Department of Transportation December 2011 – Federal Register Recent Federal Regulation Documents

This document confirms the effective date of the direct final rule amending the time period for compliance with the full fare and other advertising requirements in 14 CFR 399.84 from January 24, 2012, to January 26, 2012.

This action modifies Class E airspace at Show Low Regional Airport, Show Low, AZ. Controlled airspace is necessary to accommodate aircraft using Area Navigation (RNAV) Global Positioning System (GPS) standard instrument approach procedures at Show Low Regional Airport. This improves the safety and management of Instrument Flight Rules (IFR) operations at the airport.

The Federal Aviation Administration is requesting public comment on the Erie Regional Airport Authority's request to release airport property for use by the Pennsylvania Department of Transportation (PennDOT) to construct and maintain additional roadway and drainage facilities along the west side of Asbury Road. The request contains five (5) components consisting of a permanent release of land, release of land for drainage easement, release of land for temporary construction easement, release of land for substitute right-of-way, and release of land for permanent gas line easement.

We propose to supersede an existing airworthiness directive (AD), for all International Aero Engines AG (IAE) V2500-A1, V2525-D5 and V2528-D5 turbofan engines, and certain serial numbers (S/Ns) of IAE V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, and V2533-A5 turbofan engines. The existing AD currently requires initial and repetitive on-wing ultrasonic inspections (USIs) of certain high- pressure compressor (HPC) stage 3 to 8 drums, and replacement of drum attachment nuts. This proposed AD would expand the affected population for initial and repetitive on-wing inspections of the HPC stage 3 to 8 drum, introduce an eddy current inspection (ECI) procedure, and require additional cleaning and repetitive on-wing USI or ECI of some HPC stage 3 to 8 drums. We are proposing this AD to prevent failure of the HPC stage 3 to 8 drum, uncontained engine failure, and damage to the airplane.

We are revising an existing airworthiness directive (AD) for Thielert Aircraft Engines GmbH models TAE 125-02-99 and TAE 125-01 reciprocating engines. That AD currently requires replacing the existing rail pressure control valve with an improved rail pressure control valve. This new AD requires the same actions but relaxes the initial compliance time from within 100 flight hours to within 600 flight hours for TAE 125-01 reciprocating engines. This AD was prompted by the determination that our AD was inadvertently more restrictive than European Aviation Safety Agency AD 2008-0128. We are issuing this AD to prevent engine in-flight shutdown, possibly resulting in reduced control of the aircraft.

This action amends two VHF Omnidirectional Range (VOR) Federal airways in Alaska, V-320 and V-440, due to the relocation of the Anchorage VOR navigation aid. The FAA is taking this action to ensure the continued safe and efficient management of Instrument Flight Rules (IFR) operations within the National Airspace System.

We are adopting a new airworthiness directive (AD) for certain Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model L-1011-385-1, L-1011-385-1-14, L-1011-385-1-15, and L-1011-385-3 airplanes. This AD was prompted by results from a damage tolerance analysis conducted by the manufacturer indicating that fatigue cracking could occur in wing rear spar and upper surface zones. This AD requires repetitive inspections for cracking of the wing rear spar and upper surface zones, and repair if necessary. We are issuing this AD to detect and correct such fatigue cracking, which could result in cracking that grows large enough to reduce the wing strength below certificated requirements and possibly cause fracture of the rear spar, resulting in extensive damage to the wing and possible fuel leaks.

We are adopting a new airworthiness directive (AD) for the products listed above, with certain part number (P/N) high-pressure compressor (HPC) stages 2-5 spools installed. This AD was prompted by an aborted takeoff caused by liberation of small pieces from the HPC stages 1-2 seal teeth and two shop findings of cracks in the seal teeth. This AD requires eddy current inspection (ECI) or spot fluorescent penetrant inspection (FPI) of the stages 1-2 seal teeth of the HPC stages 2-5 spool for cracks. This AD only allows installation of either HPC stator stage 1 interstage seals that are pregrooved or previously worn seals with acceptable wear marks to prevent heavy rubs. We are issuing this AD to detect cracks in the HPC stages 1-2 seal teeth due to heavy rubs that could result in failure of the seal of the HPC stages 2-5 spool, uncontained engine failure, and damage to the airplane.

In compliance with the Paperwork Reduction Act of 1995 (44 U.S.C. chapter 35), this notice announces that the Information Collection Request (ICR) abstracted below will be submitted to the Office of Management and Budget (OMB) for review. The ICR describes the nature of the information collection and its expected burden. A Federal Register Notice with a 60-day comment period soliciting public comments on the following information collection was published on June 13, 2011 (Federal Register/Vol. 76, No. 113/pp. 34290-34291).

