[fltsim.0]
title=152 #1
sim=SingleEngineProp
model=
panel=
panel_alias=c172\panel
sound=
sound_alias=c172\sound
texture=
kb_checklists=
kb_reference=
atc_id=N4BEN
ui_manufacturer=Cessna
ui_type=Cessna 152
ui_variation=
description=The first great nose wheel aircraft, the Cessna 152, was produced by the Cessna Comapny of Wichita, Kansas. This light, two seat trainer was very popular and continues to be very popular for recreation and training. Cruising up to 110KIAS with a sturdy Lycombing 110 HP, 4 stroke, air cooled engine it provided the safety and power people were looking for. The Cessna 152 carried 26 Gal. (24.5 Gal. Usable) and only burned appx. 6 Gal.\/ Hr. This planes design and cockpit have been borrowed, but the flight dynamics have been changed by a C152 Pilot, to bring you the closest to flying a real Cessna 152. Climb in, buck up, and enjoy the ride. Flight Dynamics by Bennett Gray United States
atc_heavy=0
atc_airline=
atc_flight_number=
[General]
atc_type=CESSNA
atc_model=152
performance=Maximum Speed\t120 kts\nCruise Speed\t110 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
[WEIGHT_AND_BALANCE]
max_gross_weight = 1670.000
empty_weight = 1081.000
reference_datum_position = 3.660, 0.000, 0.000
empty_weight_CG_position = -3.500, 0.000, 0.000
max_number_of_stations = 50
station_load.0 =200.000000, -3.080000, 0.000000, 0.000000, longitudinal
station_load.2 =0.000000, -6.200000, -1.500000, 0.000000, longitudinal
station_load.3 = 0, -6.2, 1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = 0, -8.0, 0.0, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 1829.000
empty_weight_roll_MOI = 1208.000
empty_weight_yaw_MOI = 2439.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
station_load.1=0.000000, 0.000000, 0.000000, 0.000000, Station 2
[flight_tuning]
cruise_lift_scalar =0.712
parasite_drag_scalar =0.851
induced_drag_scalar =0.790
elevator_effectiveness =0.972
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 =0.754
[GeneralEngineData]
engine_type = 0
Engine.0 = 2.340, 0.000, 0.000
fuel_flow_scalar= 1.000
min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser
[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=1.202
idle_rpm_friction_scalar=0.981
[propeller]
thrust_scalar =1.000
propeller_type= 1
propeller_diameter= 6.650
propeller_blades= 2
propeller_moi= 5.700
beta_max= 0.000
beta_min= 0.000
min_gov_rpm= 1400.000
prop_tc= 0.000
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= 0.000
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000
[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, 5 , 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 2 , 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
//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
[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, 0.000, 0.000, 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, 0.000, 0.000, 2.000, 0.000, 0.000
point.2 = 1.000, -4.760, 4.500, -4.050, 1574.803, 2.000, 0.509, 0.000, 0.300, 2.500, 0.700, 0.000, 0.000, 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
max_number_of_points = 21
static_pitch= 3.494
static_cg_height= 3.755
gear_system_type=0 //Electric
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 0.0 //Flap angle that activates warning at idle
flap_limit_power = 16.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.0 //Brake scalar
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,0,0,0 //pumps on Eng1
[Views]
eyepoint= -3.95, -0.85, 2.1 //(feet) longitudinal, lateral, vertical distance from reference datum
[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, 0
Adf.1 = 1
Transponder.1 = 1
Marker.1 = 1
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, -2.88, -18.11, 2.90, fx_navred
light.1 = 3, -2.88, 18.11, 2.90, fx_navgre
light.2 = 2, -3.15, -18.31, 2.90, fx_strobe
light.3 = 2, -3.15, 18.31, 2.90, fx_strobe
light.4 = 1, -20.60, 0.00, 6.18, fx_beacon
light.5 = 4, -2.27, 0.00, 1.40, fx_vclight
[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
elevator = 100, 180
aileron = 200, 1000
rudder = 200, 1000
[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
turn_indicator.0=1,1 //Turn AND Bank
direction_indicator.0=1,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
LeftMain = -3.910, -2.100, 2.500, 13.000, 0.750
RightMain = -3.910, 2.100, 2.500, 13.000, 0.750
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
[airplane_geometry]
wing_area = 200.000
wing_span = 34.000
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 = 18.000
aileron_area = 15.000
rudder_area = 6.650
elevator_up_limit = 25.890
elevator_down_limit = 19.890
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
[Reference Speeds]
flaps_up_stall_speed = 54.000
full_flaps_stall_speed = 43.200
cruise_speed = 129.000
max_indicated_speed= 140.000
[autopilot]
autopilot_available= 0
flight_director_available= 0
default_vertical_speed= 700.0
autothrottle_available= 0
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
pitch_takeoff_ga= 8.000
[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
[stall_warning]
type=1
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 7.000
system_type= 0
damaging-speed= 95.000
blowout-speed= 120.000
lift_scalar= 1.750
drag_scalar= 0.500
pitch_scalar= 0.500
flaps-position.0= 0.000, 0.000
flaps-position.1= 12.666, 0.000
flaps-position.2= 25.332, 0.000
flaps-position.3= 35.000, 0.000
