[fltsim.0]
title=Boeing 744-400 Air France
sim=ge
model=AF
panel=
sound=
texture=Air France Combi
kb_checklists=
kb_reference=
atc_id=AF
atc_airline=Air France 
atc_flight_number=1123
ui_manufacturer=AI
ui_type=Boeing 747-400
ui_variation=Air France
atc_heavy=1
description=A Boeing 747-400 by AI Aardvark designed especially for AI traffic.
atc_id_color=0000000000
visual_damage=0

[fltsim.1]
title=Boeing 744-400 British Airways
sim=rr
model=BAW
panel=
sound=
texture=British Airways
kb_checklists=
kb_reference=
atc_id=BAW
atc_airline=British
atc_flight_number=1123
ui_manufacturer=AI
ui_type=Boeing 747-400
ui_variation=British Airways
atc_heavy=1
description=A Boeing 747-400 by AI Aardvark designed especially for AI traffic.  
atc_id_color=0000000000
visual_damage=0

[fltsim.2]
title=Boeing 744-400 KLM
sim=ge
model=KLM
panel=
sound=
texture=KLM
kb_checklists=
kb_reference=
atc_id=KLM
atc_airline=KLM 
atc_flight_number=1123
ui_manufacturer=AI
ui_type=Boeing 747-400
ui_variation=KLM
atc_heavy=1
description=A Boeing 747-400 by AI Aardvark designed especially for AI traffic.
atc_id_color=0000000000
visual_damage=0

[fltsim.3]
title=Boeing 744-400 Lufthansa
sim=ge
model=LUFT
panel=
sound=
texture=Lufthansa
kb_checklists=
kb_reference=
atc_id=N747
atc_airline=Lufthansa 
atc_flight_number=1123
ui_manufacturer=AI
ui_type=Boeing 747-400
ui_variation=Lufthansa
atc_heavy=1
description=A Boeing 747-400 by AI Aardvark designed especially for AI traffic.
atc_id_color=0000000000
visual_damage=0


[General] 
atc_type=BOEING 
atc_model=B744 
editable=0 
performance="Cruise Speed \n477 kts 550 mph 885 km\/h\n\nEngines \nCFM56-3C1\n\nMaximum Range \n2,059 nm 2,370 mi 3,810 km\n\nService Ceiling \n36, 089 ft 11,000 m\n\nFuel Capacity \n5,311 U.S. gal 20,104 L\n\nEmpty Weight-Standard \n76,180 lb 34,550 kg\n\nMaximum Gross Weight\n150,000 lb 68,039 kg\n\nLength \n120 ft 36.45 m\n\nWingspan \n94 ft, 9 in 25.9 m\n\nHeight \n36.5 ft 11.13 m\n\nSeating \nSeats 147 to 168\n\nCargo Capacity \n1,373 ft3 38.93 m3\n\n" 

[pitot_static] 
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI 

[weight_and_balance] 

// ACM V2.3 
max_gross_weight = 150000 
empty_weight = 102170 
reference_datum_position = 0, 0, 0 
empty_weight_CG_position = 0, 0, 0 
empty_weight_pitch_MOI = 3160000 
empty_weight_roll_MOI = 3262183 
empty_weight_yaw_MOI = 4337024 
empty_weight_coupled_MOI = 0 
max_number_of_stations = 9 

station_load.0 = "170.0, 41.0, -1.5, 0.0, Pilot" 
station_load.1 = "170.0, 41.0, 1.5, 0.0, Co-Pilot" 
station_load.2 = "510.0, 0.0, 0.0, 0.0, Crew" 
station_load.3 = "1360.0, 25.5, 0.0, 0.0, First Class" 
station_load.4 = "8160.0, 11.0, 0.0, 0.0, Coach 3-10" 
station_load.5 = "8160.0, -10.0, 0.0, 0.0, Coach 11-18" 
station_load.6 = "7140.0, -30.5, 0.0, 0.0, Coach 19-25" 
station_load.7 = "10000.0, 20.5, 0.0, 0.0, Forward Baggage" 
station_load.8 = "4000.0, -27.5, 0.0, 0.0, Aft Baggage" 

[lights] 

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing 

light.0 = 3, -46.19, -103.51, 8.27, fx_navred 
light.1 = 3, -46.18, 103.52, 8.27, fx_navgre 
light.2 = 2, -46.32, -103.56, 8.28, fx_strobe 
light.3 = 2, -46.37, 103.56, 8.27, fx_strobe 
light.4 = 2, 9.16, 0, -5.88, fx_beacon 
light.5 = 1, 67.28, 0, 19.73, fx_beacon 
light.6 = 3, -120.78, -0.15, 11.85, fx_navwhi 
light.7 = 3, -120.78, 0.15, 11.85, fx_strobe 


[GeneralEngineData] 

