Department of Transportation July 17, 2012 – Federal Register Recent Federal Regulation Documents

Environmental Justice: Final Circular
Document Number: 2012-17404
Type: Notice
Date: 2012-07-17
Agency: Federal Transit Administration, Department of Transportation
The Federal Transit Administration (FTA) has placed in the docket and on its Web site final guidance in the form of a Circular (hereinafter ``EJ Circular'') on incorporating environmental justice principles into plans, projects, and activities that receive funding from FTA. This final guidance provides recommendations to State Departments of Transportation, Metropolitan Planning Organizations, public transportation providers, and other recipients of FTA funds on how to fully engage environmental justice populations in the public transportation decision-making process; how to determine whether environmental justice populations would be subjected to disproportionately high and adverse human health or environmental effects as a result of a transportation plan, project, or activity; and how to avoid, minimize, or mitigate these effects.
Airworthiness Directives; Cessna Aircraft Company Airplanes
Document Number: 2012-17395
Type: Proposed Rule
Date: 2012-07-17
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for certain Cessna Aircraft Company Model 750 airplanes. This proposed AD was prompted by reports of loss of displayed airspeed. This proposed AD would require inspecting certain logic modules to determine if certain cabin altitude/pitot static heater module assemblies are installed and replacing those assemblies with a new assembly; and revising the Non- Normal Procedures Section of the airplane flight manual (AFM) to include procedures for resetting the pitot switch in the event of pitot heater failure and for total loss of airspeed indication. We are proposing this AD to prevent the loss of all displayed airspeed, which could result in reduced ability to control the airplane.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2012-17393
Type: Proposed Rule
Date: 2012-07-17
Agency: Federal Aviation Administration, Department of Transportation
We are revising an earlier proposed airworthiness directive (AD) for all The Boeing Company Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747SR, and 747SP series airplanes. That NPRM proposed to require performing repetitive operational tests of the engine fuel suction feed of the fuel system, and other related testing if necessary. That NPRM was prompted by reports of two in-service occurrences on Model 737-400 airplanes of total loss of boost pump pressure of the fuel feed system, followed by loss of fuel system suction feed capability on one engine, and in- flight shutdown of the engine. This action revises that NPRM by proposing to require repetitive operational tests, and corrective actions if necessary. We are proposing this supplemental NPRM to detect and correct loss of the engine fuel suction feed capability of the fuel system, which in the event of total loss of the fuel boost pumps could result in dual engine flameout, inability to restart the engines, and consequent forced landing of the airplane. Since these actions impose an additional burden over that proposed in the previous NPRM, we are reopening the comment period to allow the public the chance to comment on these proposed changes.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2012-17391
Type: Proposed Rule
Date: 2012-07-17
Agency: Federal Aviation Administration, Department of Transportation
We are revising an earlier proposed airworthiness directive (AD) for certain The Boeing Company Model 737-600, -700, -700C, -800, and -900 series airplanes. That NPRM proposed to require inspecting the orientation of both sides of the coil cord connector keyways of the number 2 windows on the flight deck; re-clocking the connector keyways to 12 o'clock, if necessary; and replacing the coil cord assemblies on both number 2 windows on the flight deck. That NPRM was prompted by reports of arcing and smoke at the left number 2 window in the flight deck. This action revises that NPRM by changing the keyway position of certain receptacle connectors and adding airplanes to the applicability. We are proposing this supplemental NPRM (SNPRM) to prevent arcing, smoke, and fire in the flight deck, which could lead to injuries to or incapacitation of the flightcrew. Since these actions impose an additional burden over that proposed in the NPRM, we are reopening the comment period to allow the public the chance to comment on these proposed changes.
Petition for Exemption; Reopening of Comment Period
Document Number: 2012-17370
Type: Notice
Date: 2012-07-17
Agency: Federal Aviation Administration, Department of Transportation
This action reopens the comment period for a petition for exemption that was published on May 24, 2012. The relief sought in the petition for exemption would permit ICON Aircraft to incorporate a Spin-Resistant Airframe (SRA) in the ICON A5 at a weight above the current Light-Sport Aircraft (LSA) definition. Independent Aircraft Inc. has requested a reopening of the comment period to allow additional time to address issues associated with an increase in weight of the ICON A5.
Bleed Air Cleaning and Monitoring Equipment and Technology
Document Number: 2012-17368
Type: Proposed Rule
Date: 2012-07-17
Agency: Federal Aviation Administration, Department of Transportation
The FAA seeks information from industry developers, manufacturers, and the public related to effective air cleaning technology and sensor technology for the engine and auxiliary power unit bleed air supplied to the passenger cabin and flight deck of a pressurized aircraft. The information obtained will inform the agency of potential research and development plans.
Requested Administrative Waiver of the Coastwise Trade Laws: Vessel GUILDING LIGHT; Invitation for Public Comments
Document Number: 2012-17352
Type: Notice
Date: 2012-07-17
Agency: Maritime Administration, Department of Transportation
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.
