Federal Aviation Administration August 15, 2016 – Federal Register Recent Federal Regulation Documents

In accordance with the Paperwork Reduction Act of 1995, FAA invites public comments about our intention to request the Office of Management and Budget (OMB) approval for a new information collection. The FAA is launching a rebate program to emphasize the urgent need for pilots to comply with Automatic Dependent Surveillance Broadcast (ADS- B) Out requirements ahead of the January 1, 2020, compliance deadline. This program will defray costs associated with the ADS-B equipment and installation for eligible general aviation aircraft, and help ensure that all general aviation aircraft are equipped by the compliance date.

The FAA is issuing this notice to advise the public of a meeting of Sixty-Eighth Meeting, Special Committee 135, Environmental Conditions and Test Procedures for Airborne Equipment.

The FAA is issuing this notice to advise the public of a meeting of TWENTY-NINTH MEETING Special Committee 216 Aeronautical Systems Security.

This action modifies the Boise, ID, Class C airspace area by amending the legal description to contain the current Boise Air Terminal/Gowen Field airport name and updated airport reference point (ARP) information. This action does not change the boundaries, altitudes, or operating requirements of the Class C airspace area.

This action proposes to modify Class E airspace at Albany Municipal Airport, Albany, OR. Advances in Global Positioning System (GPS) mapping accuracy and a reliance on precise geographic coordinates to define airport and airspace reference points have made airspace redesign necessary for the safety and management of Instrument Flight Rules (IFR) operations.

We are superseding Airworthiness Directive (AD) 2016-13-10, for certain The Boeing Company Model 737-300, -400, and -500 series airplanes. AD 2016-13-10 required repetitive external detailed inspections and nondestructive inspections to detect cracks in the fuselage skin along the chem-mill steps at stringers S-1 and S-2R, between station (STA) 400 and STA 460, and repair if necessary. AD 2016-13-10 also required a preventive modification of the fuselage skin at crown stringers S-1 and S-2R. This AD requires the same actions as AD 2016-13-10, and clarifies certain regulatory text. This AD was prompted by the determination that certain regulatory text in AD 2016- 13-10 requires clarification. We are issuing this AD to detect and correct fatigue cracking of the fuselage skin panels at the chem-mill steps, which could result in sudden fracture and failure of the fuselage skin panels, and consequent rapid decompression of the airplane.