§25.1717 Circuit protective devices; EWIS

CS-25 · Subpart H — Electrical Wiring Interconnection System · at CS25-28 (current)

Text in force at CS25-28: from CS25-5, effective 5 Sep 2008.

(See AMC 25.1717) EWIS components must be designed and installed so they are compatible with the circuit protection devices required by CS 25.1357, so that a fire or smoke hazard cannot be created under temporary or continuous fault conditions.

ED Decision 2008/006/R · Source

Version history

Version	Effective	Published
CS25-5	5 Sep 2008	ED Decision 2008/006/R

Rulemaking for CS25-5

easa npa NPA 2007-01
easa decision ED Decision 2008/006/R source

Aircraft using this section

AIRBUS S.A.S. A330-743L entry 7 at CS25-5
AIRBUS S.A.S. A330-743L entry 9 at CS25-5
AIRBUS S.A.S. A330-743L entry 12 at CS25-5
AIRBUS S.A.S. A330-743L entry 17 at CS25-5
AIRBUS S.A.S. A330-743L entry 26 at CS25-5
AIRBUS S.A.S. A330-743L entry 31 at CS25-5
AIRBUS S.A.S. A330-743L entry 33 at CS25-5
Airbus Defence and Space S.A C-295 entry 46 at CS25-5
Bombardier Inc. BD-700-2A12 entry 3 at CS25-5
DASSAULT AVIATION Falcon 6X entry 1 at CS25-5
GULFSTREAM AEROSPACE LP (GALP) Gulfstream G280 entry 5 at CS25-5
Gulfstream Aerospace Corporation GVII-G500 entry 24 at CS25-5
Gulfstream Aerospace Corporation GVII-G500 entry 27 at CS25-5
Gulfstream Aerospace Corporation GVII-G600 entry 21 at CS25-5
Gulfstream Aerospace Corporation GVII-G600 entry 24 at CS25-5
Textron Aviation Inc. 680A entry 10 at CS25-5
Textron Aviation Inc. 680A entry 16 at CS25-5
Textron Aviation Inc. 680A entry 23 at CS25-5
Textron Aviation Inc. 680A entry 29 at CS25-5
Textron Aviation Inc. 680A entry 32 at CS25-5

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