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MED1439 Isacco
Addetto biglietteria
Italy
Messaggi: 26 |
 Lasciato il - 30 Dec 2009 : 20:26:06
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ok ecco qua!!!
[fltsim.0]
title=Learjet 45
sim=Lear45
model=
panel=
sound=
texture=
kb_checklists=Lear45_check
kb_reference=Lear45_ref
atc_id=N456LJ
ui_manufacturer=Bombardier
ui_type="Learjet 45"
ui_variation="Bianco con oro e nero"
description="Il modello 45 è il primo aeromobile Learjet completamente nuovo da quando Bill Lear costruì il suo primo modello 23. Sebbene abbia l'aspetto di un Learjet, il modello 45 ha soltanto la metà dei componenti del modello 35, grazie a un notevole progresso nella progettazione. I parametri in base al quale è stato costruito il modello 45 richiedevano le prestazioni del Learjet 35, la semplicità di manovra del Learjet 31A, e un maggiore spazio in cabina rispetto agli aerei prodotti dalla concorrenza."
[fltsim.1]
title=Learjet 45 Limited Edition
sim=Lear45
model=
panel=
sound=
texture=1
kb_checklists=Lear45_check
kb_reference=Lear45_ref
atc_id=N45LR
ui_manufacturer=Bombardier
ui_type="Learjet 45"
ui_variation="Edizione dell'anniversario"
description="Il modello 45 è il primo aeromobile Learjet completamente nuovo da quando Bill Lear costruì il suo primo modello 23. Sebbene abbia l'aspetto di un Learjet, il modello 45 ha soltanto la metà dei componenti del modello 35, grazie a un notevole progresso nella progettazione. I parametri in base al quale è stato costruito il modello 45 richiedevano le prestazioni del Learjet 35, la semplicità di manovra del Learjet 31A, e un maggiore spazio in cabina rispetto agli aerei prodotti dalla concorrenza."
[fltsim.2]
title=Mediterranea Learjet 45
sim=Lear45
model=
panel=
sound=
texture=med
kb_checklists=Lear45_check
kb_reference=Lear45_specifiche
atc_id_color=0xc0ad0a
atc_id=I-MIAV
atc_flight_number=2005
atc_airline=Mediterranea
atc_parking_codes=
atc_parking_types=GATE
ui_manufacturer=Bombardier
ui_type="Learjet 45"
ui_variation="Mediterranea"
visual_damage=1
description="Mediterranea livery by Massimo Garofano - The Model 45 is Learjet's first all-new aircraft since Bill Lear's first Model 23. Although it looks like a Learjet, it has only half the parts of a Model 35, reflecting a significant design progression. The parameters set down for the 45 called for it to have the performance of the Learjet 35, the handling of the Learjet 31A, and greater cabin space than the competition."
[General]
atc_type=Learjet
atc_model=
editable=0
performance="Velocità di crociera\t\nMach 0,81 464 nodi 859 km/h\n\nMotori\t\nAllied Signal TFE731-20 3.500 libbre di spinta\n\nAutonomia massima\t\n2.200 miglia nautiche 2.532 miglia terrestri \t 4.074 km\n\nTangenza pratica\t\n51.000 piedi 15.545 m\n\nCapacità carburante\t\n6.062 libbre 2.722 kg\n3.424 litri \n\nPeso massimo a pieno carico\t\n20.450 libbre 9.276 kg\n\nPeso massimo al decollo - peso lordo\t\n20.200 libbre \t9.163 kg\n\nCarico utile\t\n8.750 libbre \t3.969 kg\n\nLunghezza\t\n58,4 piedi\t 17,7 m\n\nApertura alare\t\n47,8 piedi\t 14,6 m\n\nAltezza\t\n14,3 piedi\t 4,3 m\n\nPosti a sedere\t\nMassimo 9"
[WEIGHT_AND_BALANCE]
max_gross_weight = 20450.0 // (pounds)
empty_weight = 11700.0 // (pounds)
reference_datum_position = 34.5, 0, 0 // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -35.79, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = "170, -17.0, -1.2, 0.0, Pilota" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170, -17.0, 1.2, 0.0, Copilota" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "170, -22.5, -1.2, 0.0, Passeggero 1" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "170, -22.5, 1.2, 0.0, Passeggero 2" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "170, -26.7, -1.2, 0.0, Passeggero 3" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = "170, -26.7, 1.2, 0.0, Passeggero 4" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = "0, -30.9, -1.2, 0.0, Passeggero 5" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = "0, -30.9, 1.2, 0.0, Passeggero 6" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = "0, -35.1, -1.2, 0.0, Passeggero 7" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.9 = "0, -35.1, 1.2, 0.0, Passeggero 8" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.10 = "100, -42.0, 0.0, 0.0, Bagaglio 1" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.11 = "50, -45.0, 0.0, 0.0, Bagaglio 2" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 50000
empty_weight_roll_MOI = 45000
empty_weight_yaw_MOI = 70000
empty_weight_coupled_MOI = 0.0
[electrical]
max_battery_voltage = 12.0
generator_alternator_voltage = 13.8
max_generator_alternator_amps = 40.0
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus = 0, 5 , 9.5
avionics = 1, 5 , 9.5
additional_system = 0, 2 , 9.5
marker_beacon = 1, 2 , 9.0
fuel_pump = 0, 5 , 9.0
