§27.481 Tail-down landing conditions

CS-27 · Subpart C — Strength Requirements · at CS27-10 (current)

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

(a) The rotorcraft is assumed to be in the maximum nose-up attitude allowing ground clearance by each part of the rotorcraft. (b) In this attitude, ground loads are assumed to act perpendicular to the ground.

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

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.