Department of Transportation April 21, 2005 – Federal Register Recent Federal Regulation Documents
Results 1 - 21 of 21
Pipeline Safety: Grant of Waiver; Tractebel Power, Inc.
The Pipeline and Hazardous Materials Safety Administration's (PHMSA), formerly the Research and Special Programs Administration (RSPA), Office of Pipeline Safety (OPS) is granting Tractebel Power, Inc.'s (TPI) petition for a waiver of the pipeline safety regulations to employ a 1.0 longitudinal joint factor (LJF) for austenitic stainless steel pipe in its Tractebel Calypso Pipeline (TCP) project.
Pipeline Safety: Drug and Alcohol Testing
This notice advises operators of gas, hazardous liquid and carbon dioxide pipelines and liquefied natural gas facilities that the Pipeline and Hazardous Materials Safety Administration (PHMSA), Office of Pipeline Safety (OPS), intends to issue an Advisory Bulletin to begin collecting annual drug and alcohol testing data for contractor employees performing covered functions in the pipeline industry. The collection of contractor testing data is necessary for the calculation of the minimum annual percent rate for random drug testing, which is based on the reported positive rate for the entire industry. No regulatory change is necessary because the current rule already requires operators to report testing data for covered employees to OPS. The Advisory Bulletin will end the deferment period addressed in the preamble to the current rule for reporting contractor data and suggest a method for reporting the data that minimizes the problems associated with duplication. This notice proposes a method for reporting contractor data, seeks public comment on the method, and encourages suggestions for alternative approaches for reporting contractor testing data.
Pipeline Safety: Pipeline Integrity Management in High Consequence Areas for Hazardous Liquid Operators
OPS will sponsor a 1\1/2\ day workshop to review the initial Integrity Management (IM) inspections of hazardous liquid pipeline operators. Workshop topics will cover the lessons learned, accomplishments, and future expectations for such programs from both the OPS and industry perspectives.
Pearl Crossing LNG Terminal LLC Liquefied Natural Gas Deepwater Port License Application; Draft Environmental Impact Statement
The U.S. Coast Guard and the Maritime Administration (MARAD) announce the availability of the draft environmental impact statement (DEIS) on the Pearl Crossing LLC Deepwater Port License Application and Pearl Crossing Pipeline LLC Application for a Certificate of Public Convenience and Necessity. The application describes a project that would be located in the Gulf of Mexico, Outer Continental Shelf West Cameron Block 220, approximately 41 miles south of Cameron, Louisiana. The Coast Guard and the Maritime Administration, as well as the cooperating agencies (i.e., Federal Energy Regulatory Commission and U.S. Army Corps of Engineers) request public comment on the DEIS.
Notice of Receipt of Petition for Decision That Nonconforming 2001-2005 Mercedes Benz Sprinter Trucks Are Eligible for Importation
This document announces receipt by the National Highway Traffic Safety Administration (NHTSA) of a petition for a decision that 2001-2005 Mercedes Benz Sprinter trucks that were not originally manufactured to comply with all applicable Federal motor vehicle safety standards, are eligible for importation into the United States because (1) they are substantially similar to vehicles that were originally manufactured for sale in the United States and that were certified by their manufacturer as complying with the safety standards, and (2) they are capable of being readily altered to conform to the standards.
Notice of Receipt of Petition for Decision That Nonconforming 2002-2003 Hobby Wohnwagenwerk Exclusive 650 KMFE Trailers Are Eligible for Importation
This document announces receipt by the National Highway Traffic Safety Administration (NHTSA) of a petition for a decision that 2002-2003 Hobby Wohnwagenwerk Exclusive 650 KMFE trailers that were not originally manufactured to comply with all applicable Federal motor vehicle safety standards are eligible for importation into the United States because they have safety features that comply with, or are capable of being altered to comply with, all such standards.
