[fltsim.0]
title=Cessna 177RG EC-JAS
sim=Cessna 177RG Cardinal
model=
panel=
sound=
texture=
checklists=

kb_reference=DF177RG_REF
atc_id=N33267
atc_airline=
atc_flight_number=
atc_heavy=0
ui_manufacturer=cessna
ui_type=C177 RG FREEWARE
ui_variation=EC-JAS
visual_damage=0
description=DreamFleet 1978 Cessna 177RG Cardinal - Copyright 2002-2003 by DreamFleet 2000 & Flight One Software. Development Team: Louis Betti, Elmar Calbo, Ron Friemuth, Nick Jacobs, Tom Main, Mikko Maliniemi, Aaron Swindle, Fraser Turner. With Special thanks to Keith Peterson of Cardinal Flyers On Line.



[General]
atc_type=Cessna
atc_model=C175  //Required by FS2002 for Cardinal ID (C177)
editable=0
performance=Standard RG: Maximum Cruise Speed\t\n156 kts            180 mph\t288 km\/h\n\nNormal Cruise Speed\t\n148 kts            171 mph \t274 km\/h\n\nEngine\t\nTextron Lycoming IO-360-A1B6D     200 hp\n\nPropeller\t\nTwo-blade McCauley constant speed\n\nMaximum Range No Reserve\t\n888 nm          1080 sm \t1,644 km\n\nService Ceiling\t\n17,100 ft \t       5,211 m\n\nFuel Capacity\t\n61 U.S. gal      231 L \n\nEmpty Weight\t\n1,643 lb \t        866 kg\n\nMaximum Gross Weight\t\n2,800 lb \t        1,269 kg\n\nLength\t\n27.3 ft\t        8.27 m\n\nWingspan\t\n35.5 ft\t        10.8 m\n\nHeight\t\n8.6 ft\t        2.6 m\n\nSeating\t\nUp to 4 \n\nUseful Load\t\n857 lb  \t         389 kg



;*******************************************************************************************
[Views]
eyepoint=-8.3, -0.9, 1.45 

//Longitudinal, Lateral, Vertical (feet)    

;*******************************************************************************************

[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit    
light.0=3,  -8.05,  -17.80,   2.4,  fx_navred
light.1=3,  -8.05,   17.80,   2.4,  fx_navgre
light.2=2,  -8.25,  -18.11,   2.4,  fx_strobe
light.3=2,  -8.25,   18.11,   2.4,  fx_strobe
light.4=1, -23.15,    0.00,   6.0,  fx_beacon
light.5=4,  -8.15,    0.00,   0.00, fx_vclight_df177  
light.6=2, -16.55,    0.00,  -1.4,  fx_strobe

;*******************************************************************************************


[Weight_and_Balance]
max_gross_weight=2800   //2x00 Utility
empty_weight=1765   //1643
;61 gallons fuel: 366 lb
;fueled weight:  2131 lb
;payload & extra: 669 lb
;Useful load: 633 - 1035 lb

empty_weight_roll_MOI=1137.0
empty_weight_pitch_MOI=1400.0
empty_weight_yaw_MOI=2360.0
empty_weight_coupled_MOI=0.0


//                        long,  lat, vert distance from specified datum
reference_datum_position=8.35, 0.00, 0.00  //-100.2" (54" fwd firewall)
empty_weight_CG_position=-8.57, 0.00, 0.00  //-102.8"; -8.35 -100.2"

;Seats: 2 at +93"(90"-97") (7.75 ft), 2 at +134" (11.17 ft)
;Baggage: 120 lb at 162" (13.5 ft)
;25% MAC: 9.083 ft, 109"
;CoG Limits:
;Normal: 102" to 114.5", -8.5 to -9.54 ft at 2500 lb
;Utility: 102" to 109", -8.5 to -9.08 ft at 2200 lb

max_number_of_stations=20

//          Weight,   long,  lat, vert  positions from datum
station_load.0=170, -7.75, -1.0, 0.0
station_load.1=170, -7.75, 1.0, 0.0
station_load.2=151, -11.17, -1.0, 0.0
station_load.3=152, -11.17, 1.0, 0.0
station_load.4=25, -13.50, 0.0, -2.0
station_load.5=001, -15.00,  0.0, +1.0  //Hat Shelf
;Maximum: 669 lb at 61 gal fuel

;station_load.0=170,  -7.75, -1.0,  0.0   // 93*170 = 15.81 in-lb/1000
;station_load.1=170,  -7.75,  1.0,  0.0   // 93*170 = 15.81
;station_load.2=100, -11.17, -1.0,  0.0   //134*100 = 13.40
;station_load.3=100, -11.17,  1.0,  0.0   //134*100 = 13.40
;station_load.4=016, -13.50,  0.0, -2.0   // 16*162 =  2.59
;station_load.5=001, -15.00,  0.0,  1.0   //  1*180 =   .18
; Load Moment  (See Weight & Balance in PoH)          61.19 in-lb/1000
; Fuel (50gal)  300,  -9.33,  0.0,  2.5     300*112=33.60
; Aircraft     1643,  -8.57,  0.0,  0.0    1643*103=169.90
; Total        2500,  -8.81,  0.0,  0.0             264.4  (limit 287")
station_load.6=
station_load.7=
station_load.8=
station_load.9=
station_load.10=
station_load.11=
station_load.12=
station_load.13=
station_load.14=
station_load.15=
station_load.16=
station_load.17=
station_load.18=
station_load.19=

