[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