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CS 27.483  One-wheel landing conditions

ED Decision 2003/15/RM

For the one-wheel landing condition, the rotorcraft is assumed to be in the level attitude and to contact the ground on one aft wheel. In this attitude:

(a)     The vertical load must be the same as that obtained on that side under CS 27.479(b)(1); and

(b)     The unbalanced external loads must be reacted by rotorcraft inertia.
Details
Source-Title: CS 27.483 One-wheel landing conditions View latest amendments
Erulesid: ERULES-1963177438-4910 Compare versions
Domain: Initial airworthiness
Amendedby: Initial issue
Applicabilitydate: 14 November, 2003
Entryintoforcedate: 14 November, 2003
Regulatorysource: ED Decision 2003/15/RM Navigate
Regulatorysubject: CS-27
Typeofcontent: CS (Certification specification)
Origin: EASA
Category: EAR