// 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
