[fltsim.0]
title=Project Opensky - Boeing 737-800 Air Algerie
sim=OSBoeing737-800
model=
panel=
sound=
texture=airalgerie
kb_checklists=Boeing737-800_check
kb_reference=Boeing737-800_ref
atc_id=7T-VJK
atc_airline=ALG
atc_flight_number=754
atc_heavy=0
atc_parking_types=GATE, RAMP
atc_parking_code=ALG
ui_manufacturer=Boeing
ui_type=737-800
ui_variation=Air Algerie
visual_damage=1
description=Project Opensky - Boeing 737-800\nVersion - Version 2004.9.2\n\nModel Designer\n Hiroshi Igami\n\nFlight Dynamics/Scenario/Effects Designer\n Warren C. Daniel\n\nMaster Texture Designer\n Tom Harlaar\n\nTest Pilots\n Project Opensky Members\n\nMaximun Range: \n 3,383 nautical miles
[General]
atc_type=BOEING
atc_model=B738
editable=0
performance=Passengers\n2-class conf: 162\n\nCargo\nTotal lower hold volume: \n1,555 cu ft (44 cu m)\n\nDimensions\nSpan 112 ft 7 in (34.3 m)\nLength 129 ft 6 in (39.5 m)\nHeight 41 ft 2 in (12.5 m)\nEngines: GE CFM56-7B\nTO Thrust Rating: 27,300 lb (121 kN)\n\nMax Fuel Cap.: 6,875 US gal (26,035 L)\nMaxTOW: 174,200 lb\n\nTypical Cruise Speed\n @ FL350: M.785
[pitot_static]
vertical_speed_time_constant = 999 //Increasing this value will cause a more instantaneous reaction in the VSI
[WEIGHT_AND_BALANCE]
max_gross_weight = 174700.000
empty_weight = 91300.000
reference_datum_position = 5.000, 0.000, 0.000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0.000, 0.000, 0.000 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
// New FS2004 Numbers
// Max 2-class - 160, Max Econ only - 184
// Actual Total PAX - 38,150 lbs
station_load.0 = 2720.000000, 25.000000, 0.000000, 0.000000, 1st Class-16
station_load.1 =24140.000000, 0.000000, 0.000000, 0.000000, Econ Class-142
// Total Opensky Cargo - 17,350 lbs
station_load.2 =5925.000000, 20.000000, 0.000000, 0.000000, Lwr Dk Cgo Fwd
station_load.3 =5925.000000, -61.000000, 0.000000, 0.000000, Lwr Dk Cgo Aft
station_load.4 = 174.000000, -67.000000, 0.000000, 0.000000, Lwr Dk Cgo Bulk
// Moments of Inertia
empty_weight_pitch_MOI = 1595057.280
empty_weight_roll_MOI = 1649603.980
empty_weight_yaw_MOI = 2742152.520
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =1.201
induced_drag_scalar =1.201
elevator_effectiveness =1.500
aileron_effectiveness =0.350
rudder_effectiveness =0.251
pitch_stability =1.000
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =0.751
aileron_trim_effectiveness =0.501
rudder_trim_effectiveness =0.501
[GeneralEngineData]
engine_type = 1
Engine.0 = 4.750, -16.100, -4.500
Engine.1 = 4.750, 16.100, -4.500
fuel_flow_scalar = 1.30
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]
bypass_ratio = 5.1
fuel_flow_gain = 0.002
inlet_area = 20.270
rated_N2_rpm = 29920.000
static_thrust = 26000.000 //Lbs, Per AA
//static_thrust = 27300 //Lbs, Per GE
afterburner_available = 0
reverser_available = 1.000
[jet_engine]
thrust_scalar =1.000
[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
[contact_points]
//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)
//
// Nose Gear
point.0 = 1, 48.450, -0.67, -8.85, 1181.1, 0, 1.777, 75.00, 1.000, 1.500, 0.550, 9.000, 9.000, 0, 235.0, 320.0
point.1 = 1, 48.450, 0.67, -8.85, 1181.1, 0, 1.777, 75.00, 1.000, 1.500, 0.550, 9.000, 9.000, 0, 235.0, 320.0
// Left Main Gear
point.2=1, -5.00, -9.99, -9.20, 1574.8, 1, 1.442, 0.00, 1.0, 2.5, 0.650, 6.9, 6.9, 2, 230.0, 320.0
point.3=1, -5.00, -7.16, -9.20, 1574.8, 1, 1.442, 0.00, 1.0, 2.5, 0.650, 6.9, 6.9, 2, 230.0, 320.0
// Right Main Gear
point.4=1, -5.00, 9.99, -9.20, 1574.8, 2, 1.442, 0.00, 1.0, 2.5, 0.650, 7.1, 7.1, 3, 230.0, 320.0
point.5=1, -5.00, 7.16, -9.20, 1574.8, 2, 1.442, 0.00, 1.0, 2.5, 0.650, 7.1, 7.1, 3, 230.0, 320.0
//
//
//=======================================================================================================================================================
//
//FUll Motion, Realistic feel, true footprint contact points
//
// Nose Gear
//point.0 = 1, 48.450, -0.67, -9.85, 1181.1, 0, 1.777, 75.00, 3.000, 1.500, 0.650, 9.000, 9.000, 0, 235.0, 320.0
//point.1 = 1, 48.450, 0.67, -9.85, 1181.1, 0, 1.777, 75.00, 3.000, 1.500, 0.650, 9.000, 9.000, 0, 235.0, 320.0
//
// Left Main Gear
//point.2=1, -5.000, -9.99, -10.50, 1574.8, 1, 1.442, 0.00, 3.000, 2.000, 0.650, 6.900, 6.900, 2, 230.0, 320.0
//point.3=1, -5.000, -7.16, -10.50, 1574.8, 1, 1.442, 0.00, 3.000, 2.000, 0.650, 6.900, 6.900, 2, 230.0, 320.0
//
// Right Main Gear
//point.4=1, -5.000, 9.99, -10.50, 1574.8, 2, 1.442, 0.00, 3.000, 2.000, 0.650, 8.100, 7.100, 3, 230.0, 320.0
