[fltsim.0]
title=Project Opensky - Boeing 747-200F British Airways SCD Cargo
sim=747-200F-RR-RB-211-524
model=
panel=
sound=
texture=BA
kb_checklists=boeing747_check
kb_reference=boeing747_ref
atc_airline=SPEED BIRD
atc_flight_number=625
atc_parking_types=CARGO
atc_parking_code=BA
ui_typerole=Commercial Airliner
ui_createdby=Project Opensky
ui_manufacturer=Project Opensky
ui_type=747-200F
ui_variation=British Airways SCD Cargo
visual_damage=1
atc_heavy=1
atc_id=G-KILO
description=Project Opensky \nBoeing 747-200F\nVersion 2006.9.7-FSX\n\nEngine Type RR RB.211-524\n\n747-200 Commercial Version \n\nModel Designer\n Hiroshi Igami\n\nFlight Dynamics Designer\n Warren C. Daniel\n Brandon D. Henry\n\nMaster Texture Designer\n Corey Ford\n\nTest Pilots\n Project Opensky Members\n\nCathay Pacific textures by Andrew Horeckyj using the POSKY paintkit\n\nMaximun Range: 6,620 nm\n\nTypical city pairs: \n Tokyo-NY\n Bangkok-Paris\n London-Johannesburg\n\nFor proper operation: See B747 manual at: \n www.projectopensky.com
[General]
performance=Cargo\nAft Bulk: 520 ft3 (9,720 lb) \nLower Deck Aft: 2800 ft3 (57,500 lb)\nLower Deck Fwd: 2800 ft3 (61,000 lb)\nMain Deck: 21,117 ft3 (load dependant)\n\nDimensions\nSpan 195 ft 8 in \nLength 231 ft 10 in\nHeight 63 ft 5 in\n\nMax Fuel Cap.: 53,644 US Gal.\nMax Gross Taxi Weight: 803,000 lb\nMax Gross TOW: 800,000 lb\nMLW: 630,000 lb\nMax Payload 244,670 lb\nOEW: 351,930 lb\n\nWheels\/Brakes: BF Goodrich\/Carbon Brakes\nNoise Compliance: Stage II\nApproach Category: CAT II
atc_type=BOEING AIRCRAFT
atc_model=B742
editable=0
[pitot_static]
vertical_speed_time_constant=999 //Increasing this value will cause a more instantaneous reaction in the VSI
[WEIGHT_AND_BALANCE]
reference_datum_position = 97.0, 0, 0
empty_weight_CG_position = -97.0, 0, 0
max_number_of_stations = 8
station_load.0 = "9720, -150.0, 0.0, 0.0, Aft Bulk - Payload" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "57500, -150.0, 0.0, 0.0, LD aft - Payload" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "61000, -40.0, 0.0, 0.0, LD fwd - Payload" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "111020,-107.0, 0.0, 0.0, Main Dk - Payload" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "2640, -50.0, 0.0, 20.0, Upper Dk - Payload" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
empty_weight= 345330.000
max_gross_weight= 836000.000
// Moments of Inertia
empty_weight_roll_MOI= 14807465.000
empty_weight_pitch_MOI= 31142081.000
empty_weight_yaw_MOI= 46873072.000
empty_weight_coupled_MOI= 0.000
[fuel]
Center1 = -97.000, 0.0, -4.0, 17011.7, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -102.000, -35.0, -4.0, 12434.6, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux = -108.500, -52.0, -3.0, 4971.4, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -102.000, 35.0, -4.0, 12434.6, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux = -108.500, 52.0, -3.0, 4971.4, 3.0 //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=1
[airplane_geometry]
wing_area= 5500.000
wing_span= 196.000
wing_root_chord= 23.000
wing_dihedral= 6.998
wing_incidence= 2.000
wing_twist= -0.994
oswald_efficiency_factor= 0.830
wing_winglets_flag= 0
wing_sweep= 37.500
wing_pos_apex_lon= -55.100
wing_pos_apex_vert= 0.000
htail_area= 1470.000
htail_span= 72.750
htail_pos_lon= -213.000
htail_pos_vert= 10.000
htail_incidence= 0.000
htail_sweep= 37.500
