Federal Aviation Administration May 2008 – Federal Register Recent Federal Regulation Documents

In a proposed order published on March 18, 2008, the Federal Aviation Administration (FAA) tentatively identified the parameters of an order that would temporarily limit scheduled flight operations at Newark Liberty International Airport (EWR).\1\ The FAA issued the proposal as a result of persistent congestion and delays at EWR during the peak operating hours, as well as a dramatic projected increase in flight delays at the airport during the summer of 2008 if proposed schedules were implemented as requested by carriers. After evaluating the written comment submitted to the public docket in this matter, the FAA is issuing this final Order, which will take effect at 6 a.m., Eastern Time, on June 20, 2008.

We are adopting a new airworthiness directive (AD) for certain Boeing Model 747-100, 747-100B, 747-200B, 747-200C, 747-200F, 747-300, 747SR, and 747SP series airplanes. This AD requires an inspection to determine if acceptable external skin doublers are installed at the stringer 6 (S-6) lap splices, between station (STA) 340 and STA 400. For airplanes without the acceptable external skin doublers, this AD requires repetitive related investigative actions and corrective actions if necessary. This AD also provides an optional terminating modification for the repetitive related investigative actions. This AD results from a report of cracked fastener holes at the right S-6 lap splice between STA 340 and STA 380. We are issuing this AD to detect and correct cracking in the fuselage skin, which could result in rapid decompression and loss of structural integrity.

We propose to adopt a new airworthiness directive (AD) for the products listed above. 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:

We propose to adopt a new airworthiness directive (AD) for the products listed above. 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:

The FAA proposes to adopt a new airworthiness directive (AD) for Lycoming Engines (formerly Textron Lycoming) models 320, 360, and 540 series, ``Parallel Valve'' reciprocating engines, with certain Engine Components Inc. (ECi) cylinder assemblies, part number (P/N) AEL65102 series ``Titan'', installed. This proposed AD would require initial and repetitive visual inspections and compression tests to detect cracks at the head-to-barrel interface, replacement of cylinder assemblies found cracked, and replacement of certain cylinder assemblies, at new reduced times-in-service. This proposed AD results from reports of 45 failures with head separations of ECi cylinder assemblies. We are proposing this AD to prevent loss of engine power due to cracks at the head-to-barrel interface in the cylinder assemblies and possible engine failure caused by separation of a cylinder head, which could result in loss of control of the aircraft.

The FAA proposes to supersede an existing airworthiness directive (AD) that applies to various aircraft equipped with certain Honeywell Primus II RNZ-850( )/-851( ) integrated navigation units (INUs). The existing AD, as one alternative for compliance, provides for a one-time inspection to determine whether a certain modification has been installed on the Honeywell Primus II NV-850 navigation receiver module (NRM), which is part of the INU. In lieu of accomplishing this inspection, and for aircraft found to have an affected NRM, that AD provides for revising the aircraft flight manual to include new limitations for instrument landing system approaches. That AD also requires an inspection to determine whether certain other modifications have been done on the NRM; and doing related investigative, corrective, and other specified actions, as applicable; as well as further modifications to address additional anomalies. This proposed AD would extend the compliance time for a certain inspection and associated actions. This proposed AD would also revise the applicability to include additional affected INUs. This proposed AD results from reports indicating that erroneous localizer and glideslope indications have occurred on certain aircraft equipped with the subject INUs. We are proposing this AD to ensure that the flight crew has accurate localizer and glideslope deviation indications. An erroneous localizer or glideslope deviation indication could lead to the aircraft making an approach off the localizer, which could result in impact with an obstacle or terrain.

This notice contains a summary of a petition seeking relief from specified requirements of 14 CFR. The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of FAA's regulatory activities. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of the petition or its final disposition.

This action amends the Class E airspace area at Waynesburg, PA, to accommodate a new Standard Instrument Approach Procedure (SIAP) that has been developed for Green County Airport. As a result, controlled airspace extending upward from 700 feet Above Ground Level (AGL) will be expanded to contain the SIAP and other Instrument Flight Rules (IFR) operations at Green County Airport. The operating status of the airport will change from Visual Flight Rules (VFR) to include IFR operations concurrent with the publication of the SIAP. A minor correction is also being made in the geographic position coordinates of the Green County Airport.

The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. SFAR 36 (to part 121) relieves qualifying applicants involved in aircraft repair of the burden to obtain FAA approval of data developed by them for the major repairs on a case-by- case basis; and provides for one-time approvals.

The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. Respondents conducting general operation and flight of aircraft or any activity that could encroach on airspace must apply for approval.

The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. Aircraft operators seeking operational approval to conduct RVSM operations within the 48 contiguous United States (U.S.), Alaska and a portion of the Gulf of Mexico must submit an application to the Certificate Holding District Office.

This action confirms the effective date of a direct final rule published in the Federal Register (73 FR 9443) that modifies Class E Airspace at Bradford, PA. The modified controlled airspace from nearby Bradford Regional Airport will now adequately support the Area Navigation (RNAV) Global Positioning System (GPS) Special Instrument Approach Procedure (IAP) developed for medical flight operations for the University of Pittsburgh.

The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. Pursuant to Public Law 104-50, the FAA implements an acquisition management system that addresses the unique needs of the agency. This document established the policies and internal procedures for the FAA's acquisition system.

The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. The information to be collected includes data required for performing launch site location analysis.

The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. The Advanced Qualification Program (AQP) incorporates data driven quality control processes for validating and maintaining the effectiveness of air carrier training program curriculum content.

The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a current information collection. This information allows the FAA to evaluate its certification standards, maintenance programs, and regulatory requirements. It is also the basis for issuance of Airworthiness Directives designed to prevent unsafe conditions and accidents.

