// Shorts330 // Design: Jean-Pierre Brisard // Chk/Ref HTML Docs by Barry Blaisdell // Master Textures & Livery by Bob May // Copyright 2009 - Premier Aircraft Design // v2.0 Fuselage & tail re-design 22-03-2009 [fltsim.0] title=S330_Air Ecosse Cargo sim=PAD_s330 model=cargo panel=s360x sound=0 texture=airecosse kb_checklists=S330_check kb_reference=S330_ref atc_id=G-BKDN atc_heavy=0 atc_airline=regional atc_flight_number=AE16 atc_parking_types=cargo,ramp atc_parking_codes= ui_manufacturer=Shorts ui_type=S330 ui_variation=Shorts 330 Air Ecosse Cargo (1985) description=Shorts 330\nTwin Turboprop Regional/Commuter Airliner\nVisit the Premier Aircraft Design Web Site\nwww.premaircraft.com\nAll Files Copyright 2009. [fltsim.1] title=S330_Air Ecosse Passenger sim=PAD_s330 model=pax panel=s360x sound=0 texture=airecosse kb_checklists=S330_check kb_reference=S330_ref atc_id=G-BKDN atc_heavy=0 atc_airline=regional atc_flight_number=AE18 atc_parking_types=gate,ramp atc_parking_codes= ui_manufacturer=Shorts ui_type=S330 ui_variation=Shorts 330 Air Ecosse Passenger (1985) description=Shorts 330\nTwin Turboprop Regional/Commuter Airliner\nVisit the Premier Aircraft Design Web Site\nwww.premaircraft.com\nAll Files Copyright 2009. [General] performance=30 Pax Regional Airliner\nLength: 58.0 ft\nWing Span: 74.8 ft\nWeight:14,727 lb Empty\nMax T\/O Weight:22,000 lb\nPower: 2 x 1,327 SHP P&W PT6A65R Turboshafts\n 5 blades prop\nMax speed: 218 Kts TAS\ncruise: 185 kts TAS\nCeiling: 11,000 ft\nRange: 550 Naut Miles atc_type=SHORTS atc_model=SH33 Category=airplane [WEIGHT_AND_BALANCE] max_gross_weight = 22900 // (pounds) empty_weight = 14000 // (pounds) reference_datum_position= 31.0, 0, 0 // (feet) distance from FlightSim Ref position: (1/4 chord,c/l, waterline) empty_weight_CG_position=-28.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = "170, -12, -1.75, 0.0, Pilot" //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = "170, -12, 1.75, 0.0, Front Passenger" //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = "3500, -25.0, 0.0, 0.0, Payload" //Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 111701 empty_weight_roll_MOI = 61201 empty_weight_yaw_MOI = 161691 empty_weight_coupled_MOI = 0 [Views] eyepoint= -12.5,-1.0,-2.6 //(feet) longitudinal, lateral, vertical distance from reference datum [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=Landing light.0 = 1, -31.26, 0.0, 1.9 , fx_beaconh , light.1 = 2, -61.8, 11.9, -2.85, fx_navwhi , light.2 = 2, -29.49, 36.7, 1.76, fx_strobeh, light.3 = 2, -29.49, -36.7, 1.76, fx_strobeh, light.4 = 3, -29.43, -37.0, 1.76, fx_navred , light.5 = 3, -29.43, 37.0, 1.76, fx_navgre , light.6 = 1, -40.68, 0.0, -8.5, fx_beaconh , light.7 = 4, -11.0, -1.50, -4.00, fx_vclightwhi , light.8 = 4, -11.0, 1.50, -4.00, fx_vclightwhi , light.9 = 4, -11.0, -2.0, -6.00, fx_vclightwhi , light.10 = 4, -11.0, 2.0, -6.00, fx_vclightwhi , [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 1000.0 autothrottle_available= 0 pitch_takeoff_ga=8.0 use_no_default_bank=1 use_no_default_pitch=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 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=1.50 induced_drag_scalar=1.000 elevator_effectiveness=0.8 aileron_effectiveness=1.1 rudder_effectiveness=0.8 pitch_stability=2.0 roll_stability=2.0 yaw_stability=2.0 elevator_trim_effectiveness=0.300 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [GeneralEngineData] engine_type = 5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = -28.4, -13.3, 1.5 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1 = -28.4, 13.3, 1.5 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar = 1.00 //Scalar for fuel flow efficiency min_throttle_limit = -0.50 //Minimum percent throttle. Generally negative for turbine reverser [propeller] thrust_scalar = 1.15 //Propeller thrust scalar propeller_type = 0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter = 13.0 //Propeller Diameter, (feet) propeller_blades = 5 //Number of propeller blades propeller_moi = 77 //Propeller moment of inertia beta_max = 45 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min = 12 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm = 25520 //Miminum governed RPM prop_tc = 0.004 //Prop time-constant gear_reduction_ratio = 17.0 //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 = 1 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available = 1 //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 = 1000 //Minimum RPM for prop feathering beta_feather = 79.3 //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 = -14.0 //Minimum pitch angle in reverse, (degrees) [TurbineEngineData] fuel_flow_gain = 0.011 //Gain on fuel flow inlet_area = 3.00 //Square Feet, engine nacelle inlet area rated_N2_rpm = 29920 //RPM, second stage compressor rated value static_thrust = 200 //Lbs, max rated static thrust at Sea Level [turboprop_engine] power_scalar = 1.00 //Scalar on Turboprop power maximum_torque = 7878 //Maximum torque available (ft-lbs) [electrical] //BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) //BusType, MaxAmpLoad, MinVoltage autopilot = 0, 5 , 1.0 avionics_bus = 0, 10, 10.0 avionics = 1, 5 , 10.0 gear_warning = 0, 2 , 1.0 fuel_pump = 0, 5 , 1.0 light_nav = 0, 5 , 1.0 light_beacon = 0, 5 , 1.0 light_landing = 0, 5 , 7.0 light_taxi = 0, 5 , 7.0 light_strobe = 0, 5 , 7.0 light_panel = 0, 5 , 1.0 pitot_heat = 0, 15, 1.0 additional_system = 0, 20, 1.0 marker_beacon = 1, 2, 1.0 starter1 = 0, 20, 1.0 starter2 = 0, 20, 1.0 starter3 = 0, 20, 1.0 starter4 = 0, 20, 1.0 auto_brakes = 0, 15, 1.0 hydraulic_pump = 0, 2, 1.0 fuel_transfer_pump = 0, 5, 1.0 max_battery_voltage=28.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=160.0 electric_always_available=0 //0 Class <0=none,1=wheel, 2=scrape, 3=float> //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 //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) [contact_points] point.0 = 1, -7.215, 0.00, -11.47, 2500, 0, 1.00, 70.0, 0.200, 2.0, 0.9, 5.0, 6.0, 0, 0.0 , 0.0 point.1 = 1, -32.825, -7.5, -11.50, 3000, 1, 1.605, 0.0, 0.40, 2.5, 0.8, 6.0, 7.0, 0, 0.0 , 0.0 point.2 = 1, -32.825, 7.5, -11.50, 3000, 2, 1.605, 0.0, 0.40, 2.5, 0.8, 6.0, 7.0, 0, 0.0 , 0.0 point.3 = 2, -7.6, 0.0, -5.0, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 5 //Nose point.4 = 2, -31.1, -37.50, 1.3, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 5 //Lwing point.5 = 2, -31.1, 37.50, 1.3, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 6 //Rwing point.6 = 2, -68.6, 0.00, -3.1, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 9 //Tail point.7 = 2, -31.0, 0.00, -9.0, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 4 //Belly point.8= 5, -30.90, 0.0, -7.300, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 1.1, 1.5, 0, 0.0, 0.0 max_number_of_points = 21 static_pitch = 0.0 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height = 11.00 //feet, altitude of CG when at rest on the ground gear_system_type=1 //Hydraulic [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 15.0 //Flap angle that activates warning at idle flap_limit_power = 30.0 //Flap angle that activates warning at above idle [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 [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 1.06 //Brake scalar [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [flaps.0] type = 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 6 // seconds flaps-position.0 = 0 // degrees, KIAS flaps-position.1 = 5 // degrees, KIAS flaps-position.2 = 15 // degrees, KIAS flaps-position.3 = 35 // degrees, KIAS damaging-speed = 250 // KIAS blowout-speed = 300 drag_scalar=1.30 lift_scalar=1.30 // KIAS [flaps.1] type = 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 6 // seconds flaps-position.0 = 0 // degrees, KIAS flaps-position.1 = 5 // degrees, KIAS flaps-position.2 = 15 // degrees, KIAS flaps-position.3 = 35 // degrees, KIAS damaging-speed = 250 // KIAS blowout-speed = 300 drag_scalar=1.30 lift_scalar=1.30 // KIAS [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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] Center1= -31.1, 0, 3.9, 348.0, 0.0 //368 Center2= -32.0, 0, 3.9, 348.0, 0.0 LeftAux=-31.1, -10.1, 0.0, 20.0, 0.0 RightAux=31.1, 10.1, 0.0, 20.0, 0.0 fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 electric_pump=1 [airplane_geometry] wing_area = 544.0 //Square feet wing_span = 74.85 //Feet wing_root_chord = 7.0 //Feet wing_dihedral = 4.0 //Degrees wing_incidence = 0.500 //Degrees wing_twist = -3.0 //Degrees oswald_efficiency_factor= 0.7500 //Measure of lift effeciency of wing wing_winglets_flag = 0 //Are winglets available? wing_sweep = 3.0 //Degrees, wing leading edge wing_pos_apex_lon = -25.0 //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 = 97.0 //Square feet htail_span = 26.0 //Feet htail_pos_lon = -58.9 //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 = -2.500 //Degrees htail_sweep = 8.0 //Degrees, horizontal tail leading edge vtail_area = 106.0 //Square feet vtail_span = 11.7 //Feet, tip to body vtail_sweep = 30.0 //Degrees, vertical tail leading edge vtail_pos_lon = -54.9 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 3.4 //Feet, vertical distance from reference point, positive going up elevator_area = 53.5 //Square feet aileron_area = 12.1 //Square feet rudder_area = 46.4 //Square feet elevator_up_limit = 17.0 //Degrees elevator_down_limit = 17.0 //Degrees aileron_up_limit = 18.0 //Degrees aileron_down_limit = 18.0 //Degrees rudder_limit = 20.0 //Degrees rudder_trim_limit = 60.0 elevator_trim_limit = 85.0 //Degrees spoiler_limit = 60.0 //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=1 spoiler_extension_time=2.000000 positive_g_limit_flaps_up=3.000000 positive_g_limit_flaps_down=2.000000 negative_g_limit_flaps_up=-2.000000 negative_g_limit_flaps_down=-2.000000 [Reference Speeds] flaps_up_stall_speed = 92.0 //Knots True (KTAS) full_flaps_stall_speed = 72.0 //Knots True (KTAS) cruise_speed = 220 //Knots True (KTAS) max_indicated_speed = 242 //Red line (KIAS) max_mach=0.560000 [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= 150.0, 250.0 aileron= 150.0, 250.0 rudder= 150.0, 250.0 [stall_warning] type=1 stick_shaker=1 [direction_indicators] direction_indicator.0=3,0 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [direction_indicators] direction_indicator.0=3,0 [brakes] toe_brakes_scale=1.062532 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=30.022988 flap_limit_idle=15.011494 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [pitot_static] pitot_heat=1.000000 [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=1.000000 [deice_system] structural_deice_type=2 [folding_wings] // normally shift+K wing_fold_system_type=4 fold_rates=0.12,0.12 [smokesystem] smoke.0= -24.4, -13.3, 1.5 , fx_turbo_exhaust.fx //The longitudinal, lateral, and vertical position of the smoke emitter, and the effect file name. smoke.1= -24.4, 13.3, 1.5 , fx_turbo_exhaust.fx