[fltsim.0]
title=Cessna 185
sim=Cessna C185 Skywagon
model=
panel=
sound=
texture=
checklists=
atc_type=Cessna
atc_id_enable=1
atc_id=N12AS
editable=1
ui_manufacturer=Cessna
ui_type=C185 Skywagon
ui_variation=Yellow and white
checklists=
description=Created by Mikko Maliniemi November 2001. Panel By Ian Grant November 2001. Sounds by Aaron Swindle. C185 Skywagon Flight Dynamics © Steve Small FSD 11\/2001. \n\n\n\n\n\n\n\n
atc_heavy=0
atc_airline=
atc_flight_number=

[fltsim.1]
title=Cessna 185 Paint_1
sim=Cessna C185 Skywagon
model=
panel=
sound=
texture=1
checklists=
atc_type=Cessna
atc_id_enable=1
atc_id=N12AS
editable=1
ui_manufacturer=Cessna
ui_type=C185 Skywagon
ui_variation=Red and white
checklists=
description=Created by Mikko Maliniemi November 2001. Panel By Ian Grant November 2001. Sounds by Aaron Swindle. C185 Skywagon Flight Dynamics © Steve Small FSD 11\/2001. \n\n\n\n\n\n\n\n
atc_heavy=0
atc_airline=
atc_flight_number=

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit        
light.0=3,  0.3, -18.146, 2.224, fx_navred
light.1=3,  0.3,  18.146, 2.224, fx_navgre
light.2=1, -14.85,   0.00, 5.6, fx_beacon
light.3=4,  0.00,   0.00, 1.00, fx_vclight
light.4=3,  -17.5, 0 , 0.23, fx_navwhi

[Views]
eyepoint=-0.294763,-0.820210,1.320025

[General]
performance=Cessna A185 F II Skywagon\s  Continental IO-520-L rated @ 300BHP\s Gross Weight: 3350 lbs\s Top Speed: 155 kts Empty Weight: 1750 lbs\s Cruise Speed: 145 kts Fuel Capacity: 88.00 gal\s Stall Speed (dirty): 49 kts Range: 645 nm\n
atc_type=SKYWAGON
atc_model=C185

[WEIGHT_AND_BALANCE]
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=0.000000,0.000000,0.000000,0.000000
empty_weight= 2250.000
empty_weight_roll_MOI= 3000.000
empty_weight_pitch_MOI= 6250.000
empty_weight_yaw_MOI= 4250.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 2778.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[fuel]
LeftMain= 0.000, -4.700, 2.500, 44.000, 0.000
RightMain= 0.000, 4.700, 2.500, 44.000, 0.000
fuel_type=1.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area= 190.000
wing_span= 39.583
wing_root_chord= 4.917
wing_dihedral= 1.736
wing_incidence= 1.500
wing_twist= -2.999
oswald_efficiency_factor= 0.818
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 1.229
wing_pos_apex_vert= 0.000
htail_area= 39.000
htail_span= 11.667
htail_pos_lon= -14.667
htail_pos_vert= 0.000
htail_incidence= 3.246
htail_sweep= 3.000
vtail_area= 18.000
vtail_span= 4.837
vtail_sweep= 10.000
vtail_pos_lon= -12.583
vtail_pos_vert= 1.500
elevator_area= 12.000
aileron_area= 16.800
rudder_area= 7.500
elevator_up_limit= 25.000
elevator_down_limit= 23.000
aileron_up_limit= 20.000
aileron_down_limit= 15.000
rudder_limit= 24.000
elevator_trim_limit= 20.500
spoiler_limit= 0.000
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000

[GeneralEngineData]
engine_type= 0
Engine.0= 6.000, 0.000, 0.000
fuel_flow_scalar= 1.000

[piston_engine]
cylinder_displacement= 87.000
compression_ratio= 8.500
number_of_cylinders= 6
max_rated_rpm= 2700.000
max_rated_hp= 300.000
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
fuel_flow_scalar=1.000
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
power_scalar=1.000

[propeller]
propeller_type= 0
propeller_diameter= 6.950
propeller_blades= 3
propeller_moi= 5.700
beta_max= 39.000
beta_min= 11.000
min_gov_rpm= 1400.000
prop_tc= 0.100
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
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000

[Reference Speeds]
flaps_up_stall_speed= 54.000
full_flaps_stall_speed= 43.200
cruise_speed= 133.831

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[autopilot]
use_no_default_pitch=1 
use_no_default_bank=1 
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
autoland_available=0

[direction_indicators]
direction_indicator.0=1,0

[flight_tuning]
cruise_lift_scalar=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000


[contact_points]
point.0= 1.000, -17.917, 0.000, -1.633, 3500.000, 0.000, 0.519, 42.900, 0.191, 2.500, 1.082, 0.000, 0.000, 0.000, 0.000, 0.000
point.1= 1.000, 2.000, -4.000, -5.827, 3500.000, 1.000, 0.519, 0.000, 0.569, 2.500, 0.626, 0.000, 0.000, 2.000, 0.000, 0.000
point.2= 1.000, 2.000, 4.000, -5.827, 3500.000, 2.000, 0.519, 0.000, 0.569, 2.500, 0.626, 0.000, 0.000, 3.000, 0.000, 0.000
point.3= 2.000, 1.083, -18.000, 3.667, 1573.938, 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, 1.083, 18.000, 3.667, 1573.938, 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, -18.333, 0.000, 0.167, 1573.938, 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, 7.250, 0.000, -1.667, 1573.938, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= 9.998
static_cg_height= 4.881



[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 7.000
system_type= 0
damaging-speed= 180.000
blowout-speed= 230.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 12.500, 0.000
flaps-position.2= 25.000, 0.000
flaps-position.3= 40.000, 0.000