ED Decision 2018/015/R
1. The AMC to CS-29 consists of FAA AC 29-2C — Change 7, dated 4 February 2016, with the changes/additions given in this BOOK 2 of CS-29.
2. The primary reference for each of these AMCs is the CS-29 paragraph. Where there is an appropriate paragraph in FAA AC 29-2C — Change 7, dated 4 February 2016, this is added as a secondary reference.
[Amdt No: 29/2]
[Amdt No: 29/4]
[Amdt No: 29/6]
ED Decision 2016/025/R
(a) These certification specifications are applicable to large rotorcraft.
(b) Large rotorcraft must be certificated in accordance with either the Category A or Category B requirements. A multi-engine rotorcraft may be type certificated as both Category A and Category B with appropriate and different operating limitations for each category.
(c) Rotorcraft with a maximum weight greater than 9072 kg (20 000 pounds) and 10 or more passenger seats must be type certificated as Category A rotorcraft.
(d) Rotorcraft with a maximum weight greater than 9072 kg (20 000 pounds) and nine or less passenger seats may be type certificated as Category B rotorcraft provided the Category A requirements of Subparts C, D, E, and F are met.
(e) Rotorcraft with a maximum weight of 9072 kg (20 000 pounds) or less but with 10 or more passenger seats may be type certificated as Category B rotorcraft provided the Category A requirements of CS 29.67(a)(2), 29.87, 29.1517, and of Subparts C, D, E, and F are met.
(f) Rotorcraft with a maximum weight of 9072 kg (20 000 pounds) or less and nine or less passenger seats may be type certificated as Category B rotorcraft.
[Amdt 29/4]