[fltsim.0]
title=Learjet 45 AW
sim=lear45_AW
model=
panel=
sound=
texture=
checklists=
kb_checklists=Lear45_check
kb_reference=Lear45_ref
atc_id=L45
ui_manufacturer=Learjet
ui_type=45
ui_variation=Learjet AW
visual_damage=1
description=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.  FDE by Al Whitney.



[General]
ATC_type=Learjet
ATC_model=
Editable=0
performance=Cruise 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\n2,650 lb  \t1,202 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

[Jet_Engine]
Thrust_Scalar=1.000

[Flight_Tuning]
Cruise_Lift_Scalar=     1.000
Parasite_Drag_Scalar=   1.000
Induced_Drag_Scalar=    1.000
Pitch_Stability=        1.000
Roll_Stability=         0.900
Yaw_Stability=          1.000
Elevator_Effectiveness= 0.800
Aileron_Effectiveness=  0.700
Rudder_Effectiveness=   1.000

[WEIGHT_AND_BALANCE]
Max_Gross_Weight=20450.0
Reference_Datum_Position=0,0,0
Empty_Weight_CG_position=0,0,0
Empty_Weight=11700.0

Max_Number_of_Stations = 50
//      Load #  = Wt.   Long   Lat  Vert.
station_load.0  = 170,   0.0, -1.2, 0.0    // Pilot
station_load.1  = 170,   0.0,  1.2, 0.0    // Co-Pilot
station_load.2  = 170,   0.0, -1.2, 0.0    // Pax 1
station_load.3  = 170,   0.0,  1.2, 0.0    // Pax 2
station_load.4  = 170,   0.0, -1.2, 0.0    // Pax 3
station_load.5  = 170,   0.0,  1.2, 0.0    // Pax 4
station_load.6  =   0,   0.0, -1.2, 0.0    // Pax 5
station_load.7  =   0,   0.0,  1.2, 0.0    // Pax 6
station_load.8  =   0,   0.0, -1.2, 0.0    // Pax 7
station_load.9  =   0,   0.0,  1.2, 0.0    // Pax 8
station_load.10 = 140,   0.0,  0.0, 0.0    // Bag 1
station_load.11 = 140,   0.0,  0.0, 0.0    // Bag 2

// ***************************************
// BACAL LJ45 "Air" File Parameters      *   Default 2k2 Lear
// Zero Lift Drag    = 0.02148 --> Clean <-- 0.02148
// Flap Drag         = 0.08984           *   0.08008
// Gear Drag         = 0.01709           *   0.01709
// ---------------------------           *   -------
// Total Drag        = 0.12841 --> Dirty <-- 0.11865
// ______________________________________*__________
// Spoiler Drag      = 0.04492           *   0.04785
// ***************************************
// Empty Weight       = 11,700 lbs.
// Pax + Baggage      =  1,300 lbs.
// -------------------------------
// Zero Fuel Weight   = 13,000 lbs.
// Max Fuel (900gal)  =  6,030 lbs. (Fuel Weight = 6.7 lb/gal)
// -------------------------------
// Take Off Weight    = 19,030 lbs.
// --------------------------------

empty_weight_roll_MOI = 51576.0
empty_weight_pitch_MOI= 43509.0
empty_weight_yaw_MOI  = 71814.0
empty_weight_coupled_MOI=1300.0

// --------- Lear45 Electrical Start ---
// BusType, MaxAmpLoad, MinVoltage - 
// BusTypes: 0=MainBus,1=AvionicsBus,2=BatteryBus,
// 3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)

[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 40.0
avionics_bus       = 0, 10, 9.5
avionics           = 1, 5 , 9.5
additional_system  = 0, 20, 9.5
marker_beacon      = 1, 2 , 9.0
fuel_pump          = 0, 5 , 9.0
// -------- Lear45 Electrical End ---

// Increasing value = faster reaction in the VSI, better A/P Lockup.
[pitot_static]
vertical_speed_time_constant=10.0

