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[fltsim.0]
title=SMS B737-800 China Airlines (No VC)
sim=Boeing737-800
model=a
panel=
sound=
texture=CAL
atc_id=B-18609
atc_id_color=0xffffffff
atc_airline=Dynasty
atc_flight_number=557
ui_manufacturer=Simmer's Sky
ui_type=Boeing 737-800
ui_variation=CHINA AIRLINES B-18609 (No VC)
description=Overland Co.,Ltd. Products --- Boeing 737-800\nTYPE A Cockpit Window\nNo Winglet\nL1 Cabin Door [Shift+E] then [1]\nAirstair Wing Fold/Extend\nCargo Door Water Rudder Up/Down\nL2/R2 Cabin Door Tailhook Extend/Retruct
[fltsim.1]
title=SMS B737-800 China Airlines with WL (No VC)
sim=Boeing737-800
model=a_wl
panel=
sound=
texture=CAL_wl
atc_id=B-18610
atc_id_color=0xffffffff
atc_airline=Dynasty
atc_flight_number=557
ui_manufacturer=Simmer's Sky
ui_type=Boeing 737-800
ui_variation=CHINA AIRLINES B-18610 (No VC)
description=Overland Co.,Ltd. Products --- Boeing 737-800\nTYPE A Cockpit Window\nWinglet\nL1 Cabin Door [Shift+E] then [1]\nAirstair Wing Fold/Extend\nCargo Door Water Rudder Up/Down\nL2/R2 Cabin Door Tailhook Extend/Retruct
[fltsim.2]
title=SMS B737-800 China Eastern Airlines (No VC)
sim=Boeing737-800
model=a
panel=
sound=
texture=CES
atc_id=B-2660
atc_airline=China Eastern
atc_flight_number=1125
ui_manufacturer=Simmer's Sky
ui_type=Boeing 737-800
ui_variation=CHINA EASTERN AIRLINES B-2660 (No VC)
visual_damage=1
description=Overland Co.,Ltd. Products --- Boeing 737-800\nTYPE A Cockpit Window\nNo Winglet\nL1 Cabin Door [Shift+E] then [1]\nAirstair Wing Fold/Extend\nCargo Door Water Rudder Up/Down\nL2/R2 Cabin Door Tailhook Extend/Retruct
[fltsim.3]
title=SMS B737-800 China Eastern Airlines with WL (No VC)
sim=Boeing737-800
model=b_wl
panel=
sound=
texture=CES_wl
atc_id=B-5101
atc_airline=China Eastern
atc_flight_number=1125
ui_manufacturer=Simmer's Sky
ui_type=Boeing 737-800
ui_variation=CHINA EASTERN AIRLINES B-5101 (No VC)
visual_damage=1
description=Overland Co.,Ltd. Products --- Boeing 737-800\nTYPE B Cockpit Window\nWinglet\nL1 Cabin Door [Shift+E] then [1]\nAirstair Wing Fold/Extend\nCargo Door Water Rudder Up/Down\nL2/R2 Cabin Door Tailhook Extend/Retruct
[fltsim.4]
title=SMS B737-800 Turkish Airlines (No VC)
sim=Boeing737-800
model=a
panel=
sound=
texture=THY
atc_id=TC-JFV
atc_airline=Turkair
atc_flight_number=505
ui_manufacturer=Simmer's Sky
ui_type=Boeing 737-800
ui_variation=TURKISH AIRLINES TC-JFV (No VC)
visual_damage=0
description=Overland Co.,Ltd. Products --- Boeing 737-800\nTYPE A Cockpit Window\nNo Winglet\nL1 Cabin Door [Shift+E] then [1]\nAirstair Wing Fold/Extend\nCargo Door Water Rudder Up/Down\nL2/R2 Cabin Door Tailhook Extend/Retruct
[fltsim.5]
title=SMS B737-800 Turkish Airlines with WL (No VC)
sim=Boeing737-800
model=a_wl
panel=
sound=
texture=THY_wl
atc_id=TC-JFT
atc_airline=Turkair
atc_flight_number=505
ui_manufacturer=Simmer's Sky
ui_type=Boeing 737-800
ui_variation=TURKISH AIRLINES TC-JFT (No VC)
visual_damage=0
description=Overland Co.,Ltd. Products --- Boeing 737-800\nTYPE A Cockpit Window\nWinglet\nL1 Cabin Door [Shift+E] then [1]\nAirstair Wing Fold/Extend\nCargo Door Water Rudder Up/Down\nL2/R2 Cabin Door Tailhook Extend/Retruct
[fltsim.6]
title=SMS B737-800 Korean Air (No VC)
sim=Boeing737-800
model=a
panel=
sound=
texture=KAL
atc_id=HL7568
atc_airline=Korean Air
atc_flight_number=502
ui_manufacturer=Simmer's Sky
ui_type=Boeing 737-800
ui_variation=KOREAN AIR LINES HL7568 (No VC)
visual_damage=0
description=Overland Co.,Ltd. Products --- Boeing 737-800\nTYPE A Cockpit Window\nNo Winglet\nL1 Cabin Door [Shift+E] then [1]\nAirstair Wing Fold/Extend\nCargo Door Water Rudder Up/Down\nL2/R2 Cabin Door Tailhook Extend/Retruct
[fltsim.7]
title=SMS B737-800 China Airlines (VC)
sim=Boeing737-800
model=a_VC
panel=
sound=
texture=CAL
atc_id=B-18609
atc_id_color=0xffffffff
atc_airline=DYNASTY
atc_flight_number=557
ui_manufacturer=Simmer's Sky
ui_type=Boeing 737-800
ui_variation=CHINA AIRLINES B-18609
