§27.1527 Maximum operating altitude

CS-27 · Subpart G — Operating Limitations And Information · at CS27-10 (current)

Text in force at CS27-10: from CS27-0, effective 14 Nov 2003.

The maximum altitude up to which operation is allowed, as limited by flight, structural, powerplant, functional, or equipment characteristics, must be established.

ED Decision 2003/015/RM · Source

Version history

Version	Effective	Published
CS27-0	14 Nov 2003	ED Decision 2003/015/RM

Rulemaking for CS27-0

easa decision ED Decision 2003/015/RM source

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