vtail_area= 1060.000
vtail_span= 37.121
vtail_sweep= 45.000
vtail_pos_lon= -200.500
vtail_pos_vert= 20.083
elevator_area= 326.800
aileron_area= 225.200
rudder_area= 229.900
elevator_up_limit= 24.000
elevator_down_limit= 18.000
aileron_up_limit= 20.000
aileron_down_limit= 20.000
rudder_limit= 30.000
elevator_trim_limit= 24.000
spoiler_limit= 45.000
spoilerons_available= 0
aileron_to_spoileron_gain= 0
min_ailerons_for_spoilerons= 0
min_flaps_for_spoilerons= 0
[Reference Speeds]
flaps_up_stall_speed = 150.0 //Knots True (KTAS)
full_flaps_stall_speed = 126.0 //Knots True (KTAS)
cruise_speed = 478.0 //Knots True (KTAS)
max_indicated_speed=365.000000
max_mach=0.920000
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 25 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 5 // degrees
flaps-position.2 = 10 // degrees
flaps-position.3 = 15 // degrees
flaps-position.4 = 20 // degrees
flaps-position.5 = 25 // degrees
flaps-position.6 = 30 // degrees
damaging-speed = 200 // KIAS
blowout-speed = 250 // KIAS
lift_scalar = 0.28
drag_scalar = 0.40
pitch_scalar= 0.45
system_type = 1 //Hydraulic
[flaps.1]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.2 // 0.0 .. 1.0
extending-time = 25 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 5 // degrees
flaps-position.2 = 10 // degrees
flaps-position.3 = 15 // degrees
flaps-position.4 = 20 // degrees
flaps-position.5 = 25 // degrees
flaps-position.6 = 30 // degrees
damaging-speed = 200 // KIAS
blowout-speed = 250 // KIAS
lift_scalar = 0.28
drag_scalar = 0.40
pitch_scalar= 0.45
system_type = 1 //Hydraulic
[flaps.2]
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 12 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 10.0 // degrees
flaps-position.2 = 20.0 // degrees
flaps-position.3 = 20.0 // degrees
flaps-position.4 = 20.0 // degrees
flaps-position.5 = 20.0 // degrees
flaps-position.6 = 20.0 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.28
drag_scalar = 0.40
pitch_scalar= 0.45
system_type = 1 //Hydraulic
[flaps.3]
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 12 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 20.0 // degrees
flaps-position.2 = 20.0 // degrees
flaps-position.3 = 20.0 // degrees
flaps-position.4 = 20.0 // degrees
flaps-position.5 = 20.0 // degrees
flaps-position.6 = 20.0 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.28
drag_scalar = 0.40
pitch_scalar= 0.45
system_type = 1 //Hydraulic
[flaps.4]
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.2 // 0.0 .. 1.0
extending-time = 12 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 20.0 // degrees
flaps-position.2 = 20.0 // degrees
flaps-position.3 = 20.0 // degrees
flaps-position.4 = 20.0 // degrees
flaps-position.5 = 20.0 // degrees
flaps-position.6 = 20.0 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.28
drag_scalar = 0.40
pitch_scalar= 0.45
system_type = 1 //Hydraulic
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 1.25
aileron_effectiveness = 1.50
rudder_effectiveness = 0.75
pitch_stability = 1.0
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 0.75
aileron_trim_effectiveness = 0.65
rudder_trim_effectiveness = 0.65
[GeneralEngineData]
engine_type= 1
Engine.0= -107.600, -69.500, 0.000
Engine.1= -78.110, -39.167, -7.000
Engine.2= -78.110, 39.167, -7.000
Engine.3= -107.600, 69.500, 0.000
fuel_flow_scalar=0.8349
min_throttle_limit=-0.319946
