Department of Transportation July 11, 2006 – Federal Register Recent Federal Regulation Documents

Notice of Order To Show-Cause; International Air Transport Association Tariff Conference Proceeding
Document Number: E6-10792
Type: Notice
Date: 2006-07-11
Agency: Office of the Secretary, Department of Transportation
The Department is directing all interested persons to show cause why it should not issue an order withdrawing its approval under 49 U.S.C. 41309 for an International Air Transport Association (``IATA'') agreement, the Provisions for the Conduct of the IATA Traffic Conferences, insofar as that agreement establishes conferences whereby IATA's member carriers discuss and agree upon passenger fares and cargo rates for U.S.-Australia/Europe markets. If the Department withdraws its approval for the agreement, the agreement will no longer have immunity from the antitrust laws under 49 U.S.C. 41308 for conference discussions of fares and rates for the U.S.-Australia/Europe markets.
Airworthiness Directives; CTRM Aviation Sdn. Bhd. (Formerly Eagle Aircraft (Malaysia) Sdn. Bhd.) Model Eagle 150B Airplanes
Document Number: E6-10773
Type: Proposed Rule
Date: 2006-07-11
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to supersede Airworthiness Directive (AD) 2004-11-04, which applies to all CTRM Aviation Sdn. Bhd. (Formerly Eagle Aircraft (Malaysia) Sdn. Bhd.) Model Eagle 150B airplanes. AD 2004-11-04 currently requires you to inspect certain canard inboard flap hinge support brackets (initially before further flight and repetitively before the first flight of each day) and perform any necessary follow-up action. This proposed AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Malaysia to require the installation of improved design inboard flap hinge brackets as terminating action for the repetitive inspections. Consequently, this proposed AD would initially retain the requirement that you inspect certain canard inboard flap hinge support brackets (initially before further flight and repetitively before the first flight of each day) and then require that you replace the parts with new design inboard flap hinge brackets as terminating action for the repetitive inspections or if cracks are found. We are issuing this proposed AD to detect and correct cracks in the canard inboard flap hinge support brackets, which could result in loss of retention of controls and consequently, loss of airplane control.
Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG (Formerly Rolls-Royce, plc.) Dart 528, 529, 532, 535, 542, and 555 Series Turbofan Engines
Document Number: E6-10772
Type: Proposed Rule
Date: 2006-07-11
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for Rolls-Royce Deutschland Ltd & Co KG (RRD) Dart 528, 529, 532, 535, 542, and 555 series turbofan engines. This proposed AD would require a dimensional inspection of the intermediate pressure turbine (IPT) disk or an ultrasonic inspection of the seal arm contact between the high pressure turbine (HPT) and the IPT disk seal arm and rework or replacement of the IPT disk if wear outside acceptable limits is found. This proposed AD results from reports of a number of HPT disk failures, some of which resulted in portions of the HPT disk being released. We are proposing this AD to prevent HPT disk failure, which can result in an uncontained engine failure and damage to the airplane.
Airworthiness Directives; Rolls-Royce plc RB211-524 Series Turbofan Engines
Document Number: E6-10771
Type: Proposed Rule
Date: 2006-07-11
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to supersede an existing airworthiness directive (AD) for Rolls Royce plc (RR) RB211-524 series turbofan engines with certain part number (P/N) intermediate pressure compressor (IPC) stage 5 disks installed. That AD currently requires new reduced IPC stage 5 disk cyclic limits. This proposed AD would require the same reduced IPC stage 5 disk cyclic limits, the requirement to remove from service affected disks that already exceed the new reduced cyclic limit, and to remove from service other affected disks before exceeding their cyclic limits using a drawdown schedule. This proposed AD also would exempt disks reworked to RR Service Bulletin (SB) RB.211-72-E182, Revision 1, dated July 30, 2004, and would allow an on-wing eddy current inspection (ECI) on RB211-524G and RB211-524H series engines. This proposed AD results from the manufacturer issuing a revised Alert Service Bulletin (ASB) to remove certain disks from applicability, and to allow an on-wing ECI on RB211-524G and RB211-524H series engines. We are proposing this AD to prevent failure of the IPC stage 5 disk, which could result in uncontained engine failure and possible damage to the airplane.
Pilkington Glass of Canada Ltd., Grant of Petition for Decision of Inconsequential Noncompliance
Document Number: E6-10763
Type: Notice
Date: 2006-07-11
Agency: National Highway Traffic Safety Administration, Department of Transportation
Marine Transportation System National Advisory Council
Document Number: E6-10756
Type: Notice
Date: 2006-07-11
Agency: Maritime Administration, Department of Transportation
The Maritime Administration announces that the Marine Transportation System National Advisory Council (MTSNAC) will hold a meeting to discuss MTS needs, regional MTS outreach and education initiatives, Committee on the Marine Transportation System (CMTS) coordination, congestion issues, and disaster response and recovery efforts. A public comment period is scheduled for 8:30 a.m. to 9 a.m. on Thursday, July 27, 2006. To provide time for as many people to speak as possible, speaking time for each individual will be limited to three minutes. Members of the public who would like to speak are asked to contact Richard J. Lolich by July 20, 2006. Commenters will be placed on the agenda in the order in which notifications are received. If time allows, additional comments will be permitted. Copies of oral comments must be submitted in writing at the meeting. Additional written comments are welcome and must be filed by August 4, 2006.