This Rule establishes, amends, suspends, or revokes STANDARD Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums and Obstacle Departure Procedures for operations at certain airports. These regulatory actions are needed because of the adoption of new or revised criteria, or because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, adding new obstacles, or changing air traffic requirements. These changes are designed to provide safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.

The Federal Aviation Administration is requesting public comment on the proposed release of 5.67 acres of land currently owned by the Elkins Randolph County Airport, Elkins, West Virginia. The parcel is located at Chenoweth Creek; Beverly District, Elkins, West Virginia. The property is undeveloped and is not needed for aeronautical purposes. Once released, the land will be exchanged for 5.67 acres of land situated within the approach of Runway 23. This property is to be exchanged to facilitate Runway Protection Zone requirements. The airport land being released is not needed for airport development as shown on the Airport Layout Plan. Fair Market Value of the land has been established for the land exchange between the Elkins Randolph Airport and the aforementioned property.

We propose to adopt a new airworthiness directive (AD) for the products listed above. 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:

We propose to adopt a new airworthiness directive (AD) for the products listed above. 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:

This action proposes to modify Class E Airspace at Roanoke, VA. Additional airspace is necessary to allow for a lower vectoring altitude known as the Minimum Vectoring Altitude (MVA) for vectoring of both Visual Flight Rule (VFR) and Instrument Flight Rule (IFR) aircraft for spacing within 20 miles of Roanoke, VA. This action would enhance the safety and airspace management around the Roanoke Regional/Woodrum Field Airport area.

This notice announces the FAAs intensions to cancel all Omega Technical Standard Orders (TSOs) and revoke all associated Technical Standard Order Authorizations (TSOAs). If you have reason to believe that this proposed action will negatively impact aviation safety, we would like to solicit your comments.

The FAA is issuing this Notice of Availability to advise the public that a Draft EIS will be available for public review beginning May 16, 2008. The document was prepared pursuant to major environmental directives to comply with NEPA: Section 102(2)(c) of the National Environmental Policy Act of 1969 (Pub. L. 91-190); Section 106 consultation for impacts to historic structures, as identified in 36 CFR 800.8, Coordination with the National Environmental Policy Act; U.S. Department of Transportation Section 303(c) consultation; and other applicable Federal and State environmental laws, regulations, and Executive Orders. The Draft EIS was prepared in response to a proposal presented to the FAA by the Columbus Regional Airport Authority (CRAA), the owner and operator of CMH and identified in the Draft EIS as the Airport Sponsor, for environmental review. The FAA prepared this Draft EIS to analyze and disclose potential environmental impacts related to possible Federal actions at CMH. Numerous Federal actions would be necessary if airfield development were to be implemented. Proposed improvements include replacement of Runway 10R/28L, Development of a New Passenger Terminal, and other airfield projects (see below). The Draft EIS presents the purpose and need for the proposed Federal action, analysis of reasonable alternatives, including the No Action alternative, discussion of impacts for each reasonable alternative, and supporting appendices. The FAA will consider all information contained in this Draft EIS and additional information that may be provided during the public comment period before issuing a Final EIS and Agency decision regarding the possible alternatives and Federal actions. The Airport Sponsor proposes to replace Runway 10R/28L at CMH, approximately 700 feet south of the existing Runway 10R/28L; develop new terminal facilities in the midfield area; provide ancillary facilities in support of the replacement runway and midfield terminal; and implement noise abatement air traffic procedures developed for the replacement runway. The replacement runway would be 10,113 feet long. This length would maintain CMH's ability to accommodate current and projected airport operations. Existing Runway 10R/28L would be decommissioned as a runway and converted into a taxiway upon commissioning of the replacement runway. In addition, a south taxiway and north parallel taxiways to proposed Runway 10R/28L would be constructed. To meet future aircraft parking and passenger processing requirements, new midfield terminal facilities are needed. The Draft EIS assesses a development envelope that is defined as an area large enough to encompass Phase I and II of the CRAA terminal development program. The Draft EIS discusses the number of gates, approximate square footage, approximate curb frontage, and the number of passengers that the terminal would accommodate. Ancillary facilities in support of the replacement runway and midfield terminal would be constructed. The facilities include roadway relocations and construction; parking improvements; property acquisition; and relocation of residences, as necessary. The CRAA has prepared a 14 CFR Part 150 Noise Compatibility Study Update (Part 150 Update) to address the current and future noise conditions. The Part 150 Update includes an analysis of the potential noise and land use impacts resulting from the proposed development of relocating Runway 10R/28L to the south, as well as possible mitigation options. The noise abatement air traffic options recommended through the Part 150 Update are included in the EIS as part of the proposed project. In addition, the land use mitigation that is recommended in the Part 150 Update is included in the EIS as mitigation for impacts resulting from the proposed project. Public Comment and Information Workshop/Public Hearing: The public comment period on the Draft EIS will start May 16, 2008 and will end on July 11, 2008. Two Public Information Workshops and Public Hearings will be held on June 11 and 12, 2008 from 5 p.m. to 8 p.m. at the following locations:

This document supersedes Airworthiness Directive (AD) 2001-24- 07 R1 and adopts AD 2007-26-52, which was sent previously to all known U.S. owners and operators of Agusta S.p.A. (Agusta) Model A109C, A109E, and A109K2 helicopters by individual letters. This AD requires inspections for swelling, deformation, bonding separation, or a crack on each main rotor blade (MRB) with a certain tip cap installed, and if any of these conditions are found that exceed the prescribed limits, replacing the MRB before further flight. This amendment is prompted by a report of the in-flight loss of part of a tip cap. The actions specified in this AD are intended to prevent an increase in vibration of the MRB and subsequent loss of control of the helicopter.