.0
pitch_scalar= 0.0
system_type = 1                                         //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None

[flaps.2]       //Trailing Edge Flaps drag
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.5                                  // 0.0 .. 1.0
extending-time   = 10                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 10                                   // degrees
flaps-position.2 = 20                                   // degrees
flaps-position.3 = 32                                   // degrees
flaps-position.4 = 45                                   // degrees
damaging-speed   = 130                                  // KIAS
blowout-speed    = 175                                  // KIAS
lift_scalar = 0.0
drag_scalar = 1.0
pitch_scalar= 0.0
system_type = 1                                         //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None

[flaps.3]       //Trailing Edge Flaps pitch
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.5                                  // 0.0 .. 1.0
extending-time   = 10                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 10                                   // degrees
flaps-position.2 = 20                                   // degrees
flaps-position.3 = 32                                   // degrees
flaps-position.4 = 45                                   // degrees
damaging-speed   = 130                                  // KIAS
blowout-speed    = 175                                  // KIAS
lift_scalar = 0.0
drag_scalar = 0.0
pitch_scalar= 1.0
system_type = 1                                         //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None

[views]
eyepoint = -6.8, -1.2, 3.2

[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,  -55.75,   0.0, -2.80, 1200.0, 0, 0.93, 180.0, 0.10, 2.50, 0.30,    0,     0,   0,     0,     0 
point.0=1,  -55.75,   0.0, -2.80, 1200.0, 0, 0.93,  72.0, 0.10, 2.50, 0.30,    0,     0,   0,     0,     0 
point.1=1,  -18.50, -9.12, -9.95, 1600.0, 1, 1.89,   0.0, 0.54, 1.33, 0.50,  8.0,  11.0, 2.0, 166.0, 166.0
point.2=1,  -18.50,  9.12, -9.95, 1600.0, 2, 1.89,   0.0, 0.54, 1.33, 0.50,  7.5,  16.0, 3.0, 166.0, 166.0

point.3=2,  -27.75, -46.8,   1.1,  800.0, 0, 0.00,   0.0, 0.000, 0.0, 0.000,  0.0,  0.0, 5.0, 0.0, 0.0
point.4=2,  -27.75,  46.8,   1.1,  800.0, 0, 0.00,   0.0, 0.000, 0.0, 0.000,  0.0,  0.0, 6.0, 0.0, 0.0
point.5=2,  -62.75,   0.0,  13.0,  800.0, 0, 0.00,   0.0, 0.000, 0.0, 0.000,  0.0,  0.0, 9.0, 0.0, 0.0
point.6=2,   -4.00,   0.0,  -2.2,  800.0, 0, 0.00,   0.0, 0.000, 0.0, 0.000,  0.0,  0.0, 4.0, 0.0, 0.0
point.7=2,  -41.00,   0.0,  -2.2,  800.0, 0, 0.00,   0.0, 0.000, 0.0, 0.000,  0.0,  0.0, 4.0, 0.0, 0.0

static_pitch = 10.4
static_cg_height = 9.3
gear_system_type=1      //Hydraulic
tailwheel_lock = 1 


[exits]
number_of_exits = 4
exit_rate.0 = 0.3                               // Percent per second
exit_rate.1 = 0.3                               // Percent per second
exit_rate.2 = 100                               
exit_rate.3 = 100 

[lights]
//new MJ
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=taxi, 7=recognition, 8=wing, 9=logo, 10=cabin
//light.0 = 1,  -57.65,   0.00,  13.6, fx_beacon ,  //un-comment for c47_2 model
light.1 = 10,  -6.05,   -0.00,  2.5, fx_c47_vclight , 
light.2 = 10,  -20.00,   0.00,  3.28, fx_vclight ,
light.3 = 10,  -26.00,   0.00,  3.28, fx_vclight ,
light.4 = 10,  -32.00,   0.00,  3.28, fx_vclight ,
light.5 = 10,  -38.00,   0.00,  3.28, fx_vclight ,
light.6 = 2
light.7 = 3
light.8 = 5
light.9 = 4

[autopilot]
autopilot_available= 1
flight_director_available= 0
default_vertical_speed=500
autothrottle_available=0
pitch_takeoff_ga=0.0
direction_indicator=1
attitude_indicator =1
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
max_pitch_velocity_hi_alt_breakpoint=28000
max_bank=25.000000
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
yaw_damper_gain = 0.0
default_bank_mode=2     //Default to Heading Hold

[airspeed_indicators]
airspeed_indicator.0 = 1.0,0

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

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

[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
direction_indicator.1=2,0

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

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

[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
Adf.2         = 1
Transponder.1 = 0
Marker.1      = 1

[electrical]
// BusType, MaxAmpLoad, MinVoltage
// BusTypes: 0=MainBus, 1=AvionicsBus, 2=BatteryBus, 3=HotBatteryBus, 4-7=Generator/AlternatorBus(1-4)
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 100
engine_generator_map = 1,1
electric_always_available = 0

flap_motor=		0,  0,  0	// hydraulic
gear_motor=		0,  0,  0	// hydraulic
autopilot=		1,  5, 22
avionics_bus=		0, 20, 20
avionics=		1,  5, 22
pitot_heat=		0,  1, 20
additional_system=	0, 10, 20       // reduced for all other stuff
marker_beacon=		1,  2, 20
gear_warning=		0,  1, 20
fuel_pump=		0,  5, 20
starter1=		0, 20, 20
starter2=		0, 20, 20
starter3=		0,  0,  0
starter4=		0,  0,  0
light_nav=		0,  2, 20
light_beacon=		0,  2, 20
light_landing=		0,  5, 20
light_taxi=		0,  0,  0       // not existant
light_strobe=		0,  0,  0       // not existant
light_panel=		0,  5, 20
light_cabin=		0,  5, 20
prop_sync=		0,  5, 20
auto_feather=		0,  0,  0       // not existant
auto_brakes		0,  0,  0       // not existant
standby_vacuum=		0,  0,  0       // not existant
hydraulic_pump=		3,  0,  0	// simulates hydraulic hand pump
fuel_transfer_pump=	0,  0,  0       // not existant
propeller_deice=	0, 10, 20       // increased
light_recognition=	0,  0,  0       // not existant
light_wing=		0,  0,  0       // not existant
light_logo=		0,  0,  0       // not existant
directional_gyro=	0,  1, 20
directional_gyro_slaving= 0,  0,  0     // not existant

[Auxiliary Power Unit]
available = 1

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    =  0.0     //Flap angle that activates warning at idle
flap_limit_power   = 15.0     //Flap angle that activates warning at above idle

[stall_warning]
type=1
stick_shaker=0

[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 0.7  //Brake scalar
differential_braking_scale = 1.0        //Delta on the amount of brake when the rudder pedals deflected
auto_brakes = 0

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

[hydraulic_system]
normal_pressure = 1025.0	// should be 887.5   //PSI
electric_pumps  = 1		// simulates hand pump
engine_map      = 1,1,0,0   //pumps on Eng1,2

[pneumatic_system]
max_pressure=0.0

[vacuum_system]
max_pressure=5.25    //PSI
vacuum_type=1   //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi
engine_map=1,1
electric_backup_pressure=4.9

[effects]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
startup=fx_Cranky_DC3_TFF
touchdown=fx_tchdwn_s, 1

[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 = 120, 180
aileron  = 120, 180
rudder   = 120, 180

[forcefeedback]
ground_bumps_magnitude1=2600            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.6
ground_bumps_magnitude2=1200            ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.085
ground_bumps_slope2=0.65
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=3500000                 ; in microseconds