14 CFR 34.10

§ 34.10 Applicability.

United States · 14 CFR — Aeronautics and Space · Status: effective

Cite this

Citation: 14 CFR 34.10, § 34.10 Applicability, United States, version 1 as recorded 2026-07-09, yourstate.us, https://yourstate.us/provision/55132
Permanent ID: ys:prov:55132@1
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Full text

(a) The provisions of this subpart are applicable to all new aircraft gas turbine engines of classes T3, T8, TSS, and TF equal to or greater than 36 kN (8,090 lb) rated output, manufactured on or after January 1, 1974, and to all in-use aircraft gas turbine engines of classes T3, T8, TSS, and TF equal to or greater than 36 kN (8,090 lb) rated output manufactured after February 1, 1974. (b) The provisions of this subpart are also applicable to all new aircraft gas turbine engines of class TF less than 36 kN (8,090 lb) rated output and class TP manufactured on or after January 1, 1975, and to all in-use aircraft gas turbine engines of class TF less than 36 kN (8,090 lb) rated output and class TP manufactured after January 1, 1975.

Legislative history

This is a federal regulation, adopted through agency rulemaking under the Administrative Procedure Act — not enacted by a recorded vote of Congress.