Federal Aviation Administration February 4, 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 to renew a previously approved information collection. The information collected is needed to determine applicant eligibility and compliance for certification of Civil Aviation mechanics and operation of aviation mechanic schools.

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 to renew an information collection. This information will be used to issue special flight authorizations for non-revenue transports and non-transport jet operations of Stage 2 airplanes at U.S. airports. Only a minimal amount of data is requested to identify the affected parties and determine whether the purpose for the flight is one of those enumerated by law.

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 to renew an information collection. Title 49 U.S.C., Section 44702 authorizes issuance of air carrier operating certificates. 14 CFR part 135 prescribes requirement for Air Carrier/Commercial Operators. The information collected shows compliance and applicant eligibility.

The FAA assigned the Aviation Rulemaking Advisory Committee (ARAC) a continuation of a task to provide recommendations regarding standards, training guidance, test management, and reference materials for airman certification purposes. The FAA added the Aircraft Mechanic Certificate with Airframe and/or Powerplant ratings to the existing list of certificates and ratings for which the ARAC will provide recommendations. This notice informs the public of the continuing ARAC activity and solicits additional membership for the existing Airman Certification System Working Group (ACS WG).

This action amends the legal description of the Class E airspace area at Rapid City Regional Airport, Rapid City, SD, eliminating the Notice to Airmen (NOTAM) part-time status of the Class E surface area airspace, and Class E airspace designated as an extension, at the airport. This is an administrative change to coincide with the FAA's aeronautical database.

This action proposes to establish Class E airspace at Hollis, OK. Controlled airspace is necessary to accommodate new Standard Instrument Approach Procedures developed at Hollis Municipal Airport, for the safety and management of Instrument Flight Rules (IFR) operations at the airport.

This action proposes to establish Class E airspace at Beach, ND. Controlled airspace is necessary to accommodate new Standard Instrument Approach Procedures developed at Beach Airport, for the safety and management of Instrument Flight Rules (IFR) operations at the airport.

This action establishes 13 high altitude Area Navigation (RNAV) routes (Q-routes) in the western United States. The routes promote operational efficiencies for users and provide connectivity to current and proposed RNAV en route and terminal procedures. The low altitude RNAV route, T-326, published in the Notice of Proposed Rulemaking, requires more coordination and is removed from this rule.

We propose to adopt a new airworthiness directive (AD) for DG Flugzeugbau GmbH Model DG-1000T gliders equipped with a Solo Kleinmotoren Model 2350 C engine that would revise AD 2015-09-04. 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 engine shaft failure and consequent propeller detachment. We are issuing this proposed AD to require actions to address the unsafe condition on these products.

We are superseding Airworthiness Directive (AD) 2004-20-14, for all Airbus Model A300 B4-2C, B4-103, and B4-203 airplanes; and all Airbus Model A300 B4-600, B4-600R, and F4-600R series airplanes. AD 2004-20-14 required repetitive inspections to detect cracking of the splice fitting at fuselage frame (FR) 47 between stringers 24 and 26 (left- and right-hand sides), and corrective actions if necessary. This new AD reduces the inspection compliance time and repetitive inspection intervals, and adds Airbus Model A300 C4-605R Variant F airplanes to the applicability. This AD was prompted by a determination that the inspection compliance time and repetitive inspection interval must be reduced to allow timely detection of cracks in the splice fitting at fuselage FR 47. We are issuing this AD to detect and correct cracking of the splice fitting at fuselage FR 47; such cracking could result in reduced structural integrity of the airplane.