Requested Administrative Waiver of the Coastwise Trade Laws: Vessel AVENIR; Invitation for Public Comments
Document Number: 2012-17350
Type: Notice
Date: 2012-07-17
Agency: Maritime Administration, Department of Transportation
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.
Notice of Opportunity for Public Comment on Surplus Property Release at Hancock County-Bar Harbor Airport, Trenton, ME
Document Number: 2012-17290
Type: Notice
Date: 2012-07-17
Agency: Federal Aviation Administration, Department of Transportation
Under the provisions of Title 49, U.S.C. Section 47153(d), notice is being given that the FAA is considering a request from Hancock County, Maine to waive the surplus property requirements for 0.77 acres of airport property located at Hancock County-Bar Harbor Airport, Trenton, Maine.
Proposed Establishment of Class E Airspace; Deer Lodge, MT
Document Number: 2012-17282
Type: Proposed Rule
Date: 2012-07-17
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish Class E airspace at Deer Lodge-City-County Airport, Deer Lodge, MT. Controlled airspace is necessary to accommodate aircraft using new Area Navigation (RNAV) Global Positioning System (GPS) standard instrument approach procedures at Deer Lodge-City-County Airport, Deer Lodge, MT. The FAA is proposing this action to enhance the safety and management of aircraft operations at the airport.
Airworthiness Directives; Sikorsky Aircraft Corporation Helicopters
Document Number: 2012-16944
Type: Rule
Date: 2012-07-17
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for Sikorsky Aircraft Corporation (Sikorsky) Model S-92A helicopters. This AD requires inspecting the main gearbox (MGB) for a crack. This AD is prompted by a crack in the cored passage of the MGB housing, which may be indicated by oil on the housing. These actions are intended to detect a crack in the MGB housing, which could result in loss of oil, failure of the MGB, and subsequent loss of control of the helicopter.
Airworthiness Directives; PZL Swidnik S.A. Helicopters
Document Number: 2012-16939
Type: Rule
Date: 2012-07-17
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for the PZL Swidnik S.A. (PZL) Model PZL W-3A helicopter with a certain generator air outlet collector (collector) installed. This AD requires modifying the generator air outlet collector attachments (collector attachments). This AD is prompted by an incident where cyclic control stick movement was restricted due to rotation of a loose collector, resulting in locking of the longitudinal control system hydraulic actuator fork end. These actions are intended to prevent rotation of the collector, which could lead to restricted cyclic control stick movement, and subsequent loss of control of the helicopter.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2012-16933
Type: Rule
Date: 2012-07-17
Agency: Federal Aviation Administration, Department of Transportation
We are superseding an existing airworthiness directive (AD) for certain The Boeing Company Model 767-200 and -300 series airplanes. That AD currently requires replacement of the existing deactivation pin, aft cascade pin bushing, and pin insert on each thrust reverser half with new, improved components. This new AD requires a dye penetrant inspection for cracking of the rivet holes of the bushing plate and repair or replacement, if necessary; and for certain airplanes, replacing the existing bushing with a new bushing and deactivation pin, and installing a new or serviceable stowage bracket for the deactivation pins on all airplanes powered by Pratt & Whitney JT9D series engines. This AD was prompted by reports that certain airplanes require installation of a new bushing and deactivation pin with increased load carrying capability and all airplanes powered by Pratt & Whitney JT9D series engines require installation of a new bracket for stowing the deactivation pin. We are issuing this AD to prevent failure of the thrust reverser deactivation pins, which could fail to prevent a deployment of a deactivated thrust reverser in flight and consequent reduced controllability of the airplane.
Airworthiness Directives; Airbus Airplanes
Document Number: 2012-16885
Type: Rule
Date: 2012-07-17
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for all Airbus Model A318, A319, and A320 series airplanes. This AD was prompted by reports of unsuccessful slide deployments during scheduled deployment tests, and failed functional tests of the release travel of the slide release mechanism. This AD requires inspecting the off-wing slide release cables on the left- and right-hand sides to determine whether a certain part number is installed, and replacement if necessary. We are issuing this AD to prevent non-availability of left- or right-hand off-wing exit slides that could impair emergency evacuation of the passengers and flightcrew, and could result in personal injuries.
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Document Number: 2012-16637
Type: Rule
Date: 2012-07-17
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Gulfstream Aerospace Corporation Model G-IV, GIV-X, GV, and GV-SP airplanes. This AD requires measuring to determine paint thickness on the flight control surfaces and corrective actions if necessary, and revising the Airplane Flight Manual (AFM). This AD was prompted by reports of failure to inspect or document the paint thickness on flight controls (ailerons, rudder, elevator), potentially having a negative impact on the flutter characteristics of the airplane. We are issuing this AD to detect and correct paint thickness on flight controls, which could result in loss of control of the airplane due to flutter.
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