§23.934 Turbojet and turbofan engine thrust reverser systems tests.

14 CFR 23 · Powerplant · General · at 23-63 (current)

Text in force at 23-63: from 23-43, effective 10 May 1993.

[Thrust reverser systems of turbojet or turbofan engines must meet the requirements of Sec. 33.97 of this chapter or it must be demonstrated by tests that engine operation and vibratory levels are not affected.]

58 FR 18971 · Source

Version history

Version	Effective	Published
23-43	10 May 1993	58 FR 18971

Rulemaking for 23-43

nprm 90-23 17 Sep 1990
final rule 26344 29 Mar 1993

Aircraft using this section

Cirrus Design Corporation SR20 entry 1 at 23-43
Cirrus Design Corporation SR22 entry 1 at 23-43
Cirrus Design Corporation SR22T entry 1 at 23-43
Costruzioni Aeronautiche Tecnam S.P.A. P2006T entry 1 at 23-43
Daher Aircraft Design, LLC Kodiak 200 entry 1 at 23-43
Diamond Aircraft Industries GmbH DA 42 entry 2 at 23-43
Diamond Aircraft Industries GmbH DA 42 M-NG entry 2 at 23-43
Diamond Aircraft Industries GmbH DA 42 NG entry 2 at 23-43
Diamond Aircraft Industries GmbH DA 62 entry 2 at 23-43
Diamond Aircraft Industries Inc. DA 40 entry 2 at 23-43
Diamond Aircraft Industries Inc. DA 40 entry 6 at 23-43
Diamond Aircraft Industries Inc. DA 40 F entry 2 at 23-43
Diamond Aircraft Industries Inc. DA 40 F entry 6 at 23-43
Diamond Aircraft Industries Inc. DA 40 NG entry 2 at 23-43
Diamond Aircraft Industries Inc. DA 40 NG entry 11 at 23-43
Diamond Aircraft Industries Inc. DA 62 entry 1 at 23-43
Epic Aircraft, LLC E1000 entry 1 at 23-43
Honda Aircraft Company LLC HA-420 entry 1 at 23-43
Korean Aerospace Industries, LTD KC-100 entry 1 at 23-43
Pilatus Aircraft Ltd PC-24 entry 1 at 23-43
Piper Aircraft, Inc. PA-46-600TP entry 5 at 23-43
Piper Aircraft, Inc. PA-46-701TP entry 5 at 23-43
Piper Aircraft, Inc. PA-46-701TP entry 6 at 23-43
Textron Aviation Inc. 525B entry 2 at 23-43
Textron Aviation Inc. LC40-550FG entry 1 at 23-43
Textron Aviation Inc. LC41-550FG entry 1 at 23-43
Textron Aviation Inc. LC42-550FG entry 1 at 23-43

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