§25.1709 System Safety; 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 25.1709) EWIS must be designed and installed so that: (a) Each catastrophic failure condition (1) is extremely improbable; and (2) does not result from a single failure; and (b) Each hazardous failure condition is extremely remote.

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

No aircraft in the dataset reference this section.

Report an issue

Is something wrong with what you are looking at? Tell the maintainer; the report is filed against this page.