[fltsim.0]
title=ALPHA Cessna 170B
sim=ALPHA_C170B
model=
panel=
sound=
texture=
kb_checklists=cessna170_check
kb_reference=cessna170_ref
atc_id=G-AORB
ui_manufacturer=ALPHA
ui_type=Cessna 170B
ui_variation=G-AORB
description=© AlphaSim 2008\n\nThe Cessna 170 is a classic single-engined general aviation aircraft which was produced by Cessna between 1948 and 1956. Powered by a 145hp Continental engine, the 170 provides an exciting yet relaxed flying experience. The real G-AORB is one of only five 170Bs currently registered in the UK and dates from 1955. The Cessna 170 made its debut in 1948 and late in the same year the all metal Cessna 170A appeared still with straight wings. With the 170B the wings were given 3 degrees dihedral and this model was produced between 1952 and 1956. Typically, the aircaft cruises at 118 m.p.h. on 65% power at 4000-7000 feet and lands at 52 m.p.h. Two adults, two children in the rear and 100 lbs. of luggage can be accommodated.
atc_heavy=0
atc_airline=
atc_flight_number=
[General]
atc_type=CESSNA
atc_model=C170B
performance=Model: C Lampard\nTextures: C Lampard\nFlight Model: AlphaSim\n\nMaximum Speed\n126 kts 230 km\/hr\n\nCruise Speed\n105 kts 195 km\/hr\n\nEngine\nContinental O-300-A 145 bhp\n\nPropeller\nTwo-Bladed Macauley Fixed Pitch\n\nMaximum Range\n638 nm 734 mi 1181 km\n\nService Ceiling\n15,500 ft\t 4,724 m\n\nFuel Capacity\n56 gal\t 212 L\t \n\nEmpty Weight\n1,665 lb\t 1,002 kg\n\nMaximum Gross Weight\n2,550 lb\t 1,157 kg\n\nLength\n27 ft, 2 in 8.2 m\n\nWingspan\n36 ft, 1 in\t 11 m\n\nHeight\n8 ft, 11 in\t 2.72 m\n\nSeating\t 4\n\nUseful Load\n893 lb\t 405 kg\n
[WEIGHT_AND_BALANCE]
max_gross_weight = 2550.000
empty_weight = 1650.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.000, 0.000, 0.000
max_number_of_stations = 50
station_load.0 =170.000000, 0.000000, -1.500000, 0.000000, Pilot
station_load.1 =170.000000, 0.600000, 1.500000, 0.000000, Front Passenger
station_load.2 =0.000000, -2.600000, -1.500000, 0.000000, Rear Passenger
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 = 1400.000
empty_weight_roll_MOI = 1137.000
empty_weight_yaw_MOI = 2360.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[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 =5.000
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 =5.000
[GeneralEngineData]
engine_type = 0
Engine.0 = 7.000, 0.000, 0.000
fuel_flow_scalar= 0.880
min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser
[piston_engine]
power_scalar =1.000
cylinder_displacement= 82.000
compression_ratio= 8.500
number_of_cylinders= 6
max_rated_rpm= 2700.000
max_rated_hp= 145.000
fuel_metering_type= 0
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= 6.300
propeller_blades= 2
propeller_moi= 5.000
beta_max= 0.000
beta_min= 0.000
min_gov_rpm= 0.000
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, -16.550, 0.000, -0.640, 1500.000, 0.000, 0.500, 22.000, 0.250, 2.500, 0.700, 0.000, 0.000, 0.000, 0.000, 0.000
point.1 = 1.000, 1.780, -3.790, -4.650, 3500.000, 1.000, 0.500, 0.000, 0.400, 2.500, 0.900, 0.000, 0.000, 2.000, 0.000, 0.000
point.2 = 1.000, 1.780, 3.790, -4.650, 3500.000, 2.000, 0.500, 0.000, 0.400, 2.500, 0.900, 0.000, 0.000, 3.000, 0.000, 0.000
point.3 = 2.000, -1.000, -18.000, 3.000, 1800.000, 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, -1.000, 18.000, 3.000, 1800.000, 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, -15.200, 0.000, 0.750, 1800.000, 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, 5.000, 0.000, -1.500, 1800.000, 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, -19.200, 0.000, 5.830, 1800.000, 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, -1.300, 0.000, -2.000, 1800.000, 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= 12.000
static_cg_height= 3.410
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.68 //Brake scalar
[hydraulic_system]
normal_pressure = 0.0 //PSI
[Views]
eyepoint= -0.70, -0.85, 2.0 //(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 = 4, 1.0, -0.5, 1.0, 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
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=1,1 //Turn AND Bank
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
LeftMain = -3.900, -2.100, 2.500, 26.500, 0.000
RightMain = -3.900, 2.100, 2.500, 26.500, 0.000
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
[airplane_geometry]
wing_area = 174.000
wing_span = 36.200
wing_root_chord = 4.900
wing_dihedral = 1.700
wing_incidence = 1.500
wing_twist = -3.000
oswald_efficiency_factor= 0.680
wing_winglets_flag = 0
wing_sweep = 0.000
wing_pos_apex_lon = 0.000
wing_pos_apex_vert = 0.000
htail_area = 39.000
htail_span = 11.700
htail_pos_lon = -15.000
htail_pos_vert = 0.000
htail_incidence = 3.200
htail_sweep = 10.000
vtail_area = 18.000
vtail_span = 4.800
vtail_sweep = 40.000
vtail_pos_lon = -15.500
vtail_pos_vert = 0.000
elevator_area = 16.600
aileron_area = 18.300
rudder_area = 20.000
elevator_up_limit = 28.000
elevator_down_limit = 23.000
aileron_up_limit = 20.000
aileron_down_limit = 15.000
rudder_limit = 17.000
elevator_trim_limit = 13.000
spoiler_limit = 15.000
spoilerons_available = 1
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
[Reference Speeds]
flaps_up_stall_speed = 50.000
full_flaps_stall_speed = 43.000
cruise_speed = 105.000
max_indicated_speed = 140 //Red line (KIAS)
[autopilot]
autopilot_available= 1
flight_director_available= 0
default_vertical_speed= 700.0
autothrottle_available= 0
pitch_takeoff_ga=8.0
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 = 0.0
[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= 100.000
blowout-speed= 122.000
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= 32.000, 0.000
flaps-position.4= 38.000, 0.000
