[fltsim.0]
title=AI IR 74L
sim=b747sp
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=VH-EAA
atc_airline=QANTAS
atc_flight_number=7376
atc_heavy=1
ui_manufacturer=Boeing
ui_type=747 SP
ui_variation=Qantas Airways
description=Powerplants
Four 218.4kN (48,750lb) Pratt & Whitney JT9D7AW turbofans, or 222.8kN (50,100lb) RollsRoyce RB211524Bs or 229.5kN (51,600lb) RB211524Cs, or 206.8kN (46,500lb) General Electric CF645A2s or CF650E2F.
Performance
Max speed 1000km/h (540kt). Range with 331 passengers and baggage 10,840km (5855nm), range with 276 passengers 12,325km (6650nm), ferry range with max fuel and 13,610kg (30,000lb) payload 15,400km (8315nm).
Weights
Operating empty 147,420kg (325,000lb), max takeoff 317,515kg (700,000lb).
Dimensions
Wing span 59.64m (195ft 8in), length 56.31m (184ft 9in), height 19.94m (65ft 5in). Wing area 511m2 (5500sq ft).
Capacity
Flightcrew of three comprising two pilots and one flight engineer. Max high density single class seating for 440, typical two class seating for 28 first class and 288 economy class passengers
Production
Just 45 747SPs were built, of which approximately 25 remain in service.
visual_damage=1
[General]
atc_type=BOEING
atc_model=74S
editable=1
performance=Cruise Speed\n0.85 Mach 565 mph 910 km\/h\n\nEngine options\nPratt & Whitney PW4062\nRolls-Royce RB211-524H\nGeneral Electric CF6-80C2B5F\n\nMaximum Range\n7,325 nm 13,570 km\n\nMaximum Certified Operating Altitude 45,100 ft 13,747 m\n\nFuel Capacity\n57,285 gal 216,840 L\n\nBasic Empty Weight\n394,088 lb 178,755 kg\n\nMax Gross Weight 875,000 lb 396,893 kg\n\nLength\n231 ft, 10 in 70.6 m\n\nWingspan\n211 ft, 5 in 64.4 m\n\nHeight\n63 ft, 8 in 19.4 m\n\nSeating Typical 3-class configuration - 416\nTypical 2-class configuration - 524
[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 = 700000.000
empty_weight = 325000.000
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
station_load.1 = "170.0, 55.0, 2.0, 8.0, Co-Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "1200.0, 0.0, 0.0, 0.0, Crew" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "3400.0, 40.0, 0.0, 0.0, First Class" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "34000.0, -10.0, 0.0, 0.0, Coach" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = "9000.0, 28.0, 0.0, -6.0, Forward Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = "3000.0, -43.0, 0.0, -6.0, Aft Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_roll_MOI = 10000000.000
empty_weight_pitch_MOI = 20000000.000
empty_weight_yaw_MOI = 40000000.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[fuel]
LeftMain = 0.000, -28.000, 0.000, 12546.000, 0.000
RightMain = 0.000, 28.000, 0.000, 12546.000, 0.000
LeftAux = 0.000, -36.500, 0.000, 4482.000, 0.000
RightAux = 0.000, 36.500, 0.000, 4482.000, 0.000
LeftTip = 0.000, -73.000, 0.000, 1322.000, 0.000
RightTip = 0.000, 73.000, 0.000, 1322.000, 0.000
Center1 = 0.000, 0.000, 0.000, 17164.000, 0.000
Center2 = 0.000, 0.000, 0.000, 3300.000, 0.000
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=0
[airplane_geometry]
wing_area = 5500.000
wing_span = 195.000
wing_root_chord = 48.000
wing_dihedral = 7.000
wing_incidence = 1.000
wing_twist = -1.000
oswald_efficiency_factor= 0.700
wing_winglets_flag = 0
wing_sweep = 37.500
wing_pos_apex_lon = 20.000
wing_pos_apex_vert = 0.000
htail_area = 1470.000
htail_span = 72.000
htail_pos_lon = -70.000
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 37.500
vtail_area = 1060.000
vtail_span = 37.100
vtail_sweep = 45.000
vtail_pos_lon = -70.000
vtail_pos_vert = 15.000
elevator_area = 300.000
aileron_area = 225.000
rudder_area = 240.000
elevator_up_limit = 25.000
elevator_down_limit = 15.000
aileron_up_limit = 25.000
aileron_down_limit = 15.000
rudder_limit = 32.000
elevator_trim_limit = 20.000
spoiler_limit = 45.000
spoilerons_available = 1
aileron_to_spoileron_gain = 3.000
min_ailerons_for_spoilerons = 10.000
