Federal Aviation Administration September 2007 – Federal Register Recent Federal Regulation Documents

Results 101 - 116 of 116
Establishment of Class E Airspace; Lady Lake, FL
Document Number: 07-4326
Type: Rule
Date: 2007-09-07
Agency: Federal Aviation Administration, Department of Transportation
This action established Class E airspace at Lady Lake, FL, to accommodate a new Standard Instrument Approach Procedure (SIAP) helicopter point in space approach that has been developed for Lady Lake Hospital. Controlled airspace extending upward from 700 feet Above Ground Level (AGL) is needed to contain the SIAP.
Amendment to Class E Airspace; Lee's Summit, MO
Document Number: 07-4323
Type: Rule
Date: 2007-09-07
Agency: Federal Aviation Administration, Department of Transportation
This action amends the Class E airspace area at Lee's Summit Municipal Airport, Lee's Summit, MO. A review of the legal description revealed an incorrect coordinate describing the Airport Reference Point (ARP) for Lee's Summit Municipal Airport. This action corrects that error.
Proposed Establishment of Class E5 Airspace; Prairie Du Sac, WI
Document Number: 07-4285
Type: Proposed Rule
Date: 2007-09-07
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish Class E airspace at Prairie Du Sac, WI. Additional controlled airspace is necessary to accommodate aircraft using a new Area Navigation (RNAV) Global Positioning System (GPS) Instrument Approach Procedure (IAP) at Sauk-Prairie Airport. The FAA is proposing this action to enhance the safety and management of aircraft operations at Sauk-Prairie Airport, Prairie Du Sac, WI.
Airworthiness Standards; Aircraft Engine Standards for Pressurized Engine Static Parts
Document Number: E7-17626
Type: Proposed Rule
Date: 2007-09-06
Agency: Federal Aviation Administration, Department of Transportation
The FAA is proposing to amend the aircraft engine type certification standards by adding standards for pressurized engine static parts that are equivalent to those already adopted by European Aviation Safety Agency (EASA). The proposed rule would establish uniform standards for the certification of these parts in the United States and in Europe. U.S. manufacturers already meet the EASA requirements.
Airworthiness Directives; Boeing Model 737-600, -700, -700C, -800, and -900 Series Airplanes
Document Number: E7-17586
Type: Proposed Rule
Date: 2007-09-06
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for all Boeing Model 737-600, -700, -700C, -800, and -900 series airplanes. This proposed AD would require a one-time inspection to determine the material of the forward and aft gray water drain masts. For airplanes having composite gray water drain masts, this proposed AD would also require installation of a copper bonding jumper between a ground and the clamp on the tube of the forward and aft gray water composite drain masts. This proposed AD results from a report of charred insulation blankets and burned wires around the forward gray water composite drain mast found during an inspection of the forward cargo compartment on a Model 767-300F airplane. We are proposing this AD to prevent a fire near a composite drain mast and possible disruption of the electrical power system caused by a lightning strike on a composite drain mast, which could result in the loss of several functions essential for safe flight.
Airworthiness Directives; Airbus Model A318, A319, A320, and A321 Airplanes
Document Number: E7-17385
Type: Rule
Date: 2007-09-06
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD), which applies to all Airbus Model A318-100, A319-100, A320-200, A321-100, and A321-200 series airplanes, and Model A320-111 airplanes. That AD currently requires an inspection to determine whether certain braking and steering control units (BSCUs) are installed or have ever been installed. For airplanes on which certain BSCUs are installed or have ever been installed, the existing AD requires an inspection of the nose landing gear (NLG) upper support, and corrective action if necessary; and a check of the NLG strut inflation pressure, and an adjustment if necessary. For some of these airplanes, the existing AD also requires a revision to the aircraft flight manual to incorporate an operating procedure to recover normal steering in the event of a steering failure. This new AD instead requires repetitive inspections of the NLG upper support, and related investigative/corrective actions in accordance with new service information; and removes the one-time inspection that was required by the existing AD. This new AD also provides an optional terminating action for the repetitive inspections. This AD results from a report of an incident where an airplane landed with the NLG turned 90 degrees from centerline, and from additional reports of NLG upper support anti-rotation lugs rupturing in service. We are issuing this AD to prevent landings with the NLG turned 90 degrees from centerline, which could result in reduced controllability of the airplane.
Standard Instrument Approach Procedures; Miscellaneous Amendments
Document Number: E7-17359
Type: Rule
Date: 2007-09-06
Agency: Federal Aviation Administration, Department of Transportation
This rule amends Standard Instrument Approach Procedures (SIAPs) for operations at certain airports. These regulatory actions are needed because of changes in the National Airspace System, such as the commissioning of new navigational facilities, adding of new obstacles, or changing air traffic requirements. These changes are designed to provide safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.
Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous Amendments
Document Number: E7-17345
Type: Rule
Date: 2007-09-06
Agency: Federal Aviation Administration, Department of Transportation
This Rule establishes, amends, suspends, or revokes Standard Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums and Obstacle Departure Procedures for operations at certain airports. These regulatory actions are needed because of the adoption of new or revised criteria, or because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, adding new obstacles, or changing air traffic requirements. These changes are designed to provide safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.
