NPRM FAA-2010-0474

Became AD 2010-21-05

Proposed airworthiness directive · BAE Systems

Published
May 10, 2010 · 75 FR 25785
Comments due
June 24, 2010
Action
Notice of proposed rulemaking (NPRM)
Docket
FAA-2010-0474
Project
2009-NM-056-AD
FR document
2010-10996
Products
Aircraft

A proposal is not in force. If adopted, it becomes an AD, usually with changes. Only the Federal Register edition is official.

Summary

We propose to adopt a new airworthiness directive (AD) for the products listed above that would supersede an existing AD. This proposed AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as: During ground maneuvering, prolonged operation with either engine in the restricted range between 82% and 90% RPM [revolutions per minute] will result in damage [e.g., cracking of the blade or hub] to the propeller assembly that could eventually result in the release of a propeller blade. EASA AD 2007- 0268 [which corresponds to FAA AD 2008-13-02] was issued to require the installation of a Propeller Warning Placard and implementation of a corresponding Aircraft Flight Manual (AFM) limitation instructing the flight crew to taxi with the condition lever at FLIGHT in order to minimise the time spent by the engines in the restricted range. BAE Systems has now developed a Propeller Speed Warning System. A released propeller blade could result in engine failure and loss of control of the airplane. The proposed AD would require actions that are intended to address the unsafe condition described in the MCAI.

The resulting AD

Notices in this docket · 1