[fltsim.0]
title=Big Sky Airlines Fairchild SA-227DC Metro 23
sim=SA227 Metro 3 AI
model=
sound=
texture=
ui_manufacturer=Active Korea FS Traffic
ui_type="SA227 Metro 23"
ui_variation=Big Sky Express (Transair)
atc_airline=Transair
atc_flight_number=Metro23
atc_id_color=0xff000000
atc_parking_types=RAMP,GATE
atc_parking_codes=BIG
description=Fairchild Metro 23 for AI traffic use. Model by Dee Waldron.
[fltsim.1]
title=Bahamasair Fairchild Merlin/Metro
sim=SA227 Metro 3 AI
model=
sound=
texture=1
ui_manufacturer=Active Korea FS Traffic
ui_type="SA227 Metro 23"
ui_variation=Western Air/ Bahamasair
atc_airline=Bahamasair
atc_flight_number=Metro
atc_parking_types=GATE
atc_parking_codes=BHS
description=Fairchild Metro 23 for AI traffic use. Model by Dee Waldron. Repaint by Hernan Anibarro.
[fltsim.2]
title=OLT Fairchild Metro III
sim=SA227 Metro 3 AI
model=
sound=
texture=2
ui_manufacturer=Active Korea FS Traffic
ui_type="SA227 Metro 23"
ui_variation=OLT (OC)
atc_id=D-CNAG
atc_airline=Oltra
atc_flight_number=Metro
atc_parking_types=RAMP
atc_parking_codes=OLT
description=Dee Waldron AI Metroliner III
[fltsim.3]
title=OLT Saab 2000 Metro III
sim=SA227 Metro 3 AI
model=
sound=
texture=2
ui_manufacturer=Active Korea FS Traffic
ui_type="SA227 Metro 23"
ui_variation=OLT (2000)
atc_id=D-CNAG
atc_airline=Oltra
atc_flight_number=Metro
atc_parking_types=RAMP
atc_parking_codes=OLT
description=Dee Waldron AI Metroliner III
[fltsim.4]
title=Swearingen Metro III IBC Airways
sim=SA227 Metro 3 AI
model=
sound=
texture=4
ui_manufacturer=Active Korea FS Traffic
ui_type="SA227 Metro 23"
ui_variation=IBC Airways
atc_airline=Chasqui
atc_flight_number=Metro
atc_parking_types=CARGO
atc_parking_codes=CSQ
description=Fairchild Metro 23 for AI traffic use. Model by Dee Waldron.
[fltsim.5]
title=Shorts 360-200 IBC Airways
sim=SA227 Metro 3 AI
model=
sound=
texture=4
ui_manufacturer=Active Korea FS Traffic
ui_type="SA227 Metro 23"
ui_variation=Shorts 360-200
atc_airline=Chasqui
atc_flight_number=Metro
atc_parking_types=CARGO
atc_parking_codes=CSQ
description=Fairchild Metro 23 for AI traffic use. Model by Dee Waldron.
[General]
atc_type=FAIRCHILD AIRCRAFT
atc_model=SW3
editable=1
performance=\n\n
[WEIGHT_AND_BALANCE]
max_gross_weight=15000                        // (pounds)
empty_weight=9090                             // (pounds)
reference_datum_position=0.0, 0, 0       // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0.0, 0, 0       // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50
station_load.0=170,  5.0, -2.0, 0.0           //Pilot           Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1=170,  5.0,  2.0, 0.0           //Co-Pilot        Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2=170, -2.1, -2.0, 0.0           //Passenger       Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3=170, -2.1,  2.0, 0.0           //Passenger       Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4=170, -5.3, -2.0, 0.0           //Passenger       Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5=170, -5.3,  2.0, 0.0           //Passenger       Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI=30000
empty_weight_roll_MOI=18200
empty_weight_yaw_MOI=36500
empty_weight_coupled_MOI=0.0
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[GeneralEngineData]
engine_type=5                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=-8.3, -4.8, 0.5                      //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=-8.3,  4.8, 0.5                      //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.0                   //Scalar for fuel flow efficiency
min_throttle_limit=-0.250000
[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=4                     //Number of propeller blades
propeller_moi=24                    //Propeller moment of inertia
beta_max=45                    //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=15.2                  //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=17.6                  //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=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=TRUEprop_reverse_available=1                     //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta= 1.000
minimum_reverse_beta= -14.000
prop_reverse_available= 1
[TurbineEngineData]
fuel_flow_gain=0.011                 //Gain on fuel flow
inlet_area=1.0                   //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920                 //RPM, second stage compressor rated value
static_thrust=158                   //Lbs, max rated static thrust at Sea Level
[turboprop_engine]
power_scalar=1.0                   //Scalar on Turboprop power
maximum_torque=3270                  //Maximum torque available (ft-lbs)
[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 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                        <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,  18.20,   0.00, -4.3, 1181, 0, 0.596, 45.0, 0.296, 2.5, 0.9516,  4.8,  4.8, 0, 0.0, 0.0