description=Overland Co.,Ltd. Products --- Boeing 737-800\nTYPE A Cockpit Window\nNo Winglet\nL1 Cabin Door [Shift+E] then [1]\nAirstair Wing Fold/Extend\nCargo Door Water Rudder Up/Down\nL2/R2 Cabin Door Tailhook Extend/Retruct
[fltsim.8]
title=SMS B737-800 China Airlines with WL (VC)
sim=Boeing737-800
model=a_wlVC
panel=
sound=
texture=CAL_wl
atc_id=B-18610
atc_id_color=0xffffffff
atc_airline=DYNASTY
atc_flight_number=557
ui_manufacturer=Simmer's Sky
ui_type=Boeing 737-800
ui_variation=CHINA AIRLINES B-18610
description=Overland Co.,Ltd. Products --- Boeing 737-800\nTYPE A Cockpit Window\nWinglet\nL1 Cabin Door [Shift+E] then [1]\nAirstair Wing Fold/Extend\nCargo Door Water Rudder Up/Down\nL2/R2 Cabin Door Tailhook Extend/Retruct
[fltsim.9]
title=SMS B737-800 China Eastern Airlines (VC)
sim=Boeing737-800
model=a_VC
panel=
sound=
texture=CES
atc_id=B-2660
atc_airline=China Eastern
atc_flight_number=1125
ui_manufacturer=Simmer's Sky
ui_type=Boeing 737-800
ui_variation=CHINA EASTERN AIRLINES B-2660
visual_damage=1
description=Overland Co.,Ltd. Products --- Boeing 737-800\nTYPE A Cockpit Window\nNo Winglet\nL1 Cabin Door [Shift+E] then [1]\nAirstair Wing Fold/Extend\nCargo Door Water Rudder Up/Down\nL2/R2 Cabin Door Tailhook Extend/Retruct
[fltsim.10]
title=SMS B737-800 China Eastern Airlines with WL (VC)
sim=Boeing737-800
model=b_wlVC
panel=
sound=
texture=CES_wl
atc_id=B-5101
atc_airline=China Eastern
atc_flight_number=1125
ui_manufacturer=Simmer's Sky
ui_type=Boeing 737-800
ui_variation=CHINA EASTERN AIRLINES B-5101
visual_damage=1
description=Overland Co.,Ltd. Products --- Boeing 737-800\nTYPE B Cockpit Window\nWinglet\nL1 Cabin Door [Shift+E] then [1]\nAirstair Wing Fold/Extend\nCargo Door Water Rudder Up/Down\nL2/R2 Cabin Door Tailhook Extend/Retruct
[fltsim.11]
title=SMS B737-800 Turkish Airlines (VC)
sim=Boeing737-800
model=a_VC
panel=
sound=
texture=THY
atc_id=TC-JFV
atc_airline=Turkair
atc_flight_number=505
ui_manufacturer=Simmer's Sky
ui_type=Boeing 737-800
ui_variation=TURKISH AIRLINES TC-JFV
visual_damage=0
description=Overland Co.,Ltd. Products --- Boeing 737-800\nTYPE A Cockpit Window\nNo Winglet\nL1 Cabin Door [Shift+E] then [1]\nAirstair Wing Fold/Extend\nCargo Door Water Rudder Up/Down\nL2/R2 Cabin Door Tailhook Extend/Retruct
[fltsim.12]
title=SMS B737-800 Turkish Airlines with WL (VC)
sim=Boeing737-800
model=a_wlVC
panel=
sound=
texture=THY_wl
atc_id=TC-JFT
atc_airline=Turkair
atc_flight_number=505
ui_manufacturer=Simmer's Sky
ui_type=Boeing 737-800
ui_variation=TURKISH AIRLINES TC-JFT
visual_damage=0
description=Overland Co.,Ltd. Products --- Boeing 737-800\nTYPE A Cockpit Window\nWinglet\nL1 Cabin Door [Shift+E] then [1]\nAirstair Wing Fold/Extend\nCargo Door Water Rudder Up/Down\nL2/R2 Cabin Door Tailhook Extend/Retruct
[fltsim.13]
title=SMS B737-800 Korean Air (VC)
sim=Boeing737-800
model=a_VC
panel=
sound=
texture=KAL
atc_id=HL7568
atc_airline=Korean Air
atc_flight_number=502
ui_manufacturer=Simmer's Sky
ui_type=Boeing 737-800
ui_variation=KOREAN AIR LINES HL7568
visual_damage=0
description=Overland Co.,Ltd. Products --- Boeing 737-800\nTYPE A Cockpit Window\nNo Winglet\nL1 Cabin Door [Shift+E] then [1]\nAirstair Wing Fold/Extend\nCargo Door Water Rudder Up/Down\nL2/R2 Cabin Door Tailhook Extend/Retruct
[General]
atc_type=BOEING
atc_model=B737
editable=1
performance="Cruise Speed \n492 kts 573 mph 912 km\/h\n\nEngines \nCFM56-7B\n\nMaximum Range \n1990 nm 3,585 km\n\nService Ceiling \n30,000 ft 9,144 m\n\nFuel Capacity \n6,875 U.S. gal 26,024 L\n\nEmpty Weight-Standard \n90,710 lb 41,145 kg\n\nMaximum Gross Weight\n155,500 lb 70,535 kg\n\nLength \n129 ft, 6 in 39.47 m\n\nWingspan \n112 ft, 7 in 34.31 m\n\nHeight \n41 ft, 2 in 12.55 m\n\nSeating \nSeats 162 to 189\n\n"
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
[WEIGHT_AND_BALANCE]
max_gross_weight = 174700 // (pounds)
empty_weight = 90710 // (pounds)
