[fltsim.0]
title=P-38L (British)
sim=P-38L-5-LO
model=
panel=
sound=
texture=
KB_checklists=P-38L-5-LO_check

[WEIGHT_AND_BALANCE]
empty_weight=12264				// (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=19696
empty_weight_roll_MOI=16104
empty_weight_yaw_MOI=29242


[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
//rotation= -1,1		//Engine 1,2,3,... Rotation direction. 1 = CW, -1 = CCW

[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,   6.96,  0.00, -7.75, 1600, 0, 0.93, 37.7, 0.40, 2.5, 0.95, 2.5, 3.0, 0, 0, 152
point.1=1,  -3.20, -8.12, -6.75, 2200, 1, 1.40,  0.0, 0.55, 2.5, 0.75, 5.5, 5.0, 2, 0, 152
point.2=1,  -3.20,  8.12, -6.75, 2200, 2, 1.40,  0.0, 0.55, 2.5, 0.75, 6.5, 5.0, 3, 0, 152
point.3=2,   0.00,-26.25,  0.00, 1200, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5, 0,   0
point.4=2,   0.00, 26.25,  0.00, 1200, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6, 0,   0
point.5=2, -23.00,  0.00, -2.50, 1200, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9, 0,   0
point.6=2,   5.10,  0.00, -4.00, 1200, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4, 0,   0

static_cg_height=6.47		//(feet) altitude of CG when at rest (altitude when loaded on ground)
static_pitch=6.39		//degrees (pitch when loaded on ground)

[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=25					// degrees, KIAS
flaps-position.2=50					// degrees, KIAS
damaging-speed=191					// KIAS
blowout-speed=290					// KIAS

[Views]
eyepoint=1.5,0.000000,2.4

[LIGHTS]
panel=0.00, 0.10, 0.35, fx_vclight