15-08-2005, 03:45 PM
hey tanz, sorry but i would be most grateful if you would do a L-1011
[fltsim.20]
title=Lockheed L-1011-500 Tristar Paint92
sim=L-1011
model=
panel=
sound=
texture=92
kb_checklists=L-1011_check
kb_reference=L-1011_ref
atc_id=
atc_airline=Egypt Air
atc_flight_number=L500
atc_heavy=1
ui_manufacturer=Lockheed
ui_type=L-1011-500 Tristar
ui_variation=EgyptAir
description=Development of the Lockheed L-1011 Tristar began in 1966 when American Airlines announced a need for a short to
medDevelopment of the Lockheed L-1011 Tristar began in 1966 when American Airlines announced a need for a short to medium-
range, large-capacity transport. In March of 1968, production began when Lockheed received orders for their design from TWA and
Eastern Airlines. Although Production was slowed when Rolls- Royce, the developer of the L1011's engines, was forced to declare
bankruptcy, Lockheed managed to deliver the Tristar for operation with Eastern and TWA in 1972. The longer-range L1011-200 came in
1977 and the L1011-250, which featured larger fuel-capacity, started operations with Delta Airlines in 1986. The original version of inter-
continental L1011-500 was delivered to British Airways in 1979 and the next year Pan Am put the extended wing version into service.
atc_parking_types=Gate
atc_parking_codes=MSR
visual_damage=0
[General]
atc_type=LOCKHEED
atc_model=L-1011
editable=0
performance="Cruise Speed\n0.84 Mach 525 KTAS 930 km\/h\n\nEngine options\n3 Rolls-Royce RB-211-524B
turbofans\n\nMaximum Range\n5,260 nm 10,000 km\n\nFuel Capacity\n45.000 gal 374.850 Pounds\n\nBasic Empty
Weight\n281.680 Pounds \n\nMax Gross Weight 660.000 Pounds\n\nLength\n164 ft, 2 in 50.0 m\n\nWingspan\n164 ft, 4
in 50.4 m\n\nHeight\n55 ft, 4 in 16.9 m
[WEIGHT_AND_BALANCE]
max_gross_weight = 660000 // (pounds)
empty_weight = 281680 // (pounds)
reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations =50
station_load.0 = "170.0, 41.0, -1.5, 0.0, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum
(feet)
station_load.1 = "170.0, 41.0, 1.5, 0.0, Co-Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "510.0, 0.0, 0.0, 0.0, Crew" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "3840.0, 25.5, 0.0, 0.0, First Class" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "17850.0, 11.0, 0.0, 0.0, Coach 3-10" //Weight (lbs), longitudinal, lateral, vertical positions from datum
(feet)
station_load.5 = "17850.0, -10.0, 0.0, 0.0, Coach 11-18" //Weight (lbs), longitudinal, lateral, vertical positions from datum
(feet)
station_load.6 = "20230.0, -30.5, 0.0, 0.0, Coach 19-25" //Weight (lbs), longitudinal, lateral, vertical positions from datum
(feet)
station_load.7 = "10000.0, 20.5, 0.0, 0.0, Forward Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum
(feet)
station_load.8 = "4000.0, -27.5, 0.0, 0.0, Aft Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum
(feet)
;Moments of Inertia
empty_weight_pitch_MOI = 18000000
empty_weight_roll_MOI = 5500000
empty_weight_yaw_MOI = 16300000
empty_weight_coupled_MOI= 0.0
[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=15, -33, -9 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=15, 33, -9 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.2 =-39, 0, 15
fuel_flow_scalar = 1
min_throttle_limit=-0.250000
[TurbineEngineData]
fuel_flow_gain=0.002
inlet_area=113.000
rated_N2_rpm=29920.000
static_thrust=56750.000
afterburner_available=0
reverser_available=1
[jet_engine]
thrust_scalar=1.5
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-
7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 17.0
marker_beacon=1, 2 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
starter1=0, 20, 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
//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)
[contact_points]
point.0=1.000, 57.000, 0.000, -17.130, 1181.100, 0.000, 4.521, 90.000, 0.400, 2.500, 0.724, 4.000, 4.000, 0.000, 0.000, 0.000
point.1=1.000, -3.300, -17.000, -17.330, 1574.800, 1.000, 4.521, 0.000, 0.500, 2.500, 0.747, 6.900, 6.900, 2.000, 0.000, 0.000
point.2=1.000, -3.300, 17.000, -17.330, 1574.800, 2.000, 4.521, 0.000, 0.500, 2.500, 0.747, 7.100, 7.100, 3.000, 0.000, 0.000
point.3=2.000, -14.170, -47.330, 0.000, 787.400, 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, -14.170, 47.330, 0.000, 787.400, 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, -83.330, 0.000, 2.500, 787.400, 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, 42.670, 0.000, -3.750, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch=0.0
static_cg_height=16.500
gear_system_type=0
[Views]
eyepoint = 76.7, -1.9, 2.7
[flaps.0] //Inboard Trailing Edge
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 = 0 // degrees
flaps-position.2 = 5 // degrees
flaps-position.3 = 15 // degrees
flaps-position.4 = 20 // degrees
flaps-position.5 = 25 // degrees
flaps-position.6 = 30 // degrees
damaging-speed = 260 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.55
drag_scalar = 0.55
pitch_scalar= 0.55
system_type = 1 //Hydraulic
[flaps.1] //Outboard Trailing Edge