min_flaps_for_spoilerons = 0.000
[Reference Speeds]
flaps_up_stall_speed = 140.000
full_flaps_stall_speed = 110.000
cruise_speed =490
max_mach = 0.92
max_indicated_speed = 365.0 //Red line (KIAS)
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =1.000
induced_drag_scalar =1.000
elevator_effectiveness =1.000
aileron_effectiveness =1.000
rudder_effectiveness =1.000
pitch_stability =2.002
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =0.503
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
[GeneralEngineData]
engine_type = 1
Engine.0 = -17.000, -69.000, -2.000
Engine.1 = 10.000, -39.000, -5.000
Engine.2 = 10.000, 39.000, -5.000
Engine.3 = -17.000, 69.000, -2.000
fuel_flow_scalar = 1.000
min_throttle_limit = -0.25; //Minimum percent throttle. Generally negative for turbine reverser
[TurbineEngineData]
fuel_flow_gain = 0.002
inlet_area = 60.000
rated_N2_rpm = 29920.000
static_thrust = 50000.000
afterburner_available = 0
reverser_available = 1
[jet_engine]
thrust_scalar =1.111
[autopilot]
use_no_default_bank=1
use_no_default_pitch=1
autopilot_available = 1
flight_director_available = 1
default_vertical_speed = 1800.0
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=16.00
nav_integrator_control=0.17
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control = 18.0
gs_integrator_control = 0.33
gs_derivative_control = 0.00
gs_integrator_boundary = 0.70
gs_derivative_boundary = 0.00
yaw_damper_gain = 1.0
[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)
point.0 = 1.000, 48.000, 0.000, -14.800, 1000.000, 0.000, 2.000, 70.000, 1.000, 2.500, 0.900, 5.000, 5.000, 0.000, 0.000, 0.000
point.1 = 1.000, -12.000, -18.000, -16.500, 2000.000, 1.000, 2.000, 0.000, 2.000, 2.500, 0.900, 6.000, 6.000, 2.000, 0.000, 0.000
point.2 = 1.000, -12.000, 18.000, -16.500, 2000.000, 2.000, 2.000, 0.000, 2.000, 2.500, 0.900, 6.000, 6.000, 3.000, 0.000, 0.000
point.3 = 2.000, -50.000, -98.000, 7.000, 700.000, 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, -50.000, 98.000, 7.000, 700.000, 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, -93.000, 0.000, 7.000, 700.000, 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, 76.000, 0.000, 4.000, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch = -1.500
static_cg_height = 16.500
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 = 1.24 //Brake scalar
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,1,1 //pumps on Eng1,2,3,4
[Views]
eyepoint = 55.61, -1.95, 15.44 ; 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)
autopilot = 0, 5 , 17.0
avionics_bus = 0, 5 , 17.0
avionics = 1, 5 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 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
[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, -53.05, -97.46, 7.06, fx_navredh ,
light.1 = 3, -53.05, 97.46, 7.06, fx_navgreh ,
light.2 = 3, -94.74, 0.00, 7.70, fx_navwhih ,
light.3 = 2, -48.96, -97.46, 7.06, fx_strobeh ,
light.4 = 2, -48.96, 97.46, 7.06, fx_strobeh ,
light.6 = 1, 36.78, 0.00, 18.77, fx_beaconh ,
light.7 = 1, 3.50, 0.00, -8.30, fx_beaconb ,
light.8 = 4, 55.30, 0.00, 16.61, fx_vclighth,
[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 = 2
attitude_indicator.1 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[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 = 150, 250
aileron = 150, 250
rudder = 150, 250
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
[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]
type= 1
span-outboard= 0.600
extending-time= 10.000
system_type= 1
damaging-speed= 200.000
blowout-speed= 250.000
lift_scalar= 0.700
drag_scalar= 0.900
pitch_scalar= 0.900
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 5.000, 0.000
flaps-position.3= 10.000, 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= 2.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.300
drag_scalar= 0.100
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