reference_datum_position = 0, 0, -2.4 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 6.8, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = "170.0, 41.0, -1.5, 0.0, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170.0, 41.0, 1.5, 0.0, Co-Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "510.0, 0.0, 0.0, 0.0, Crew" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "1360.0, 25.5, 0.0, 0.0, First Class" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "8160.0, 1.0, 0.0, 0.0, Coach 3-10" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = "8160.0, -20.0, 0.0, 0.0, Coach 11-18" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = "7140.0, -48.5, 0.0, 0.0, Coach 19-25" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = "2500.0, 20.5, 0.0, 0.0, Forward Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = "5000.0, -32.5, 0.0, 0.0, Aft Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 4172439
empty_weight_roll_MOI = 2262183
empty_weight_yaw_MOI = 3337024
empty_weight_coupled_MOI = 1000
[flight_tuning]
cruise_lift_scalar = 1.08
parasite_drag_scalar = 1.18
induced_drag_scalar = 1.21
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 = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 1.75, -17.2, -3.35 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 1.75, 17.2, -3.35 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 0.65 //Scalar for fuel flow efficiency
min_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reverser
max_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear
[TurbineEngineData]
fuel_flow_gain = 0.002 //Gain on fuel flow
inlet_area = 19.6 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 27300 //Lbs, max rated static thrust at Sea Level
afterburner_available = 0 //Afterburner available?
reverser_available = 1 //Thrust reverser available?
[jet_engine]
thrust_scalar = 1.0
[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, 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 <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, 45.00, 0.00, -8.02, 1181.1, 0, 1.442, 55.92, 0.6, 2.5, 0.9, 4.0, 4.0, 0, 220.0, 250.0
point.1=1, -2.75, -9.28, -9.08, 1574.8, 1, 1.442, 0.00, 1.0, 2.5, 0.9, 6.9, 6.9, 2, 220.0, 250.0
point.2=1, -2.75, 9.28, -9.08, 1574.8, 2, 1.442, 0.00, 1.0, 2.5, 0.9, 7.1, 7.1, 3, 220.0, 250.0
point.3=2, -14.17, -47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -14.17, 47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -54.00, 0.00, 2.83, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, 42.67, 0.00, -3.75, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
point.7= 5, -70.90, -15.250, -17.300, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 1.0, 1.2, 0, 0.0, 0.0
point.8= 5,-400.90, 15.250, -17.300, 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=-0.29 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=10.48 //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 = 5.0 //Flap angle that activates warning at idle
flap_limit_power = 25.5 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.885 //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
//----------------------------------- START-- EYE POINT---------------------------------------------------------------------
[Views] // cockpit
eyepoint=54.300, -1.53, 4.62 //(feet) longitudinal, lateral, vertical distance from reference datum
//[Views] // cabin L wing
eyepoint=0, -1.53, 4.55 //(feet) longitudinal, lateral, vertical distance from reference datum
//[Views] // cabin R wing
eyepoint=0, 1.53, 4.55 //(feet) longitudinal, lateral, vertical distance from reference datum
//[Views] // cabin economy
eyepoint=-22, 1.53, 4.55 //(feet) longitudinal, lateral, vertical distance from reference datum
//[Views] // cabin first
eyepoint=32, 1.53, 4.55 //(feet) longitudinal, lateral, vertical distance from reference datum
//-------------------------------------END --- EYE POINT ----------------------------------------------------------------
[flaps.0] //Trailing Edge Flaps
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 35 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 1 // degrees
flaps-position.2 = 5 // degrees
flaps-position.3 = 10 // degrees
flaps-position.4 = 15 // degrees
flaps-position.5 = 20 // degrees
