Federal Aviation Administration March 26, 2015 – Federal Register Recent Federal Regulation Documents
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Recommendations for Facilities Realignments To Support Transition to NextGen as Part of Section 804 of the FAA Modernization and Reform Act of 2012; Request for Comments
This document announces the availability of the FAA National Facilities Realignment and Consolidation Report, Year 1 Part 1. The report was developed in response to Section 804 of the FAA Modernization and Reform Act of 2012 (Pub. L. 112-95). The report and recommendations contained therein have been developed collaboratively with the National Air Traffic Controllers Association (NATCA) and the Professional Aviation Safety Specialists (PASS) Labor Unions and with input from stakeholders. The FAA seeks comments on this report.
Prohibition of Fixed-Wing Special Visual Flight Rules Operations at Washington-Dulles International Airport
This action prohibits fixed-wing special visual flight rules operations at Washington-Dulles International Airport. This action is necessary to support aviation safety and the efficient use of the navigable airspace by managing operations in the busy and complex airspace around the airport.
Airworthiness Directives; The Boeing Company Airplanes
We propose to supersede Airworthiness Directive (AD) 2012-18- 05, which applies to The Boeing Company Model DC-9-10, DC-9-20, DC-9- 30, DC-9-40, and DC-9-50 series airplanes; and Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), MD-88, and MD-90-30 airplanes; equipped with a center wing fuel tank and Boeing original equipment manufacturer-installed auxiliary fuel tanks. AD 2012-18-05 currently requires adding design features to detect electrical faults and to detect a pump running in an empty fuel tank. Since we issued AD 2012-18-05, we have determined that it is necessary to clarify the actions for airplanes on which the auxiliary fuel tanks are removed. This proposed AD would allow certain actions as optional methods of compliance. We are proposing this AD to reduce the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane.
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