Department of Transportation June 6, 2008 – Federal Register Recent Federal Regulation Documents

Aviation Proceedings, Agreements Filed the Week Ending January 18, 2008
Document Number: E8-12784
Type: Notice
Date: 2008-06-06
Agency: Office of the Secretary, Department of Transportation
Airworthiness Directives; Boeing Model 737-300, -400, and -500 Series Airplanes
Document Number: E8-12752
Type: Proposed Rule
Date: 2008-06-06
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for all Boeing Model 737-300, -400, and -500 series airplanes. This proposed AD would require performing repetitive operational tests of the engine fuel suction feed of the fuel system, and other related testing if necessary. This proposed AD results from a report of in-service occurrences of loss of fuel system suction feed capability, followed by total loss of pressure of the fuel feed system. We are proposing this AD to detect and correct failure of the engine fuel suction feed of the fuel system, which could result in dual engine flameout, inability to restart the engines, and consequent forced landing of the airplane.
Airworthiness Directives; Boeing Model 757 Airplanes
Document Number: E8-12749
Type: Proposed Rule
Date: 2008-06-06
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for all Boeing Model 757 airplanes. This proposed AD would require performing repetitive operational tests of the engine fuel suction feed of the fuel system, and other related testing if necessary. This proposed AD results from a report of in-service occurrences of loss of fuel system suction feed capability, followed by total loss of pressure of the fuel feed system. We are proposing this AD to detect and correct failure of the engine fuel suction feed of the fuel system, which could result in dual engine flameout, inability to restart the engines, and consequent forced landing of the airplane.
Airworthiness Directives; Airbus Model A300-600 Airplanes
Document Number: E8-12727
Type: Proposed Rule
Date: 2008-06-06
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for the products listed above. This proposed AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Airworthiness Directives; Boeing Model 747-400, -400D, and -400F Series Airplanes
Document Number: E8-12725
Type: Proposed Rule
Date: 2008-06-06
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for certain Boeing Model 747-400, -400D, and -400F series airplanes. This proposed AD would require performing repetitive operational tests of the engine fuel suction feed of the fuel system, and other related testing if necessary. This proposed AD results from a report of in- service occurrences of loss of fuel system suction feed capability, followed by total loss of pressure of the fuel feed system. We are proposing this AD to detect and correct failure of the engine fuel suction feed of the fuel system, which could result in multi-engine flameout, inability to restart the engines, and consequent forced landing of the airplane.
Airworthiness Directives; Boeing Model 747 Airplanes
Document Number: E8-12712
Type: Proposed Rule
Date: 2008-06-06
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for all Boeing Model 747 airplanes. This proposed AD would require inspecting for cracks in the left- and right-side Stringer 11 longeron adjacent to the horizontal stabilizer pivot bulkhead, and related investigative and corrective actions if necessary. This proposed AD results from a report of a crack found in the right-side Stringer 11 longeron horizontal flange, adjacent to the horizontal stabilizer pivot bulkhead, during a routine maintenance inspection. We are proposing this AD to detect and correct fatigue cracking of the longeron, which can propagate and cause damage to the adjacent horizontal stabilizer pivot bulkhead. This damage could result in loss of structural integrity and consequent inability of the bulkhead to carry flight loads, which could adversely affect controllability of the airplane.
Airworthiness Directives; Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747SR, and 747SP Series Airplanes
Document Number: E8-12692
Type: Proposed Rule
Date: 2008-06-06
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, 747SR, and 747SP series airplanes. This proposed AD would require performing repetitive operational tests of the engine fuel suction feed of the fuel system, and other related testing if necessary. This proposed AD results from a report of in- service occurrences of loss of fuel system suction feed capability, followed by total loss of pressure of the fuel feed system. We are proposing this AD to detect and correct failure of the engine fuel suction feed of the fuel system, which could result in multi-engine flameout, inability to restart the engines, and consequent forced landing of the airplane.