Airworthiness Directives; Airbus Model A320 Series Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Model A320 series airplanes. This proposed AD would require installing insulator and cable ties to the electrical cables of the S routes at the gaps in the raceway in the wing trailing edge and the wing tip and wing root areas. This proposed AD is prompted by the results of fuel system reviews conducted by the manufacturer. We are proposing this AD to prevent injection of high voltage current into the low voltage wiring that passes through the fuel tanks, which could result in a possible fuel tank explosion.
Special Conditions: Garmin International Inc.; Cessna Model 182T/T182T Airplane; Installation of Electronic Flight Instrument System and the Protection of the System From High Intensity Radiated Fields (HIRF)
These special conditions are issued for Garmin International Inc., 1200 E. 151st St., Olathe, KS 66062, for a Supplemental Type Certificate on the Cessna Model 182T/T182T airplanes. These airplanes, as modified by Garmin, will have a novel or unusual design feature(s) associated with the installation of a Garmin GFC-700 digital autopilot system. These special conditions address the protection of these systems from the effects of high intensity radiated field (HIRF) environments. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These 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.
Advisory Circular: Change 1 to 23-21, Airworthiness Compliance Checklists Used To Substantiate Major Alterations for Small Airplanes
This notice announces the issuance of change 1 to Advisory Circular (AC) 23-21, Airworthiness Compliance Checklists Used to Substantiate Major Alterations for Small Airplanes. The most significant change is a revision in all locations to the signature required so the aircraft may be returned to service after major alteration. The Aviation Safety Inspector in the Flight Standards District Office must now sign instead of an Airframe and Powerplant mechanic. Other changes were minor.
Notice of Intent To Rule on Application To Impose a Passenger Facility Charge (PFC) at Fort Lauderdale International Airport, Fort Lauderdale, FL
The FAA proposes to rule and invites public comment on the application to impose a PFC at Fort Lauderdale International Airport under the provisions of the Aviation Safety and Capacity Expansion Act of 1990 (Title IX of the Omnibus Budget Reconciliation Act of 1990) (Pub. L. 101-508) and part 158 of the Federal Aviation Regulations (14 CFR part 158).
Notice of Submission Deadline for International Slots for the Winter 2005/2006 Scheduling Season
On October 1, 1999, the FAA amended the regulations governing takeoff and landing slots and slot allocation procedures at certain High Density Traffic Airports as a result of the ``Open Transborder'' Agreement between the Government of the United States and the Government of Canada. One element of this final rule established that the deadline for submission of requests for international slots will be published in a Federal Register notice for each scheduling season. The purpose of the amendment is for the FAA deadline for international slots requests to coincide with the International Air Transport Association deadline for submission of international requests. In accordance with this amendment, the FAA announces in this notice that the deadline for submitting requests for international slots at John F. Kennedy International Airport (JFK) for allocation under 14 CFR 93.217 is May 12, 2005. Additionally, the FAA has designated Chicago's O'Hare International Airport (O'Hare) as a Level 2, Schedules Facilitated Airport under the IATA Guidelines. As such, the FAA requests carriers intening to conduct international service to O'Hare submit their intended schedules following the same procedures used for submitting requests for slots at JFK.
Notice of Intent To Rule on Application 05-05-C-00-SGF To Impose and Use the Revenue From a Passenger Facility Charge (PFC) at Springfield-Branson Regional Airport, Springfield, MO
The FAA proposes to rule and invites public comment on the application to impose and use the revenue from a PFC at Springfield- Branson Regional Airport under the provisions of the Aviation Safety and Capacity Expansion Act of 1990 (Title IX of the Omnibus Budget Reconciliation Act of 1990) (Pub. L. 101-508) and part 158 of the Federal Aviation Regulations (14 CFR part 158).
Notice of Intent To Rule on Application 05-05-C-00-LAS To Impose and Impose and Use Passenger Facility Charge (PFC) at McCarran International Airport, and Use the PFC Revenue at McCarran International, Henderson Executive, and North Las Vegas Airports, Las Vegas, NV
The FAA proposes to rule and invites public comment on the application to impose and impose and use a PFC at McCarran International Airport, and use the revenue of a PFC at McCarran International Airport, Henderson Executive Airport, and North Las Vegas Airport under the provisions of the Aviation Safety and Capacity Expansion Act of 1990 (Title IX of the Omnibus Budget Reconciliation Act of 1990) (Pub. L. 101-508) and part 158 of the Federal Aviation Regulations (14 CFR part 158).
