CFR > Title 14 - Aeronautics and Space > CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION > SUBCHAPTER C—AIRCRAFT (parts 21 to 50) > PART 33—AIRWORTHINESS STANDARDS: AIRCRAFT ENGINES > SUBPART C—Design and Construction; Reciprocating Aircraft Engines (§33.31 to §33.39) > 33.34—Turbocharger rotors.

33.34—Turbocharger rotors.

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.

Code of Federal Regulations

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