Airworthiness Directives; Boeing Model 777 Airplanes
Document Number: E8-12691
Type: Proposed Rule
Date: 2008-06-06
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for all Boeing Model 777 airplanes. This proposed AD would require performing repetitive operational tests of the engine fuel suction feed of the fuel system, and other related testing if necessary. This proposed AD results from a report of in-service occurrences of loss of fuel system suction feed capability, followed by total loss of pressure of the fuel feed system. We are proposing this AD to detect and correct failure of the engine fuel suction feed of the fuel system, which could result in dual engine flameout, inability to restart the engines, and consequent forced landing of the airplane.
Airworthiness Directives; Boeing Model 737-600, -700, -700C, -800, -900, and -900ER Series Airplanes
Document Number: E8-12685
Type: Proposed Rule
Date: 2008-06-06
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for certain Boeing Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes. This proposed AD would require performing repetitive operational tests of the engine fuel suction feed of the fuel system, and other related testing if necessary. This proposed AD results from a report of in-service occurrences of loss of fuel system suction feed capability, followed by total loss of pressure of the fuel feed system. We are proposing this AD to detect and correct failure of the engine fuel suction feed of the fuel system, which could result in dual engine flameout, inability to restart the engines, and consequent forced landing of the airplane.
Airworthiness Directives; Boeing Model 767 Airplanes
Document Number: E8-12684
Type: Proposed Rule
Date: 2008-06-06
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for all Boeing Model 767 airplanes. This proposed AD would require performing repetitive operational tests of the engine fuel suction feed of the fuel system, and other related testing if necessary. This proposed AD results from a report of in-service occurrences of loss of fuel system suction feed capability, followed by total loss of pressure of the fuel feed system. We are proposing this AD to detect and correct failure of the engine fuel suction feed of the fuel system, which could result in dual engine flameout, inability to restart the engines, and consequent forced landing of the airplane.
Petition for Exemption; Summary of Petition Received
Document Number: E8-12675
Type: Notice
Date: 2008-06-06
Agency: Federal Aviation Administration, Department of Transportation
This notice contains a summary of a petition seeking relief from specified requirements of 14 CFR. The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of FAA's regulatory activities. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of the petition or its final disposition.
Notice of Final Federal Agency Actions on the I-94 North-South Corridor Study in Wisconsin and Illinois
Document Number: E8-12674
Type: Notice
Date: 2008-06-06
Agency: Federal Highway Administration, Department of Transportation
This notice announces actions taken by the FHWA that are final within the meaning of 23 U.S.C. 139(l)(1). The actions relate to the I- 94 North-South Corridor Study in Lake County, Illinois, and Kenosha, Racine and Milwaukee Counties, Wisconsin. Those actions grant licenses, permits, and approvals for the project.
Southwest Gulf Railroad Company-Construction and Operation Exemption-in Medina County, TX
Document Number: E8-12668
Type: Notice
Date: 2008-06-06
Agency: Surface Transportation Board, Department of Transportation
The Section of Environmental Analysis (SEA) issued the Final EIS in the above-captioned proceeding on May 30, 2008, and published a notice of availability of the Final EIS in the Federal Register on the same day. It has come to our attention that a statement on page 2 of the notice of availability is incorrect. Therefore, we will strike this language: Parties who wish to file an administrative appeal of the Board's final decision may do so in writing within 30 days from the publication of the notice of the FEIS. * * * [T]he deadline for filing administrative appeals will be July 7, 2008. And replace it with: Parties who wish to file an administrative appeal of the Board's final decision may do so in writing within 20 days of the service date of the Board's final decision. Please correct your copies accordingly.
Revision of Class E Airspace; Deadhorse, AK
Document Number: E8-12585
Type: Rule
Date: 2008-06-06
Agency: Federal Aviation Administration, Department of Transportation
This action revises Class E airspace at Deadhorse, AK, to provide adequate controlled airspace to contain aircraft executing Standard Instrument Approach Procedures (SIAPs). Eight Standard Instrument Approach Procedures (SIAPs) and a textual Departure Procedure (DP) are being amended for the Deadhorse Airport. This action revises existing Class E airspace upward from the surface and from 700 feet (ft.) and 1,200 ft. above the surface at Deadhorse Airport, Deadhorse, AK.
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