[fltsim.0] title=CESSNA C152 NPI sim=CESSNA C152 model= panel= sound= texture= checklists=152Full_Checklist description=New Plymouth Aero Club, Cessna 152 (ZK-NPI). Repainted By Che Ridland ui_manufacturer=Cessna ui_type=C152 Sparrowhawk ui_variation=NPI atc_heavy=0 atc_id=NPI atc_airline= atc_flight_number= [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=1.000 PARASITE_DRAG_SCALAR=1.000 INDUCED_DRAG_SCALAR=1.000 ELEVATOR_EFFECTIVENESS=1.000 AILERON_EFFECTIVENESS=1.000 RUDDER_EFFECTIVENESS=1.000 PITCH_STABILITY=1.000 ROLL_STABILITY=1.000 YAW_STABILITY=1.000 ELEVATOR_TRIM_EFFECTIVENESS=0.702 AILERON_TRIM_EFFECTIVENESS=1.000 RUDDER_TRIM_EFFECTIVENESS=0.800 [PISTON_ENGINE] POWER_SCALAR=1.000 cylinder_displacement= 90.252 compression_ratio= 8.500 number_of_cylinders= 4 max_rated_rpm= 2550.000 max_rated_hp= 110.000 fuel_metering_type= 2 cooling_type= 0 normalized_starter_torque= 0.300 turbocharged= 0 max_design_mp= 0.000 min_design_mp= 0.000 critical_altitude= 0.000 emergency_boost_type= 0 emergency_boost_mp_offset= 0.000 emergency_boost_gain_offset= 0.000 fuel_air_auto_mixture= 0 auto_ignition= 0 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 [PROPELLER] THRUST_SCALAR=1.000 propeller_type= 0 propeller_diameter= 6.650 propeller_blades= 2 propeller_moi= 5.700 beta_max= 50.000 beta_min= 10.000 min_gov_rpm= 1400.000 prop_tc= 0.100 gear_reduction_ratio= 1.000 fixed_pitch_beta= 20.000 low_speed_theory_limit= 80.000 prop_sync_available= 0 prop_deice_available= 0 prop_feathering_available= 0 prop_auto_feathering_available= 0 min_rpm_for_feather= 0.000 beta_feather= 0.000 power_absorbed_cf= 0.000 defeathering_accumulators_available= 0 prop_reverse_available= 0 minimum_on_ground_beta= 0.000 minimum_reverse_beta= 0.000 [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= 975.000 reference_datum_position= 3.660, 0.000, 0.000 empty_weight_CG_position= -3.500, 0.000, 0.000 ;Moments of Inertia empty_weight_pitch_MOI= 1829.000 empty_weight_roll_MOI= 1208.000 empty_weight_yaw_MOI= 2439.000 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= 200.000, -3.080, 0.000, 0.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 1322.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [General] performance=Maximum Speed\t110 kts\nCruise Speed\t106 kts\nMaximum Range\t350 nm\nService Ceiling\t14,700 ft\nFuel Capacity\t24.5 U.S gal\nMax Gross Weight\t1,670 lb\nSeating\t\t2\nUseful Load\t589 lb\n\n\n atc_type=CESSNA atc_model=C152 [fuel] LeftMain= -3.910, -2.100, 2.500, 12.250, 0.000 RightMain= -3.910, 2.100, 2.500, 12.250, 0.000 fuel_type=1.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area= 165.000 wing_span= 33.333 wing_root_chord= 4.917 wing_dihedral= 2.499 wing_incidence= -0.253 wing_twist= -0.994 oswald_efficiency_factor= 0.642 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= -2.431 wing_pos_apex_vert= 0.000 htail_area= 35.000 htail_span= 10.000 htail_pos_lon= -18.327 htail_pos_vert= 0.000 htail_incidence= 3.246 htail_sweep= 0.000 vtail_area= 18.000 vtail_span= 4.837 vtail_sweep= 0.000 vtail_pos_lon= -16.243 vtail_pos_vert= 1.500 elevator_area= 16.610 aileron_area= 18.300 rudder_area= 6.650 elevator_up_limit= 28.000 elevator_down_limit= 20.999 aileron_up_limit= 19.996 aileron_down_limit= 15.000 rudder_limit= 23.995 elevator_trim_limit= 19.498 spoiler_limit= 0.000 spoilerons_available= 0 aileron_to_spoileron_gain= 0.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 [contact_points] point.0= 1.000, 1.840, 0.000, -4.167, 1574.803, 0.000, 0.509, 33.960, 0.300, 2.500, 0.700, 5.000, 5.000, 0.000, 0.000, 0.000 point.1= 1.000, -5.160, -5.000, -4.000, 1574.803, 1.000, 0.509, 0.000, 0.300, 2.500, 0.700, 5.000, 5.000, 2.000, 0.000, 0.000 point.2= 1.000, -5.160, 5.000, -4.000, 1574.803, 2.000, 0.509, 0.000, 0.300, 2.500, 0.700, 5.000, 5.000, 3.000, 0.000, 0.000 point.3= 2.000, -3.660, -17.917, 2.083, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4= 2.000, -3.660, 17.917, 2.083, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5= 2.000, -19.993, 0.000, 0.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6= 2.000, 1.340, 0.000, -1.333, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.7= 2.000, -19.993, 0.000, 6.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000 point.8= 2.000, -4.660, 0.000, -1.333, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000 static_pitch= 3.494 static_cg_height= 3.755 [GeneralEngineData] engine_type= 0 Engine.0= 2.340, 0.000, 0.000 fuel_flow_scalar= 1.000 [Reference Speeds] flaps_up_stall_speed= 48.000 full_flaps_stall_speed= 38.400 cruise_speed= 102.177 [keyboard_response] elevator=100.000000,180.000000 aileron=200.000000,1000.000000 rudder=200.000000,1000.000000 [Views] eyepoint=0.671734,-0.768947,1.384104 [autopilot] autopilot_available=0 flight_director_available=0 default_vertical_speed=700.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 [direction_indicators] direction_indicator.0=1,0 [Lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 4.88,-17.0, 2.40, fx_navred light.1=3, 4.88, 17.0, 2.40, fx_navgre light.2=3,-13.00, 0.0, 0.00, fx_navwhi light.3=2, 4.55,-17.0, 2.40, fx_strobe light.4=2, 4.55, 17.0, 2.40, fx_strobe light.5=1,-10.20, 0.0, 4.18, fx_beacon light.6=4, 3.27, 0.0, 1.40, fx_vclight [Efffects] dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [Direction_indicators] direction_indicator.0=1,0 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 7.000 system_type= 0 damaging-speed= 0.000 blowout-speed= 0.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 12.666, 0.000 flaps-position.2= 25.332, 0.000 flaps-position.3= 37.999, 0.000
