//FSX Cessna 177RG ... Brett Henderson 2007
[fltsim.0]
title=Cessna 177RG
sim=c177rg
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=N177MJ
ui_manufacturer="Cessna"
ui_type="Cardinal"
ui_variation="White, Green"
ui_typerole="Single Engine Prop"
ui_createdby="Brett Henderson"
description="Cessna's one-time replacement for the 172."
[General]
atc_type=Cessna
atc_model=c177rg
editable=0
performance="Maximum Speed\t\n155 kts 178 mph\t287 kmh\n\nCruise Speed\t\n130 kts 150 mph \t240 kmh\n\nEngine\t\nTextron Lycoming IO-360-1AB6 200 hp\n\nPropeller\t\nThree-bladed McCauley constant speed\n\nMaximum Range\t\n550 nm 630 sm \t1,015 km\n\nService Ceiling\t\n13,000 ft 4,000 m\n\nFuel Capacity\t\n60 U.S. gal 227 L \n\nEmpty Weight\t\n1,770 lb \t 803 kg\n\nMaximum Gross Weight\t\n2,810 lb \t 1,275 kg\n\nUseful Load\t\n1,040 lb \t 472 kg\n\nLength\t\n27.75 ft\t 8.45 m\n\nWingspan\t\n35.5 ft\t 10.8 m\n\nHeight\t\n8.33 ft\t 2.5 m\n\nSeating\t\nUp to 4"
Category = airplane
[CameraDefinition.0]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = 9.0, 0.3, 0.0
InitialPbh = 5, 0, 275
XyzAdjust = TRUE
Category=Aircraft
CycleHidden=Yes
ClipMode=Minimum
[CameraDefinition.1]
Title = "Left Wing"
Guid = {3A09FD6C-D406-4d8f-A5CD-FA4F5E0C12ED}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = -9.0, 0.3, 0.0
InitialPbh = 5, 0, 85
XyzAdjust = TRUE
Category=Aircraft
CycleHidden=Yes
ClipMode=Minimum
[CameraDefinition.2]
Title = "Tail"
Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64A}
Description = Looking forward from the tip of the vertical stabilizer
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.60
ShowWeather = Yes
InitialXyz = 0, 2.0, -8.5
InitialPbh = 10, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.001]
Title = "Right Seat"
Guid = {195EAB58-9E4A-1E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.75
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
CycleHidden=Yes
InitialXyz=0.45, -0.02, 0.0
InitialPbh=0, 0, 0
[WEIGHT_AND_BALANCE]
max_gross_weight = 2810 // (pounds)
empty_weight = 1770 // (pounds)
reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0, 0, -0.8 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 170, 0.8, -1.25, 0.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170, 0.8, 1.25, 0.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = 000, -2.25, -1.25, 0.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = 000, -2.25, 1.25, 0.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = 33, -5.6, 0.0, 0.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.0 = "Pilot"
station_name.1 = "Front Passenger"
station_name.2 = "Rear Passenger"
station_name.3 = "Rear Passenger"
station_name.4 = "Baggage"
;Moments of Inertia
empty_weight_pitch_MOI = 6306
empty_weight_roll_MOI = 5831
empty_weight_yaw_MOI = 3932
empty_weight_coupled_MOI = 0.0
[pitot_static]
vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat = 1.0 //Scalar on heat effectiveness, 0 = not available
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
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 = 6.89, 0.0, -1.4 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 1.0 //Fuel flow scalar
min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser
[piston_engine]
power_scalar = 1.1 //Piston power scalar
cylinder_displacement= 90.3 //Cubic inches per cylinder
compression_ratio= 8.0 //Compression ratio
number_of_cylinders=4 //Number of cylinders
max_rated_rpm= 2700 //Max rated RPM
max_rated_hp= 200 //Max rated HP
fuel_metering_type= 0 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3 //Starter torque factor
turbocharged= 0 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 32 //Max design manifold pressure, (inHg)
min_design_mp= 1 //Min design manifold pressure, (inHg)
critical_altitude= 13000 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
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= 1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction
[propeller]
thrust_scalar = 1.13 //Propeller thrust scalar
propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 6.1 //Propeller Diameter, (feet)
propeller_blades= 3 //Number of propeller blades
propeller_moi= 8.0 //Propeller moment of inertia
beta_max= 43 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 15 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1100 //Miminum governed RPM
prop_tc= 0.1 //Prop time-constant
gear_reduction_ratio= 1.0 //Propeller gear reduction ratio
fixed_pitch_beta= 0 //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= 1 //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)
[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, 6.80, 0.0, -5.37, 1181.1, 0, 0.470, 33.66, 0.12, 2.0, 0.78, 4.0, 4.0, 0, 130.0, 145.0
point.1=1, -1.00, -3.9, -5.39, 1574.8, 1, 0.523, 0.00, 0.17, 2.5, 0.6, 4.7, 4.7, 2, 130.0, 145.0
point.2=1, -1.00, 3.9, -5.39, 1574.8, 2, 0.523, 0.00, 0.17, 2.5, 0.6, 5.2, 5.2, 3, 130.0, 145.0
