§27.235 Taxying condition

CS-27 · Subpart B — Flight · at CS27-10 (current)

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

The rotorcraft must be designed to withstand the loads that would occur when the rotorcraft is taxied over the roughest ground that may reasonably be expected in normal operation.

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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