§27.161 Trim control

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

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

The trim control: (a) Must trim any steady longitudinal, lateral, and collective control forces to zero in level flight at any appropriate speed; and (b) May not introduce any undesirable discontinuities in control force gradients.

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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