[TurbineEngineData]
bypass_ratio=4.970000
fuel_flow_gain=0.001000
inlet_area=37.558941
rated_N2_rpm=26928.000000
static_thrust=53110.000000
afterburner_available=0
reverser_available=1
[jet_engine]
thrust_scalar = 1.0
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=800.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=105.000000
pitch_takeoff_ga=8.000000
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=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.03000
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
[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)
point.0 = 1.000, -20.333, 0.000, -13.833, 5181.102, 0.000, 2.042, 70.000, 0.300, 0.500, 0.880, 11.000, 11.000, 0.000, 240.000, 280.000 // Nose Gear
point.1 = 1.000, -110.583, -6.350, -15.403, 3574.803, 1.000, 1.917, 0.000, 1.620, 1.150, 0.741, 12.900, 14.900, 2.000, 240.000, 280.000 // Main Center Gear - Left
point.2 = 1.000, -110.583, 6.350, -15.403, 3574.803, 2.000, 1.917, 0.000, 1.620, 1.150, 0.741, 13.100, 15.400, 3.000, 240.000, 280.000 // Main Center Gear - Right
point.3 = 1.000, -102.083, -18.000, -15.403, 3574.803, 0.000, 1.917, 0.000, 1.620, 1.150, 0.741, 12.900, 14.900, 2.000, 240.000, 280.000 // Main Wing Gear - Left
point.4 = 1.000, -102.083, 18.000, -15.403, 3574.803, 0.000, 1.917, 0.000, 1.620, 1.150, 0.741, 13.100, 15.400, 3.000, 240.000, 280.000 // Main Wing Gear - Right
point.5 = 2.000, -146.000, -98.900, 7.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.6 = 2.000, -146.000, 98.900, 7.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.7 = 2.000, -189.667, 0.000, -2.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.8 = 2.000, -9.167, 0.000, -5.750, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.9 = 2.000, -229.667, 0.000, 55.500, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000
point.10= 2.000, -106.400, -69.500, -5.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.11= 2.000, -76.300, -39.167, -9.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.12= 2.000, -76.300, 39.167, -9.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.13= 2.000, -106.400, 69.500, -5.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.14= 2.000, 0.000, 0.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= 1.000
static_cg_height= 12.500
gear_system_type=0
// Nose gear
//point.0= 1.000, -20.333, -1.500, -13.750, 2181.102, 0.000, 2.000, 70.000, 0.300, 0.500, 0.880, 11.000, 11.000, 0.000, 240.000, 280.000
//point.1= 1.000, -20.333, 1.500, -13.750, 2181.102, 0.000, 2.000, 70.000, 0.300, 0.500, 0.880, 11.000, 11.000, 0.000, 240.000, 280.000
//
// Main Wing Gear (left)
//point.2= 1.000, -104.583, -18.000, -16.533, 1574.803, 1.000, 2.000, -13.000, 2.602, 2.500, 0.551, 12.900, 14.900, 2.000, 240.000, 280.000
//point.3= 1.000, -104.583, -14.000, -16.533, 1574.803, 1.000, 2.000, -13.000, 2.602, 2.500, 0.551, 12.900, 14.900, 2.000, 240.000, 280.000
//point.4= 1.000, -99.583, -18.000, -16.533, 1574.803, 1.000, 2.000, -13.000, 2.602, 2.500, 0.551, 12.900, 14.900, 2.000, 240.000, 280.000
//point.5= 1.000, -99.583, -14.000, -16.533, 1574.803, 1.000, 2.000, -13.000, 2.602, 2.500, 0.551, 12.900, 14.900, 2.000, 240.000, 280.000
//
// Main Wing Gear (right)
//point.6= 1.000, -104.583, 18.000, -16.533, 1574.803, 2.000, 2.000, -13.000, 2.602, 2.500, 0.551, 15.100, 16.400, 3.000, 240.000, 280.000
