[fltsim.0]
title=Learjet 45 INTER
sim=Lear45
model=
panel=
sound=
texture=moz
kb_checklists=Lear45_check
kb_reference=Lear45_ref
atc_id_enable=1
atc_id=C8-MZK
ui_manufacturer=Bombardier
ui_type=Learjet 45
ui_variation=gold Private
description=Texturized in Metallic Reflective Innovation color of Private Mozambique by Mario Coelho\nwww.bluestarsim.cjb.net\n"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."
atc_airline=INTER
atc_flight_number=
atc_heavy=0
visual_damage=1
[General]
atc_type=LEARJET
atc_model=LJ45
editable=1
performance=Revised by Mario Coelho OUT2003\nCruise Speed\t\nMach 0.81 464 kts 859 kmh\n\nEngines\t\nAllied Signal TFE731-20 3,500 lb thrust\n\nMaximum Range\t\n2,200 nm 2,532 sm \t 4,074 km\n\nService Ceiling\t\n51,000 ft 15,545 m\n\nFuel Capacity\t\n6,062 lb 2,722 kg\n905 U.S. gal 3,424 L \n\nMaximum Gross Weight\t\n20,450 lb 9,276 kg\n\nMaximum Takeoff Weight - HGW\t\n20,200 lb \t9,163 kg\n\nUseful Load\t\n8,750 lb \t3,969 kg\n\nLength\t\n58.4 ft\t 17.7 m\n\nWingspan\t\n47.8 ft\t 14.6 m\n\nHeight\t\n14.3 ft\t 4.3 m\n\nSeating\t\nUp to 9
[WEIGHT_AND_BALANCE]
max_gross_weight= 20450.000
empty_weight= 11700.000
reference_datum_position= 34.500, 0.000, 0.000
empty_weight_CG_position= -35.790, 0.000, 0.000
max_number_of_stations=50
station_load.0=0.000, 0.000, 0.000, 0.000
station_load.1="170, -17.0, 1.2, 0.0, Co-Pilot" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2="170, -22.5, -1.2, 0.0, Passenger 1" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3="170, -22.5, 1.2, 0.0, Passenger 2" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4="170, -26.7, -1.2, 0.0, Passenger 3" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5="170, -26.7, 1.2, 0.0, Passenger 4" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6="0, -30.9, -1.2, 0.0, Passenger 5" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7="0, -30.9, 1.2, 0.0, Passenger 6" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8="0, -35.1, -1.2, 0.0, Passenger 7" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.9="0, -35.1, 1.2, 0.0, Passenger 8" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.10="100, -42.0, 0.0, 0.0, Baggage1" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.11="50, -45.0, 0.0, 0.0, Baggage2" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI= 50000.000
empty_weight_roll_MOI= 45000.000
empty_weight_yaw_MOI= 70000.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[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=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
[GeneralEngineData]
engine_type= 1
Engine.0= -42.800, -4.800, 0.800
Engine.1= -42.800, 4.800, 0.800
fuel_flow_scalar= 1.000
min_throttle_limit=-0.25 //Minimum percent throttle. Generally negative for turbine reverser
[TurbineEngineData]
fuel_flow_gain= 0.003
inlet_area= 4.290
rated_N2_rpm= 29920.000
static_thrust= 3500.000
afterburner_available= 0
reverser_available= 1
[jet_engine]
thrust_scalar=1.000
//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= 1.000, -10.000, 0.000, -4.350, 1181.100, 0.000, 0.635, 46.800, 0.300, 2.500, 0.910, 10.000, 10.000, 0.000, 0.000, 0.000
point.1= 1.000, -37.250, -4.750, -4.870, 1574.800, 1.000, 0.635, 0.000, 0.480, 2.500, 0.546, 9.000, 9.000, 2.000, 260.000, 438.894
point.2= 1.000, -37.250, 4.750, -4.870, 1574.800, 2.000, 0.635, 0.000, 0.480, 2.500, 0.546, 9.000, 9.000, 3.000, 260.000, 438.894
point.3= 2.000, -37.830, -23.920, -3.000, 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, -37.830, 23.920, -3.000, 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, -57.170, 0.000, 0.000, 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, -11.470, 0.000, -1.500, 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= -0.500
static_cg_height= 3.760
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,
[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= -41.400, 0.000, -1.500, 359.000, 0.000
LeftMain= -36.300, -10.000, -1.500, 268.500, 0.000
RightMain= -36.300, 10.000, -1.500, 268.500, 0.000
fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=1
[airplane_geometry]
wing_area= 312.000
wing_span= 45.800
wing_root_chord= 9.900
wing_dihedral= 2.500
wing_incidence= 0.500
wing_twist= -1.500
oswald_efficiency_factor= 0.800
wing_winglets_flag= 1
wing_sweep= 13.400
wing_pos_apex_lon= -31.500
wing_pos_apex_vert= 0.000
htail_area= 67.000
htail_span= 17.200
htail_pos_lon= -59.100
htail_pos_vert= 0.000
htail_incidence= 2.000
htail_sweep= 25.000
vtail_area= 42.000
vtail_span= 7.400
vtail_sweep= 30.000
vtail_pos_lon= -55.000
vtail_pos_vert= 4.100
elevator_area= 17.000
aileron_area= 13.500
rudder_area= 7.300
elevator_up_limit= 17.000
elevator_down_limit= 15.500
aileron_up_limit= 18.000
aileron_down_limit= 18.000
rudder_limit= 30.000
elevator_trim_limit= 15.000
spoiler_limit= 60.000
spoilerons_available= 1
aileron_to_spoileron_gain= 4.600
min_ailerons_for_spoilerons= 5.000
min_flaps_for_spoilerons= 0.000
[Reference Speeds]
flaps_up_stall_speed= 112.000
full_flaps_stall_speed= 102.000
cruise_speed= 464.000
max_mach=0.81
max_indicated_speed=330 //Red line (KIAS)
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1200.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;
use_no_default_bank=1
use_no_default_pitch=1
default_pitch_mode=0
default_bank_mode=0
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
[SMOKESYSTEM]
smoke.0=7.00,-73.00,-8.70,fx_smoke_rx.fx ,//left engine;
smoke.1=7.00,-73.00, 8.70,fx_smoke_rx.fx ,//right engine;
[exits]
number_of_exits=2
exit_rate.0=0.4
exit_rate.1=0.4
[Flaps.0]
type= 0
span-outboard= 0.000
extending-time= 0.000
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
[Flaps.1]
type= 1
span-outboard= 0.800
extending-time= 5.000
system_type= 0
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 8.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 40.000, 0.000
