Department of Transportation October 8, 2008 – Federal Register Recent Federal Regulation Documents

Airworthiness Directives; Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes
Document Number: E8-23828
Type: Proposed Rule
Date: 2008-10-08
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for all Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. For all airplanes, this proposed AD would require repetitive overhaul of the retract actuator beam of the main landing gear (MLG). For certain airplanes, this proposed AD would require repetitive inspections for damage of the retract actuator beam, and related investigative and corrective actions if necessary. This proposed AD results from reports of broken retract actuator beams of the MLG and the subsequent failure of the MLG to fully retract. We are proposing this AD to detect and correct broken retract actuator beams of the MLG, which could cause damage to the beam arm, hydraulic tubing, and flight control cables. Damage to the flight control cables could result in loss of control of the airplane.
Airworthiness Directives; Boeing Model 747 Airplanes
Document Number: E8-23824
Type: Proposed Rule
Date: 2008-10-08
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to certain Boeing Model 747 airplanes. The existing AD currently requires repetitive inspections to detect evidence of wear damage in the area at the interface between the vertical stabilizer seal and fuselage skin, and corrective actions, if necessary. The existing AD also provides for an optional terminating action for the repetitive inspections. For all airplanes, this proposed AD would require doing repetitive inspections for wear damage and cracks of the fuselage skin in the interface area of the vertical stabilizer seal and fuselage skin, doing a detailed inspection for wear damage and cracks of the surface of any skin repair doubler in the area, and doing corrective actions. For airplanes on which the fuselage skin has been blended to remove wear damage, this proposed AD would require doing repetitive external detailed inspections or high frequency eddy current inspections for cracks of the blended area of the fuselage skin, and corrective actions if necessary. This proposed AD results from reports of wear damage on airplanes with fewer than 8,000 total flight cycles. In addition, there have been three reports of skin wear damage on airplanes that applied BMS 10-86 Teflon-filled coating (terminating action per AD 2002-26-15). We are issuing this AD to detect and correct wear damage and cracks of the fuselage skin in the interface area of the vertical stabilizer seal and fuselage skin in sections 46 and 48, which could cause in-flight depressurization of the airplane.
Airworthiness Directives; Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747SR, and 747SP Series Airplanes
Document Number: E8-23821
Type: Proposed Rule
Date: 2008-10-08
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for certain Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747- 200C, 747-200F, 747-300, 747-400, 747SR, and 747SP series airplanes. This proposed AD would require inspecting for skin cracks at the shear tie end fastener locations of the fuselage frames, and repair if necessary. This proposed AD results from a wide-spread fatigue damage assessment of Model 747 airplanes. We are proposing this AD to detect and correct cracks in the fuselage skin that can propagate and grow, resulting in a loss of structural integrity and a sudden decompression of the airplane during flight.
Establishment of Class E Airspace; Lexington, OK
Document Number: E8-23777
Type: Rule
Date: 2008-10-08
Agency: Federal Aviation Administration, Department of Transportation
This action confirms the effective date of the direct final rule that established Class E airspace at Muldrow Army Heliport, Lexington, OK, published in the Federal Register August 6, 2008 (73 FR 45607) Docket No. FAA-2008-0003.
Amendment of Class E Airspace; Black River Falls, WI
Document Number: E8-23770
Type: Rule
Date: 2008-10-08
Agency: Federal Aviation Administration, Department of Transportation
This action confirms the effective date of the direct final rule that amended Class E airspace at Black River Falls, WI, published in the Federal Register August 6, 2008 (73 FR 45606) Docket No. FAA- 2008-0024.
Reports, Forms, and Record Keeping Requirements
Document Number: E8-23742
Type: Notice
Date: 2008-10-08
Agency: National Highway Traffic Safety Administration, Department of Transportation
Before a Federal agency can collect certain information from the public, it must receive approval from the Office of Management and Budget (OMB). Under procedures established by the Paperwork Reduction Act of 1995, before seeking OMB approval, Federal agencies must solicit public comment on proposed collections of information, including extensions and reinstatements of previously approved collections. This document describes one collection of information for which NHTSA intends to seek OMB approval.
Fair Market Value and Design-Build Amendments
Document Number: E8-23729
Type: Proposed Rule
Date: 2008-10-08
Agency: Federal Highway Administration, Department of Transportation
This NPRM proposes to amend FHWA regulations, to require State departments of transportation (DOT) and other public authorities to negotiate for and obtain fair market value as part of any concession agreement involving a facility acquired or constructed with Federal-aid highway funds. Additionally, this NPRM proposes to amend FHWA regulations to permit public agencies to compete against private entities for the right to obtain a concession agreement involving such facilities. Also, this notice proposes to amend the design-build regulations to permit contracting agencies to incorporate unsuccessful offerors' ideas into a design-build contract upon the acceptance of a stipend.
Environmental Impact Statement: Sussex County, DE
Document Number: E8-23669
Type: Notice
Date: 2008-10-08
Agency: Federal Highway Administration, Department of Transportation
The FHWA is updating a previous notice of intent (issued on Friday, June 3, 2005) to advise the public that an Environmental Impact Statement (EIS) will be prepared for a proposed highway improvement project along US 113 in south central Sussex County, Delaware.
Federal Motor Vehicle Safety Standards; Designated Seating Positions and Seat Belt Assembly Anchorages
Document Number: E8-23577
Type: Rule
Date: 2008-10-08
Agency: National Highway Traffic Safety Administration, Department of Transportation
Today's final rule amends the definition of the term, ``designated seating position,'' as used in the Federal motor vehicle safety standards (FMVSS), to indicate more clearly which areas within the interior of a vehicle meet that definition. Today's final rule also establishes a calculation procedure for determining the number of designated seating positions at a seat location for trucks and multipurpose passenger vehicles with a gross vehicle weight rating less than 10,000 lbs, passenger cars, and buses. Further, this document eliminates the existing exclusion of auxiliary seats (i.e., temporary or folding jump seats) from the definition of ``designated seating position.'' Today's final rule encourages manufacturers to use a variety of visual cues in the design of the vehicle interior to help improve occupant awareness as to which areas of a vehicle are not intended to be used as seating positions. This will help to ensure that occupants sit in locations where they are afforded the crash protection required by the FMVSSs.
This site is protected by reCAPTCHA and the Google Privacy Policy and Terms of Service apply.