[fltsim.0]
title=Boeing 747-200 EAL
sim=747-200B-PW-JT9D-7R4G2
model=
panel=
sound=
texture=
checklists=
atc_airline=EUROPE
atc_id=GBDXH
atc_flight_number=0001
atc_heavy=1
ui_manufacturer=Boeing
ui_type=747-200B
ui_variation=European Aircharter
visual_damage=1
description=Project Opensky \nBoeing 747-200B\nVersion 2002.3.2\n\nEngine Type PW JT9D-7R4G2\n\n747-200 Commercial Version \n\nModel Designers\n Mitsushi Yutaka\n Hiroshi Igami \n\nFlight Dynamics Designer\n Warren C. Daniel\n\nTechnical Resource\n Simon Ng\n Shigeo Kitaguchi\n\nTest Pilots\n Project Opensky Members\n\nMaximun Range: 6,560 nm\n\nTypical city pairs: \n Tokyo-NY\n Bangkok-Paris\n London-Johannesburg\n\nFor proper operation: See B747 manual at: \n www.project-opensky.com
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 2.0
aileron_effectiveness = 2.0
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
[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
[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= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000
max_number_of_stations= 50
station_load.0= 0.000, 0.000, 0.000, 0.000
empty_weight= 538340.000
empty_weight_roll_MOI= 11331310.000
empty_weight_pitch_MOI= 36732189.000
empty_weight_yaw_MOI= 32844259.000
empty_weight_coupled_MOI= 1000.000
max_gross_weight= 833000.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[fuel]
Center1 = 0.000, 0.000, -4.000, 17153.000, 3.000
//Center2 = -193.5, 0.0, 6.0, 3298.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -5.000, -35.000, -4.000, 12538.000, 3.000
LeftAux = -11.500, -52.000, -3.000, 5761.000, 3.000
RightMain = -5.000, 35.000, -4.000, 12538.000, 3.000
RightAux = -11.500, 52.000, -3.000, 5761.000, 3.000
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 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= 0.000
wing_pos_apex_vert= 0.000
htail_area= 1470.000
htail_span= 72.750
htail_pos_lon= -17.167
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 37.500
vtail_area= 1060.000
vtail_span= 37.121
vtail_sweep= 45.000
vtail_pos_lon= -16.500
vtail_pos_vert= 6.083
elevator_area= 326.800
aileron_area= 225.200
rudder_area= 229.900
elevator_up_limit= 13.751
elevator_down_limit= 10.313
aileron_up_limit= 31.513
aileron_down_limit= 31.513
rudder_limit= 17.189
elevator_trim_limit= 9.167
spoiler_limit= 25.783
spoilerons_available= 0
aileron_to_spoileron_gain= 3.000
min_ailerons_for_spoilerons= 11.459
min_flaps_for_spoilerons= 0.000
[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, 67.333, 0.000, -13.850, 1181.102, 0.000, 5.812, 78.480, 0.859, 0.500, 0.518, 11.000, 11.000, 0.000, 0.000, 0.000
point.1= 1.000, -12.583, -18.000, -13.833, 1574.803, 1.000, 5.812, 0.000, 0.602, 0.500, 0.551, 14.900, 14.900, 2.000, 0.000, 0.000
point.2= 1.000, -12.583, 18.000, -13.833, 1574.803, 2.000, 5.812, 0.000, 0.602, 0.500, 0.551, 17.100, 17.100, 3.000, 0.000, 0.000
point.3= 2.000, -14.167, -96.167, 0.000, 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.4= 2.000, -14.167, 96.167, 0.000, 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.5= 2.000, -132.667, 0.000, 2.500, 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.6= 2.000, 88.167, 0.000, -3.750, 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.7= 2.000, -14.167, -96.167, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
point.8= 2.000, -132.667, 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
static_pitch= -1.000
static_cg_height= 13.625
// Nose gear
//point.0= 1.000, 67.333, -1.500, -14.333, 1181.102, 0.000, 2.000, 70.000, 1.859, 2.500, 0.518, 9.000, 11.000, 0.000, 240.000, 280.000
//point.1= 1.000, 67.333, 1.500, -14.333, 1181.102, 0.000, 2.000, 70.000, 1.859, 2.500, 0.518, 9.000, 11.000, 0.000, 240.000, 280.000
//
// Main Wing Gear (left)
//point.2= 1.000, -7.583, -18.000, -15.833, 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, -7.583, -14.000, -15.833, 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, -2.583, -18.000, -15.833, 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, -2.583, -14.000, -15.833, 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, -7.583, 18.000, -15.833, 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, -7.583, 14.000, -15.833, 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, -2.583, 18.000, -15.833, 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, -2.583, 14.000, -15.833, 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, -18.583, -8.000, -15.833, 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, -18.583, -4.000, -15.833, 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, -12.583, -8.000, -15.833, 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, -12.583, -4.000, -15.833, 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, -18.583, 8.000, -15.833, 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, -18.583, 4.000, -15.833, 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, -12.583, 8.000, -15.833, 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, -12.583, 4.000, -15.833, 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, -14.167, -96.167, 0.000, 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, -14.167, 96.167, 0.000, 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, -132.667, 0.000, 2.500, 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, 88.167, 0.000, -3.750, 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, -14.167, -96.167, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
//point.23= 2.000, -132.667, 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
//
//static_pitch= -1.000
//static_cg_height= 13.625
[GeneralEngineData]
engine_type= 1
Engine.0= -14.917, -69.500, 0.000
Engine.1= 14.917, -39.167, -7.000
Engine.2= 14.917, 39.167, -7.000
Engine.3= -14.917, 69.500, 0.000
fuel_flow_scalar= 0.842
[TurbineEngineData]
bypass_ratio=4.970000
fuel_flow_gain= 0.001
inlet_area= 47.500
rated_N2_rpm= 26928.000
static_thrust= 54750.000
afterburner_available= 0
reverser_available= 1
[Reference Speeds]
flaps_up_stall_speed= 150.000
full_flaps_stall_speed= 126.000
cruise_speed= 424.337
[keyboard_response]
elevator= 100.000, 200.000
aileron= 100.000, 200.000
rudder= 150.000, 250.000
[Views]
eyepoint= 77.330, -1.487, 20.005
[General]
performance=Passengers\n3-class conf: 366 \n2-class conf: 452 \n1-class conf: N\/A\n\nCargo\nTotal lower hold volume:\n 5,497 ft3 (155.6 m3) \n\nDimensions\nSpan 195 ft 8 in\nLength 231 ft 10 in\nHeight 63 ft 5 in\n\nEngines: PW JT9D-7R4G2\nTO Thrust: 54,750 lb x 4\n\nMax Fuel Cap.: 52,410 US Gal.\nMaxTOW: 833,000 lbs\nMLW: 630,000 lbs\nZFW: 538,340 lbs\nOEW: 388,010 lbs\n\nMax Range: 6,560 nm\nTypical Cruise Speed \n @ FL350: M.84
atc_type=BOEING AIRCRAFT
atc_model=B742
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 800.000
autothrottle_available= 1
autothrottle_arming_required= 1
autothrottle_takeoff_ga= 1
autothrottle_max_rpm= 105.000
pitch_takeoff_ga= 8.000
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.
[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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[direction_indicators]
direction_indicator.0=3,0
[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
[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 25.000
system_type= 1
damaging-speed= 200.000
blowout-speed= 250.000
lift_scalar= 0.700
drag_scalar= 1.000
pitch_scalar= 0.900
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
[Flaps.1]
type= 2
span-outboard= 0.800
extending-time= 12.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.300
drag_scalar= 1.000
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 20.000, 0.000
