//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