[fuel]
Center1=  0.0,0.0,0.0,360.0,0.0
LeftMain= 0.0,0.0,0.0,270.0,0.0
RightMain=0.0,0.0,0.0,270.0,0.0
fuel_type=2
number_of_tank_selectors=1

[airplane_geometry]
wing_area=312.0
wing_span=45.8
wing_root_chord=7.3
wing_dihedral=0.35
wing_incidence=1.43
wing_twist=-1.0
oswald_efficiency_factor=0.8
wing_winglets_flag=1
wing_sweep=35.0
wing_pos_apex_lon=0.0
wing_pos_apex_vert=0.0
htail_area=63.0
htail_span=17.5
htail_pos_lon=-25.5
htail_pos_vert=0.0
htail_incidence=0.0
htail_sweep=25.0
vtail_area=50.0
vtail_span=8.0
vtail_sweep=30.0
vtail_pos_lon=-24.0
vtail_pos_vert=5.8
elevator_area=15.75
aileron_area=13.52
rudder_area=8.50
elevator_up_limit=27.5
elevator_down_limit=20.6
aileron_up_limit=19.5
aileron_down_limit=14.8
rudder_limit=23.5
elevator_trim_limit=19.4
spoiler_limit=59.0
spoilerons_available=0
aileron_to_spoileron_gain=0
min_ailerons_for_spoilerons=0
min_flaps_for_spoilerons=0

// Landing Gear Positions Guide
// 0  Class Type                   1=Gear, 2 = Scrape
// 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]
//    # 0     1       2      3     4     5    6      7    8    9    10  11 12   13
point.0=1,  23.33,   0.00, -4.08, 1575, 0.0, 0.64, 46.0, 0.2, 2.5, 0.85, 5, 5, 0,0,0
point.1=1,  -1.15,  -4.83, -4.90, 1575, 1.0, 0.64,  0.0, 0.5, 2.5, 0.53, 5, 5, 2,0,0
point.2=1,  -1.15,   4.83, -4.90, 1575, 2.0, 0.64,  0.0, 0.5, 2.5, 0.53, 5, 5, 3,0,0
point.3=2,   3.16, -22.83, -1.00, 1575, 0.0, 0.00,  0.0, 0.0, 0.0, 0.00, 0, 0, 5,0,0
point.4=2,   3.16,  22.83, -1.00, 1575, 0.0, 0.00,  0.0, 0.0, 0.0, 0.00, 0, 0, 6,0,0
point.5=2, -24.41,   0.00, -0.83, 1575, 0.0, 0.00,  0.0, 0.0, 0.0, 0.00, 0, 0, 9,0,0
point.6=2,  26.41,   0.00, -2.83, 1575, 0.0, 0.00,  0.0, 0.0, 0.0, 0.00, 0, 0, 4,0,0

static_pitch=0.0
static_cg_height=4.41

[Views]
eyepoint=-14.0, -1.31, 1.64

[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

[Flaps.0]
type             = 1          // 1 - tail, 2 - lead
span-outboard    = 0.8        // 0.0 .. 1.0
extending-time   = 5          // seconds
system_type      = 0
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

[GeneralEngineData]
engine_type=1
Engine.0=-8.4,-5.0,0.83       // Long, Lat, Vert
Engine.1=-8.4, 5.0,0.83       // Long, Lat, Vert
Fuel_Flow_Scalar=1.60

[TurbineEngineData]
fuel_flow_gain=0.0022
inlet_area=4.5
rated_N2_rpm=29920.0
static_thrust=3600.0
afterburner_available=0
reverser_available=1

[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)

[Autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=2000.0
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_max_rpm=90
autothrottle_takeoff_ga=0
pitch_takeoff_ga=8.0
use_no_default_bank=1
use_no_default_pitch=1

[keyboard_response]
elevator= 150.0,250.0
aileron=  150.0,250.0
rudder=   150.0,250.0

[direction_indicators]
direction_indicator.0=3,0

[SMOKESYSTEM]
smoke.0=0.8,-48.8,-4.8, fx_smoke_w                  
smoke.1=0.8,-48.8,4.8, fx_smoke_w

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


[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