[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