10 August 2006
5 December 1984
LIGHTING, EMERGENCY EGRESS, SUBASSEMBLY
This specification is approved for use by the Naval Air Systems Command and is available for
use by all Departments and Agencies of the Department of Defense.
1.1 Scope. This specification establishes the Emergency Egress Lighting Subassembly
(EELS) requirements for fixed wing, rotary wing, lighter-than-air, and tilt-rotor aircraft and fixed
wing or rotary wing aircraft configured as passenger carrying aircraft.
2. APPLICABLE DOCUMENTS.
2.1 General. The documents listed in this section are specified in sections 3 and 4 of this
specification. This section does not include documents cited in other sections of this
specification or recommended for additional information or as examples. While every effort has
been made to ensure the completeness of this list, document users are cautioned that they must
meet all specified requirements of documents cited in sections 3 and 4 of this specification,
whether or not they are listed.
2.2 Government documents.
2.2.1 Specifications, standards, and handbooks. The following specifications, standards,
and handbooks form a part of this document to the extent specified herein. Unless otherwise
specified, the issues of these documents are those cited in the solicitation or contract.
Comments, suggestions, or questions on this document should be addressed to the Naval Air
Systems Command (Commander, Naval Air Warfare Center Aircraft Division, Code
491000B120-3, Highway 547, Lakehurst, NJ 08733-5100), or by email to
firstname.lastname@example.org. Since contact information can change, you may want to verify the
currency of this address information using the ASSIST Online database at
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