//point.7= 1.000, -104.583, 14.000, -16.533, 1574.803, 2.000, 2.000, -13.000, 2.602, 2.500, 0.551, 15.100, 16.400, 3.000, 240.000, 280.000
//point.8= 1.000, -99.583, 18.000, -16.533, 1574.803, 2.000, 2.000, -13.000, 2.602, 2.500, 0.551, 15.100, 16.400, 3.000, 240.000, 280.000
//point.9= 1.000, -99.583, 14.000, -16.533, 1574.803, 2.000, 2.000, -13.000, 2.602, 2.500, 0.551, 15.100, 16.400, 3.000, 240.000, 280.000
//
// Main Center Gear (left)
//point.10= 1.000, -115.583, -8.000, -16.533, 1574.803, 1.000, 2.000, 0.000, 2.602, 2.500, 0.551, 13.400, 14.900, 2.000, 240.000, 280.000
//point.11= 1.000, -115.583, -4.000, -16.533, 1574.803, 1.000, 2.000, 0.000, 2.602, 2.500, 0.551, 13.400, 14.900, 2.000, 240.000, 280.000
//point.12= 1.000, -109.583, -8.000, -16.533, 1574.803, 1.000, 2.000, 0.000, 2.602, 2.500, 0.551, 13.400, 14.900, 2.000, 240.000, 280.000
//point.13= 1.000, -109.583, -4.000, -16.533, 1574.803, 1.000, 2.000, 0.000, 2.602, 2.500, 0.551, 13.400, 14.900, 2.000, 240.000, 280.000
//
// Main Center Gear (right)
//point.14= 1.000, -115.583, 8.000, -16.533, 1574.803, 2.000, 2.000, 0.000, 2.602, 2.500, 0.551, 11.500, 17.500, 3.000, 240.000, 280.000
//point.15= 1.000, -115.583, 4.000, -16.533, 1574.803, 2.000, 2.000, 0.000, 2.602, 2.500, 0.551, 11.500, 17.500, 3.000, 240.000, 280.000
//point.16= 1.000, -109.583, 8.000, -16.533, 1574.803, 2.000, 2.000, 0.000, 2.602, 2.500, 0.551, 11.500, 17.500, 3.000, 240.000, 280.000
//point.17= 1.000, -109.583, 4.000, -16.533, 1574.803, 2.000, 2.000, 0.000, 2.602, 2.500, 0.551, 11.500, 17.500, 3.000, 240.000, 280.000
//
//Scrape points
//point.18 = 2.000, -146.000, -98.900, 7.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
//point.19 = 2.000, -146.000, 98.900, 7.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
//point.20 = 2.000, -189.667, 0.000, -2.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
//point.21 = 2.000, -9.167, 0.000, -5.750, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
//point.22 = 2.000, -229.667, 0.000, 55.500, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000
//point.23 = 2.000, -106.400, -69.500, -5.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
//point.24 = 2.000, -76.300, -39.167, -9.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
//point.25 = 2.000, -76.300, 39.167, -9.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
//point.26 = 2.000, -106.400, 69.500, -5.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
//point.27 = 2.000, 0.000, 0.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
//
//static_pitch= 0.000
//static_cg_height= 13.625
//gear_system_type=0
[TailHook] // For opening cargo door.
tailhook_length=1 ;(feet)
tailhook_position = 0.0, 0.0, 0.0 ;(feet) longitudinal, lateral, vertical positions from datum
[folding_wings] // For opening main deck cargo door.
wing_fold_system_type = 4 ;0=None
fold_rates = 0.05,0.05 ;Percent per second
cable_force_adjust = 1.0
[Views]
eyepoint=-14.000, -2.000, 14.800 // Longitude, Latitude and Vertical position from Reference Point, (FEET)
[electrical]
// ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor = 1, 0 , 1.0
gear_motor = 0, 5 , 17.0
avionics_bus = 0, 0 , 1.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 0 , 1.0
additional_system = 0, 0 , 1.0
marker_beacon = 1, 2 , 17.0
gear_warning = 7, 0 , 99.0
gear_motor = 4, 0 , 1.0
fuel_pump = 0, 0 , 1.0
fuel_transfer_pump = 0, 0 , 1.0
starter1 = 0, 20, 17.0
starter2 = 0, 0 , 1.0