The Federal Aviation Administration (FAA) is considering a proposal to change a portion of airport land from aeronautical use to non-aeronautical use and to authorize the sale of the airport property. The proposal consists of all or portions of Parcels 209A, 213, 217, 218, 219, 220, 221, 314, 315, 401, 402, 404, 406, 407, 408, 409, 410, 411, 412, 413, 414, and 416, totaling 605.3 acres. Presently the land is vacant and used as open land for control of FAR Part 77 surfaces and compatible land use and is not needed for aeronautical use, as shown on the Airport Layout Plan. The Parcels were acquired without Federal participation. It is the intent of the DuPage Airport Authority, as owner and operator of the DuPage Airport (DPA) to sell the aforementioned Parcels (605.3 Acres) in fee to the DuPage County (22.7 acres for Kress Creek floodplain control), the City of West Chicago (37.7 acres for the ownership and maintenance of existing roadways), the Illinois Department of Transportation (11.3 acres for the improvement of State Route 38), and to private entities (533.6 acres for corporate/industrial development). This notice announces that the FAA is considering the proposal to authorize the disposal of the subject airport property at the DuPage Airport, West Chicago, IL. Approval does not constitute a commitment by the FAA to financially assist in disposal of the subject airport property nor a determination that all measures covered by the program are eligible for grant-in-aid funding from the FAA. The disposition of proceeds from the disposal of the airport property will be in accordance with FAA's Policy and Procedures Concerning the Use of Airport Revenue, published in the Federal Register on February 16, 1999. In accordance with section 47107(h) of Title 49, United States Code, this notice is required to be published in the Federal Register 30 days before modifying the land-use assurance that requires the property to be used for an aeronautical purpose.

We are revising an earlier proposed airworthiness directive (AD) for Goodrich Evacuation Systems approved under Technical Standard Order (TSO) TSO-C69b and installed on Airbus Model A330-200 and -300 series airplanes, Model A340-200 and -300 series airplanes, and Model A340-500 and -600 series airplanes. That NPRM proposed to supersede an existing AD. That NPRM proposed inspecting to determine the part number of the pressure relief valves on the affected Goodrich evacuation systems, replacing certain pressure relief valves, and adding airplanes to the applicability. That NPRM was prompted by reports that during workshop testing, certain pressure relief valves, which were required by the existing AD, did not seal and allowed the pressure in certain slides/rafts to fall below the minimum raft mode pressure for the unit. This action revises that NPRM by adding certain airplanes to the applicability. We are proposing this supplemental NPRM to correct the unsafe condition on these products. Since these actions impose an additional burden over that proposed in the NPRM, we are reopening the comment period to allow the public the chance to comment on these proposed changes.

Pursuant to Section 10(a)(2) of the Federal Advisory Committee Act (Pub. L. 92-463, 5 U.S.C. App. 2), notice is hereby given of a teleconference of the Commercial Space Transportation Advisory Committee (COMSTAC) Risk Management Working Group. The teleconference will take place on Tuesday, January 24, 2012, starting at 1:30 p.m. Eastern Standard Time. Individuals who plan to participate should contact Susan Lender, Designated Federal Officer (DFO), (the Contact Person listed below) by phone or email for the teleconference call in number. The National Aeronautics and Space Administration (NASA) and the FAA Office of Commercial Space Transportation (AST) have agreed to prepare a study on the availability of commercial insurance sufficient to meet the needs of NASA's Commercial Crew Program commercial providers for missions transporting NASA astronauts to and from the International Space Station. NASA's Commercial Crew Program requested this study (via a signed memorandum of understanding with the FAA AST) be conducted by AST because of its knowledge and resources in the commercial space industry. The purpose of the teleconference is to: 1. Brief the COMSTAC Risk Management Working Group on the study, 2. Request assistance from the working group in preparing a response to NASA, and 3. Respond to any questions from the working group on the nature of this task. Interested members of the public may submit relevant written statements for the COMSTAC members to consider under the advisory process. Statements may concern the issues mentioned above or additional issues that may be relevant for the U.S. commercial space transportation industry. Interested parties wishing to submit written statements should contact Susan Lender, DFO, (the Contact Person listed below) in writing (mail or email) by January 17, 2012, so that the information can be made available to COMSTAC members for their review and consideration before the January 24, 2012, teleconference. Written statements should be supplied in the following formats: one hard copy with original signature or one electronic copy via email. This notice will be posted on the FAA Web site at https:// www.faa.gov/go/ast. Individuals who plan to participate and need special assistance should inform the Contact Person listed below in advance of the meeting.

