[fltsim.0] title=CESSNA C152 NPH AEROBAT sim=CESSNA C152 Aerobat model= panel= sound= texture= checklists=152Full_Checklist description=New Plymouth Aero Club, Cessna 152 (ZK-NPH). Repainted By Che Ridland ui_manufacturer=Cessna ui_type=C152 Sparrowhawk ui_variation=NPH Aerobat atc_heavy=0 atc_id=NPH 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=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [Piston_engine] power_scalar=1.000 cylinder_displacement= 58.250 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= 1 propeller_diameter= 6.000 propeller_blades= 2 propeller_moi= 4.000 beta_max= 0.000 beta_min= 0.000 min_gov_rpm= 0.000 prop_tc= 0.100 gear_reduction_ratio= 1.000 fixed_pitch_beta= 43.900 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=Main,1=Avionics,2=Battery,3=HotBattery,4-7=Generator/Alternator(1-4) flap_motor=0, 5, 17.0 avionics_bus0, 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] Reference_datum_position= 0.000, 0.000, 0.000 Empty_weight_CG_position= -1.270, 0.000, 0.000 max_gross_weight= 1670.000 empty_weight= 1139.000 ;Moments of Inertia empty_weight_roll_MOI= 570.000 empty_weight_pitch_MOI= 808.000 empty_weight_yaw_MOI= 1119.000 empty_weight_coupled_MOI= 10.000 max_number_of_stations=5 ;Wgt (lbs), longitudinal, lateral, vertical positions from datum (ft) station_load.0= 170.000, -0.640, -0.860, 0.000 station_load.1= 170.000, -0.640, 0.860, 0.000 station_load.2=0,-3.00, 0.00,0.0 //Baggage (120 lb max) 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= -0.750, -2.750, 2.200, 13.000, 0.750 RightMain= -0.750, 2.750, 2.200, 13.000, 0.750 fuel_type=1.0 number_of_tank_selectors=1 [Airplane_geometry] wing_area= 159.500 wing_span= 33.167 wing_root_chord= 5.330 wing_dihedral= 1.000 wing_incidence= 1.000 wing_twist= -1.000 oswald_efficiency_factor= 0.750 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 1.310 wing_pos_apex_vert= 2.420 htail_area= 27.860 htail_span= 10.000 htail_pos_lon= -13.230 htail_pos_vert= 0.500 htail_incidence= 0.000 htail_sweep= 9.000 vtail_area= 18.000 vtail_span= 4.837 vtail_sweep= 30.000 vtail_pos_lon= -14.000 vtail_pos_vert= 0.500 elevator_area= 11.020 aileron_area= 15.010 rudder_area= 6.320 elevator_up_limit= 25.000 elevator_down_limit= 18.000 aileron_up_limit= 20.000 aileron_down_limit= 15.000 rudder_limit= 23.000 elevator_trim_limit= 23.000 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, 4.500, 0.000, -4.067, 1500.000, 0.000, 0.511, 34.000, 0.200, 2.500, 0.700, 0.000, 0.000, 0.000, 0.000, 0.000 point.1= 1.000, -2.500, -3.833, -3.900, 3000.000, 1.000, 0.511, 0.000, 0.300, 2.500, 0.700, 0.000, 0.000, 2.000, 0.000, 0.000 point.2= 1.000, -2.500, 3.833, -3.900, 3000.000, 2.000, 0.511, 0.000, 0.300, 2.500, 0.700, 0.000, 0.000, 3.000, 0.000, 0.000 point.3= 2.000, 0.000, -18.000, 2.250, 1574.000, 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, 0.000, 18.000, 2.250, 1574.000, 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, -16.300, 0.000, 0.833, 1574.000, 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, 5.900, 0.000, -1.333, 1574.000, 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, -16.300, 0.000, 6.833, 1574.000, 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, -1.000, 0.000, -1.333, 1574.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000 static_pitch= 2.000 static_cg_height= 3.700 [GeneralEngineData] engine_type= 0 Engine.0= 5.800, 0.000, 0.000 fuel_flow_scalar= 1.000 [Reference Speeds] flaps_up_stall_speed= 48.000 full_flaps_stall_speed= 43.000 cruise_speed= 107.000 [Keyboard_response] elevator=100.0,150.0 aileron=100.0,150.0 rudder=100.0,150.0 [Views] eyepoint=4.331734,-0.768947,1.384104 [Autopilot] autopilot_available=0 flight_director_available=0 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1,1 Com.2=1,1 Nav.1=1,1,1 Nav.2=1,1,1 Adf.1=1 Transponder.1=1 Marker.1=1 [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= 3.000 system_type= 3 damaging-speed= 74.000 blowout-speed= 100.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 10.000, 0.000 flaps-position.2= 20.000, 0.000 flaps-position.3= 30.000, 0.000