[fltsim.0]
title=Boeing 747-400 Pan Am Paint rare 1 Ai
sim=Boeing747-400
model=
panel=
sound=
texture=Pan Am P1
kb_checklists=Boeing747-400_check
kb_reference=Boeing747-400_ref
atc_id=N700MS
atc_airline=Pan Am
atc_flight_number=1123
atc_heavy=1
ui_manufacturer=MelJet
ui_type=747-400
ui_variation=Pan Am rare livery
visual_damage=1
description=More than 30 years ago, the 747 made its first trip from New York to London. Since then, it's become the standard by which other large passenger jets are judged. Its size, range, speed and capacity were then, and are now, the best in its class.
[fltsim.1]
title=Boeing 747-400 Pan Am new livery Ai
sim=Boeing747-400
model=
panel=
sound=
texture=Pan Am P2
kb_checklists=Boeing747-400_check
kb_reference=Boeing747-400_ref
atc_id=N700MS
atc_airline=Pan Am
atc_flight_number=1123
atc_heavy=1
ui_manufacturer=MelJet
ui_type=747-400
ui_variation=Pan Am new livery
visual_damage=1
description=More than 30 years ago, the 747 made its first trip from New York to London. Since then, it's become the standard by which other large passenger jets are judged. Its size, range, speed and capacity were then, and are now, the best in its class.
[General]
atc_type=BOEING
atc_model=B744
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 Operating Weight 403,486 lb 182,020 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=875000 // (pounds)
empty_weight=401100 // (pounds)
reference_datum_position=83.5, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-90.5, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50
station_load.0=40000, -80.0, 0.0, 0.0 //Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_roll_MOI=15352310
empty_weight_pitch_MOI=24223159
empty_weight_yaw_MOI=39531785
empty_weight_coupled_MOI=0
[fuel]
Center1=-83.5, 0.0, -7.0, 19545.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center2=-193.5, 0.0, 6.0, 3300.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain=-112.0, -35.0, -4.0, 16720.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux=-118.5, -52.0, -3.0, 500.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-112.0, 35.0, -4.0, 16720.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux=-118.5, 52.0, -3.0, 500.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
[airplane_geometry]
wing_area=5825.0 //Square feet
wing_span=211.4 //Feet
wing_root_chord=48.8 //Feet
wing_dihedral=7.0 //Degrees
wing_incidence=2.0 //Degrees
wing_twist=-1.0 //Degrees
oswald_efficiency_factor=0.68 //Measure of lift effeciency of wing
wing_winglets_flag=1 //Are winglets available?
wing_sweep=37.5 //Degrees, wing leading edge
wing_pos_apex_lon=-68.2 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=0 //Feet, vertical distance from reference point, positive going up
htail_area=1470 //Square feet
htail_span=72.8 //Feet
htail_pos_lon=-210.0 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence=0.0 //Degrees
htail_sweep=37.5 //Degrees, horizontal tail leading edge
vtail_area=1060 //Square feet
vtail_span=37.1 //Feet, tip to body
vtail_sweep=45.0 //Degrees, vertical tail leading edge
vtail_pos_lon=-198.5 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=26.1 //Feet, vertical distance from reference point, positive going up
elevator_area=327 //Square feet
aileron_area=225 //Square feet
rudder_area=230 //Square feet
elevator_up_limit=25 //Degrees
elevator_down_limit=15 //Degrees
aileron_up_limit=25 //Degrees
aileron_down_limit=15 //Degrees
rudder_limit=31.5 //Degrees
elevator_trim_limit=20 //Degrees
spoiler_limit=45 //Degrees
spoilerons_available=1 //Spoilerons Available?
aileron_to_spoileron_gain=3 //Aileron to spoileron gain
min_ailerons_for_spoilerons=10 //Degrees
min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate
[Reference Speeds]
flaps_up_stall_speed=140.0 //Knots True (KTAS)
full_flaps_stall_speed=112.0 //Knots True (KTAS)
cruise_speed=505.0 //Knots True (KTAS)
[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=1 // degrees
flaps-position.2=5 // degrees
flaps-position.3=10 // 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=0.7
drag_scalar=0.9
pitch_scalar=0.9
system_type=1 //Hydraulic
[flaps.1]
type=2 // 1 - tail, 2 - lead
span-outboard=0.8 // 0.0 .. 1.0
extending-time=2 // seconds
flaps-position.0=0 // degrees
flaps-position.1=1.0 // degrees
damaging-speed=250 // KIAS
blowout-speed=300 // KIAS
lift_scalar=0.3
drag_scalar=0.1
pitch_scalar=0.1
system_type=1 //Hydraulic
[flight_tuning]
cruise_lift_scalar=1.0
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
[GeneralEngineData]
engine_type=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=-107.5, -69.5, -6.9 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=-76.0, -38.9, -10.4 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.2=-76.0, 38.9, -10.4 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.3=-107.5, 69.5, -6.9 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.0 //Scalar for fuel flow efficiency
[TurbineEngineData]
fuel_flow_gain=0.002 //Gain on fuel flow
inlet_area=60.0 //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920 //RPM, second stage compressor rated value
static_thrust=56750 //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
[autopilot]
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;
[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, -25.0, 0.0, -18.0, 1000.0, 0, 2.0, 70.0, 0.5, 3.5, 0.900, 9.0, 8.0, 0, 220, 250
point.1 = 1, -114.0, -18.0, -18.5, 2000.0, 1, 2.0, 13.0, 0.5, 2.5, 0.900, 11.0, 9.0, 2, 220, 250
point.2 = 1, -114.0, 18.0, -18.5, 2000.0, 2, 2.0, 13.0, 0.5, 2.5, 0.900, 11.0, 9.0, 3, 220, 250
point.3 = 2, -152.6, -103.5, 3.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 5, 0, 0
point.4 = 2, -152.6, 103.5, 3.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 6, 0, 0
point.5 = 2, 3.0, 0.0, 0.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 9, 0, 0
point.6 = 2, -222.7, 0.0, 4.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0
static_pitch = -1.5
static_cg_height = 18.6
[Views]
eyepoint = -20.00, -1.97, 9.4 ; 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, 10, 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, -196.50, 0.00, 6.40, fx_navwhih ,
light.1 = 1, -10.30, 0.00, 16.75, fx_beaconh ,
light.2 = 1, -58.70, 0.00, -11.25, fx_beaconb ,
[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=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
