[FLTSIM.0]
TITLE=CESSNA C152 XB-PCM
SIM=CESSNA C152
MODEL=
PANEL=
SOUND=
TEXTURE=
KB_CHECKLISTS=152Full_Checklist
KB_REFERENCE=
ATC_TYPE=CESSNA
ATC_ID_ENABLE=0
ATC_ID=MCV
EDITABLE=1


[FORCEFEEDBACK]
GEAR_BUMP_NOSE_MAGNITUDE=6000		; 0 - 10000
GEAR_BUMP_NOSE_DIRECTION=18000		; 0 - 35999 DEGREES
GEAR_BUMP_NOSE_DURATION=250000		; IN MICROSECONDS
GEAR_BUMP_LEFT_MAGNITUDE=6000		; 0 - 10000
GEAR_BUMP_LEFT_DIRECTION=35500		; 0 - 35999 DEGREES
GEAR_BUMP_LEFT_DURATION=250000		; IN MICROSECONDS
GEAR_BUMP_RIGHT_MAGNITUDE=6000		; 0 - 10000
GEAR_BUMP_RIGHT_DIRECTION=00500		; 0 - 35999 DEGREES
GEAR_BUMP_RIGHT_DURATION=250000		; IN MICROSECONDS
GROUND_BUMPS_MAGNITUDE1=3250		; 0 - 10000
GROUND_BUMPS_ANGLE1=8900		; 0 - 35999 DEGREES
GROUND_BUMPS_INTERCEPT1=5.0
GROUND_BUMPS_SLOPE1=0.48
GROUND_BUMPS_MAGNITUDE2=750		; 0 - 10000
GROUND_BUMPS_ANGLE2=9100		; 0 - 35999 DEGREES
GROUND_BUMPS_INTERCEPT2=0.075
GROUND_BUMPS_SLOPE2=1.0
CRASH_MAGNITUDE1=10000			; 0 - 10000
CRASH_DIRECTION1=01000			; 0 - 35999 DEGREES
CRASH_MAGNITUDE2=10000			; 0 - 10000
CRASH_DIRECTION2=9000			; 0 - 35999 DEGREES
CRASH_PERIOD2=75000			; IN MICROSECONDS
CRASH_DURATION2=2500000			; IN MICROSECONDS

[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=0.7
AILERON_TRIM_EFFECTIVENESS=1.0
RUDDER_TRIM_EFFECTIVENESS=0.8

[PISTON_ENGINE]
POWER_SCALAR=1.00

[PROPELLER]
THRUST_SCALAR=1.00

[GROUND_REACTION]
MAIN_GEAR_STATIC_COMPRESSION=0.3		// (FEET), THE DISTANCE THE MAIN GEAR STRUT IS COMPRESSED WHEN AT REST ON THE GROUND
CENTER_GEAR_STATIC_COMPRESSION=0.3            // (FEET), THE DISTANCE THE CENTER GEAR STRUT IS COMPRESSED WHEN AT REST ON THE GROUND
MAIN_GEAR_DAMPING_RATIO=0.7		// MAIN GEAR STRUT DAMPING, 0 = UNDAMPED OSCIALLATIONS, 1 = CRITICALLY DAMPED
CENTER_GEAR_DAMPING_RATIO=0.7		// CENTER GEAR STRUT DAMPING, 0 = UNDAMPED OSCIALLATIONS, 1 = CRITICALLY DAMPED

[ELECTRICAL]
;BUSTYPE, MAXAMPLOAD, MINVOLTAGE       BUSTYPES:0=MAINBUS,1=AVIONICSBUS,2=BATTERYBUS,3=HOTBATTERYBUS,4-7=GENERATOR/ALTERNATORBUS(1-4)
FLAP_MOTOR=0, 5 , 17.0
GEAR_MOTOR=0, 5 , 17.0
AUTOPILOT=0, 5 , 17.0
AVIONICS_BUS=0, 10, 17.0
AVIONICS=1, 5 , 17.0
PITOT_HEAT=0, 2 , 17.0
ADDITIONAL_SYSTEM=0, 20, 17.0
MARKER_BEACON=1, 2 , 17.0
GEAR_WARNING=0, 2 , 17.0
FUEL_PUMP=0, 5 , 17.0
STARTER1=0, 20, 17.0
LIGHT_NAV=0, 5 , 17.0
LIGHT_BEACON=0, 5 , 17.0
LIGHT_LANDING=0, 5 , 17.0
LIGHT_TAXI=0, 5 , 17.0
LIGHT_STROBE=0, 5 , 17.0
LIGHT_PANEL=0, 5 , 17.0

[WEIGHT_AND_BALANCE]
empty_weight=975		// (pounds)

reference_datum_position=3.66, 0, 0	// (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-3.50, 0, 0       // (feet) longitudinal, lateral, vertical distance from specified datum

;Moments of Inertia
empty_weight_pitch_MOI=1829.0
empty_weight_roll_MOI=1208.0
empty_weight_yaw_MOI=2439.0


MTW = 1600 //
MLW = 1600 // 
empty_weight = 960// 
Orginal_empty_weight = 960 // 
Total_Weight = 1170 //
Fuel_Capacity = 135 // 
Cargo_Capacity = 10 //
1Class_Pax = 0 // 
2Class_Pax = 0 // 
3Class_Pax = 0 // 
max_number_of_stations = 2
station_load.0 = 200, -3.08, 0, 0.0		//Pilot           Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)