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 23 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 0 // degrees
flaps-position.2 = 5 // degrees
flaps-position.3 = 15 // degrees
flaps-position.4 = 20 // degrees
flaps-position.5 = 25 // degrees
flaps-position.6 = 30 // degrees
damaging-speed = 260 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.35
drag_scalar = 0.35
pitch_scalar= 0.35
system_type = 1 //Hydraulic
[flaps.2] //Inboard Leading Edge Slats
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 4 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 0.5 // degrees
flaps-position.2 = 0.5 // degrees
flaps-position.3 = 0.5 // degrees
flaps-position.4 = 0.5 // degrees
flaps-position.5 = 1.0 // degrees
flaps-position.6 = 1.0 // degrees
damaging-speed = 260 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.05
drag_scalar = 0.05
pitch_scalar= 0.05
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
[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
[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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -25, -71.5, 0.8, fx_navredh ,
light.1 = 1, -77.4, 0, 35.8, fx_beaconh ,
light.2 = 4, 76.7, -1.9, 2, fx_vclighth ,
light.3 = 4, 76.7, 1.9, 2, fx_vclighth ,
light.4 = 4, 73, 0, 2.2, fx_vclighth ,
light.5 = 3, -25, 71.5, 0.8, fx_navgreh ,
light.6 = 2, -25.8, -71.8, 0.8, fx_strobeh ,
light.7 = 2, -25.8, 71.8, 0.8, fx_strobeh ,
light.8 = 3, -36.4, -71.8, 0.95, fx_navwhi ,
light.9 = 3, -36.4, 71.8, 0.95, fx_navwhi ,
light.10 = 1, 13.7, 0, 9.9, fx_beaconh ,
light.11 = 1, 4.3, 0, -9.6, fx_beaconh ,
light.12 = 2, -84.4, 0, 7.5, fx_strobeh ,
light.13 = 3, 40.7, -9.05, -1.85, fx_navwhi ,
light.14 = 3, 40.7, 9.05, -1.85, fx_navwhi ,
[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
[folding_wings]
wing_fold_system_type =2
fold_rates =5.0,5.0
[fuel]
Center1 = 0.0, 0.0, -4.0, 12400.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -3.0, -35.0, 0.0, 16400.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -3.0, 35.0, 0.0, 16400.0, 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=0
[airplane_geometry]
wing_area = 4605.0 //Square feet
wing_span = 200.0 //Feet
wing_root_chord = 23.0 //Feet
wing_dihedral = 6.2 //Degrees
wing_incidence = 1.0 //Degrees
wing_twist = -0.5 //Degrees
oswald_efficiency_factor= 0.6 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 32.0 //Degrees, wing leading edge
wing_pos_apex_lon = 25.0 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_area = 1090.0 //Square feet
htail_span = 70.7 //Feet
htail_pos_lon = -100.0 //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 = 40.0 //Degrees, horizontal tail leading edge
vtail_area = 573.0 //Square feet
vtail_span = 27.3 //Feet, tip to body
vtail_sweep = 35.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -108.3 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 5.8 //Feet, vertical distance from reference point, positive going up
elevator_area = 137.0 //Square feet
aileron_area = 68.0 //Square feet
rudder_area = 232.0 //Square feet
elevator_up_limit = 30.0 //Degrees
elevator_down_limit = 30.0 //Degrees
aileron_up_limit = 30.0 //Degrees
aileron_down_limit = 15.0 //Degrees
rudder_limit = 25.0 //Degrees
elevator_trim_limit = 20.0 //Degrees
spoiler_limit = 60.0 //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 = 150.0 //Knots True (KTAS)
full_flaps_stall_speed = 120.0 //Knots True (KTAS)
cruise_speed = 425.0 //Knots True (KTAS)
max_indicated_speed=355.000000
max_mach=0.840000
[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;
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
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=0.000000
[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
[brakes]
toe_brakes_scale=1.0
parking_brake=1
[gear_warning_system]
gear_warning_available=1
[hydraulic_system]
electric_pumps=1
engine_map=1,1,1,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[fltsim.20]
title=Lockheed L-1011-500 Tristar Paint92
sim=L-1011
model=
panel=
sound=
texture=92
kb_checklists=L-1011_check
kb_reference=L-1011_ref
atc_id=
atc_airline=Egypt Air
atc_flight_number=L500
atc_heavy=1
ui_manufacturer=Lockheed
ui_type=L-1011-500 Tristar
ui_variation=EgyptAir
description=Development of the Lockheed L-1011 Tristar began in 1966 when American Airlines announced a need for a short to
medDevelopment of the Lockheed L-1011 Tristar began in 1966 when American Airlines announced a need for a short to medium-
range, large-capacity transport. In March of 1968, production began when Lockheed received orders for their design from TWA and
Eastern Airlines. Although Production was slowed when Rolls- Royce, the developer of the L1011's engines, was forced to declare
bankruptcy, Lockheed managed to deliver the Tristar for operation with Eastern and TWA in 1972. The longer-range L1011-200 came in
1977 and the L1011-250, which featured larger fuel-capacity, started operations with Delta Airlines in 1986. The original version of inter-
continental L1011-500 was delivered to British Airways in 1979 and the next year Pan Am put the extended wing version into service.