[pitot_static]
vertical_speed_time_constant=20

[ground_reaction]
main_gear_damping_ratio=0.8
center_gear_damping_ratio=1.0

[fuel]
LeftMain=-9.33,-2.1, 2.0, 30.5, 0.5  //112"
RightMain=-9.33, 2.1, 2.0, 30.5, 0.5  //24.5 usable
fuel_type=1
number_of_tank_selectors=1

//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)
electric_pump=1
//11 Extension Time              (seconds)
//12 Retraction Time             (seconds)
//13 Sound Type
[contact_points]                                                  //4.0    
point.0=1, -3.9,  0.00,-3.78,1181, 0, 0.52,45.00, 0.300, 2.5, 1.00, 6.0, 0.0, 0, 0.00, 0.00 //Nose Wheel
point.1=1,-10.3, -4.50,-3.53,1476, 1, 0.52, 0.00, 0.244, 2.5, 0.80, 6.0, 0.0, 2, 0.00, 0.00 //L. Main
point.2=1,-10.3,  4.50,-3.53,1476, 2, 0.52, 0.00, 0.244, 2.5, 0.80, 6.0, 0.0, 3, 0.00, 0.00 //R. Main
point.3=2, -3.6,-17.25, 1.80, 300, 0, 0.00, 0.00, 0.000, 0.0, 0.00, 0.0, 0.0, 5, 0.00, 0.00 //Wing tip
point.4=2, -3.6, 17.25, 1.80, 300, 0, 0.00, 0.00, 0.000, 0.0, 0.00, 0.0, 0.0, 6, 0.00, 0.00 //Wing tip
point.5=2,-26.5,  6.16, 0.83, 600, 0, 0.00, 0.00, 0.000, 0.0, 0.00, 0.0, 0.0, 9, 0.00, 0.00 //Fin tip
point.6=2, -1.7,  0.00,-2.50, 300, 0, 0.00, 0.00, 0.000, 0.0, 0.00, 0.0, 0.0, 4, 0.00, 0.00 //Prop?
point.7=2,-26.5,  0.00, 6.83, 300, 0, 0.00, 0.00, 0.000, 0.0, 0.00, 0.0, 0.0, 7, 0.00, 0.00 //Tail 
point.8=2, -9.4,  0.00,-2.00, 300, 0, 0.00, 0.00, 0.000, 0.0, 0.00, 0.0, 0.0, 8, 0.00, 0.00 //Fuselage
static_pitch=3.0
static_cg_height=3.15
gear_system_type=0
;Nose Wheel at 47.2" 3.93 ft; Main at 123.8" 10.32 ft


[electrical]
max_battery_voltage=25.2          //Battery Voltage - charged 14, 17 AH
generator_alternator_voltage=28.5 //Alternator/Generator Voltage
max_generator_alternator_amps=30  //spec 60 A

;BusType, MaxAmpLoad, MinVoltage  BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 10, 17.0   // 24 V system (22 AH)
autopilot=0,  2, 19.0
avionics_bus=0,  5, 17.0
avionics=1,  2, 17.5
pitot_heat=0,2.5, 16.0
additional_system=0,  1, 15.5   //Clock, Turn Coordinator
marker_beacon=1,  1, 20.0
fuel_pump=0,  1, 17.0
starter1=0,150, 15.0
light_nav=0,  4, 17.0
light_beacon=0,  2, 21.0
light_landing=0,  3, 18.0
light_taxi=0,  2, 16.0
light_strobe=0,  2, 19.0
light_panel=0,  2, 16.0

[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, 1
Adf.1=1
Transponder.1=1
Marker.1=1

[exits]
number_of_exits=2
exit_rate.0=0.4
exit_rate.1=0.4

[effects]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1

[TailHook]
tailhook_length=1
tailhook_position=-8.05, -17.8, 2.1
cable_force_adjust=1

[GeneralEngineData]
engine_type=0
//Engine.0=-1.75, 0.00, 0.70
Engine.0=-1.75, -0.40, 0.70
fuel_flow_scalar=1.00
min_throttle_limit=0.000000

