//  PREMIER AIRCRAFT DESIGN
//  Shorts360 
//  Design: Jean-Pierre Brisard
//  Chk/Ref HTML Docs by Barry Blaisdell
//  Master Textures by Bob May
//  Loganair livery by Piran Smith
//  Copyright 2009 - Premier Aircraft Design



[fltsim.0]
title=Shorts 360 Tiara Air
sim=PAD_s360
model=
panel=s360x       
sound=0
texture=tiara
kb_checklists=S360_check
kb_reference=S360_ref
atc_id=P4-TIA
atc_heavy=0
atc_airline=regional
atc_flight_number=TA41
atc_parking_types=gate,ramp
atc_parking_codes=
ui_manufacturer=Shorts
ui_type=S360
ui_variation=Tiara Air



description=Shorts 360\nTwin Turboprop Regional/Commuter Airliner\nVisit the Premier Aircraft Design Web Site\nwww.premaircraft.com\nAll Files Copyright 2009.

[General]
performance=36 Pax Regional Airliner\nLength: 70.83 ft\nWing Span: 74.83 ft\nWeight:16900 lb Empty\nMax T\/O Weight:26,000 lb\nPower: 2 x 1,327 SHP P&W PT6A65R Turboshafts\n 5 blades prop\nMax Cruise: 220 Kts TAS\nCeiling: 11,000 ft\nRange: 550 Naut Miles
atc_type=SHORTS
atc_model=SH36
Category=airplane

[WEIGHT_AND_BALANCE]
max_gross_weight = 26000                     // (pounds)
empty_weight = 14900                     // (pounds)

reference_datum_position= 31.0, 0, 0 // (feet) distance from FlightSim Ref position: (1/4 chord,c/l, waterline)
empty_weight_CG_position=-26.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 50

station_load.0 = "170,  -9.8, -1.75, 0.0, Pilot"                  //Pilot           Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170,  -9.8,  1.75, 0.0, Front Passenger"        //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "3500, -26.0,  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, 1.5 , fx_beaconh ,
light.1 = 2,   -69.5, 0.0,  -1.53, 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,  -8.9, 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=1.00
induced_drag_scalar=1.000
elevator_effectiveness=0.8
aileron_effectiveness=1.1
rudder_effectiveness=0.8
pitch_stability=1.5
roll_stability=2.0
yaw_stability=2.0
elevator_trim_effectiveness=0.500
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, 2.7                    //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -28.4,  13.3, 2.7                    //(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    //700               //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,  -9.648,    0.00, -11.50, 2500, 0, 0.250,  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, 1.250,  0.4, 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, 1.250,  0.4, 0.40, 2.5, 0.8, 6.0, 7.0, 0, 0.0 , 0.0
point.3 = 2,  0.0, 0.0,  -8.0, 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, -10.2, 1200, 0, 0.000,  0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 4   //Belly
point.8= 5, -30.90,  5.250, -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 = 11.0          //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=1.00                                 // 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=1.00                                 // 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]
LeftMain  = -32.00,-6.00, -1.00, 368.00, 0.00  
'LeftAux   = 0.00, -6.00, -1.50,  79.50, 0.00
RightMain =-32.00, 6.00, -1.00, 368.00, 0.00
'RightAux  = 0.00,  6.00, -1.50,  79.50, 0.00
fuel_type = 2                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    
electric_pump=0






[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


[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