Federal Aviation Administration June 7, 2006 – Federal Register Recent Federal Regulation Documents

Modification of Control 1234L Offshore Airspace Area; AK
Document Number: E6-8850
Type: Rule
Date: 2006-06-07
Agency: Federal Aviation Administration, Department of Transportation
This action amends Control 1234L offshore airspace area in Alaska. Specifically, this action modifies Control 1234L in the immediate vicinity of the Saint Paul Island Airport, AK, by lowering the airspace floor from 2,000 feet above ground level (AGL) to 700 AGL. Additionally, outside the vicinity of the airport this action lowers the airspace floor from 2,000 AGL to 1,200 feet AGL within a 73-mile radius of the St. Paul Island Airport. The FAA is taking this action to provide additional controlled airspace for aircraft instrument flight rules (IFR) operations at the St. Paul Island Airport.
Modification of Offshore Airspace Area: Control 1487L; Alaska
Document Number: E6-8848
Type: Rule
Date: 2006-06-07
Agency: Federal Aviation Administration, Department of Transportation
This action modifies Control 1487L offshore airspace area in the vicinity of the Sitka Rocky Gutierrez Airport, Sitka, AK; Merle K. Mudhole Smith Airport, Cordova, AK; and Middleton Island Airport, Middleton Island, AK, by lowering the affected airspace floors associated within Control 1487L. The FAA is taking this action to provide additional controlled airspace for the safety of aircraft executing instrument flight rules (IFR) operations at the Sitka Rocky Gutierrez Airport, Merle K. Mudhole Smith Airport, and Middleton Island Airport.
Airworthiness Directives; Boeing Model 767-200 and -300 Series Airplanes
Document Number: E6-8823
Type: Proposed Rule
Date: 2006-06-07
Agency: Federal Aviation Administration, Department of Transportation
The FAA is revising an earlier proposed airworthiness directive (AD) for certain Boeing Model 767-200 and -300 series airplanes. For certain airplanes, the original NPRM would have required repetitive inspections for discrepancies of the tube assemblies and insulation of the metered fire extinguisher system and the bleed air duct couplings of the auxiliary power unit (APU) located in the aft cargo compartment; and corrective actions if necessary. For certain other airplanes, the original NPRM would have required a one-time inspection for sufficient clearance between the fire extinguishing tube and the APU bleed air duct in the aft cargo compartment, and modification if necessary. The original NPRM resulted from one report indicating that an operator found a hole in the discharge tube assembly for the metered fire extinguishing system; and another report indicating that an operator found chafing of the fire extinguishing tube against the APU duct that resulted in a crack in the tube. This action revises the original NPRM by expanding the applicability and adding an inspection for signs of chafing and to verify sufficient clearance between the fire extinguisher system and the bleed air duct couplings of the APU. We are proposing this supplemental NPRM to prevent fire extinguishing agent from leaking out of the tube assembly in the aft cargo compartment which, in the event of a fire in the aft cargo compartment, could result in an insufficient concentration of fire extinguishing agent, and consequent inability of the fire extinguishing system to suppress the fire.
Announcement of Policy for Landing Performance Assessments After Departure for All Turbojet Operators
Document Number: 06-5196
Type: Proposed Rule
Date: 2006-06-07
Agency: Federal Aviation Administration, Department of Transportation
The following advance notice of policy and information would provide clarification and guidance for all operators of turbojet aircraft for establishing operators' methods of ensuring that sufficient landing distance exists for safely making a full stop landing with an acceptable safety margin, on the runway to be used, in the conditions existing at the time of arrival, and with the deceleration means and airplane configuration to be used.
Establishment of Class E Airspace; Nicholasville, KY; Correction
Document Number: 06-5186
Type: Rule
Date: 2006-06-07
Agency: Federal Aviation Administration, Department of Transportation
This document contains a correction to the final rule (FAA- 2005-23075; 05-ASO-12), which was published in the Federal Register of February 28, 2006, (71 FR 9908), establishing Class E airspace at Nicholasville, KY. This action corrects an error in the geographic coordinates for the Class E5 airspace at Nicholasville, KY.
Amendment of Class D Airspace Pompano Beach; FL, Amendment of Class D Airspace, Fort Lauderdale Executive Airport, FL
Document Number: 06-5185
Type: Rule
Date: 2006-06-07
Agency: Federal Aviation Administration, Department of Transportation
This action will amend Class D airspace at Pompano Beach, FL and Fort Lauderdale Executive Airport, FL. As a result of the decommissioning of the Pompano Beach VHF Omnidirectional Range (VOR), the legal description for the Class D airspace at Pompano Beach, FL, and Fort Lauderdale Executive Airport, FL, must be changed.
Removal of Class D and E Airspace; Roosevelt Roads, PR Amendment of Class E Airspace; Isla de Vieques, PR
Document Number: 06-5184
Type: Rule
Date: 2006-06-07
Agency: Federal Aviation Administration, Department of Transportation
This action will remove the Class D and E airspace at Roosevelt Roads, PR, and amend the Class E airspace at Isla de Vieques, PR. The Roosevelt Roads Naval Station, Ofstie Field, PR, is permanently closed and no longer operational. The closure necessitates the removal of Class D and E airspace. The removal of Class E airspace at Roosevelt Roads, PR, requires the amendment of Class E airspace at Isla de Vieques, PR, since it is included as part of the Roosevelt Roads, PR, Class E airspace.