Consumer Information; Uniform Tire Quality Grading Standards
The Uniform Tire Quality Grading Standards (UTQGS) contain detailed testing procedures for generating consumer information about the treadwear, traction, and temperature resistance of passenger car tires. To ensure the uniformity of treadwear grades, the grading procedures specify a 400-mile test course located near San Angelo, Texas. Two or four-vehicle convoys equipped with candidate tires travel along this course to evaluate the tire treadwear performance. Because of flooding now affecting several water crossings along a small portion of the test course, NHTSA is issuing this interim final rule to revise the specified treadwear test course route. This change will not compromise the reliability of the treadwear grades, and will not impose or relax any substantive requirements or burdens on manufacturers.
Airworthiness Directives; Glaser-Dirks Flugzeugbau GmbH Model DG-800B Sailplanes
The FAA adopts a new airworthiness directive (AD) for all Glaser-Dirks Flugzeugbau GmbH (DG Flugzeugbau) Model DG-800B sailplanes equipped with a SOLO 2625 engine or a Mid-West AE 50T engine. This AD requires you to modify the coolant pump and fuel pump electrical circuits, remove the non-resettable digital engine indicator (DEI) circuit breaker (4-ampere) and replace with a resettable 5-ampere circuit breaker, secure (for sailplanes with a SOLO 2625 engine) the choke butterfly valve axis, install edge protection at the sharp edges of the resettable 5-ampere DEI circuit breaker, and incorporate changes in the FAA-approved sailplane flight manual. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to prevent electrical failure of the fuel and coolant pumps if a non-resettable circuit breaker trips. This could result in power loss with the inability to restart the fuel pump during a critical phase of flight (for example, takeoff under own power).
Airworthiness Directives; CENTRAIR 101 Series Gliders
The FAA adopts a new airworthiness directive (AD) for certain CENTRAIR 101 series gliders. This AD requires you to replace non- strengthened rudder pedals with reinforced rudder pedals. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for France. We are issuing this AD to replace the non-strengthened rudder pedals and to prevent failure of the rudder controls. This failure could lead to loss of directional control of the glider.
Airworthiness Directives; McDonnell Douglas Model DC-8-33 and -43 Airplanes; Model DC-8F-54 and DC-8F-55 Airplanes; and Model DC-8-50, -60, -60F, -70, and -70F Series Airplanes
The FAA is superseding an existing airworthiness directive (AD), which applies to certain McDonnell Douglas series airplanes. That AD currently requires repetitive inspections of the electrical connectors of the explosive cartridge wiring of the engine fire extinguisher containers to verify if the identification number labels are installed and legible; repetitive electrical tests of all explosive cartridge wiring of the engine fire extinguisher containers to verify proper installation and function; and corrective actions if necessary. This new AD requires an inspection of the emergency shut off wire assembly; installation of lanyards on the electrical connectors for the engine fire extinguishing agent containers and for the auxiliary power unit fire extinguishing agent containers if applicable; and related investigative/corrective actions, as applicable. This AD is prompted by reports of cross-wired electrical connectors of the engine fire extinguishing agent containers. We are issuing this AD to detect and correct cross-wired electrical connectors of the fire extinguishing system, which could release fire extinguishing agent into the incorrect engine nacelle in the event of an engine fire.
Airworthiness Directives; Pilatus Aircraft Limited Models B4-PC11, B4-PC11A, and B4-PC11AF Sailplanes
The FAA adopts a new airworthiness directive (AD) for all Pilatus Aircraft Limited (Pilatus) Models B4-PC11, B4-PC11A, and B4- PC11AF sailplanes. This AD requires you to repetitively inspect the control-column support for cracks and, if any cracks are found, replace the control-column support with a new support. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. We are issuing this AD to detect and correct cracks in the control-column support, which could result in failure of the support. This failure could lead to loss of the primary flight control system.
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