[fltsim.0] title=ATC Pitts S-1S sim=Cessna172SP model= panel= sound= texture= checklists= atc_id=N38GS ui_manufacturer=ATC ui_type=Pitts S-1S ui_variation=N38GS description=While a number of enhancements make it a step forward in development, the 182S retains the remarkable characteristics that have made the 182 a popular airplane: power, stability, and good load hauling capabilities. The Skylane 182S is an ideal airplane for pilot training. If you're new to flying, you'll find Rod Machado's flight lessons in the 182S very helpful. You'll find them in the Flight Simulator 2000 Pilot's Handbook. For enhanced instrument flight rules (IFR) panels, choose the 182S IFR. See the Aircraft Information section of Help for tips on flying this aircraft. --- [WEIGHT_AND_BALANCE] reference_datum_position=3.6, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=-3.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum station_load.0=170, -3.0, -1.5, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=170, -3.0, 1.5, 0.0 //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2=0, -6.2, -1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3=0, -6.2, 1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4=0, -8.0, 0.0, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=1400.0 empty_weight_roll_MOI=1137.0 empty_weight_yaw_MOI=2360.0 empty_weight_coupled_MOI=0.0 --- [flight_tuning] cruise_lift_scalar=1.4 parasite_drag_scalar=1.4 induced_drag_scalar=1.4 elevator_effectiveness=0.8 aileron_effectiveness=1.0 rudder_effectiveness=1.0 [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=12.7 // degrees flaps-position.2=25.3 // degrees flaps-position.3=38 // degrees damaging-speed=120 // KIAS blowout-speed=150 // KIAS lift_scalar=1.0 drag_scalar=1.0 pitch_scalar=1.0 system_type=0 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None --- [GeneralEngineData] engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = 2.0, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=0.88 //Fuel flow scalar --- [propeller] 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=5.0 //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 fixed_pitch_beta=20 //Fixed pitch angle of fixed pitch prop, (degrees) --- [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=1.8 // was 1.5 //Degrees wing_twist=-3.0 //Degrees oswald_efficiency_factor=0.58 //was 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=3.2 //Degrees 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=21.0 //Degrees aileron_up_limit=20.0 //Degrees aileron_down_limit=15.0 //Degrees rudder_limit=24.0 //Degrees elevator_trim_limit=19.5 //Degrees