[fltsim.0]
title=F4U1-A Corsair Truly American
sim=F4U1A_Corsair
model=
panel=
sound=
texture=
KB_checklists=f4u1a_corsair_check

[WEIGHT_AND_BALANCE]
empty_weight = 8873				// (pounds)

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,  -3.0, 0.0, 3.0		//Pilot           Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI = 11059.0
empty_weight_roll_MOI  =  7243.0
empty_weight_yaw_MOI   = 14484.0


[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

[piston_engine]
power_scalar = 1.0

[propeller]
thrust_scalar = 1.0

[folding_wings]
wing_fold_system_type = 4			;0=None
fold_rates = 0.12,0.11				;Percent per second

[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

[TailHook]
tailhook_length=4				;(feet)
tailhook_position = -15.0, 0.0, -1.0		;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust = 1.0


[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, -18.00,   0.00, -3.35, 3200.0, 0, 0.50,180.0, 0.25, 2.5, 0.90, 1.0, 4.00, 0, 0, 200		//tail wheel
point.1= 1,   1.80,  -5.93, -7.65, 2200.0, 1, 1.35,  0.0, 0.54, 2.5, 0.76, 5.5, 4.50, 2, 0, 200     //left wheel
point.2= 1,   1.80,   5.93, -7.65, 2200.0, 2, 1.35,  0.0, 0.54, 2.5, 0.76, 5.5, 4.50, 3, 0, 200     //right wheel
point.3= 2,   0.00, -20.00, -1.25, 1200.0, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 5 	        //left wing
point.4= 2,   0.00,  20.00, -1.25, 1200.0, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 6 	        //Right wing
point.5= 2, -20.25,   0.00, -1.66, 2400.0, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 9 	        //tail
point.6= 2,   5.41,   0.00, -3.50, 1200.0, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 4 	        //belly
point.7= 2,   0.00,  -5.43, -3.75, 1200.0, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 5 	        //left gull
point.8= 2,   0.00,   5.43, -3.75, 1200.0, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.00, 6 	        //right gull

static_cg_height = 6.60		//(feet) altitude of CG when at rest (altitude when loaded on ground)
static_pitch     = 11.9		//degrees (pitch when loaded on ground)

[Views]
eyepoint= -6.2, 0.00, 3.55	//(feet) longitudinal, lateral, vertical distance from reference datum

[flaps.0]
type=1								// 1 - tail, 2 - lead
span-outboard=0.125					// 0.0 .. 1.0
extending-time=5					// seconds
flaps-position.0=0					// degrees, KIAS
flaps-position.1=16					// degrees, KIAS
flaps-position.2=32					// degrees, KIAS
flaps-position.3=48					// degrees, KIAS
flaps-position.4=64					// degrees, KIAS
flaps-position.5=80					// degrees, KIAS
damaging-speed=201					// KIAS
blowout-speed=305					// KIAS

[LSO]
LSOAdjustSpeed=1.2

[LIGHTS]
panel=0.00, 0.45, -2.00, fx_vclight