Proposed Establishment of Class E Airspace; Mooresville, NC
Document Number: 06-5183
Type: Proposed Rule
Date: 2006-06-07
Agency: Federal Aviation Administration, Department of Transportation
Proposed Establishment of Class E airspace at Mooresville, NC. An Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedure (SIAP) Runway (RWY) 14 has been developed for Lake Norman Airpark, As a result, controlled airspace extending upward from 700 feet Above Ground Level (AGL) is needed to contain the SIAP and for Instrument Flight Rules (IFR) operations at Lake Norman Airpark. The operating status of the airport will change from Visual Flight Rules (VFR) to include IFR operations concurrent with the publication of the SIAP.
Revision of Class E Airspace; Vandenberg AFB, CA
Document Number: 06-5159
Type: Rule
Date: 2006-06-07
Agency: Federal Aviation Administration, Department of Transportation
This action revises Class E airspace at Vandenberg AFB, CA. This airspace change places aircraft in controlled airspace from final descent to runway and protects Category E aircraft while conducting a circling approach to land.
Receipt of Noise Compatibility Program and Request for Review
Document Number: 06-5158
Type: Notice
Date: 2006-06-07
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 Fresno Yosemite International Airport (FAT) under the provisions of 40 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 city of Fresco, California. This program was submitted subsequent to a determination by FAA that associated noise exposure maps submitted under 14 CFR Part 150 for FAT were in compliance with applicable requirements, effective July 6, 2005 (70 FR 50437-50438). The proposed noise compatibility program will be approved or disapproved on or before November 22, 2006.
Airworthiness Directives; Boeing Model 747-100B, 747-200B, 747-200F, 747-300, 747-400, 747-400F, and 747SP Series Airplanes
Document Number: 06-5125
Type: Rule
Date: 2006-06-07
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain 747-100B, 747-200B, 747-200F, 747-300, 747-400, 747-400F, and 747SP series airplanes. This AD requires doing inspections of the midpivot bolt and midpivot bolt access door of the spring beam of the inboard side of the outboard struts for discrepancies, installing a placard on the midpivot bolt access door, and applicable corrective actions if necessary. This AD results from reports indicating that the midpivot bolt and midpivot bolt access door of the spring beam of the inboard side of the outboard struts were installed in the incorrect position. We are issuing this AD to ensure that the subject midpivot bolts and midpivot bolt access doors are installed in the correct position. If not installed in the correct position, a midpivot bolt could be overloaded and crack or fracture, which could result in the loss of the spring load path and consequent separation of the associated outboard strut and engine from the airplane.
Airworthiness Directives; Airbus Model A300 B4 Series Airplanes; Model A300 B4-600 Series Airplanes; Model A300 C4-605R Variant F Airplanes; Model A310-200 Series Airplanes; and Model A310-300 Series Airplanes
Document Number: 06-5122
Type: Rule
Date: 2006-06-07
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD), which applies to certain Airbus Model A300 B4-600 and A300 C4-600 series airplanes. That AD currently requires a one-time inspection to detect damage of the pump diffuser guide slots (bayonet) of the center tank fuel pumps, the pump diffuser housings, and the pump canisters; repetitive inspections to detect damage of the fuel pumps and the fuel pump canisters; and corrective action, if necessary. This new AD adds, for new airplanes, repetitive inspections of the pump bodies for cracking, damage, and missing and broken fasteners; repetitive inspections of the fuel pump canisters for a cracked flange web; and corrective actions if necessary. For all airplanes, this new AD also adds replacement of the fuel pump canisters with new reinforced fuel pump canisters, which ends the repetitive inspections. This AD results from fuel system reviews conducted by the manufacturer. We are issuing this AD to detect and correct damage of the center tank fuel pumps and fuel pump canisters, which could result in separation of a pump from its electrical motor housing, loss of flame trap capability, and a possible fuel ignition source in the center fuel tank.
Airworthiness Directives; Airbus Model A321-100 Series Airplanes
Document Number: 06-5121
Type: Rule
Date: 2006-06-07
Agency: Federal Aviation Administration, Department of Transportation
The FAA is revising an existing airworthiness directive (AD) that applies to certain Airbus Model A321-111, -112, and -131 airplanes. That AD currently requires repetitive inspections to detect fatigue cracking in the area surrounding certain attachment holes of the forward pintle fittings of the main landing gear (MLG) and the actuating cylinder anchorage fittings on the inner rear spar; and repair, if necessary. That AD also provides for optional terminating action for the repetitive inspections, adds inspections of three additional mounting holes, and revises the thresholds for the currently required inspections. We issued that AD to detect and correct fatigue cracking on the inner rear spar of the wings, which could result in reduced structural integrity of the airplane. This new AD retains the requirements and revises the applicability of that AD. This AD results from the discovery of a typographical error in the applicability of that AD, which could cause the unsafe condition on an affected airplane to remain uncorrected. We are issuing this AD to detect and correct fatigue cracking on the inner rear spar of the wings, which could result in reduced structural integrity of the airplane.
Airworthiness Directives; Boeing Model 737-300, -400, -500, -700, and -800 Series Airplanes; Model 747-400 and -400F Series Airplanes; Model 757-200 Series Airplanes; Model 767-300 Series Airplanes; and Model 777-300 Series Airplanes Equipped With Certain Driessen or Showa Galleys or Driessen Closets
Document Number: 06-5120
Type: Rule
Date: 2006-06-07
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Boeing transport category airplanes. This AD requires inspecting to determine if certain galleys and closets are installed, and replacing the spiral wire wrapping of the electrical cables of the galleys and closets with new spiral wire wrapping if necessary. This AD results from testing and reports from the manufacturer indicating unacceptable flammability properties of wire wrapping installed in certain galleys and closets. We are issuing this AD to prevent fire propagation or smoke in the cabin area due to electrical arcing or sparking and ignition of the spiral wire wrapping.