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Eclipse 500 - 2.5 Primary Sensors; 2.6 Aircraft Subsystems

Eclipse 500
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Section 1. Aircraft Overview Eclipse 5OO Systems Manual
Copyright © — Eclipse Aviation Corporation
Version 2.0 April 2007 11
1.7.2 Emergency Exits
The aircraft has a designated emergency exit located on the right side of the aircraft
to be used in the event that the primary (left-side) exit is rendered unavailable. This
door weighs approximately 12 lbs. To open the door:
Remove the cover
Pull the red handle to release the door
Pull the door in to rotate approximately 9
Place door through exit hatch and discard on aircraft wing.
Figure 8. Emergency Exit

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