atc_parking_types=Gate
atc_parking_codes=MSR
visual_damage=0
[General]
atc_type=LOCKHEED
atc_model=L-1011
editable=0
performance="Cruise Speed\n0.84 Mach 525 KTAS 930 km\/h\n\nEngine options\n3 Rolls-Royce RB-211-524B
turbofans\n\nMaximum Range\n5,260 nm 10,000 km\n\nFuel Capacity\n45.000 gal 374.850 Pounds\n\nBasic Empty
Weight\n281.680 Pounds \n\nMax Gross Weight 660.000 Pounds\n\nLength\n164 ft, 2 in 50.0 m\n\nWingspan\n164 ft, 4
in 50.4 m\n\nHeight\n55 ft, 4 in 16.9 m
[WEIGHT_AND_BALANCE]
max_gross_weight = 660000 // (pounds)
empty_weight = 281680 // (pounds)
reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations =50
station_load.0 = "170.0, 41.0, -1.5, 0.0, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum
(feet)
station_load.1 = "170.0, 41.0, 1.5, 0.0, Co-Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "510.0, 0.0, 0.0, 0.0, Crew" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "3840.0, 25.5, 0.0, 0.0, First Class" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "17850.0, 11.0, 0.0, 0.0, Coach 3-10" //Weight (lbs), longitudinal, lateral, vertical positions from datum
(feet)
station_load.5 = "17850.0, -10.0, 0.0, 0.0, Coach 11-18" //Weight (lbs), longitudinal, lateral, vertical positions from datum
(feet)
station_load.6 = "20230.0, -30.5, 0.0, 0.0, Coach 19-25" //Weight (lbs), longitudinal, lateral, vertical positions from datum
(feet)
station_load.7 = "10000.0, 20.5, 0.0, 0.0, Forward Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum
(feet)
station_load.8 = "4000.0, -27.5, 0.0, 0.0, Aft Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum
(feet)
;Moments of Inertia
empty_weight_pitch_MOI = 18000000
empty_weight_roll_MOI = 5500000
empty_weight_yaw_MOI = 16300000
empty_weight_coupled_MOI= 0.0
[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=15, -33, -9 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=15, 33, -9 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.2 =-39, 0, 15
fuel_flow_scalar = 1
min_throttle_limit=-0.250000
[TurbineEngineData]
fuel_flow_gain=0.002
inlet_area=113.000
rated_N2_rpm=29920.000
static_thrust=56750.000
afterburner_available=0
reverser_available=1
[jet_engine]
thrust_scalar=1.5
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-
7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 17.0
marker_beacon=1, 2 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
starter1=0, 20, 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
//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)
[contact_points]
point.0=1.000, 57.000, 0.000, -17.130, 1181.100, 0.000, 4.521, 90.000, 0.400, 2.500, 0.724, 4.000, 4.000, 0.000, 0.000, 0.000
point.1=1.000, -3.300, -17.000, -17.330, 1574.800, 1.000, 4.521, 0.000, 0.500, 2.500, 0.747, 6.900, 6.900, 2.000, 0.000, 0.000
point.2=1.000, -3.300, 17.000, -17.330, 1574.800, 2.000, 4.521, 0.000, 0.500, 2.500, 0.747, 7.100, 7.100, 3.000, 0.000, 0.000
point.3=2.000, -14.170, -47.330, 0.000, 787.400, 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, -14.170, 47.330, 0.000, 787.400, 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, -83.330, 0.000, 2.500, 787.400, 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, 42.670, 0.000, -3.750, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch=0.0
static_cg_height=16.500
gear_system_type=0
[Views]
eyepoint = 76.7, -1.9, 2.7
[flaps.0] //Inboard Trailing Edge
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 = 0 // degrees
flaps-position.2 = 5 // degrees
flaps-position.3 = 15 // degrees
flaps-position.4 = 20 // degrees
flaps-position.5 = 25 // degrees
flaps-position.6 = 30 // degrees
damaging-speed = 260 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.55
drag_scalar = 0.55
pitch_scalar= 0.55
system_type = 1 //Hydraulic
[flaps.1] //Outboard Trailing Edge
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 23 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 0 // degrees
