Federal Aviation Administration June 30, 2006 – Federal Register Recent Federal Regulation Documents

Revocation of Low Altitude Reporting Point; AK
Document Number: E6-10285
Type: Rule
Date: 2006-06-30
Agency: Federal Aviation Administration, Department of Transportation
This action revokes the Bishop Nondirectional Radio Beacon (NDB) as an Alaskan low altitude reporting point. The FAA has determined that this reporting point should be removed from the National Airspace System (NAS), since the Bishop NDB was de- commissioned and is no longer in service.
Establishment of Offshore Airspace Area 1485L and Revision of Control 1485H; Barrow, AK
Document Number: E6-10282
Type: Rule
Date: 2006-06-30
Agency: Federal Aviation Administration, Department of Transportation
This action establishes Control 1485L and revises Control 1485H offshore airspace in the vicinity of Barrow, AK. This action establishes controlled airspace outside of 12 nautical miles (NM) of the U.S. shoreline upward from 1,200 feet mean sea level (MSL) along the North Slope of Alaska. Additionally, this action revises the altitudes of Control 1485H from FL 230/FL 450 to FL 180/FL 600. This action provides additional controlled airspace for aircraft executing instrument flight rules (IFR) operations at the airfields along the North Slope of Alaska in anticipation of establishing terminal arrival areas associated with Area Navigation (RNAV) Standard Instrument Arrival Procedures (SIAPs).
Receipt of Noise Compatibility Program and Request for Review
Document Number: 06-5925
Type: Notice
Date: 2006-06-30
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) announces that it is reviewing a proposed noise compatibility program that was submitted for McClellan-Palomar Airport under the provisions of 49 U.S.C. 47501 et seq. (the Aviation Safety and Noise Abatement Act, hereinafter referred to as ``the Act'') and 14 CFR Part 150 by the County of San Diego. This program was submitted subsequent to a determination by FAA that associated noise exposure maps submitted under 14 CFR Part 150 for McClellan-Palomar Airport were in compliance with applicable requirements, effective April 26, 2005, which was published in the Federal Register, Volume 70, No. 89, page 24671, on May 10, 2005. The proposed noise compatibility program will be approved or disapproved on or before December 17, 2006.
Notice of Opportunity for Public Comment on Grant Acquired Property Release at Orangeburg Municipal Airport, Orangeburg, SC
Document Number: 06-5924
Type: Notice
Date: 2006-06-30
Agency: Federal Aviation Administration, Department of Transportation
Under the provisions of Title 49, U.S.C. Section 47153(c), notice is being given that the FAA is considering a request from the City of Orangeburg to waive the requirement that approximately .34- acres of airport property, located at the Orangeburg Municipal Airport, be used for aeronautical purposes.
Final General Conformity Determination for Proposed Operations of Southwest Airlines Co. at Denver International Airport, Denver, CO
Document Number: 06-5888
Type: Notice
Date: 2006-06-30
Agency: Federal Aviation Administration, Department of Transportation
Pursuant to Section 176(c) of the Clean Air Act Amendments of 1990, the FAA announces the availability of the Final General Conformity Determination for Operations of Southwest Airlines Co. (Southwest) at Denver International Airport (DEN). FAA has determined that emissions from Southwest's operations at DEN conform to the Colorado State Implementation Plan (SIP). In accordance with the requirements of 40 CFR 93.156 (b), the Draft Conformity Determination, Proposed Operations of Southwest Airlines Co. at Denver International Airport, Denver, CO was made available for public review beginning April 21, 2006. Notice of the draft determination was published in the Rocky Mountain News, Denver, Colorado on April 21, 2006, and copies of the draft determination were made available at DEN. The Notice of Draft General Conformity Determination was published in the Federal 1Register on April 27, 2006 (71 FR 24903). No comments were submitted during the public comment period, which ended on May 30, 2006. Consequently, the Final General Conformity Determination consists of the Draft General Conformity Determination, with the following typographical corrections. The corrections are needed to clarify terms describing aircraft operations and to correct the reference to the maximum foreseeable aircraft activity used to predict aircraft emissions, as documented in Table 1. 1. Page 24903, last sentence on this page under SUPPLEMENTARY INFORMATION shall be revised to read: ``At that time Southwest indicated an interest in increasing service to as many as 50 or 60 daily landing/take-off cycles (LTOs) at DEN, but agreed to maintain * * *'' 2. Page 24904, second sentence of the last paragraph under SUPPLEMENTARY INFORMATION shall be revised to read: ``This General Conformity Determination addresses FAA's proposed Federal action to amend Southwest's operation specifications (OpSpecs) to accommodate future aircraft activity as high as 60 daily LTOs at DEN * * *'' 3. Page 24904, fourth sentence of the 1st paragraph under Aircraft and Supporting Equipment Emissions shall be revised to read: ``Under the Proposed Action scenario, aircraft emissions were quantified based on this maximum foreseeable level and conservatively assumed to occur every day of the year for a total of 21,900 LTOs per year.''
