§25.934 Turbojet engine thrust reverser system tests.

14 CFR 25 · Powerplant · General · at 25-153 (current)

Text in force at 25-153: from 25-23, effective 8 May 1970.

[Thrust reversers installed on turbojet engines must meet the requirements of Sec. 33.97 of this chapter.]

35 FR 5677 · Source

Version history

Version	Effective	Published
25-23	8 May 1970	35 FR 5677

Rulemaking for 25-23

nprm 68-18 16 Aug 1968
final rule 9079 1 Apr 1970

Aircraft using this section

Airbus Defence and Space S.A C-212-CB entry 3 at 25-23
Airbus Defence and Space S.A C-212-CC entry 3 at 25-23
Airbus Defence and Space S.A C-212-CD entry 3 at 25-23
Airbus Defence and Space S.A C-212-CE entry 3 at 25-23
Airbus Defence and Space S.A C-212-DD entry 3 at 25-23
Airbus Defence and Space S.A C-212-EE entry 3 at 25-23
Airbus Defence and Space S.A C-212-EE entry 4 at 25-23
Airbus Defence and Space S.A C-212-VA entry 3 at 25-23
GULFSTREAM AEROSPACE LP (GALP) GALAXY entry 2 at 25-23
GULFSTREAM AEROSPACE LP (GALP) GULFSTREAM 200 entry 2 at 25-23
GULFSTREAM AEROSPACE LP (GALP) Gulfstream G150 entry 2 at 25-23
Gulfstream Aerospace Corporation GVII-G500 entry 2 at 25-23
Gulfstream Aerospace Corporation GVII-G600 entry 2 at 25-23
Textron Aviation Inc. 4000 entry 1 at 25-23
The Boeing Company 767-200 entry 4 at 25-23
The Boeing Company 767-300 entry 4 at 25-23

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