//point.5=1, -5.000, 7.16, -10.50, 1574.8, 2, 1.442, 0.00, 3.000, 2.000, 0.650, 8.100, 7.100, 3, 230.0, 320.0
//
//
//
// Scrape Points
// Fuselage
point.6 = 2, 64.000, 0.000, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Nose
point.7 = 2, 54.000, 0.000, -3.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage bottom fwd
point.8 = 2, 0.000, 0.000, -3.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage bottom center
point.9 = 2, -25.000, 0.000, -3.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage bottom aft
point.10= 2, 38.000, 0.000, 16.800, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage top fwd
point.11= 2, 0.000, 0.000, 16.800, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage top center
point.12= 2, -35.000, 0.000, 16.800, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage top aft
point.13= 2, 38.000, -6.170, 1.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width fwd lt
point.14= 2, 38.000, 6.170, 1.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width fwd rt
point.15= 2, 0.000, -6.170, 1.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width center lt
point.16= 2, 0.000, 6.170, 1.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width center rt
point.17= 2, -35.000, -6.170, 1.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width aft left
point.18= 2, -35.000, 6.170, 1.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width aft right
point.19= 2, -45.000, 0.000, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Tailskid aft
point.20= 2, -60.900, 0.000, 10.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Tail-APU
// Tailplane, vert/horiz stabs
point.21= 2, -57.600, 0.000, 31.750, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7, 0.000, 0.000 // Vertical stab fwd
point.22= 2, -62.600, 0.000, 31.750, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7, 0.000, 0.000 // Vertical stab aft
point.23= 2, -65.650, -23.550, 17.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.000, 0.000 // Horizontal Stab aft lt
point.24= 2, -65.650, 23.550, 17.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.000, 0.000 // Horizontal Stab aft rt
// Wings
point.25= 2, -15.000, -56.350, 10.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.000, 0.000 // Left wingtip fwd
point.26= 2, -20.000, -56.350, 10.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.000, 0.000 // Left wingtip aft
point.27= 2, -15.000, 56.350, 10.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.000, 0.000 // Right wingtip fwd
point.28= 2, -20.000, 56.350, 10.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.000, 0.000 // Right wingtip aft
point.29= 2, -2.000, -37.000, 5.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.000, 0.000 // Left wing-mid fwd
point.30= 2, -12.000, -37.000, 5.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.000, 0.000 // Left wing-mid aft
point.31= 2, -2.000, 37.000, 5.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.000, 0.000 // Right wing-mid fwd
point.32= 2, -12.000, 37.000, 5.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.000, 0.000 // Right wing-mid aft
// Engines
point.33= 2, 20.900, -15.830, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8, 0.000, 0.000 // Left engine fwd
point.34= 2, 20.900, 15.830, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8, 0.000, 0.000 // Right engine fwd
point.35= 2, 15.000, -15.830, -6.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8, 0.000, 0.000 // Left engine bottom
point.36= 2, 15.000, 15.830, -6.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8, 0.000, 0.000 // Right engine bottom
max_number_of_points = 37
static_pitch= -1.000
//static_cg_height=7.67
static_cg_height=8.10
gear_system_type=1 //Hydraulic
[gear_warning_system]
gear_warning_available = 0 //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 = 0.43 //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
[Views]
eyepoint=55.00, -1.31, 3.7 //(feet) longitudinal, lateral, vertical distance from reference datum - Opensky Model
//eyepoint=38.70, -1.31, 3.7 // Default FS VC
[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, 6=taxi, 7=recognition, 8=wing, 9=logo
light.1 = 1, 1.600, 0.000, -4.500, Opensky_beacon ,
light.2 = 1, 9.300, 0.000, 9.300, Opensky_beacon ,
light.3 = 4, 57.000, 0.000, 3.500, Opensky_Boeing_vclight ,
light.4 = 3, 30.000, 0.000, -3.000, Opensky_nacelle_refl , // front cargo
light.5 = 3, -33.000, 0.000, -2.000, Opensky_nacelle_refl , // rear cargo
light.6 = 3, 40.000, 0.000, 4.000, Opensky_nacelle_refl , // pax door
light.7 = 8, 14.000, -36.000, 5.000, Opensky_wing_light , // wing/LE slat rays from inspection lights
