Federal Aviation Administration December 20, 2005 – Federal Register Recent Federal Regulation Documents

The FAA invites public comments about our intention to request the Office of Management and Budget's (OMB) approval for the renewal of a currently approved information collection. 14 CFR Part 61 requires airmen to notify the FAA of any conviction or administrative action resulting from any alcohol or drug related motor vehicle offense within 60 days of the offense. A notice was published in the Federal Register announcing our intention to request renewal of this collection on September 6, 2005, vol 70, 171, pages 53039-53040.

The FAA invites public comments about our intention to request the Office of Management and Budget's (OMB) approval for a new information collection. The FAA has undertaken an effort to improve aviation safety by collecting data on pilots' training and experience with transport category rudder control systems. A Federal Register notice for public comment was published on April 12, 2005, vol 70, 69, page 19144.

This document revises an earlier proposed airworthiness directive (AD), applicable to certain McDonnell Douglas Model DC-9-10, -20, -30, -40, and -50 series airplanes; Model DC-9-81 (MD-81), -82 (MD-82), -83 (MD-83), and -87 (MD-87) airplanes; and Model MD-88 airplanes. That proposed AD would have required repetitive inspections and functional tests of the static port heater assemblies, an inspection of the static port heaters and insulators, and corrective actions if necessary. This new action revises the proposed AD by adding repetitive inspections of the static port heaters and insulators and revising the functional test of the static port heater. The actions specified by this new proposed AD are intended to prevent an electrical short of the static port heater from sparking and igniting the insulation blanket adjacent to the static port heater, which could result in smoke and/or fire in the cabin area. This action is intended to address the identified unsafe condition.

The FAA proposes to supersede an existing airworthiness directive (AD) that applies to certain 747-100, -200, and -300 series airplanes. The existing AD currently requires repetitive inspections to detect cracking of certain lower lobe fuselage frames, and repair if necessary. This proposed AD would retain all the requirements of the existing AD, and add airplanes to the applicability. This proposed AD results from reports indicating that fatigue cracks were found in lower lobe frames on the left side of the fuselage. We are proposing this AD to detect and correct fatigue cracking of certain lower lobe fuselage frames, which could lead to fatigue cracks in the fuselage skin, and consequent rapid decompression of the airplane.

This action revises Class E airspace at Koliganek, AK to provide adequate controlled airspace to contain aircraft executing two new Standard Instrument Approach Procedures (SIAPs). This rule results in revised Class E airspace upward from 700 feet (ft.) and 1,200 ft. above the surface at Koliganek Airport, AK.

This action proposes to revise the Class E airspace at Sand Point, AK. Three new Standard Instrument Approach Procedures (SIAPs), a revised Departure Procedure (DP) and a revised SIAP are being published for the Sand Point Airport. Adoption of this proposal would result in revised Class E airspace upward from 700 feet (ft.) and 1,200 ft. above the surface at Sand Point, AK.

This action establishes Class E airspace at New Stuyahok, AK to provide adequate controlled airspace to contain aircraft executing two new Standard Instrument Approach Procedures (SIAPs). This rule results in new Class E airspace upward from 700 feet (ft.) above the surface at New Stuyahok Airport, AK.

The FAA is adopting a new airworthiness directive (AD) for certain Dassault Model Falcon 2000 airplanes. This AD requires an inspection for the presence of fail-safe pins, nuts, and washers on each engine, and replacement of the fail-safe fastener assembly with a new assembly if necessary. This AD results from a report of a missing pin of a fail-safe fastener. We are issuing this AD to prevent reduced structural integrity of an engine mount due to a missing pin of a fail- safe fastener, and possible separation of an engine from the airplane during flight.

The FAA is adopting a new airworthiness directive (AD) for certain Airbus Model A300 B2 series airplanes, A300 B4-103 and B4-203 airplanes, and A310-203 airplanes. This AD requires a one-time inspection for missing or incorrect rivets in the structural area affected by conversion from passenger to freight configuration, and corrective action if necessary. This AD results from a report of rivets missing from the passenger-to-freight converted area. We are issuing this AD to prevent structural failure of the main deck and main deck cargo door areas.