[fltsim.0]
title=Eclipse 500
sim=Eclipse500
model=
panel=
sound=
texture=
checklists=
atc_heavy=0
atc_airline=ECLIPSE
atc_flight_number=500
atc_parking_types=GATE,RAMP
atc_parking_codes=ECL
kb_checklists=Eclipse500_check
kb_reference=Eclipse500_ref
atc_id=N616NA
ui_manufacturer=Eclipse
ui_type=Model 500
ui_variation=Luxury Corporate LTD.
description=Eclipse Aviation has created a luxurious six-place, twin-turbofan aircraft that costs less than most used turboprops. It is more economical to own and operate than most of todays single engine pistons and all multi-engine pistons and turboprops. For those who dont want to pilot themselves, we anticipate that aircraft charter and air taxi services, complete with professional pilots, will typically be competitive with a full-fare airline ticket.
The Eclipse 500 cruises at a brisk 375 kts and has a generous 1,280 nautical mile range with 4 occupants, NBAA IFR reserve (1,395 nm with 45-minute IFR reserve). A 41,000-foot ceiling avoids most severe weather and the 67-knot stall speed makes safe landings easier. Excellent performance at high altitudes and hot temperatures builds in an extra margin of safety. The Eclipse 500 will be certified for single-pilot operation to FAR Part 23.
Eclipse Aviation is creating a luxurious six-place, twin-turbofan aircraft that costs less than most used turboprops. It is more economical to own and operate than most of todays single engine pistons and all multi-engine pistons and turboprops. For those who dont want to pilot themselves, we anticipate that aircraft charter and air taxi services, complete with professional pilots, will typically be competitive with a full-fare airline ticket.
The Eclipse 500 cruises at a brisk 375 kts and has a generous 1,280 nautical mile range with 4 occupants, NBAA IFR reserve (1,395 nm with 45-minute IFR reserve). A 41,000-foot ceiling avoids most severe weather and the 67-knot stall speed makes safe landings easier. Excellent performance at high altitudes and hot temperatures builds in an extra margin of safety. The Eclipse 500 will be certified for single-pilot operation to FAR Part 23.
In building the Eclipse 500, Eclipse Aviation is pioneering the use of innovative manufaturing processes that speed production and lower costs. Tehnologies such as friction stir welding, which replaces more than sixty percent of the rivets on major aircraft assemblies, reduce assembly time drastically while producing superior joins on the aluminum aircraft.
The Eclipse 500 is an entirely new concept that puts high-performance jet ownership within reach for the first time.
[General]
atc_type=Eclipse
atc_model=500
editable=1
performance=Cruise Speed\t\nMach 0.64 375 kts 694 kmh\n\nEngines\t\nPratt & Whitney PW610F 900 lb thrust\n\nMaximum Range\t\n1,395 nm 1280 sm \t 2584 km\n\nService Ceiling\t\n41,000 ft 15,545 m\n\nFuel Capacity\t\n1,540 lb 699 kg\n230 U.S. gal 871 L \n\nMaximum Gross Weight\t\n8,081 lb 2,576 kg\n\nMaximum Takeoff Weight - HGW\t\n5,640 lb \t2,588 kg\n\nUseful Load\t\n2,250 lb \t1,021 kg\n\nLength\t\n33.1 ft\t 10.1 m\n\nWingspan\t\n37.4 ft\t 11.4 m\n\nHeight\t\n11.0 ft\t 3.4 m\n\nSeating\t\nUp to 6
[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 = 8081.000
empty_weight = 5640.000
reference_datum_position = 0.0, 0.0, 0.0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0.0, 0.0, 0.0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = "170, 5.25, -1.10, 1.20, Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170, 5.25, 1.10, 1.20, Front Passenger" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "160, 1.55, -1.10, 1.20, Rear Passenger" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "160, 1.55, 1.10, 1.20, Rear Passenger" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "60, -3.35, 0.00, 1.25, Baggage" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 30000
empty_weight_roll_MOI = 18200
empty_weight_yaw_MOI = 36500
empty_weight_coupled_MOI= 0.0
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =1.000
induced_drag_scalar =1.000
elevator_effectiveness =1.000
aileron_effectiveness =1.500
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 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -7.5, -2.70, 2.40 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -7.5, 2.70, 2.40 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 0.7 //Scalar for fuel flow efficiency
min_throttle_limit= -0.999999;
max_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear
[fuel]
//Tanks Position and capacity:
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = 0.00, -3.00, 0.90, 115.0, 0.00
RightMain= 0.00, 3.00, 0.90, 115.0, 0.00
//Fuel type: 1 = Avgas, 2 = JetA
fuel_type=2
number_of_tank_selectors = 1
electric_pump=0
[TurbineEngineData]
fuel_flow_gain = 0.0025 //Gain on fuel flow
inlet_area = 2.2495 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 1800 //Lbs, max rated static thrust at Sea Level
afterburner_available = 0 //Afterburner available?
reverser_available = 1 //Thrust reverser available?