[piston_engine]   //Lycoming O-360-A1B6 or O-360-A1B6D
power_scalar=1.0
cylinder_displacement=90.252
compression_ratio=8.50
number_of_cylinders=4
max_rated_rpm=2700.0
max_rated_hp=200.0    //180
fuel_metering_type=0  //0=Fuel Injected
cooling_type=0
normalized_starter_torque=0.10
turbocharged=1
max_design_mp=31.0 //28.5
min_design_mp=4.0
critical_altitude=6800  //for 31.0", 8000 ft for rated MP
emergency_boost_type=0
emergency_boost_mp_offset=0.0
emergency_boost_gain_offset=0.0
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.00
idle_rpm_mechanical_efficiency_scalar=1.00
max_rpm_friction_scalar=1.00
idle_rpm_friction_scalar=1.00

[propeller]   //McCauley   B2D34C206/78TA or B2D34C207/78TCA
thrust_scalar=1.0
propeller_type=0
propeller_diameter=6.50  //6.33 180 HP non-RG
propeller_blades=2
propeller_moi=2.2   //49.8 lb
beta_max=27.5       //26.0
beta_min=12.9       //12.1
min_gov_rpm=1600.0
prop_tc=0.20
gear_reduction_ratio=1.00
fixed_pitch_beta=20.0
low_speed_theory_limit=80.0
prop_sync_available=0
prop_deice_available=0  //1 optional
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0
beta_feather=0.0
power_absorbed_cf=0.05  //Affects idle friction
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=12.9 //0.0
minimum_reverse_beta=0.0

[airplane_geometry]
wing_area=174.0
wing_span=35.5
wing_root_chord=4.917     //MAC
wing_dihedral=1.75
wing_incidence=1.5
wing_twist=-3.0
oswald_efficiency_factor=0.809
wing_winglets_flag=0
wing_sweep=0.0
wing_pos_apex_lon=-7.421  //MAC at -8.65 -103.8" (-7.621: 8.85 106.2"; -7.121: -8.35 -100.2")
wing_pos_apex_vert=2.00

htail_area=0.0      //39.0
htail_span=0.0      //11.83
htail_pos_lon=-26.5
htail_pos_vert=0.00
htail_incidence=4.0
htail_sweep=0.0

vtail_area=18.0
vtail_span=4.84
vtail_sweep=0.0
vtail_pos_lon=-26.5 // 293.6" (tail strobe)
vtail_pos_vert=1.50
//Tail Moment arm=26.5-8.35 = 18.15 ft, 218"

elevator_area=39.0
aileron_area=18.30
rudder_area=6.65
elevator_up_limit=20.0
elevator_down_limit=5.0
aileron_up_limit=20.0
aileron_down_limit=15.0
rudder_limit=24.0
elevator_trim_limit=13.0  //5.0 up, 13.0 down
spoiler_limit=0.1
spoilerons_available=0
aileron_to_spoileron_gain=0.0
min_ailerons_for_spoilerons=0.0
min_flaps_for_spoilerons=0.0


[Flaps.0]
type=1
span-outboard=
extending-time=7.0
system_type=0
flaps-position.0=0.00, 0
flaps-position.1=10.0, 0
flaps-position.2=15.0, 0
flaps-position.3=20.0, 0
flaps-position.4=30.0, 0

[Reference Speeds]
flaps_up_stall_speed=54.0
full_flaps_stall_speed=43.2
cruise_speed=140
max_indicated_speed=167.000000

[keyboard_response]
elevator=100,180
aileron=200,350
rudder=200,350

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=1000.000000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=105.000
pitch_takeoff_ga=8.000000
use_no_default_pitch=1
use_no_default_bank=1
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000



//[autopilot]
//autopilot_available=1
//flight_director_available=0
//default_vertical_speed=700
//autothrottle_available=0  //1
//pitch_takeoff_ga=10.0
//autothrottle_arming_required=0
//autothrottle_takeoff_ga=0 //1 
//autothrottle_max_rpm=105.0
//use_no_default_pitch=1    //0
//use_no_default_bank=1     //0
//default_pitch_mode=0
//default_bank_mode=0
//max_pitch=10.000000
//max_pitch_acceleration=1.000000
//max_pitch_velocity_lo_alt=2.000000
//max_pitch_velocity_hi_alt=1.500000
//max_pitch_velocity_lo_alt_breakpoint=20000.000000
//max_pitch_velocity_hi_alt_breakpoint=28000.000000
//max_bank=25.000000
//max_bank_acceleration=1.800000
//max_bank_velocity=3.000000
//max_throttle_rate=0.100000
//nav_proportional_control=9.000000
//nav_integrator_control=0.250000
//nav_derivative_control=0.000000
//nav_integrator_boundary=2.500000
//nav_derivative_boundary=0.000000
//gs_proportional_control=9.520000
//gs_integrator_control=0.260000
//gs_derivative_control=0.000000
//gs_integrator_boundary=0.700000
//gs_derivative_boundary=0.000000
//yaw_damper_gain=0.000000


[direction_indicators]
direction_indicator.0=1,0

[forcefeedback]
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000

[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
avion EC-JAS

[brakes]
toe_brakes_scale=0.854518
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[hydraulic_system]
normal_pressure=0.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