point.1=1,  -1.00,  -8.50, -4.6, 1574, 1, 0.596,  0.0, 0.642, 2.5, 0.8152,  4.5,  5.2, 2, 0.0, 0.0
point.2=1,  -1.00,   8.50, -4.6, 1574, 2, 0.596,  0.0, 0.642, 2.5, 0.8152,  4.8,  4.9, 3, 0.0, 0.0
point.3=2,  -3.33, -23.92, -3.00,  787, 0, 0.000,  0.0, 0.000, 0.0, 0.0000,  0.0,  0.0, 5, 0.0, 0.0
point.4=2,  -3.33,  23.92, -3.00,  787, 0, 0.000,  0.0, 0.000, 0.0, 0.0000,  0.0,  0.0, 6, 0.0, 0.0
point.5=2, -22.67,   0.00,  0.00,  787, 0, 0.000,  0.0, 0.000, 0.0, 0.0000,  0.0,  0.0, 9, 0.0, 0.0
point.6=2,  23.08,   0.00, -1.50,  787, 0, 0.000,  0.0, 0.000, 0.0, 0.0000,  0.0,  0.0, 4, 0.0, 0.0
static_pitch=-1.0
static_cg_height=4.3
gear_system_type=0
[Views]
eyepoint=15.50, -1.20, 4.50
[flaps.0]
type=1                                    // 1 - tail, 2 - lead
span-outboard=0.5                                  // 0.0 .. 1.0
extending-time=5                                    // seconds
flaps-position.0=0                                    // degrees
flaps-position.1=20                                   // degrees
flaps-position.2=40                                   // degrees
damaging-speed=250                                  // KIAS
blowout-speed=300                                  // KIAS
[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1
Transponder.1=1
Marker.1=1
[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, 250
aileron=150, 250
rudder=150, 250
[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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=3,   1.25, -28.80,  1.65, fx_navredm ,
light.1=3,   1.25,  28.80,  1.65, fx_navgrem ,
light.2=3, -33.40,   0.00,  3.40, fx_navwhih ,
light.3=2,   0.89, -28.80,  1.65, fx_strobeh ,
light.4=2,   0.89,  28.80,  1.65, fx_strobeh ,
light.5=1, -31.90,   0.00, 13.40, fx_beaconb ,
light.6=2,   8.60,   0.00, -0.70, fx_beaconb ,
light.7=4,  15.50,   0.00,  4.50, fx_vclight,
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
LeftMain=0.0, -14.5, -1.0, 190.0, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux=0.0,  -6.0, -1.5,  79.5, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=0.0,  14.5, -1.0, 190.0, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux=0.0,   6.0, -1.5,  79.5, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=2                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=0
[airplane_geometry]
wing_area=310.0                 //Square feet
wing_span=57.2                  //Feet
wing_root_chord=5.4                   //Feet
wing_dihedral=6.0                   //Degrees
wing_incidence=1.0                   //Degrees
wing_twist=-1.5                  //Degrees
oswald_efficiency_factor=0.7                   //Measure of lift effeciency of wing
wing_winglets_flag=1                     //Are winglets available?
wing_sweep=1.0                   //Degrees, wing leading edge
wing_pos_apex_lon=2.1                   //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=67.0                  //Square feet
htail_span=17.2                  //Feet
htail_pos_lon=-22.6                 //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=0.5                   //Degrees
htail_sweep=20.0                  //Degrees, horizontal tail leading edge
vtail_area=42.0                  //Square feet
vtail_span=7.4                   //Feet, tip to body
vtail_sweep=40.0                  //Degrees, vertical tail leading edge
vtail_pos_lon=-20.5                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=4.1                   //Feet, vertical distance from reference point, positive going up
elevator_area=17.0                  //Square feet
aileron_area=13.5                  //Square feet
rudder_area=7.3                   //Square feet
elevator_up_limit=17.0                  //Degrees
elevator_down_limit=15.5                  //Degrees
aileron_up_limit=18.0                  //Degrees
aileron_down_limit=18.0                  //Degrees
rudder_limit=30.0                  //Degrees
elevator_trim_limit=15.0                  //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
[Reference Speeds]
flaps_up_stall_speed=96.0                  //Knots True (KTAS)
full_flaps_stall_speed=76.8                  //Knots True (KTAS)
cruise_speed=315.0                 //Knots True (KTAS)
max_indicated_speed=259.000000
max_mach=0.579980
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=0
pitch_takeoff_ga=8.000000
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
[forcefeedback]
stick_shaker_magnitude=5000             ; 0 - 10000
stick_shaker_direction=0                ; 0 - 35999 degrees
stick_shaker_period=111111              ; in microseconds
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=9000           ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=27000         ; 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
[brakes]
toe_brakes_scale=1.000000
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