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop 
engine_type = 1 
fuel_flow_scalar = 1 
engine.0 = -20.86, -66.14, -2.77, 
engine.1 = 5.86, -37.82, -5.63, 
engine.2 = 5.86, 37.82, -5.63, 
engine.3 = -20.86, 66.14, -2.77, 
min_throttle_limit=-0.650000 

[effects] 
wake = fx_wake 
water = fx_spray 
dirt = fx_tchdrt 
concrete = fx_sparks 
touchdown = fx_tchdwn, 1 

[fuel] 

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) 

fuel_type = 2 
number_of_tank_selectors = 1 

Center1 = 0, 0, 0, 2313, 0 
LeftMain = -3, -19, 0, 1500, 0 
RightMain = -3, 19, 0, 1500, 0 
electric_pump=0 


[contact_points] 
static_pitch = -0.9 
static_cg_height = 13.1 
max_number_of_points = 7 

point.0 = 1, 75.5041, 0, -12.6711, 1574.8, 0, 1.442, 55.92, 0.8, 2.5, 0.6, 4, 6, 0, 220, 250 
point.1 = 1, -15.0899, -18, -14.3239, 1574.8, 1, 1.442, 0, 1, 2.5, 0.9, 6.9, 6.9, 2, 220, 250 
point.2 = 1, -15.0899, 18, -14.3239, 1574.8, 2, 1.442, 0, 1, 2.5, 0.9, 7.1, 7.1, 3, 220, 250 
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 
gear_system_type=0 


[keyboard_response] 
elevator = 150, 250 
aileron = 150, 250 
rudder = 150, 250 


[forcefeedback] 
gear_bump_nose_magnitude = 3000 
gear_bump_nose_direction = 18000 
gear_bump_nose_duration = 250000 
gear_bump_left_magnitude = 2700 
gear_bump_left_direction = 35500 
gear_bump_left_duration = 250000 
gear_bump_right_magnitude = 2700 
gear_bump_right_direction = 00500 
gear_bump_right_duration = 250000 
ground_bumps_magnitude1 = 1300 
ground_bumps_angle1 = 08900 
ground_bumps_intercept1 = 3.0 
ground_bumps_slope1 = 0.20 
ground_bumps_magnitude2 = 200 
ground_bumps_angle2 = 09100 
ground_bumps_intercept2 = 1.075 
ground_bumps_slope2 = 0.035 
crash_magnitude1 = 10000 
crash_direction1 = 01000 
crash_magnitude2 = 10000 
crash_direction2 = 9000 
crash_period2 = 75000 
crash_duration2 = 2500000 

