§23.1522 Auxiliary power unit limitations.

14 CFR 23 · Operating Limitations and Information · at 23-63 (current)

Text in force at 23-63: from 23-45, effective 7 Sep 1993.

[If an auxiliary power unit is installed, the limitations established for the auxiliary power unit must be specified in the operating limitations for the airplane.]

58 FR 42166 · Source

Version history

Version	Effective	Published
23-45	7 Sep 1993	58 FR 42166

Rulemaking for 23-45

nprm 90-18 15 Jun 1990
final rule 26269 28 Jul 1993

Aircraft using this section

Cirrus Design Corporation SR20 entry 1 at 23-45
Cirrus Design Corporation SR22 entry 1 at 23-45
Cirrus Design Corporation SR22T entry 1 at 23-45
Costruzioni Aeronautiche Tecnam S.P.A. P2006T entry 1 at 23-45
Daher Aircraft Design, LLC Kodiak 200 entry 1 at 23-45
Diamond Aircraft Industries GmbH DA 42 entry 2 at 23-45
Diamond Aircraft Industries GmbH DA 42 M-NG entry 2 at 23-45
Diamond Aircraft Industries GmbH DA 42 NG entry 2 at 23-45
Diamond Aircraft Industries GmbH DA 62 entry 2 at 23-45
Diamond Aircraft Industries Inc. DA 40 entry 2 at 23-45
Diamond Aircraft Industries Inc. DA 40 entry 6 at 23-45
Diamond Aircraft Industries Inc. DA 40 F entry 2 at 23-45
Diamond Aircraft Industries Inc. DA 40 F entry 6 at 23-45
Diamond Aircraft Industries Inc. DA 40 NG entry 2 at 23-45
Diamond Aircraft Industries Inc. DA 40 NG entry 11 at 23-45
Diamond Aircraft Industries Inc. DA 62 entry 1 at 23-45
Epic Aircraft, LLC E1000 entry 1 at 23-45
Honda Aircraft Company LLC HA-420 entry 1 at 23-45
Korean Aerospace Industries, LTD KC-100 entry 1 at 23-45
Pilatus Aircraft Ltd PC-24 entry 1 at 23-45
Piper Aircraft, Inc. PA-46-600TP entry 5 at 23-45
Piper Aircraft, Inc. PA-46-701TP entry 5 at 23-45
Piper Aircraft, Inc. PA-46-701TP entry 6 at 23-45
Textron Aviation Inc. 525B entry 2 at 23-45
Textron Aviation Inc. LC40-550FG entry 1 at 23-45
Textron Aviation Inc. LC41-550FG entry 1 at 23-45
Textron Aviation Inc. LC42-550FG entry 1 at 23-45

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