Supreme Corporation, Grant of Petition for Decision of Inconsequential Noncompliance
Supreme Corporation (Supreme), has determined that certain model year (MY) 2015-2016 Supreme Classic American Trolley buses manufactured between October 1, 2014 and November 2, 2015, do not fully comply with paragraph S6 of Federal Motor Vehicle Safety Standard (FMVSS) No. 205, Glazing Materials. Supreme filed a report dated November 20, 2015, pursuant to 49 CFR part 573, Defect and Noncompliance Responsibility and Reports. Supreme then petitioned NHTSA under 49 CFR part 556 requesting a decision that the subject noncompliance is inconsequential to motor vehicle safety.
Notice of Receipt of Petition for Decision That Nonconforming Model Year 1996 and 1997 Ferrari F50 Passenger Cars Are Eligible for Importation
This document announces receipt by the National Highway Traffic Safety Administration (NHTSA) of a petition for a decision that model year (MY) 1996 and 1997 Ferrari F50 passenger cars (PC) that were not originally manufactured to comply with all applicable Federal motor vehicle safety standards (FMVSS) are eligible for importation into the United States. A motor vehicle that was not originally manufactured to conform to all applicable FMVSS, and has no substantially similar U.S.- certified counterpart, shall be refused admission into the United States unless NHTSA has decided that the motor vehicle has safety features that comply with, or are capable of being altered to comply with, all applicable FMVSS based on destructive test data or such other evidence as NHTSA decides to be adequate.
Notice of Final Federal Agency Actions on Proposed Highway in Utah
This notice announces actions taken by the FWHA that are final within the meaning of 23 U.S.C. 139(l)(1). The actions relate to the proposed 106th South, Redwood Road to Jordan Gateway, Project in Salt Lake County in the State of Utah. These actions grant approvals for the project.
Requested Administrative Waiver of the Coastwise Trade Laws: Vessel HOLOHOLO; Invitation for Public Comments
As authorized by 46 U.S.C. 12121, the Secretary of Transportation, as represented by the Maritime Administration (MARAD), is authorized to grant waivers of the U.S.-build requirement of the coastwise laws under certain circumstances. A request for such a waiver has been received by MARAD. The vessel, and a brief description of the proposed service, is listed below.
Airworthiness Directives; Piper Aircraft, Inc. Airplanes
We propose to supersede Airworthiness Directive (AD) 95-26-13, which applies to certain Piper Aircraft, Inc. Models PA-28-140, PA-28- 150, PA-28-151, PA-28-161, PA-28-160, PA-28-180, PA-28-181, PA-28-235, PA-28-236, PA-28R-180, PA-28R-200, PA-28R-201, PA-28S-160, PA-28S-180, PA-32-260, PA-32-300, PA-32-301, PA-32-301T, PA-32R-300, PA-32R-301 (SP), PA-32R-301 (HP), PA-32R-301T, PA-32RT-300, PA-32RT-300T, and PA- 32S-300 airplanes equipped with oil cooler hose assemblies that do not meet certain technical standard order (TSO) requirements. AD 95-26-13 requires inspections, replacement, and adjustment of the oil cooler hose assemblies, as well as providing for a terminating action. Since we issued AD 95-26-13, the FAA has received requests to clarify the intent of AD 95-26-13. This proposed AD would maintain all of the actions required by AD 95-26-13 and add language to clarify those requirements. We are proposing this AD to prevent rupture or failure of the oil cooler hose assemblies, which could result in engine stoppage with consequent loss of control.
Airworthiness Directives; Airbus Airplanes
We are revising an earlier proposed airworthiness directive (AD) for all Airbus Model A318, A319, A320, and A321 series airplanes. This action revises the notice of proposed rulemaking (NPRM) by requiring an additional action for sealant application on some nuts and bolts on the National Advisory Committee for Aeronautics (NACA) duct assembly and adding a grace period to the compliance time. We are proposing this SNPRM to detect and correct corroded circlips. Such corrosion could lead to failure of the circlips and consequent movement of the FVP and result in a reduction of the flame protector capability of the FVP cartridge. Such a condition could result in damage to the airplane in case of lightning impact or fire on the ground. Since the additional actions impose an additional burden over those proposed in the NPRM, we are reopening the comment period to allow the public the chance to comment on these proposed changes.