AMC 22.481 Tail-down landing conditions

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ED Decision 2003/13/RM

Where iy cannot be determined by more rational means, a value of:

may be used:

L_R in this case to be taken as the overall length of the fuselage without rudder.

In designing the tail skid, side loads should be accounted for in addition to the vertical load determined as above.

Source-Title: AMC 22.481 Tail-down landing conditions View latest amendments

Erulesid: ERULES-1963177438-5279 Compare versions

Domain: Initial airworthiness

Amendedby: Initial issue

Applicabilitydate: 14 November, 2003

Entryintoforcedate: 14 November, 2003

Regulatorysource: ED Decision 2003/13/RM Navigate

Regulatorysubject: CS-22

Typeofcontent: AMC to CS (Acceptable means of compliance to certification specification)

Parentir: CS 22.481 Tail-down landing conditions

Origin: EASA

Category: EAR