Sec. 23.1182 — Nacelle areas behind firewalls.
Components, lines, and fittings, except those subject to the provisions of §23.1351(e), located behind the engine-compartment firewall must be constructed of such materials and located at such distances from the firewall that they will not suffer damage sufficient to endanger the airplane if a portion of the engine side of the firewall is subjected to a flame temperature of not less than 2000 °F for 15 minutes.
[Amdt. 23–14, 38 FR 31816, Nov. 19, 1973]
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