14 C.F.R. · Aeronautics and Space
14 C.F.R. § 33.66

Bleed air system.

Title 14 C.F.R. ● ACTIVE Primary Source
Regulatory Text

14 C.F.R. § 33.66 — Bleed air system.

§ 33.66 Bleed air system. The engine must supply bleed air without adverse effect on the engine, excluding reduced thrust or power output, at all conditions up to the discharge flow conditions established as a limitation under § 33.7(c)(11). If bleed air used for engine anti-icing can be controlled, provision must be made for a means to indicate the functioning of the engine ice protection system. [Amdt. 33-10, 49 FR 6851, Feb. 23, 1984]

Source: ecfr.gov · govinfo.gov — public domain Official Source ↗
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14 C.F.R. § 33.66
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The regulatory text of 14 C.F.R. § 33.66 is reproduced from the official Code of Federal Regulations as published by the Office of the Federal Register and the National Archives and Records Administration.
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