point.3=2, 0.00, -17.7, 0.59, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, 0.00, 17.7, 0.59, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -16.97, 0.0, -2.55, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, 8.96, 0.0, -1.60, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 4, 0.0, 0.0
point.7=2, -18.57, 0.0, 3.03, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 7, 0.0, 0.0
point.8=2, -0.00, 0.0, -3.88, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 8, 0.0, 0.0
max_number_of_points = 21
static_pitch = 0.0
static_cg_height = 5.39
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
auto_brakes = 0
[hydraulic_system]
normal_pressure = 0.0 //PSI
[Views]
eyepoint = 0.28, -.818,-0.48
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, 0.502, -17.582, 0.676, fx_navred
light.1 = 3, 0.502, 17.582, 0.676, fx_navgre
light.2 = 2, 0.364, -17.69, 0.676, fx_strobe
light.3 = 2, 0.364, 17.69, 0.676, fx_strobe
light.4 = 1, -16.165, 0.00, 3.087, fx_beacon
light.5 = 4, 1.00, 0.00, 0.00, fx_vclight
light.6 = 5, 7.457, -0.436, -2.234, fx_navwhih
light.7 = 6, 7.457, 0.436, -2.234, fx_navwhih
[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 7.000
system_type= 0
damaging-speed= 120.000
blowout-speed= 135.000
lift_scalar= 1.2000
drag_scalar= 0.8
pitch_scalar= 0.8
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.0, 0.000
flaps-position.2= 20.0, 0.000
flaps-position.3= 30.0, 0.000
[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
[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
[altimeters]
altimeter.0=1
altimeter.1=1
[airspeed_indicators]
airspeed_indicator.0=1
airspeed_indicator.1=1
[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
attitude_indicator.1 = 2
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,1 //Turn AND Bank
[vacuum_system]
max_pressure=5.15 //PSI
vacuum_type=1 //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi
electric_backup_pressure=4.9 //PSI
engine_map=1
[pneumatic_system]
max_pressure=0.000000
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
LeftMain = -1.00, -6.1, -0.8, 30.5, 0.51 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -1.00, 6.1, -0.8, 30.5, 0.51 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
[airplane_geometry]
wing_area = 174.0 //Square feet
wing_span = 35.66 //Feet
wing_root_chord = 5.38 //Feet
wing_dihedral = 2.0 //Degrees
wing_incidence = -2.6 //Degrees
wing_twist = -0.0 //Degrees
oswald_efficiency_factor= 0.6 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 0.0 //Degrees, wing leading edge
wing_pos_apex_lon = 0.0 //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 = 34.0 //Square feet
htail_span = 11.65 //Feet
htail_pos_lon = -14.78 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = -2.297 //Feet, vertical distance from reference point, positive going up
htail_incidence = 0.0 //Degrees
htail_sweep = 0.0 //Degrees, horizontal tail leading edge
vtail_area = 10.0 //Square feet
vtail_span = 3.6 //Feet, tip to body
vtail_sweep = 20.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -15.1 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = -1.0 //Feet, vertical distance from reference point, positive going up
elevator_area = 16.6 //Square feet
aileron_area = 18.3 //Square feet
rudder_area = 4.8 //Square feet
elevator_up_limit = 28.0 //Degrees
elevator_down_limit = 21.0 //Degrees
aileron_up_limit = 20.0 //Degrees
aileron_down_limit = 15.0 //Degrees
rudder_limit = 19.0 //Degrees
elevator_trim_limit = 19.5 //Degrees
spoiler_limit = 00.0 //Degrees
spoiler_extension_time = 0.00 //Seconds
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
auto_spoiler_available = 0
positive_g_limit_flaps_up = 4.0 //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down= 2.0 //Design G load tolerance (positive, flaps down)
negative_g_limit_flaps_up = -1.5 //Design G load tolerance (negative, flaps up)
negative_g_limit_flaps_down= -1.5 //Design G load tolerance (negative, flaps down)
load_safety_factor = 1.5 //Design G load safety factor
[Reference Speeds]
flaps_up_stall_speed = 66.0 //Knots True (KTAS)
full_flaps_stall_speed = 52.8 //Knots True (KTAS)
cruise_speed = 130.0 //Knots True (KTAS)
max_indicated_speed = 165 //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=3000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=2700 ; 0 - 10000
gear_bump_left_direction=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=00500 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=1300 ; 0 - 10000
ground_bumps_angle1=08900 ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200 ; 0 - 10000
ground_bumps_angle2=09100 ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
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
[exits]
number_of_exits = 2
exit.0 = 0.4 // (0=Main 1=Passenger)
exit.1 = 0.4 // (0=Main 1=Passenger)
[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=0 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots
