//v.1
//*************************************************************************************************
//REALAIR SIMULATIONS Cessna 172SP Flight Model and Textures commissioned
//by the Kangan Batman Tafe Aerospace Industry Training Centre,
//Melbourne, Australia. Copyright RealAir SImulations 2003 - all rights reserved
//This aircraft flight model and custom textures are the property of RealAir Simulations.
//You are granted a single user licence to use and enjoy this aircraft. This package must
//not be used for any commercial purpose, including flight school training, without the
//express and written permission of RealAir Simulations.
//This file and the accompanying .air file are digitally encrypted and can be traced. Copying,
//disassembling, or re-editing this flight model and or textures, or copying likeness or feel, is
//a breach of copyright and prohibited. This package may not be uploaded to any website without
//the written permission of RealAir SImulations.
//If you wish to add textures to this package please first write to us at www.realairsimulations.com
//and seek written permission.
//This aircraft should be flown with the general realism slider in the FS2002 aircraft/realism menu
//set to MAXIMUM (ie: fully right). This aircraft will only perform as we intended with this setting. With
//the realism slider set to Maximum you will be able to obtain up to 40 degrees side slip and spinning
//will be possible. Please see attached readme to this package for details.
//********************************************************************************************************
//Credits:
//Textures and Installer: Bill Womack
//Documentation: Sean Moloney
//Flight Model and custom sounds: Rob Young
//for and on behalf of RealAir SImulations
//Flight Testing:
//Greg Free on behalf of the Kangan TAFE Aerospace Industry Training Centre
//Stephen "Beach" Comer
//**********************************************************************************************************
[fltsim.0]
title=Cessna Skyhawk 172SP Kangan Batman TAFE by RealAir Simulations
sim=RealAirSimulationsC172SP
model=
panel=
sound=
texture=
kb_checklists=Cessna172SP_check
kb_reference=Cessna172SP_ref
atc_id=VH-KBT
atc_id_color=0xffffffff
ui_manufacturer=Cessna
ui_type=RealAir C172SP Skyhawk
ui_variation=Kangan Batman TAFE Training
description=Custom Livery and Flight Model by RealAir Simulations for The Aerospace Industry Training Department of the Kangan Batman TAFE Melbourne Australia. Copyright 2003 RealAir Simulations - All Rights Reserved.
atc_heavy=0
atc_airline=
atc_flight_number=
///RealAir 48767HGFHSSSUT28748927
[General]
atc_type=Cessna
atc_model=C172
editable=0
performance=Set General Realism Slider to Maximum!\nMaximum Speed\n126 kts 203 km\/hr\n\nCruise Speed\n124 kts 200 km\/hr\n\nEngine\nTextron Lycoming IO-360-L2A 180 bhp\n\nPropeller\nTwo-Bladed Macauley Fixed Pitch\n\nMaximum Range\n638 nm 734 mi 1181 km\n\nService Ceiling\n14,000 ft\t 4267 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 // (pounds)
empty_weight = 1650 // (pounds)
reference_datum_position = 3.6, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -3.4, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 190, -2.0, -1.5, 0.0 //Pilot (first value lbs weight)
station_load.1 = 190, -2.0, 1.5, 0.0 //Front Passenger
station_load.2 = 0.0, -6.2, -1.5, 0.0 //Rear Passenger
station_load.3 = 0.0, -6.2, 1.5, 0.0 //Rear Passenger
station_load.4 = 30, -8.0, 0.0, 0.0 //Baggage
;Moments of Inertia
empty_weight_pitch_MOI=2046.000
empty_weight_roll_MOI=1427.000
empty_weight_yaw_MOI=1280.000
empty_weight_coupled_MOI=0.000000
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.23
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[GeneralEngineData]
engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 2.4, 0.0, -0.15 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 1.0 //Fuel flow scalar
[piston_engine]
power_scalar = 1.01 //Piston power scalar
cylinder_displacement= 90.0 //Cubic inches per cylinder
compression_ratio= 8.5 //Compression ratio
number_of_cylinders=4 //Number of cylinders
max_rated_rpm= 2700 //Max rated RPM
max_rated_hp= 180 //Max rated HP
fuel_metering_type= 0 //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter
cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3 //Starter torque factor
turbocharged= 1 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 24.3 //Max design manifold pressure, (inHg)
min_design_mp= 1 //Min design manifold pressure, (inHg)
critical_altitude= 6000
emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.15 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 0.9 //Scalar on idle RPM friction
[propeller]
thrust_scalar = 1.166 //Propeller thrust scalar
propeller_type= 1 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 6.3 //Propeller Diameter, (feet)
propeller_blades= 2 //Number of propeller blades
propeller_moi= 3.0 //Propeller moment of inertia
beta_max= 0 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 0 //Miminum governed RPM
prop_tc= 0.01 //Prop time-constant
gear_reduction_ratio= 1.0 //Propeller gear reduction ratio
fixed_pitch_beta= 20.1 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit= 80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available= 0 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available= 0 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 0 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather= 0 //Minimum RPM for prop feathering
beta_feather= 0 //Feathering pitch angle (degrees)
power_absorbed_cf= 0 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available= 0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta= 0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0 //Minimum pitch angle in reverse, (degrees)
///RealAir 48767HGFHSSSUT28748927
[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
//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, 1.20, 0.00, -4.20, 1500, 0, 0.5, 30.0,0.25, 2.5, 0.5, 0.0, 0.0, 0
point.1 = 1, -4.70, -4.50, -3.95, 3500, 1, 0.5, 0.0, 0.30, 2.5, 0.7, 0.0, 0.0, 2
point.2 = 1, -4.70, 4.50, -3.95, 3500, 2, 0.5, 0.0, 0.30, 2.5, 0.7, 0.0, 0.0, 3
point.3 = 2, -3.90, -18.0, 3.00, 1800, 0, 0.0, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 5
point.4 = 2, -3.90 18.0, 3.00, 1800, 0, 0.0, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 6
point.5= 2,-20.23, 0.0, 0.30, 1800, 0, 0.0, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 9
point.6= 2, 1.48, 0.0, -2.17, 1800, 0, 0.0, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 4
point.7= 2,-22.80, 0.0, 5.83, 1800, 0, 0.0, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 7
point.8= 2, -4.90, 0.0, -2.00, 1800, 0, 0.0, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 8
max_number_of_points = 21
static_pitch=3.02 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=3.765 //feet, altitude of CG when at rest on the ground
[Views]
eyepoint= -4.3, -0.85, 2.2 //(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
direction_indicator.0=1,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
LeftMain = -3.9, -2.1, 2.5, 26.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -3.9, 2.1, 2.5, 26.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
///RealAir 48767HGFHSSSUT28748927
[airplane_geometry]
wing_area = 174.0 //Square feet
wing_span = 36.1 //Feet
wing_root_chord = 4.9 //Feet
wing_dihedral = 1.7 //Degrees
wing_incidence = 1.97 //Degrees
wing_twist = -3.0 //Degrees
oswald_efficiency_factor= 0.68 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 0 //Degrees, wing leading edge
wing_pos_apex_lon = -2.4 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_area = 39.0 //Square feet
htail_span = 11.7 //Feet
htail_pos_lon = -18.3 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence = 2.2 //Degrees 1.2
htail_sweep = 10.0 //Degrees, horizontal tail leading edge
vtail_area = 18.0 //Square feet
vtail_span = 4.8 //Feet, tip to body
vtail_sweep = 40.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -16.2 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 1.5 //Feet, vertical distance from reference point, positive going up
elevator_area = 16.6 //Square feet
aileron_area = 18.3 //Square feet
rudder_area = 6.7 //Square feet
elevator_up_limit = 28.0 //Degrees
elevator_down_limit = 22.0 //Degrees
aileron_up_limit = 20.0 //Degrees
aileron_down_limit = 15.0 //Degrees
rudder_limit = 21.0 //Degrees
elevator_trim_limit = 19.5 //Degrees
spoiler_limit = 0.0 //Degrees
spoilerons_available = 0 //Spoilerons Available?
aileron_to_spoileron_gain = 0 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
[flaps.0] //Trailing Edge Flaps
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 7 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 12 // degrees
flaps-position.2 = 20 // degrees
flaps-position.3 = 30 // degrees
damaging-speed = 120 // KIAS
blowout-speed = 150 // KIAS
lift_scalar = 1.0
drag_scalar = 0.9
pitch_scalar= 1.0
system_type = 0 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None
[Reference Speeds]
flaps_up_stall_speed = 48.0 // Indicated Airspeed at 500 feet
full_flaps_stall_speed = 42.0 // Indicated Airspeed at 500 feet
cruise_speed = 124.0
[autopilot]
autopilot_available= 1
flight_director_available= 0
default_vertical_speed= 720.0
autothrottle_available= 0
pitch_takeoff_ga=8.000000
[forcefeedback]
gear_bump_nose_magnitude=2000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=2000 ; 0 - 10000
gear_bump_left_direction=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2000 ; 0 - 10000
gear_bump_right_direction=00500 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=1250 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=350 ; 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
///RealAir 48767HGFHSSSUT28748927
