Federal Aviation Administration January 2019 – Federal Register Recent Federal Regulation Documents

Under the provisions of Title 49, notice is being given that the FAA is considering a request from the Bainbridge-Decatur County Administrator to change approximately 7.62 acres of AIP acquired airport property located on the northeastern portion of Bainbridge- Decatur County Industrial Airport from aeronautical use to non- aeronautical use. The proposed land use is for non-aeronautical lease and use for the installation of a solar panel farm and access road. The land is owned and operated by the airport, but not currently in use or planned for aeronautical use.

The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to The Boeing Company Model 787-8 airplanes powered by Rolls-Royce plc (RR) Trent 1000-A (including -A/01 and -A/01A), Trent 1000-AE (including -AE/01A), Trent 1000-C (including -C/01 and -C/01A), Trent 1000-CE (including - CE/01A), Trent 1000-D (including -D/01 and -D/01A), Trent 1000-E (including -E/01 and -E/01A), Trent 1000-G (including -G/01 and -G/ 01A), and Trent 1000-H (including -H/01 and H/01A) turbofan engines. As published, a document referenced in the regulatory text was incorrectly identified. This document corrects that error. In all other respects, the original document remains the same.

We are adopting a new airworthiness directive (AD) for The Boeing Company Model 787-8 airplanes powered by Rolls-Royce plc (RR) Trent 1000-A (including -A/01 and -A/01A), Trent 1000-AE (including - AE/01A), Trent 1000-C (including -C/01 and -C/01A), Trent 1000-CE (including -CE/01A), Trent 1000-D (including -D/01 and -D/01A), Trent 1000-E (including -E/01 and -E/01A), Trent 1000-G (including -G/01 and -G/01A), and Trent 1000-H (including -H/01 and H/01A) turbofan engines. This AD requires revising the airplane flight manual (AFM) to limit extended operations (ETOPS). This AD was prompted by a report from the engine manufacturer indicating that after an engine failure, prolonged operation at high thrust settings on the remaining engine during an ETOPS diversion may result in failure of the remaining engine before the diversion can be safely completed. We are issuing this AD to address the unsafe condition on these products.