14 CFR § 33.34 Airworthiness Standards: Aircraft Engines

§ 33.34 Turbocharger rotors.

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

⚠ 2 pending changes to Part 33

Each turbocharger case must be designed and constructed to be able to contain fragments of a compressor or turbine that fails at the highest speed that is obtainable with normal speed control devices inoperative.

[Amdt. 33-22, 72 FR 50860, Sept. 4, 2007]

← § 33.33 Vibration.§ 33.35 Fuel and induction system. →