In compliance with the Paperwork Reduction Act of 1995 (44 U.S.C. 3501 et seq.), this notice announces that the Information Collection Requirements (ICRs) abstracted below are being forwarded to the Office of Management and Budget (OMB) for review and comment. The ICRs describe the nature of the information collections and their expected burden. The Federal Register notice with a 60-day comment period soliciting comments on the following collections of information was published on October 14, 2011 (76 FR 63990).

We propose to adopt a new airworthiness directive (AD) for certain Airbus Model A330-200 freighter series airplanes; Model A330- 200 and -300 series airplanes; and Model A340-200 and -300 series airplanes. This proposed AD was prompted by a report of corrosion found on the main fitting of the nose landing gear (NLG) leg in the vicinity of the dowel pin bushes retaining the lower steering flange. This proposed AD would require modifying the NLG main fitting by adding primer paint to the cadmium around the dowel bush holes. We are proposing this AD to prevent NLG main fitting rupture, which could result in an NLG collapse.

We propose to adopt a new airworthiness directive (AD) for all Saab AB, Saab Aerosystems Model SAAB 2000 airplanes. This proposed AD was prompted by reports of hydraulic accumulator failure. This proposed AD would require replacing certain hydraulic accumulators with stainless steel hydraulic accumulators, and structural modifications in the nose landing gear bay. We are proposing this AD to prevent failure of hydraulic accumulators, which may result in damage to the airplane and injury to occupants.

We propose to adopt a new airworthiness directive (AD) for the Eurocopter Model SA330F, G, J and AS332C, L, L1, and L2 helicopters. This proposed AD is prompted by two reports of jamming of one of the fuel shut-off control levers, which originated from solidified grease in the tangential gearbox (gearbox). Corrosion was also found in a gearbox. The proposed actions are intended to prevent jamming of a fuel shut-off control lever preventing the shut off of engine fuel and preventing the parallel-mounted electrical micro switches, normally activated by shutting off both of the fuel shut-off control levers, from switching off the electrical power system during an emergency shut down.

On July 20, 2011, PHMSA published a final rule under Docket Number PHMSA-2009-0151 (HM-218F) making miscellaneous amendments to the Hazardous Materials Regulations (HMR; 49 CFR parts 171-180). The amendments made by PHMSA in the July 20, 2011 final rule promote safer transportation practices; eliminate unnecessary regulatory requirements; finalize outstanding petitions for rulemaking; facilitate international commerce; and simplify the regulations. This final rule corrects errors in the pictorial display of labels, eliminates references to transitional provisions that were previously removed from the HMR, clarifies shipping paper amendments, corrects an editorial error, and extends the effective date of certain shipping paper amendments adopted in the July 20, 2011 final rule.

Distribution pipeline operators were required to have prepared and implemented distribution integrity management plans (DIMP) by August 2, 2011. Federal and state regulators have begun inspecting those plans and their implementation. This webinar will be the first opportunity for the regulators to share their findings broadly with the regulated community. The webinar will also include discussion of analyses of the initial submissions of data concerning mechanical fitting failures in distribution pipelines.

As part of a Federal Government-wide effort to streamline the process to seek feedback from the public on service delivery, the Pipeline Hazardous Materials Safety Administration will submit a Generic Information Collection Request (Generic ICR): ``Generic Clearance for the Collection of Qualitative Feedback on Agency Service Delivery'' to the Office of Management and Budget (OMB) for approval under the Paperwork Reduction Act (PRA) (44 U.S.C. 3501 et seq.).

The FAA assigned the Aviation Rulemaking Advisory Committee (ARAC) a new task to develop a comprehensive program of voluntary accreditation for commercial air tour operators that are not required under parts 91 and 135 of Title 14 of the Code of Federal Regulations (14 CFR) to maintain their aircraft under a continuous airworthiness maintenance program (CAMP). This task addresses, in part, the ARAC recommendation developed by the Commercial Air Tours Maintenance (CATM) Working Group, which the FAA accepted on February 1, 2011. This notice informs the public of a new ARAC activity and solicits membership for the new Commercial Air Tour Voluntary Accreditation Program Working Group.

This notice announces actions taken by FHWA and other Federal agencies that are final within the meaning of 23 U.S.C. 139(l)(1). The actions relate to the East Link Light Rail Transit Project in King County Washington. These actions grant licenses, permits, and approvals for the project.

This action proposes special conditions for the XtremeAir GmbH XA42 airplane. The XA42 airplane has a novel or unusual design feature associated with its static stability. This airplane can perform at the highest level of aerobatic competition. To be competitive, the aircraft was designed with positive and, at some points, neutral stability within its flight envelope. Its lateral and directional axes are also decoupled from each other providing more precise maneuvering. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for these design features. These proposed special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards. These special conditions are only applicable to aircraft certified solely in the acrobatic category.