[fltsim.0]
title=I-16 Ishak Tip 6 "Lieutenant Wang Shou-Chang, 26th PS, CAF, Hankou area, China, 3rd August 1938"
sim=I16_Ishak_Tip6
Model=EarlyBuild
panel=EarlyBuild
sound=
texture=CAF
checklists=I16_Ishak_Tip6_Check

[fltsim.1]
title=I-16 Ishak Tip 6 "Pilot unknown, Baltic Fleet, USSR, August 1941"
sim=I16_Ishak_Tip6
Model=
panel=
sound=
texture=USSR50
checklists=I16_Ishak_Tip6_Check

[fltsim.2]
title=I-16 Ishak Tip 6 "Pilot unknown, FAF Captured, Rompotti, Finland, March 1943"
sim=I16_Ishak_Tip6
Model=FAFCaptured
panel=FAFCaptured
sound=
texture=FAFIR101
checklists=I16_Ishak_Tip6_Check


[WEIGHT_AND_BALANCE]
empty_weight=2775				// (pounds)

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

max_number_of_stations=50

station_load.0=170,  -4.8, 0.0, 1.5		//Pilot           Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI=1327.71
empty_weight_roll_MOI=1293.98
empty_weight_yaw_MOI=2182.31


[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, -13.12,  0.00, -1.82, 3200, 0, 0.30,180.0, 0.30, 2.5, 0.90, 3.0, 3.0, 0, 0, 235
point.1=1,   1.06, -3.44, -5.82, 2200, 1, 1.36,  0.0, 0.45, 2.5, 0.83, 4.5, 4.5, 2, 0, 235
point.2=1,   1.06,  3.44, -5.82, 2200, 2, 1.36,  0.0, 0.45, 2.5, 0.83, 4.5, 4.5, 3, 0, 235
point.3=2,   0.00,-15.75,  3.67, 1200, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5
point.4=2,   0.00, 15.75,  3.67, 1200, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6
point.5=2, -17.40,  0.00,  0.28, 2400, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9
point.6=2,   4.67,  0.00, -2.19, 1200, 0, 0.00,  0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4

static_cg_height =  4.98 //(feet) altitude of CG when at rest (altitude when loaded on ground)
static_pitch     = 16.87 //degrees (pitch when loaded on ground)


[Views]
eyepoint=-5.22125984,0.00000000,2.55905512	//(feet) longitudinal, lateral, vertical distance from reference datum


[LIGHTS]
panel=0.00, 0.70, -0.80, fx_vclight