Department of Transportation August 10, 2005 – Federal Register Recent Federal Regulation Documents

Office of the Secretary; Application of GoJet Airlines, LLC for Certificate Authority: Correction
Document Number: 05-15917
Type: Notice
Date: 2005-08-10
Agency: Department of Transportation
By Order 2005-7-14, served on July 15, 2005, the Department tentatively concluded that GoJet Airlines, LLC is fit, willing, and able to provide tentatively scheduled air transportation of persons, property, and mail, and should be issued a certificate of public convenience and necessity authorizing such operations, subject to conditions. At that time, we directed interested parties to file objections no later than 14 days after the service date of the order (i.e., July 29, 2005). Subsequently, the Department published a notice in the Federal Register on July 21, 2005, inadvertently directing all interested parties wishing to file objections should to do so by August 29, 2005. In order to correct this administrative error, while, at the same time, providing interested parties with a suitable period of time to file comments, we find it appropriate to direct persons wishing to file objections to our tentative decision to do so by August 15, 2005.
Application of GoJet Airlines, LLC for Certificate Authority: Correction
Document Number: 05-15916
Type: Notice
Date: 2005-08-10
Agency: Office of the Secretary, Department of Transportation
By Order 2005-7-14, served on July 15, 2005, the Department tentatively concluded that GoJet Airlines, LLC is fit, willing, and able to provide interstate scheduled air transportation of persons, property and mail, and should be issued a certificate of public convenience and necessity authorizing such operations, subject to conditions. At that time, we directed interested parties to file objections no later than 14 days after the service date of the order (i.e., July 29, 2005). Subsequently, the Department published a notice in the Federal Register on July 21, 2005, inadvertently directing all interested parties wishing to file objections to do so by August 29, 2005. In order to correct this administrative error, while, at the same time, providing interested parties with a suitable period of time to file comments, we find it appropriate to direct persons wishing to file objections to our tentative decision to do so by August 15, 2005.
Airworthiness Directives; Przedsiebiorstwo Doswiadczalno-Produkcyjne Szybownictwa “PZL-Bielsko” Model SZD-50-3 “Puchacz” Gliders
Document Number: 05-15803
Type: Proposed Rule
Date: 2005-08-10
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for all Przedsiebiorstwo Doswiadczalno-Produkcyjne Szybownictwa ``PZL- Bielsko'' Model SZD-50-3 ``Puchacz'' gliders. This proposed AD would require you to perform a visual inspection of the turnbuckle link for cracks or wear and replace if cracks or wear is found. This proposed action would only apply to those gliders where the turnbuckle is directly connected to the pedal. This proposed AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Poland. We are issuing this proposed AD to detect and correct cracks in the turnbuckle link, which could result in failure of the rudder cable. This failure could lead to loss of control of the glider.
Airworthiness Directives; Airbus Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes); and Airbus Model A310 Series Airplanes
Document Number: 05-15802
Type: Proposed Rule
Date: 2005-08-10
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus airplanes, listed above. This proposed AD would require installing two-stage relays in the electronics rack (90VU), and performing related corrective and investigative actions. This proposed AD is prompted by reports of in advertent rudder trim activation when the autopilot is on. We are proposing this AD to prevent inadvertent trim activation when the autopilot is on and the slats are extended, which could result in rudder activation when the autopilot is turned off.
Qualification of Drivers; Exemption Applications; Vision
Document Number: 05-15784
Type: Notice
Date: 2005-08-10
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
The FMCSA announces its decision to exempt 24 individuals from the vision requirement in the Federal Motor Carrier Safety Regulations (FMCSRs). The exemptions will enable these individuals to qualify as drivers of commercial motor vehicles (CMVs) in interstate commerce without meeting the vision standard prescribed in 49 CFR 391.41(b)(10).
Pipeline Safety Advisory Bulletin; Inspecting and Testing Pilot-Operated Pressure Relief Valves
Document Number: 05-15758
Type: Notice
Date: 2005-08-10
Agency: Pipeline and Hazardous Materials Safety Administration, Department of Transportation
This notice announces a pipeline safety advisory bulletin about pilot-operated pressure relief valves installed in hazardous liquid pipelines. The bulletin provides pipeline operators guidance on whether their inspection and test procedures are adequate to determine if these valves function properly. Malfunctioning of a pilot-operated pressure relief valve was a contributing factor in an accident involving a petroleum products pipeline in Bellingham Washington.
Pipeline Safety: Petition for Waiver; BOC Gases
Document Number: 05-15757
Type: Notice
Date: 2005-08-10
Agency: Pipeline and Hazardous Materials Safety Administration, Department of Transportation
PHMSA is correcting a petition for waiver published in the Federal Register on July 14, 2005 (70 FR 40780). That petition, from BOC Gases (BOC), requested a waiver from the pipeline safety standards at 49 CFR 195.306(c)(5) to allow the use of inert gas or carbon dioxide as the test medium for pressure testing an existing carbon dioxide pipeline. This notice corrects the supplementary information of that publication, which referred to a gas pipeline safety regulation when it should have referred to a hazardous liquid pipeline safety regulation.
Federal Motor Vehicle Safety Standards; Fuel System Integrity
Document Number: 05-15691
Type: Rule
Date: 2005-08-10
Agency: National Highway Traffic Safety Administration, Department of Transportation
This document responds to a petition for reconsideration from DaimlerChrysler Corporation of a final rule relating to the agency's upgrade of rear and side impact tests in Federal Motor Vehicle Safety Standard No. 301, Fuel System Integrity. Among other matters, that final rule provided manufacturers of vehicles with a gross vehicle weight rating greater than 2,722 kilograms (6,000 pounds) an additional year of lead time to certify their vehicles to the amended side impact requirements, but did not provide for a phase-in of those requirements for those vehicles. On reconsideration, NHTSA is providing manufacturers of those vehicles a two year phase-in for the side impact requirements. Ninety percent of the vehicles manufactured on or after September 1, 2005 must meet the upgraded side impact requirements, with 100 percent of the vehicles manufactured on or after September 1, 2006 meeting the requirements.
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