Which specific CS 29 sections are referenced in CS 29.64 as the climb requirements that must be complied with?

CS 29.64 references CS 29.65 and CS 29.67 as the climb requirements that must be complied with.

Under CS 29.64, what is the required condition of the engine-cooling air supply control means during climb performance demonstrations at certification temperatures and altitudes?

The cowl flaps or other means of controlling the engine-cooling air supply must be in the position that provides adequate cooling at the temperatures and altitudes for which certification is requested.

CS 29.64 Climb: General

Q: For each configuration, what centre of gravity condition must be used when showing compliance with the climb requirements of CS 29.64?

The most unfavourable centre of gravity for each configuration must be used.

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CS 29.64 Climb: General

ED Decision 2003/16/RM

Compliance with the requirements of CS 29.65 and 29.67 must be shown at each weight, altitude and temperature within the operational limits established for the rotorcraft and with the most unfavourable centre of gravity for each configuration. Cowl flaps, or other means of controlling the engine-cooling air supply, will be in the position that provides adequate cooling at the temperatures and altitudes for which certification is requested.

Details

Source-Title: CS 29.64 Climb: General View latest amendments

Erulesid: ERULES-1963177438-5481 Compare versions

Domain: Initial airworthiness

Amendedby: Initial issue

Applicabilitydate: 14 November, 2003

Entryintoforcedate: 14 November, 2003

Regulatorysource: ED Decision 2003/16/RM Navigate

Regulatorysubject: CS-29

Typeofcontent: CS (Certification specification)

Origin: EASA

Category: EAR