Airworthiness Directives; Piaggio Aero Industries S.p.A. Model P-180 Airplanes
Document Number: E7-17304
Type: Rule
Date: 2007-09-06
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued 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; Avions Marcel Dassault-Breguet Model Falcon 10 Airplanes
Document Number: E7-17288
Type: Rule
Date: 2007-09-06
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD), which applies to all Avions Marcel Dassault-Breguet Model Falcon 10 airplanes. That AD currently requires either revising the airplane flight manual (AFM) and installing a placard in the flight deck to prohibit flight into known or forecasted icing conditions, or repetitively inspecting for delamination of the flexible hoses in the wing (slat) anti-icing system and performing corrective actions if necessary. That AD also provides optional terminating action for the repetitive inspections. This new AD mandates the previously optional terminating action. This AD results from a report of in-service delamination of a flexible hose in the slat anti-icing system at a time earlier than previously reported. We are issuing this AD to prevent collapse of the flexible hoses in the slat anti-icing system, which could lead to insufficient anti-icing capability and, if icing is encountered in this situation, could result in reduced controllability of the airplane.
Proposed Establishment of Class D and E Airspace, Proposed Revision of Class E Airspace; Easton, MD
Document Number: 07-4330
Type: Proposed Rule
Date: 2007-09-06
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish Class D, E2 and E4 airspace and revise E5 airspace at Easton, MD. A federal contract tower with a weather reporting system is being constructed at Easton Airport/Newnam Field. Therefore, the airport will meet criteria for Class D, E2, and E4 surface area airspace. Class D surface area airspace and Class E4 airspace designed as an extension to Class D airspace is required when the control tower is open to contain Standard Instrument Approach Procedures (SIAPs) and other Instrument Flight Rules (IFR) operations at the airport. Class E2 surface area airspace is required when the control tower is closed to contain SIAPs and other IFR operations at the airport. This action would establish Class D and E2 airspace extending upward from the surface to and including 2,600 feet MSL within a 4-mile radius of the airport and Class E4 airspace extension that is 5.4 miles wide and extends 7.4 miles northeast of the Easton Non Directional Beacon (NDB). Additionally, a technical revision to Class E5 airspace is required as a result of a name change from the Easton Municipal Airport to Easton Airport/Newnam Field, which was effective May 25, 1993.
Notice of Intent To Rule on Request To Release Airport Property at Oceano Airport, Oceano, CA
Document Number: 07-4325
Type: Notice
Date: 2007-09-06
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) proposes to rule and invites public comment on the release of 2.43 acres of land at the Oceano Airport, Oceano, California, from all the conditions in the grant agreements under the provisions of Section 125 of the Wendell H. Ford Aviation Investment Reform Act for the 21st Century (AIR 21), now 49 U.S.C. 47107(h)(2). The land will be sold to the San Luis Obispo County Sanitation District and used for commercial purposes by the District for purposes compatible with the airport.
FAA Approval of Noise Compatibility Program; Rickenbacker International Airport, Columbus, OH
Document Number: 07-4322
Type: Notice
Date: 2007-09-06
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) announces its findings on the noise compatibility program submitted by Columbus Regional Airport authority under the provisions of 49 U.S.C. (the Aviation Safety and Noise Abatement Act, hereinafter referred to as ``the Act'') and 14 CFR part 150. These findings are made in recognition of the description of Federal and nonfederal responsibilities in Senate Report No. 96-52 (1980). On January 25, 2007, the FAA determined that the noise exposure maps submitted by Columbus Regional Airport Authority under Part 150 were in compliance with applicable requirements. On July 9, 2007, the FAA approved the Rickenbacker International Airport noise compatibility program. All of the recommendations of the program were approved.
Airworthiness Directives; Honeywell International Inc. TFE731-2C, -3B, -3BR, -3C, -3CR, -3D, -3DR, -4R, -5AR, -5BR, -5R, -20R, -20AR, -20BR, -40, -40AR, -40R, and -60 Series Turbofan Engines
Document Number: E7-17384
Type: Proposed Rule
Date: 2007-09-04
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for Honeywell International Inc. (Honeywell) TFE731-2C, -3B, -3BR, -3C, -3CR, -3D, -3DR, -4R, -5AR, -5BR, -5R, -20R, -20AR, -20BR, -40, -40AR, -40R, and -60 series turbofan engines. This proposed AD would require removal from service of certain high pressure (HP) turbine rotor assemblies with part numbers (P/Ns) 3075772-1 and 3060841-1 using a drawdown schedule, and returning them to Honeywell for curvic root radius inspection. This proposed AD results from the manufacturer's report that some HP turbine rotor discs received improperly machined radii in the root of the forward and aft curvic teeth during manufacture. We are proposing this AD to prevent uncontained failure of the HP turbine rotor assembly and damage to the airplane.
Airworthiness Standards: Safety Analysis
Document Number: E7-17372
Type: Rule
Date: 2007-09-04
Agency: Federal Aviation Administration, Department of Transportation
The FAA is amending the safety analysis type certification standard for turbine aircraft engines. This rule establishes a nearly uniform safety analysis standard for turbine aircraft engines certified in the United States under part 33 and in European countries under the Certification Specifications for Engines, thereby simplifying airworthiness approvals for import and export.
Airworthiness Standards; Aircraft Engine Standards for Engine Life-Limited Parts
Document Number: E7-17369
Type: Rule
Date: 2007-09-04
Agency: Federal Aviation Administration, Department of Transportation
The FAA is amending the certification standards for original and amended type certificates for aircraft engines by modifying the standards for engine life-limited parts. This final rule establishes new and uniform standards for the design and testing of life-limited parts for aircraft engines certificated by the FAA and the European Aviation Safety Agency (EASA). This rule retains the current lifing requirements, introduces damage tolerance requirements into the design process, and strengthens cooperation between engineering, manufacturing, and service elements of turbine engine manufacturers. These new requirements provide an added margin of safety and will reduce the number of life-limited parts failures due to material, manufacturing, and service induced anomalies. Additionally, this action adds new standards for the design of reciprocating engine turbocharger rotors.