[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 = -42.8, -4.8, 0.8 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -42.8, 4.8, 0.8 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency
min_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reverser
[TurbineEngineData]
fuel_flow_gain = 0.0025 //Gain on fuel flow
inlet_area = 4.2895 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 3500 //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
//0 Class
//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
[contact_points]
point.0=1, -10.00, 0.00, -4.35, 1181.1, 0, 0.6349, 46.8, 0.3000, 2.5, 0.9100, 10.0, 10.0, 0, 260.0, 260.0
point.1=1, -37.25, -4.75, -4.87, 1574.8, 1, 0.6349, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 2, 260.0, 260.0
point.2=1, -37.25, 4.75, -4.87, 1574.8, 2, 0.6349, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 3, 260.0, 260.0
point.3=2, -37.83, -23.92, -3.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -37.83, 23.92, -3.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -57.17, 0.00, 0.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, -11.47, 0.00, -1.50, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
static_pitch = -0.84
static_cg_height = 4.36
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 = 15.0 //Flap angle that activates warning at idle
flap_limit_power = 30.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.2 //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 = -16.385, -1.435, 3.012
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -39.00, -23.6, -0.25, fx_navredm ,
light.1 = 3, -39.00, 23.6, -0.25, fx_navgrem ,
light.2 = 3, -63.63, 0.00, 9.20, fx_navwhi ,
light.3 = 1, -37.00, 0.00, -2.59, fx_beaconb ,
light.4 = 2, -36.97, 0.00, -2.62, fx_strobe ,
light.5 = 1, -63.05, 0.00, 9.75, fx_beaconh ,
light.6 = 5, -29.7, -1.3, -1.71, fx_landing ,
light.7 = 5, -29.7, 1.3, -1.71, fx_landing ,
light.8 = 4, -16.00, 0.00, 2.25, fx_vclight,
light.9 = 4, -27.00, 0.00, 0.25, fx_vclighth,
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 5 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 8 // degrees
flaps-position.2 = 20 // degrees
flaps-position.3 = 40 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 0
Com.2 = 1, 0
Nav.1 = 1, 0, 1
Nav.2 = 1, 0, 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
[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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[fuel]
Center1 = -41.4, 0.0, -1.5, 359.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -36.3, -10.0, -1.5, 268.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -36.3, 10.0, -1.5, 268.5, 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
electric_pump=1
[airplane_geometry]
wing_area = 312.0 //Square feet
wing_span = 45.8 //Feet
wing_root_chord = 9.9 //Feet
wing_dihedral = 2.5 //Degrees
wing_incidence = 0.5 //Degrees
wing_twist = -1.5 //Degrees
oswald_efficiency_factor= 0.8 //Measure of lift effeciency of wing
wing_winglets_flag = 1 //Are winglets available?
wing_sweep = 13.4 //Degrees, wing leading edge
wing_pos_apex_lon = -31.5 //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 = 67.0 //Square feet
htail_span = 17.2 //Feet
htail_pos_lon = -59.1 //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 = 2.0 //Degrees
htail_sweep = 25.0 //Degrees, horizontal tail leading edge
vtail_area = 42.0 //Square feet
vtail_span = 7.4 //Feet, tip to body
vtail_sweep = 30.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -55.0 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 4.1 //Feet, vertical distance from reference point, positive going up
elevator_area = 17.0 //Square feet
aileron_area = 13.5 //Square feet
rudder_area = 7.3 //Square feet
elevator_up_limit = 17.0 //Degrees
elevator_down_limit = 15.5 //Degrees
aileron_up_limit = 18.0 //Degrees
aileron_down_limit = 18.0 //Degrees
rudder_limit = 30.0 //Degrees
elevator_trim_limit = 15.0 //Degrees
spoiler_limit = 60.0 //Degrees
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 4.6 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 5 //Degrees
min_flaps_for_spoilerons= 0.0 //Minimum flap handle position when spoilerons activate
[Reference Speeds]
flaps_up_stall_speed = 112.0 //Knots True (KTAS)
full_flaps_stall_speed = 102.0 //Knots True (KTAS)
cruise_speed = 464.0 //Knots True (KTAS)
max_mach = 0.81
max_indicated_speed = 330 //Red line (KIAS)
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 1
autothrottle_arming_required= 0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga= 0
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=11.00
nav_integrator_control=0.20
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
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=9000 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=27000 ; 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
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Aiuto Lear Jet 45!
