[fltsim.0] title=porter_new_roundtip_w_door_cargo_LR_9_11_2010_ski ABC sim=porter_new_roundtip_w_door_cargo_LR_9_11_2010_ski model= panel= sound= texture=abc kb_checklists= kb_reference= atc_id=N816BC atc_id_color=0xff000000 ui_manufacturer=Pilatus ui_type=Cargo LR SKI ui_variation=Cargo Ski ABC ui_thumbnailfile=ABC Cargo Ski.jpg description= The Pilatus PC-6 Porter and the Turbo Porter, best known under the name "Pilatus Porter", is a STOL- (short take off and landing) and multi-purpose airplane designed and built since 1959 by Pilatus Aircraft Ltd in Stans, Switzerland. [fltsim.1] title=porter_new_roundtip_w_door_cargo_LR_9_11_2010_ski_PVT sim=porter_new_roundtip_w_door_cargo_LR_9_11_2010_ski model= panel= sound= texture=1AK kb_checklists= kb_reference= atc_id=N101AK atc_id_color=0xff000000 ui_manufacturer=Pilatus ui_type=Cargo LR SKI ui_variation=Cargo Ski N101AK ui_thumbnailfile=PVT Cargo Ski.jpg description= The Pilatus PC-6 Porter and the Turbo Porter, best known under the name "Pilatus Porter", is a STOL- (short take off and landing) and multi-purpose airplane designed and built since 1959 by Pilatus Aircraft Ltd in Stans, Switzerland. [fltsim.2] title=porter_new_roundtip_w_door_cargo_LR_9_11_2010_ski_AAC sim=porter_new_roundtip_w_door_cargo_LR_9_11_2010_ski model= panel= sound= texture=aac kb_checklists= kb_reference= atc_id=N1AA atc_id_color=0xff000000 ui_manufacturer=Pilatus ui_type=Cargo LR SKI ui_variation=Cargo Ski AAC ui_thumbnailfile=AAC Cargo Ski.jpg description= The Pilatus PC-6 Porter and the Turbo Porter, best known under the name "Pilatus Porter", is a STOL- (short take off and landing) and multi-purpose airplane designed and built since 1959 by Pilatus Aircraft Ltd in Stans, Switzerland. [General] atc_type=Pilatus atc_model=PC6T editable=0 performance=Please download the manual/checklist for the Pilatus PC-6 Turbo Porter, written by Werner Schott, so proper power settings can be followed. I know it is available at Avsim. Don - NEW - 11/06 Category=airplane [WEIGHT_AND_BALANCE] empty_weight = 2755 // (pounds) per Airliners.net max_number_of_stations = 8 station_load.0 = 170, 2, -2.1, 0.0 station_load.1 = 170, 2, 2.1, 0.0 station_load.2 = 0, -2, -2.1, 0.0 station_load.3 = 0, -2, 2.1, 0.0 station_load.4 = 0, -5, -2.1, 0.0 station_load.5 = 0, -5, 2.1, 0.0 station_load.6 = 0, -8, -2.1, 0.0 station_load.7 = 0, -8, 2.1, 0.0 station_load.8 = 0, -10.0, 0.0, 0.0 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 14000 empty_weight_roll_MOI = 6026.96 empty_weight_yaw_MOI = 11858.54 empty_weight_coupled_MOI = 0.0 max_gross_weight= 6173.00 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.5 elevator_effectiveness = 1.0 aileron_effectiveness = 1.0 rudder_effectiveness = 1.0 pitch_stability = 1.5 roll_stability = 1.0 yaw_stability = 1.0 elevator_trim_effectiveness = .9 aileron_trim_effectiveness = .9 rudder_trim_effectiveness = 1.0 p_factor_on_yaw=0.1 torque_on_roll=0.1 [GeneralEngineData] engine_type = 5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 =11.5, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar = 1.12 //Scalar for fuel flow efficiency min_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reverser [propeller] thrust_scalar = 1.0 //Propeller thrust scalar propeller_type = 0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter = 8.8 //Propeller Diameter, (feet) propeller_blades = 3 //Number of propeller blades propeller_moi = 11.2 //Propeller moment of inertia beta_max = 35 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min = 10.6 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm = 21000 //Miminum governed RPM prop_tc = 0.004 //Prop time-constant gear_reduction_ratio = 24 //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 = 0 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available= 1 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available= 1 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather = 700 //Minimum RPM for prop feathering beta_feather = 86 //Feathering pitch angle (degrees) power_absorbed_cf = 0.9 //Coefficient of friction for power absorbed by propeller defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available = 1 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta = 1.0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta = -12.0 //Minimum pitch angle in reverse, (degrees) [TurbineEngineData] fuel_flow_gain = 0.011 //Gain on fuel flow inlet_area = 1.0 //Square Feet, engine nacelle inlet area rated_N2_rpm = 25000 //RPM, second stage compressor rated value static_thrust = 158 //Lbs, max rated static thrust at Sea Level [turboprop_engine] power_scalar = .93 //Scalar on Turboprop power maximum_torque = 1720 //Maximum torque available (ft-lbs) [Flaps.0] type=1 span-outboard=0.5 // Percent span for flap position extending-time=5.7 // Seconds, time to fully extend system_type=0 // 0 = electrical flaps-position.0= 0 // degrees flaps-position.1=10 // degrees flaps-position.2=20 // degrees flaps-position.3=30 // degrees flaps-position.4= 35 // degrees flaps-position.5=40 // degrees flaps-position.6=45 // degrees flaps-position.7=50 // degrees [pitot_static] vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI pitot_heat=1.000000 [Radios] Audio.1 =1 Com.1 =1 Com.2 =1 Nav.1 =1, 0, 1 Nav.2 =1 ADF.1 =1 Transponder.1 =1 Marker.1 =1 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, .630, -29.25, 3.04, fx_navred light.1=3, .630, 29.25, 3.04, fx_navgre light.2=1, -13.61, 0, 2.41, fx_beacon light.3=3, -26.04, 0.00, -0.035, fx_navwhi light.4=2, -0.083, 29.75, 3.042, fx_strobe light.5=2, -0.083, -29.75, 3.042, fx_strobe light.6=2, -25.663, 0.00, 0.416, fx_strobe light.7=4, .630, 0.00, 0.00, fx_vclight light.8=1, -9.020, 0, -3.486, fx_beacon [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 [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=3,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=1,0 [electrical] 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)1.454672 //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=1.0,-26.5,0.0,-2.4,2000,0.0,0.25,60,0.171646,3.500000,0.6,,0.0,0.0,0.0,0.0,0.0 point.1=1.0,1.7,-5.4,-7.8,2500,1.0,1.25,0.0,1.15,1.4,1.0,0.0,0.0,0.00,0.0,0.0 point.2=1.0,1.7,5.4,-7.8,2500,2.0,1.25,0.0,1.15,1.4,1.0,0.0,0.0,0.0,0.0,0.0 point.3 = 2, -15.90, -26.0, 3.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5 point.4 = 2, -15.90 26.0, 3.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6 point.5= 2, -25.23, 0.0, 0.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9 point.6= 2, -2.50, 0.0, -2.17, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4 point.7= 2, -22.00, 0.0, 10.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7 static_pitch=9.091187 static_cg_height=4.505617 gear_system_type=4 //Hydraulic [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 = 4 //Parking brake available toe_brakes_scale = 2 //Brake scalar [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,0,0,0 //pumps on Eng1 [Views] eyepoint= -12.1, -1.4, 2.12 //(feet) longitudinal, lateral, vertical distance from reference datum [fuel] LeftMain=0.000000,-6.700000,1.000000,85.000000,1.000000 RightMain=0.000000,6.700000,1.000000,85.000000,1.000000 fuel_type=2.000000 number_of_tank_selectors=1 electric_pump=0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [exits] number_of_exits=2 exit_rate.0=0.2 exit_rate.1=0.2 [airplane_geometry] wing_area = 324.5 //Square feet wing_span = 52.1 //Feet wing_root_chord = 6.4 //Feet wing_dihedral = 0 //Degrees wing_incidence = 1.5 //Degrees wing_twist = -1.5 //Degrees oswald_efficiency_factor= 0.7 //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 = -16.0 //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 = 55.0 //Square feet htail_span = 17 //Feet htail_pos_lon = -21 //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 = 1.5 //Degrees htail_sweep = 0 //Degrees, horizontal tail leading edge vtail_area = 25 //Square feet vtail_span = 5.8 //Feet, tip to body vtail_sweep = 0.0 //Degrees, vertical tail leading edge vtail_pos_lon = -18.8 //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 = 30 //Square feet aileron_area = 14.5 //Square feet rudder_area = 21 //Square feet elevator_up_limit = 30.0 //Degrees elevator_down_limit = 23.5 //Degrees aileron_up_limit = 20.0 //Degrees aileron_down_limit = 19.0 //Degrees rudder_limit = 32.0 //Degrees elevator_trim_limit = 19.5 //Degrees spoiler_limit = 0.0 //Degrees 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=4.000000 positive_g_limit_flaps_down=2.000000 negative_g_limit_flaps_up=-1.500000 negative_g_limit_flaps_down=-1.500000 [Reference Speeds] flaps_up_stall_speed=58.000000 full_flaps_stall_speed=52.000000 cruise_speed=117 //125kts Vne max_indicated_speed=150.000000 max_mach=0.22 [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 1000.0 autothrottle_available= 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 pitch_takeoff_ga=8.000000 [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 [stall_warning] type=1 stick_shaker=0 [SmokeSystem]//40 Smoke.0= 0, -5, 0, snow Smoke.1= 0, 5, -5, snow Smoke.2= 0, 5, 5, snow [vacuum_system] max_pressure=5.150000 vacuum_type=2 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=0.150000 [deice_system] structural_deice_type=2