14 CFR § 33.72 Airworthiness Standards: Aircraft Engines

§ 33.72 Hydraulic actuating systems.

Current through Jul 24, 2026 · Read all of Part 33

⚠ 2 pending changes to Part 33

Each hydraulic actuating system must function properly under all conditions in which the engine is expected to operate. Each filter or screen must be accessible for servicing and each tank must meet the design criteria of § 33.71.

[Amdt. 33-6, 39 FR 35467, Oct. 1, 1974]

← § 33.71 Lubrication system.§ 33.73 Power or thrust response. →