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§23.993 Fuel system lines and fittings.

14 CFR 23 · Powerplant · Fuel System Components · at 23-63 (current)

Text in force at 23-63: from 23-43, effective 10 May 1993.

(a) Each fuel line must be installed and supported to prevent excessive vibration and to withstand loads due to fuel pressure and accelerated flight conditions. (b) Each fuel line connected to components of the airplane between which relative motion could exist must have provisions for flexibility. (c) Each flexible connection in fuel lines that may be under pressure and subjected to axial loading must use flexible hose assemblies. [(d) Each flexible hose must be shown to be suitable for the particular application.] (e) No flexible hose that might be adversely affected by exposure to high temperatures may be used where excessive temperatures will exist during operation or after engine shutdown.

58 FR 18973 · Source

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