1. Regulations
  2. title 14
  3. chapter I
  4. part 34
  5. subpart C
  6. § 34.20

View all text of Subpart C [§ 34.20 - § 34.25]

§ 34.20 - Applicability.

The provisions of this subpart are applicable to all aircraft gas turbine engines of the classes specified beginning on the dates specified in § 34.21.

AUTHORITY: 42 U.S.C. 4321

SOURCE: Docket No. 25613, 55 FR 32861, Aug. 10, 1990, unless otherwise noted.

CITE AS: 14 CFR 34.20