[jet_engine]
thrust_scalar = 1.00
[smokesystem]
smoke.0 = 10.4, -12.5, -2.7, fx_smoke_w
smoke.1 = 10.4, -12.5, 2.7, fx_smoke_w
[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
//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, 26.90, 0.00, -4.460, 1181.1, 0.00, 0.490, 55.0, 0.944, 1.550, 0.309, 9.0, 10.0, 0
point.1 = 1, -2.90, -4.60, -4.500, 1574.8, 1.00, 0.670, 0.0, 0.794, 1.550, 0.269, 9.0, 11.0, 2
point.2 = 1, -2.90, 4.60, -4.500, 1574.8, 2.00, 0.670, 0.0, 0.794, 1.550, 0.269, 11.0, 13.0, 3
point.3 = 2, -3.60, -23.9, 1.17, 1574.8, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.4 = 2, -3.60, 23.9, 1.17, 1574.8, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.5 = 2, 27.93, 0.0, -0.53, 1574.8, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.6 = 2, -19.40, 0.0, 2.20, 1574.8, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
static_pitch =0.84 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=4.46 //feet, altitude of CG when at rest on the ground
gear_system_type=1
[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 = 1.5 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
[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= 5.40, -1.10, 2.95 //(feet) longitudinal, lateral, vertical distance from reference datum//fore-aft. left-right. up-down
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -2.08, -19.76, 1.72, fx_navredc ,
light.1 = 3, -2.08, 19.81, 1.76, fx_navgrec ,
light.2 = 2, -2.08, -19.76, 1.72, fx_strobe ,
light.3 = 2, -2.08, 19.81, 1.76, fx_strobe ,
light.4 = 1, 1.31, 0.00, -1.18, fx_beacon ,
light.5 = 4, 4.95, 0.00, 2.50, fx_vclight,
light.6 = 4, 6.00, 0.00, 0.50, fx_vclight,
light.7 = 2, -2.96, -19.72, 1.81, fx_strobe ,
light.8 = 2, -2.96, 19.74, 1.84, fx_strobe ,
light.9 = 1, -6.28, 0.00, 3.97, fx_beacon ,
light.10 = 4, 0.00, -1.15, 3.10, fx_vclight,
light.11 = 2, -16.31, 0.00, 8.90, fx_recog ,
light.12 = 3, -16.31, 0.00, 8.90, fx_strobe ,
light.13 = 2, 1.31, 0.00, -1.17, fx_recog ,
light.14 = 3, -8.25, -2.70, 2.40, fx_eclight,
light.15 = 3, -8.25, 2.69, 2.40, fx_eclight,
light.16 = 4, 0.00, 1.15, 3.10, fx_vclight,
light.17 = 5, 1.76, -2.27, -0.56, fx_landing ,
light.18 = 5, 1.76, 2.27, -0.56, fx_landing ,
[Flaps.0]
type= 1
span-outboard= 2.800
extending-time= 12.000
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= 15.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 35.000, 0.000
[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 =1,0
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
[exits]
number_of_exits = 1
exit_rate.0 = 0.20
[TailHook]
tailhook_length=2 ;(feet)
tailhook_position=-15.0, 0.0, -4.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=2.0
[LSO]
LSOAdjustSpeed=1.05
[folding_wings]
wing_fold_system_type = 4 ;0=None
fold_rates = 0.12,0.11 ;Percent per second
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
startup=fx_engstrt_jenny
touchdown=fx_tchdwn_s, 1
Contrail=fx_contrail_s
windshield_rain_effect_available = 1
[airplane_geometry]
wing_area = 312.0 //Square feet
wing_span = 33.8 //Feet
wing_root_chord = 7.3 //Feet
wing_dihedral = 2.5 //Degrees
wing_incidence = 0.5 //Degrees
wing_twist = -1.5 //Degrees
oswald_efficiency_factor= 1.0 //Measure of lift effeciency of wing
wing_winglets_flag = 1 //Are winglets available?
wing_sweep = 0.0 //Degrees, wing leading edge
wing_pos_apex_lon = -8.0 //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 = 67.0 //Square feet
htail_span = 13.2 //Feet
htail_pos_lon = -19.1 //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 = -18.0 //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 = 22.0 //Degrees
aileron_down_limit = 22.0 //Degrees
rudder_limit = 30.0 //Degrees
elevator_trim_limit = 15.0 //Degrees
spoiler_limit = 60.0 //Degrees
spoilerons_available = 0 //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 = 87.000
full_flaps_stall_speed = 64.000
cruise_speed = 385.000
max_indicated_speed=435.000000
max_mach=0.659990
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=101.00
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8.0
use_no_default_pitch=1
use_no_default_bank=1
default_bank_mode=0
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=30.000000
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=1.000000
default_pitch_mode=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=7500 ; in microseconds
crash_duration2=250000 ; in microseconds
[stall_warning]
type=1