light.8 = 8, 14.000, 35.000, 5.000, Opensky_wing_light , // wing/LE slat rays from inspection lights
light.9 = 8, 25.400, -6.200, 2.100, Opensky_nav_yellow , // flap inspection light
light.10= 8, 25.400, 6.200, 2.100, Opensky_nav_yellow , // flap inspection light
light.11= 8, 30.000, -6.200, -1.000, Opensky_nacelle_refl , // wing/LE slat rays from inspection lights
light.12= 8, 30.000, 6.200, -1.000, Opensky_nacelle_refl , // wing/LE slat rays from inspection lights
light.13= 8, 23.000, -12.500, -2.000, Opensky_nacelle_refl , // wing/LE slat rays from inspection lights
light.14= 8, 23.000, 12.500, -2.000, Opensky_nacelle_refl , // wing/LE slat rays from inspection lights
light.15= 6, 60.000, 0.000, -12.550, Opensky-taxi-refl , // gear bay taxi light rays from taxi lights
light.16= 3, -62.000, 0.000, 7.000, Opensky_nav_yellow , // Tail Nav Light
light.17= 2, -62.000, 0.000, 7.000, fx_strobeh , // Tail Strobe Light
[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 = 100, 200
aileron = 100, 200
rudder = 100, 200
[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 = 3
exit_rate.0 = 0.10 ;Percent per second
exit_rate.1 = 0.12 ;Percent per second
exit_rate.2 = 0.12 ;Percent per second
[folding_wings]
wing_fold_system_type=4 ;0=None
fold_rates=0.12,0.11 ;Percent per second
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=Opensky_sparks, 1
touchdown=fx_tchdwn, 1
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=0.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=96.8
pitch_takeoff_ga= 0.000
use_no_default_pitch = 1 // 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank = 1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode.
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=0.300000
max_pitch_velocity_lo_alt_breakpoint= 7000.000000
max_pitch_velocity_hi_alt_breakpoint=24000.000000
max_bank=32.000000
max_bank_acceleration=1.200000
max_bank_velocity=1.500000
max_throttle_rate=0.02800
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=1.000000
[fuel]
// Total Fuel - 46,063 lbs, 6814 US Gallons -- Total Usable Fuel - 46,000 lbs, 6804 US Gallons
//
Center1 = 5.000, 0.000, 0.000, 4260.000, 0.000 // Center Tank
LeftMain = 3.000, -19.000, 0.000, 1272.000, 0.000 // Main 1 Tank
RightMain = 3.000, 19.000, 0.000, 1272.000, 0.000 // Main 2 Tank
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=0
[airplane_geometry]
wing_area = 1137.000
wing_span = 112.700
wing_root_chord = 18.000
wing_dihedral = 6.200
wing_incidence = 1.000
wing_twist = -0.500
oswald_efficiency_factor= 0.750
wing_winglets_flag = 0
wing_sweep = 25.000
wing_pos_apex_lon = 15.000
wing_pos_apex_vert = 0.000
htail_area = 338.000
htail_span = 41.700
htail_pos_lon = -60.000
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 30.000
vtail_area = 224.000
vtail_span = 20.000
vtail_sweep = 35.000
vtail_pos_lon = -53.000
vtail_pos_vert = 5.800
elevator_area = 70.500
aileron_area = 26.900
rudder_area = 56.200
elevator_up_limit = 24.000
elevator_down_limit = 18.000
aileron_up_limit = 25.000
aileron_down_limit = 15.000
rudder_limit = 15.000
elevator_trim_limit = 15.000
spoiler_limit = 30.000
spoilerons_available = 1
aileron_to_spoileron_gain = 2.000
min_ailerons_for_spoilerons=15.000
min_flaps_for_spoilerons = 0.000
[Reference Speeds]
flaps_up_stall_speed = 142.000
full_flaps_stall_speed = 113.000
cruise_speed = 452.160
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
[flaps.0] //Trailing Edge Flaps
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.3 // 0.0 .. 1.0
extending-time = 36 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 1 // degrees
flaps-position.2 = 2 // degrees
flaps-position.3 = 5 // degrees
flaps-position.4 = 10 // degrees
flaps-position.5 = 15 // 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 = 1.00
drag_scalar = 0.40
pitch_scalar= 1.0
system_type = 1 //Hydraulic
[flaps.1] //Inboard Leading Edge Flaps
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.3 // 0.0 .. 1.0
extending-time = 36 // seconds
flaps-position.0 = 0 //
flaps-position.1 = 20 //
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.00
drag_scalar = 0.15
pitch_scalar= 1.0
system_type = 1 //Hydraulic
[flaps.2] //Outboard Leading Edge Slat
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.6 // 0.0 .. 1.0
extending-time = 36 // seconds
flaps-position.0 = 0 //
flaps-position.1 = 10 //
flaps-position.2 = 20 //
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.00
drag_scalar = 0.15
pitch_scalar= 1.0
system_type = 1 //Hydraulic
