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FAA-RD-73-98

GUIDELINES FOR LIGHTNING PROTECTION OF GENERAL AVIATION AIRCRAFT

active, Most Current
Organization: FAA
Publication Date: 1 October 1973
Status: active
Page Count: 167
scope:

Increasing numbers of single and multi-engine general aviation aircraft, and the greater availability and use of sophisticated avionics, is resulting in more frequent operation of these aircraft under instrument flight rule (IFR) conditions. As a result, their susceptibility to lightning strikes may increase. Coupled with this is another trend toward greater application of non-metallic materials in aircraft structural and fuel systems, and greater use of solid state components in avionics. This combination results in greater potential vulnerability to lightning strikes, and may require that specific lightning protective measures be developed and applied if operational reliability and flight safety are to be maintained. Protective measures suitable for all-metallic airframe, for example, may not be adequate for aircraft with some fiberglas or plastic sections. The all-metallic airframe is, in many ways, quite compatible with basic lightning protection. The same may not be true of all new aircraft designs, however.

Document History

FAA-RD-73-98
October 1, 1973
GUIDELINES FOR LIGHTNING PROTECTION OF GENERAL AVIATION AIRCRAFT
Increasing numbers of single and multi-engine general aviation aircraft, and the greater availability and use of sophisticated avionics, is resulting in more frequent operation of these aircraft...
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