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The Civil Aviation (Aerial Work-General Operations) Regulations, 2025

37. Structures and design

Edition: 2026-03-25 · In force

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37. Structures and design

(1)An external-load attaching means and a quick release device means of a rotorcraft shall be approved by the Authority.
(2)The total weight of the rotorcraft-load combination shall not exceed the total weight approved for the rotorcraft during its type certification.
(3)The location of the centre of gravity shall, for all loading conditions, be within the range established for the rotorcraft during its type certification.
(4)For Class C rotorcraft-load combinations, the magnitude and direction of the loading force shall be established at those values for which the effective location of the centre of gravity remains within its established range.
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Source: Kenya Law