[fltsim.0]
title=P-51D Duchess Arlene
sim=FDG-P51D V11b
model=
panel=
sound=
texture=

[WEIGHT_AND_BALANCE]
empty_weight=7635	// (lbs.)

reference_datum_position=0.0, 0, 0   // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0.0, 0, 0   // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50

station_load.0=170,  -2.09, 0.0, 0.5	//Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI=11442.32
empty_weight_roll_MOI=8056.44
empty_weight_yaw_MOI=15600.73


[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

[piston_engine]
power_scalar=1.0

[propeller]
thrust_scalar=1.0

[exits]
number_of_exits=1
exit_rate.0=0.4  				;Percent per second

[electrical]
max_battery_voltage=24.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=60.0

[contact_points]
	//0  Class
	//1  Longitudinal Position        (feet)
	//2  Lateral Position             (feet)
	//3  Vertical Position            (feet)
	//4  Impact Damage Threshold      (Feet Per Minute)
	//5  Brake Map 		          (0=None, 1=Left, 2=Right)
	//6  Wheel Radius	          (feet)
	//7  Steer Angle		  (degrees)
	//8  Static Compression           (feet)  (0 if rigid)
	//9  Max/Static Compression Ratio
	//10 Damping Ratio	          (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, -12.986,  0.00, -3.325,  5000, 0, 0.577, 90.0, 0.30, 2.5, 0.90, 5, 5, 0, 0, 150 //Tail Wheel
point.1=1, 3.7,  -5.855,  -7.4, 3600, 1, 1.66,   0.0, 0.45, 2.5, 0.83, 12.5, 15, 2, 0, 150 //Left Wheel
point.2=1, 3.7,   5.855,  -7.4, 3600, 2, 1.66,   0.0, 0.45, 2.5, 0.83, 12.5, 15, 2, 0, 150 //Right Wheel
point.3=2, 1.3,-17.856, -1,   1200, 0, 0.00,   0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5 //Left Wing Tip
point.4=2, 1.3, 17.856, -1,   1200, 0, 0.00,   0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6 //Right Wing Tip
point.5=2, -17.5, 0.00,  -3, 2400, 0, 0.00,   0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9 //Tail Contact Point
point.6=2,  8.9, 0.00,  -5,  1200, 0, 0.00,   0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4 //Nose Contact Point

static_cg_height = 6.17	 //(feet) altitude of CG when at rest (altitude when loaded on ground)
static_pitch     = 13.38 //degrees (pitch when loaded on ground)

[flaps.0]
type=1							// 1 - tail, 2 - lead
span-outboard=0.125					// 0.0 .. 1.0
extending-time=12					// seconds
flaps-position.0=0					// degrees, KIAS
flaps-position.1=11					// degrees, KIAS
flaps-position.2=22					// degrees, KIAS
flaps-position.3=32					// degrees, KIAS
flaps-position.4=43					// degrees, KIAS
damaging-speed=185					// KIAS
blowout-speed=250					// KIAS

[Views]
eyepoint=-1.2, 0.000000, 2.25 //(feet) longitudinal, lateral, vertical distance from reference datum

[LIGHTS]
panel=0.00, -1.5, 3.15, fx_vclight