flaps-position.2 = 5 // degrees
flaps-position.3 = 15 // degrees
flaps-position.4 = 20 // degrees
flaps-position.5 = 25 // degrees
flaps-position.6 = 30 // degrees
damaging-speed = 260 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.35
drag_scalar = 0.35
pitch_scalar= 0.35
system_type = 1 //Hydraulic
[flaps.2] //Inboard Leading Edge Slats
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 4 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 0.5 // degrees
flaps-position.2 = 0.5 // degrees
flaps-position.3 = 0.5 // degrees
flaps-position.4 = 0.5 // degrees
flaps-position.5 = 1.0 // degrees
flaps-position.6 = 1.0 // degrees
damaging-speed = 260 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.05
drag_scalar = 0.05
pitch_scalar= 0.05
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
[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
[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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -25, -71.5, 0.8, fx_navredh ,
light.1 = 1, -77.4, 0, 35.8, fx_beaconh ,
light.2 = 4, 76.7, -1.9, 2, fx_vclighth ,
light.3 = 4, 76.7, 1.9, 2, fx_vclighth ,
light.4 = 4, 73, 0, 2.2, fx_vclighth ,
light.5 = 3, -25, 71.5, 0.8, fx_navgreh ,
light.6 = 2, -25.8, -71.8, 0.8, fx_strobeh ,
light.7 = 2, -25.8, 71.8, 0.8, fx_strobeh ,
light.8 = 3, -36.4, -71.8, 0.95, fx_navwhi ,
light.9 = 3, -36.4, 71.8, 0.95, fx_navwhi ,
light.10 = 1, 13.7, 0, 9.9, fx_beaconh ,
light.11 = 1, 4.3, 0, -9.6, fx_beaconh ,
light.12 = 2, -84.4, 0, 7.5, fx_strobeh ,
light.13 = 3, 40.7, -9.05, -1.85, fx_navwhi ,
light.14 = 3, 40.7, 9.05, -1.85, fx_navwhi ,
[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
[folding_wings]
wing_fold_system_type =2
fold_rates =5.0,5.0
[fuel]
Center1 = 0.0, 0.0, -4.0, 12400.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -3.0, -35.0, 0.0, 16400.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -3.0, 35.0, 0.0, 16400.0, 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=0
[airplane_geometry]
wing_area = 4605.0 //Square feet
wing_span = 200.0 //Feet
wing_root_chord = 23.0 //Feet
wing_dihedral = 6.2 //Degrees
wing_incidence = 1.0 //Degrees
wing_twist = -0.5 //Degrees
oswald_efficiency_factor= 0.6 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 32.0 //Degrees, wing leading edge
wing_pos_apex_lon = 25.0 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_area = 1090.0 //Square feet
htail_span = 70.7 //Feet
htail_pos_lon = -100.0 //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 = 40.0 //Degrees, horizontal tail leading edge
vtail_area = 573.0 //Square feet
vtail_span = 27.3 //Feet, tip to body
vtail_sweep = 35.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -108.3 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 5.8 //Feet, vertical distance from reference point, positive going up
elevator_area = 137.0 //Square feet
aileron_area = 68.0 //Square feet
rudder_area = 232.0 //Square feet
elevator_up_limit = 30.0 //Degrees
elevator_down_limit = 30.0 //Degrees
aileron_up_limit = 30.0 //Degrees
aileron_down_limit = 15.0 //Degrees
rudder_limit = 25.0 //Degrees
elevator_trim_limit = 20.0 //Degrees
spoiler_limit = 60.0 //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 = 150.0 //Knots True (KTAS)
full_flaps_stall_speed = 120.0 //Knots True (KTAS)
cruise_speed = 425.0 //Knots True (KTAS)
max_indicated_speed=355.000000
max_mach=0.840000
[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;
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
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=0.000000
[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
[brakes]
toe_brakes_scale=1.0
parking_brake=1
[gear_warning_system]
gear_warning_available=1
[hydraulic_system]
electric_pumps=1
engine_map=1,1,1,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0