Eclipse 500 User Manual

Table of Contents Eclipse 5OO Systems Manual
Copyright © — Eclipse Aviation Corporation
xii Version 2.0 April 2007
5. Oxygen 71
Figure 46.Oxygen-ACS Interface................................................................................72
Figure 47.Oxygen Panel Location...............................................................................74
Figure 48.Oxygen Bottle Location (40 Cubic Foot).....................................................75
Figure 49.Oxygen Service Panel ................................................................................76
Figure 50.Cockpit Oxygen Pressure Gauge ...............................................................77
Figure 51.Armrest Oxygen Panel................................................................................77
Figure 52.Blowout Disc Location ................................................................................78
Figure 53.Oxygen Control Knob Activation.................................................................79
Figure 54.Crew Mask Hose Flow Indicator.................................................................79
Figure 55.Passenger Mask Selector Activation ..........................................................80
Figure 56.Pilot Quick-Don Mask Location ..................................................................81
Figure 57.Red Lever and Oxygen Mask Adjustment ..................................................82
Figure 58.Quick Don Mask Regulator.........................................................................82
Figure 59.Passenger Mask Location and Deployment (Right Switch Panel) .............83
Figure 60.Passenger Oxygen Mask Location and Deployment (Cabin).....................84
Figure 61.Passenger Oxygen Mask Flow Indicator ....................................................84
6. Ice Protection...........................................................................................................................93
Figure 62.Ice Protection-ACS Interface ......................................................................95
Figure 63.Center Switch Panel- Ice Protection...........................................................97
Figure 64.Ice Protection Synoptic ...............................................................................98
Figure 65.Windshield Heater Mat ...............................................................................99
Figure 66.Leading Edge De-Ice Boot Location.........................................................100
Figure 67.Engine Inlet Anti-Ice..................................................................................101
Figure 68.Wing Inspection Light Location.................................................................102
Figure 69.Windshield Overheat ................................................................................104
Figure 70.Windshield Heat Failure............................................................................105
Figure 71.Wing De-Ice Failure ..................................................................................106
Figure 72.Engine Anti-Ice Failure..............................................................................107
Figure 73.Pitot/AOA Probe Failure............................................................................108
Figure 74.Windshield Heat Sensor Fault ..................................................................109
7. Fuel 114
Figure 75.Fuel-ACS Interface ...................................................................................116
Figure 76.MFD Fuel Display .....................................................................................118
Figure 77.Sump Tank Quantity Display.....................................................................119
Figure 78.Fuel Synoptic- Normal ..............................................................................120
Figure 79.Estimated Fuel Used & Estimated Fuel Remaining Display.....................121
Figure 80.Fuel Synoptic- Fuel Hot Caution and Warning .........................................125
Figure 81.Fuel Synoptic: Temperature Sensor Failure ............................................126
Figure 82.Fuel Synoptic- Low Fuel Caution and Warning ........................................127
Figure 83.Fuel Synoptic- Low Fuel Pressure & Pressure Sensor Fault ...................129
Figure 84.Over wing Fuel Port-Right Wing ...............................................................131
Figure 85.Fuel Synoptic- Manual Fuel Crossfeed ....................................................132
8. Engines & Fire Protection.....................................................................................................137
Figure 86.PW 610F-A Engine ...................................................................................137
Figure 87.Thrust Control-ACS Interface ...................................................................139
Figure 88.Engine Starting-ACS Interface..................................................................141
Figure 89.Secondary Engine Parameter-ACS Interface...........................................142
Figure 90.Fire Detection and Suppression-ACS Interface .......................................143
Figure 91.Starter Assisted Air Start Envelope ...........................................................147
Figure 92.Engine Temperature Operating Envelope ................................................148
Figure 93.Engine Start Switch Panel ........................................................................149

Eclipse 500 Specifications

General

Manufacturer	Eclipse Aerospace
Model	Eclipse 500
Type	Very Light Jet
Engines	2 × Pratt & Whitney Canada PW610F turbofans
Thrust per engine	900 lbf (4.0 kN)
Wingspan	37.9 ft (11.6 m)
Height	11.0 ft (3.4 m)
Avionics	Avio NG
First Flight	August 26, 2002
Maximum Speed	430 mph
Range	1, 125 nautical miles
Service Ceiling	41, 000 ft (12, 500 m)
Crew	1 or 2
Max Takeoff Weight	6, 000 pounds
Seating Capacity	4-6
Length	33 feet 6 inches
Empty Weight	3, 550 pounds
Payload	Varies with configuration and fuel load