Committee on Technical Barriers to Trade - Notification - United States - Airplanes

NOTIFICATION

The following notification is being circulated in accordance with Article 10.6

 

1.

Notifying Member: United States of America

If applicable, name of local government involved (Article 3.2 and 7.2):

2.

Agency responsible: Federal Aviation Administration (FAA) [1409]

Name and address (including telephone and fax numbers, email and website addresses, if available) of agency or authority designated to handle comments regarding the notification shall be indicated if different from above:

Please submit comments to: USA WTO TBT Enquiry Point, Email: usatbtep@nist.gov

3.

Notified under Article 2.9.2 [X], 2.10.1 [ ], 5.6.2 [ ], 5.7.1 [ ], other:

4.

Products covered (HS or CCCN where applicable, otherwise national tariff heading. ICS numbers may be provided in addition, where applicable): Transport category airplanes

Aircraft and space vehicles in general (ICS 49.020).

5.

Title, number of pages and language(s) of the notified document: Yaw Maneuver Conditions - Rudder Reversals (9 page(s), in English)

6.

Description of content: The FAA proposes to add a new load condition to the design standards for transport category airplanes. The new load condition would require the airplane be designed to withstand the loads caused by rapid reversals of the rudder pedals and would apply to transport category airplanes that have a powered rudder control surface or surfaces. This rule is necessary because accident and incident data show that pilots sometimes make rudder reversals during flight, even though such reversals are unnecessary and discouraged by flightcrew training programs. The current design standards do not require the airplane structure to withstand the loads that may result from such reversals. If the airplane loads exceed those for which it is designed, the airplane structure may fail, resulting in catastrophic loss of control of the airplane. This proposal aims to prevent structural failure of the rudder and vertical stabilizer that may result from these rudder reversals.

7.

Objective and rationale, including the nature of urgent problems where applicable: Protection of human health or safety

8.

Relevant documents: 83 Federal Register (FR) 32807, 16 July 2018; Title 14 Code of Federal Regulations (CFR) Part 25. Will appear in the Federal Register when adopted.

9.

Proposed date of adoption: To be determined

Proposed date of entry into force: To be determined

10.

Final date for comments: 15 October 2018

11.

Texts available from: National enquiry point [ ] or address, telephone and fax numbers and email and website addresses, if available, of other body:

https://members.wto.org/crnattachments/2018/TBT/USA/18_3842_00_e.pdf