flaps-position.6 = 25 // degrees
flaps-position.7 = 30 // degrees
flaps-position.8 = 40 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1 //Hydraulic
[flaps.1] //Inboard Leading Edge Flaps
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 15 // seconds
flaps-position.0 = 0 //
flaps-position.1 = 1.0 //
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1 //Hydraulic
[flaps.2] //Outboard Leading Edge Slat
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 15 // seconds
flaps-position.0 = 0 //
flaps-position.1 = 0
flaps-position.2 = 1.0 //
flaps-position.4 = 1.0 //
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1 //Hydraulic
[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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -14.02, -56.65, 4.08, fx_navred ,
light.1 = 3, -14.02, 56.65, 4.08, fx_navgre ,
light.2 = 2, -15.22, -57.08, 4.08, fx_strobe ,
light.3 = 2, -15.22, 57.08, 4.08, fx_strobe ,
light.4 = 2, 1.60, 0.00, -4.75, fx_beaconb ,
light.5 = 1, 8.21, 0.00, 9.30, fx_beaconh ,
light.6 = 3, -62.80, 0.00, 6.82, fx_navwhi ,
light.7 = 3, -62.80, 0.00, 6.82, fx_navwhi ,
light.8 = 3, -19.12, -57.71, 3.88, fx_navwhi ,
light.9 = 3, -19.12, 57.71, 3.88, fx_navwhi ,
light.10 = 5, 13.12, -2.31, -4.38, fx_landing ,
light.11 = 5, 13.12, 2.31, -4.38, fx_landing ,
light.12 = 5, 13.62, -7.18, -0.38, fx_landing ,
light.13 = 5, 13.62, 7.18, -0.38, fx_landing ,
light.14 = 5, 31.00, 0.00, -10.00, sms_land ,
light.15 = 4, 55.2 , 0, 5.25, fx_vclighth
[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
[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=0,0
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm = 90
autothrottle_takeoff_ga=1
pitch_takeoff_ga = 8;
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=12.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=25.0
gs_integrator_control=0.53
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
[fuel]
Center1 = 0, 0, 0, 4299, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -3, -19, 0, 1288, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -3, 19, 0, 1288, 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 = 1341.0 //Square feet
wing_span = 112.7 //Feet
wing_root_chord = 18.0 //Feet
wing_dihedral = 5.2 //Degrees
wing_incidence = 1.0 //Degrees
wing_twist = 0.5 //Degrees
oswald_efficiency_factor= 0.77 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 25.0 //Degrees, wing leading edge
wing_pos_apex_lon = 15.1 //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 = 338.0 //Square feet
htail_span = 41.7 //Feet
htail_pos_lon = -49.7 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 5.7 //Feet, vertical distance from reference point, positive going up
htail_incidence = -0.91 //Degrees
htail_sweep = 30.0 //Degrees, horizontal tail leading edge
vtail_area = 224.0 //Square feet
vtail_span = 20.0 //Feet, tip to body
vtail_sweep = 35.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -43.2 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 8.9 //Feet, vertical distance from reference point, positive going up
elevator_area = 70.5 //Square feet
aileron_area = 26.9 //Square feet
rudder_area = 56.2 //Square feet
elevator_up_limit = 22.5 //Degrees
elevator_down_limit = 19.5 //Degrees
aileron_up_limit = 20.0 //Degrees
aileron_down_limit = 20.0 //Degrees
rudder_limit = 26.0 //Degrees
elevator_trim_limit = 20.0 //Degrees
spoiler_limit = 60.0 //Degrees
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 3 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 10 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
[Reference Speeds]
flaps_up_stall_speed = 142.0 //Knots True (KTAS)
full_flaps_stall_speed = 113.0 //Knots True (KTAS)
cruise_speed = 477.0 //Knots True (KTAS)
max_mach = 0.82
max_indicated_speed = 340 //Red line (KIAS)
[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=2
[folding_wings]
wing_fold_system_type=4 ;0=None
fold_rates=0.12,0.11 ;Percent per second
[TailHook]
tailhook_length=4 ;(feet)
tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=0.0