[airplane_geometry] 
//ACM_AREAW1// 0,0,0,5.4864,1.6044,1.6044,0.7480,5.9601,3.2088,3.2088 
//ACM_AREAW2// 1.4960,6.4340,4.8133,4.8133,2.2444,6.9078,6.4176,6.4176,2.9925,7.3817 
//ACM_AREAW3// 8.0221,8.0221,3.7407,7.8555,9.6266,9.6266,4.4889,8.3294,11.2306,11.2306 
//ACM_AREAW4// 5.2371,8.8030,12.8353,12.8353,5.9850,9.2770,14.4399,14.4399,6.7333,9.7509 
//ACM_AREAH1// 0,0,0,4.2367,0.7059,0.7059,0.4074,4.4324,1.4119,1.4119 
//ACM_AREAH2// 0.8151,4.6283,2.1182,2.1182,1.2230,4.8242,2.8243,2.8243,1.6303,5.0198 
//ACM_AREAH3// 3.5306,3.5306,2.0383,5.2157,4.2367,4.2367,2.4460,5.4116,4.9428,4.9428 
//ACM_AREAH4// 2.8536,5.6076,5.6489,5.6489,3.2613,5.8034,6.3550,6.3550,3.6691,5.9993 
//ACM_AREAV1// 0,0,0,6.0960,0.6772,0.6772,0.4742,6.0823,1.3545,1.3545 
//ACM_AREAV2// 0.9484,6.0689,2.0320,2.0320,1.4227,6.0556,2.7093,2.7093,1.8969,6.0423 
//ACM_AREAV3// 3.3866,3.3866,2.3712,6.0289,4.0640,4.0640,2.8454,6.0155,4.7413,4.7413 
//ACM_AREAV4// 3.3199,6.0019,5.4186,5.4186,3.7941,5.9885,6.0960,6.0960,4.2684,5.9752 
//ACM_CAREAW1// 7.2199,7.2199,6.1097,7.2069,8.0221,8.0221,6.4839,7.5264,8.8240,8.8240 
//ACM_CAREAW2// 6.8579,7.8456,9.6266,9.6266,7.2321,8.1646,10.4287,10.4287,7.6062,8.4840 
//ACM_CAREAW3// 11.2306,11.2306,7.9801,8.8030,12.0332,12.0332,8.3542,9.1224,12.8353,12.8353 
//ACM_CAREAW4// 8.7284,9.4413,13.6372,13.6372,9.1021,9.7608,14.4399,14.4399,9.4764,10.0801 
//ACM_CAREAH1// 0,0,2.1182,4.2367,0.7059,0.7059,2.5260,4.5384,1.4119,1.4119 
//ACM_CAREAH2// 2.9337,4.8400,2.1182,2.1182,3.3413,5.1420,2.8243,2.8243,3.7490,5.4436 
//ACM_CAREAH3// 3.5306,3.5306,4.1567,5.7455,4.2367,4.2367,4.5644,6.0472,4.9428,4.9428 
//ACM_CAREAH4// 4.9720,6.3488,5.6489,5.6489,5.3797,6.6508,6.3550,6.3550,5.7873,6.9524 
//ACM_CAREAV1// 0,0,1.5240,4.5720,0.6772,0.6772,1.9982,4.8024,1.3545,1.3545 
//ACM_CAREAV2// 2.4725,5.0328,2.0320,2.0320,2.9467,5.2631,2.7093,2.7093,3.4210,5.4937 
//ACM_CAREAV3// 3.3866,3.3866,3.8952,5.7241,4.0640,4.0640,4.3695,5.9545,4.7413,4.7413 
//ACM_CAREAV4// 4.8439,6.1848,5.4186,5.4186,5.3179,6.4154,6.0960,6.0960,5.7923,6.6458 
wing_area = 2037.0 
wing_span = 126.46 
wing_root_chord = 28.58 
wing_dihedral = 6.19 
wing_incidence = 1.0 
wing_twist = -0.5 
oswald_efficiency_factor = 0.85 
wing_winglets_flag = 0 
wing_sweep = 28 
wing_pos_apex_lon = 18.58 
wing_pos_apex_vert = 0 
htail_area = 338.0 
htail_span = 50.15 
htail_pos_lon = -59.65 
htail_pos_vert = 0 
htail_incidence = 0.0 
htail_sweep = 34 
vtail_area = 224.0 
vtail_span = 28.77 
vtail_sweep = 42 
vtail_pos_lon = -50.76 
vtail_pos_vert = 5.53 
elevator_area = 70.5 
aileron_area = 26.9 
rudder_area = 56.2 
elevator_up_limit = 22.5 
elevator_down_limit = 19.5 
aileron_up_limit = 20.0 
aileron_down_limit = 20.0 
rudder_limit = 26.0 
elevator_trim_limit = 20.0 
spoiler_limit = 60.0 
aileron_to_spoileron_gain = 3 
min_ailerons_for_spoilerons = 10 
min_flaps_for_spoilerons = 0 
spoilerons_available = 1 

[electrical] 
max_battery_voltage = 24 
generator_alternator_voltage = 28 
max_generator_alternator_amps = 60 
electric_always_available = 1 
flap_motor = 0, 5, 17 
gear_motor = 0, 5, 17 
autopilot = 0, 5, 17 
avionics_bus = 0, 5, 17 
avionics = 1, 5, 17 
pitot_heat = 0, 2, 17 
additional_system = 0, 2, 17 
marker_beacon = 1, 2, 17 
gear_warning = 0, 2, 17 
fuel_pump = 0, 5, 17 
starter1 = 0, 20, 17 
light_nav = 0, 5, 17 
light_beacon = 0, 5, 17 
light_landing = 0, 5, 17 
light_taxi = 0, 5, 17 
light_strobe = 0, 5, 17 
light_panel = 0, 5, 17 

[flight_tuning] 
cruise_lift_scalar=1.2 
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0 
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 

[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=14000 //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 

[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 = 0.485 //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=43.7, -1.31, 3.7 //(feet) longitudinal, lateral, vertical distance from reference datum 

[flaps.0] //Trailing Edge Flaps 
type = 1 // 1 - tail, 2 - lead 
span-outboard = 0.8 // 0.0 .. 1.0 
extending-time = 20 // 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 = 0.0 
drag_scalar = 0.0 
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 = 4 // seconds 
flaps-position.0 = 0 // 
flaps-position.4 = 0.5 
flaps-position.5 = 1.0 // 
damaging-speed = 250 // KIAS 
blowout-speed = 300 // KIAS 
lift_scalar = 0.0 
drag_scalar = 0.0 
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 = 7 // seconds 
flaps-position.0 = 0 // 
flaps-position.4 = 0.5 
flaps-position.5 = 1.0 // 
damaging-speed = 250 // KIAS 
blowout-speed = 300 // KIAS 
lift_scalar = 0.0 
drag_scalar = 0.0 
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 

[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 

[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 

[Reference Speeds] 
flaps_up_stall_speed=140.0 //Knots True (KTAS) 
full_flaps_stall_speed=113.0 //Knots True (KTAS) 
cruise_speed=477.0 //Knots True (KTAS) 
max_mach = 0.87 
max_indicated_speed = 340 //Red line (KIAS) 

[stall_warning] 
type=2


//aia747-400fde (feb. 28. 04)