Petition for Waivers of Compliance
Document Number: E6-10755
Type: Notice
Date: 2006-07-11
Agency: Federal Railroad Administration, Department of Transportation
Safe Routes to School Task Force to the Secretary of Transportation
Document Number: E6-10754
Type: Notice
Date: 2006-07-11
Agency: Federal Highway Administration, Department of Transportation
Pursuant to section 1404 (h) of the Safe, Accountable, Flexible, Efficient Transportation Equity Act: A Legacy for Users (SAFETEA-LU), the Secretary of Transportation is establishing a Safe Routes to School Task Force to study and develop a strategy for advancing safe routes to school programs nationwide. The FHWA Office of Safety will serve as sponsor of the Task Force for the Secretary. The purpose of this notice is to invite interested parties to submit comments to the FHWA on the strategy or issues that should be discussed by the Task Force, and the organizations and participants to be considered for representation on the Task Force.
Pipeline Safety: Grant of Waiver; Maritimes & Northeast Pipeline, L.L.C.
Document Number: 06-6107
Type: Notice
Date: 2006-07-11
Agency: Pipeline and Hazardous Materials Safety Administration, Department of Transportation
PHMSA is granting Maritimes & Northeast Pipeline, L.L.C. (M&N) a waiver of compliance from certain PHMSA regulations for the United States portion of its pipeline system. This waiver increases the maximum allowable operating pressure (MAOP) for the pipeline. This waiver decision also authorizes M&N to increase the design factor for its compressor station piping, grants relief from the strength testing requirements for M&N's compressor station piping, grants relief in establishing the MAOP of pipelines operating above prescribed hoop stresses, grants relief from the capacity requirements of pressure limiting stations, and authorizes M&N to maintain the pressure rating of portions of the waiver area subject to a change in class location. Before granting the waiver, PHMSA performed a thorough technical review of M&N's application and supporting documents. PHMSA requested and received supplementary information on numerous technical aspects of M&N's design, engineering, operations, and maintenance practices. The materials are available in docket PHMSA-2006-23448 at https:// dms.dot.gov. PHMSA also sought comments from the public and received positive feedback from States along the pipeline and the Technical Pipeline Safety Standards Committee. The waiver is subject to and conditional upon supplemental safety criteria set forth in this notice. The supplemental safety criteria address the life-cycle management of the subject pipeline and require M&N to adhere to maintenance, inspection, monitoring, control, and reporting standards exceeding existing regulatory requirements.
Pipeline Safety: Grant of Waiver; Alliance Pipeline L.P.
Document Number: 06-6106
Type: Notice
Date: 2006-07-11
Agency: Pipeline and Hazardous Materials Safety Administration, Department of Transportation
PHMSA is granting Alliance Pipeline L.P. (APL) a waiver of compliance from certain PHMSA regulations for the United States portion of its pipeline system. This waiver increases the maximum allowable operating pressure (MAOP) for its pipeline. It also increases the design factor for its compressor station piping, grants relief from the hydrostatic testing requirements for its compressor station piping, and grants relief from equipment requirements for pressure relieving and limiting stations. Before granting the waiver, PHMSA performed a thorough technical review of APL's application for waiver and supporting documents. PHMSA requested and received supplementary information pertaining to numerous technical aspects of APL's design, engineering, operations, and maintenance practices. PHMSA also sought comments from the public and received positive feedback from the impacted States along the pipeline and the Technical Pipeline Safety Standards Committee. The waiver is subject to and conditional upon supplemental safety criteria set forth in this notice. The supplemental safety criteria address the life cycle management of the subject pipeline and require the operator to adhere to maintenance, inspection, monitoring, control, and reporting standards exceeding existing regulatory requirements.
Pipeline Safety: Grant of Waiver; Rockies Express Pipeline
Document Number: 06-6105
Type: Notice
Date: 2006-07-11
Agency: Pipeline and Hazardous Materials Safety Administration, Department of Transportation
PHMSA is granting Rockies Express Pipeline, L.L.C. (Rockies Express) a waiver of compliance from the pipeline safety regulation that prescribes the design factor to be used in the design formula for steel pipe. This waiver allows the Rockies Express pipeline to operate at hoop stresses up to 80 percent of the specified minimum yield strength (SMYS) in Class 1 locations. The waiver also grants Rockies Express relief from equipment requirements for pressure relieving and limiting stations. Before granting the waiver, PHMSA performed a thorough technical review of Rockies Express's application and supporting documents. PHMSA requested and received supplementary information pertaining to numerous technical aspects of its metallurgy, pipeline design, and engineering practices. These materials are available in the docket PHMSA-2006-23998 at https://dms.dot.gov. PHMSA also sought comments from the public and received positive feedback from the impacted States along the pipeline and the Technical Pipeline Safety Standards Committee. The waiver is subject to and conditional upon supplemental safety criteria set forth in this notice. The supplemental safety criteria address the life cycle management of the subject pipeline and require Rockies Express to adhere to maintenance, inspection, monitoring, control, and reporting standards exceeding existing regulatory requirements.
Airworthiness Directives; Bombardier Model CL-600-2C10 (Regional Jet Series 700, 701, and 702) Airplanes, Model CL-600-2D15 (Regional Jet Series 705) Airplanes, and Model CL-600-2D24 (Regional Jet Series 900) Airplanes
Document Number: 06-6051
Type: Rule
Date: 2006-07-11
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD), which applies to certain Bombardier Model CL-600-2C10 (Regional Jet Series 700 and 701) and CL-600-2D24 (Regional Jet Series 900) series airplanes. That AD currently requires repetitive detailed inspections for cracking or deformation, or pulled or missing fasteners, on the lower panel of the left- and right-hand main landing gear (MLG) doors, as applicable, and corrective actions if necessary. This new AD reduces the repetitive inspection interval for certain airplanes. This new AD also adds airplanes to the applicability. This AD results from a report of a MLG door departing from an airplane. We are issuing this AD to prevent failure of the lower panel of the MLG door, departure of the lower panel from the airplane, and consequent damage to airplane structure, which could adversely affect the airplane's continued safe flight and landing.
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