light_nav = 0, 0 , 1.0
light_beacon = 0, 0 , 1.0
light_landing = 0, 0 , 1.0
light_taxi = 0, 0 , 1.0
light_strobe = 0, 0 , 1.0
light_panel = 0, 7 , 99.0
light_recognition = 0, 0 , 1.0
light_wing = 0, 0 , 1.0
marker_beacon = 0, 0 , 1.0
standby_vacuum = 0, 0 , 1.0
auto_brakes = 0, 0 , 1.0
hydraulic_pump = 0, 0 , 1.0
propeller_device = 0, 0 , 1.0
[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
[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
[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
[exits]
number_of_exits = 4
// SP
//exit.0 = 0.10, -43.00, -9.0, 0.0, 0 //Main Pax Door, L1 Door, Main level
//exit.1 = 0.12, -58.00, 7.0, -7.0, 1 //Fwd Lower Right Cargo Door
//exit.2 = 0.12, -128.00, 7.0, -7.0, 1 //Aft Lower Right Cargo Door
// -100, -200, -300, -400
//number_of_exits = 6
//exit.0 = 0.10, -54.00, -9.0, 0.0, 0 //Main Pax Door, L1 Door, Main level - Reserved for Cargo models
//exit.1 = 0.10, -72.00, -9.0, 0.0, 0 //Main Pax Door, L2 Door, Main level
//exit.2 = 0.12, -54.00, 7.0, -7.0, 1 //Fwd Lower Right Cargo Door
//exit.3 = 0.12, -156.00, 7.0, -7.0, 1 //Aft Lower Right Cargo Door
//exit.4 = 0.12, -156.00, -7.0, 0.0 1 //Main Deck, Large Cargo Door, Aft, Left Side - Reserved for Cargo models
//exit.5 = 0.12, -167.00, 7.0, 7.0 0 //Lower Air Stair - Reserved for VC-25A
exit.0 = 0.10, -54.00, -9.0, 0.0, 0 //Main Pax Door, L1 Door, Main level - Reserved for Cargo models
exit.1 = 0.12, -54.00, 7.0, -7.0, 1 //Fwd Lower Right Cargo Door
exit.2 = 0.12, -156.00, -7.0, 0.0 1 //Main Deck, Large Cargo Door, Aft, Left Side - Reserved for Cargo models
exit.3 = 0.12, -167.00, 7.0, 7.0 1 //Lower Air Stair - Reserved for VC-25A
[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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=Opensky_sparks, 1
touchdown=fx_tchdwn, 1
[SMOKESYSTEM]
//Aileron tip vortecies
smoke.0=0, -127.167, -86.167, Opensky_vortex
smoke.1=0, -127.167, 86.167, Opensky_vortex
//Wing condensation
smoke.2=0, -105.917, -39.167, Opensky_conden
smoke.3=0, -105.917, 39.167, Opensky_conden
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing 6=taxi, 7=recognition, 8=wing, 9=logo
light.0 = 1, -34.700, 0.600, 19.100, Opensky_beacon ,
light.1 = 1, -83.500, 0.600, -7.080, Opensky_beacon ,
light.2 = 3, -219.700, -0.250, 12.300, Opensky_nav_yellow ,
light.5 = 3, -219.700, 0.250, 12.300, Opensky_nav_yellow ,
light.6 = 2, -218.900, 0.000, 11.450, fx_strobeh ,
light.7 = 3, -13.850, 0.000, 14.850, fx_vclighth ,
light.8 = 9, -208.500, -4.500, 43.750, Opensky_wing_light , // <-----3 previously
light.9 = 9, -208.500, 4.500, 43.750, Opensky_wing_light , // <-----3 previously
light.10= 5, -79.700, -29.200, -2.000, Opensky_nacelle_refl ,
light.11= 5, -79.700, 29.200, -2.000, Opensky_nacelle_refl ,
light.12= 5, -46.500, -11.700, 0.000, Opensky_nacelle_refl ,
light.13= 5, -46.500, 11.700, 0.000, Opensky_nacelle_refl ,
light.14= 5, -40.500, -13.700, 1.900, Opensky_nacelle_refl ,
light.15= 5, -40.500, 13.700, 1.900, Opensky_nacelle_refl ,
light.16= 5, -14.333, 0.000, -2.000, Opensky_nacelle_refl ,
light.17= 3, -18.300, -6.500, 6.000, Opensky_nacelle_refl ,
light.18= 3, -52.610, -4.500, 6.000, Opensky_nacelle_refl ,
light.19= 3, -144.510, 0.000, -3.000, Opensky_wing_light ,
[brakes]
toe_brakes_scale=0.915555
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,1
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