Petitions for Exemption; Summary of Petitions Received
Document Number: 06-5881
Type: Notice
Date: 2006-06-30
Agency: Federal Aviation Administration, Department of Transportation
Pursuant to FAA's rulemaking provisions governing the application, processing, and disposition of petitions for exemption, part 11 of Title 14, Code of Federal Regulations (14 CFR), this notice contains summaries of certain petitions 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 any petition or its final disposition.
Airworthiness Directives; Eurocopter France Model AS350B, AS350B1, AS350B2, AS350B3, AS350BA, AS350C, AS350D, AS350D1, and AS355E Helicopters
Document Number: 06-5880
Type: Proposed Rule
Date: 2006-06-30
Agency: Federal Aviation Administration, Department of Transportation
This document proposes adopting a new airworthiness directive (AD) for the specified Eurocopter France (Eurocopter) model helicopters. This proposal would require replacing a certain hydraulic drive belt (drive belt). Also proposed is reducing the lubrication time interval for a certain hydraulic pump drive shaft (drive shaft). This proposal is prompted by in-flight failures of the drive belt and the drive shaft. The actions specified by this proposed AD are intended to prevent in-flight failure of the drive belt or drive shaft, loss of hydraulic power to the flight control system, and subsequent loss of control of the helicopter.
Airworthiness Directives; Boeing Model 767-200 and -300 Series Airplanes
Document Number: 06-5874
Type: Proposed Rule
Date: 2006-06-30
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to certain Boeing Model 767-200, -300, and -300F series airplanes. The existing AD currently requires an inspection of visually accessible areas for indications of overheating of the heater tape attached to the potable water fill and drain lines in the forward and aft cargo compartments, exposed foam insulation or missing or damaged protective tape around the potable water fill and drain lines, and debris or contaminants on or near the potable water fill and drain lines. That AD also requires corrective action, as necessary. This proposed AD would require repetitive inspections of the forward and aft cargo compartments, as applicable, for discrepancies of the potable water supply and gray water drain lines; and applicable corrective actions if necessary. This proposed AD also would require replacing the heater tapes on the potable water supply and gray water drain lines of the forward and aft cargo compartments, as applicable, with new ribbon heaters, which would end the repetitive inspections. This proposed AD results from a report of a fire in the aft cargo compartment. We are proposing this AD to prevent overheating of the heater tape on potable water fill and drain lines, which may ignite accumulated debris or contaminants on or near the potable water fill and drain lines, resulting in a fire in the airplane.
Airworthiness Directives; Fokker Model F27 Mark 050 and Model F.28 Mark 0070 and 0100 Airplanes
Document Number: 06-5873
Type: Proposed Rule
Date: 2006-06-30
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Fokker Model F27 Mark 050 and Model F.28 Mark 0070 and 0100 airplanes. This proposed AD would require repetitively removing the two existing escape rope assemblies in the flight compartment and installing new escape rope assemblies. This proposed AD results from reports of findings of small cracks in the polyester assembly block in which the cotton escape rope is stored. A test revealed that the escape ropes had deteriorated over time, and the load capability was considerably reduced. We are proposing this AD to ensure that flightcrew members safely reach the ground after exiting the flight compartment window during an emergency evacuation.
Airworthiness Directives; Airbus Model A300 and A310 Airplanes; and Airbus Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes)
Document Number: 06-5872
Type: Proposed Rule
Date: 2006-06-30
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus Model A300 and A310 airplanes and A300-600 series airplanes. This proposed AD would require inspecting for discrepancies of all electrical bundles located in the leading and trailing edges of the wings, and performing corrective actions if necessary. This proposed AD results from fuel system reviews conducted by the manufacturer. We are proposing this AD to prevent an ignition source, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane.