Federal Aviation Administration June 25, 2009 – Federal Register Recent Federal Regulation Documents

Airworthiness Directives; DORNIER LUFTFAHRT GmbH Models 228-100, 228-101, 228-200, 228-201, and 228-202 Airplanes
Document Number: E9-14994
Type: Proposed Rule
Date: 2009-06-25
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 777 Series Airplanes
Document Number: E9-14991
Type: Proposed Rule
Date: 2009-06-25
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for all Boeing Model 777 series airplanes. This proposed AD would require inspections for scribe lines in the skin along lap joints, butt joints, certain external doublers, and the large cargo door hinges; and related investigative and corrective actions if necessary. This proposed AD results from reports of scribe lines found at lap joints and butt joints, around external doublers, and at locations where external decals had been cut. We are proposing this AD to detect and correct scribe lines, which can develop into fatigue cracks in the skin. Undetected fatigue cracks can grow and cause sudden decompression of the airplane.
Approval of Noise Compatibility Program 14 CFR Part 150; General Mitchell International Airport, Milwaukee, WI
Document Number: E9-14988
Type: Notice
Date: 2009-06-25
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) announces its findings on the noise compatibility program (NCP) submitted by General Mitchell International Airport 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). The General Mitchell International Airport noise exposure maps were determined by FAA to be in compliance with applicable requirements on December 24, 2008. Notice of this determination was published in the Federal Register on January 15, 2009, Federal Register volume 74, number 10, page 2645.
Eighth Plenary Meeting, NextGen Mid-Term Implementation Task Force
Document Number: E9-14987
Type: Notice
Date: 2009-06-25
Agency: Federal Aviation Administration, Department of Transportation
The FAA is issuing this notice to advise the public of a meeting of the NextGen Mid-Term Implementation Task Force.
Approval of Noise Compatibility Program 14 CFR Part 150; Detroit Metropolitan Wayne County Airport, Detroit, MI
Document Number: E9-14986
Type: Notice
Date: 2009-06-25
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) announces its findings on the noise compatibility program (NCP) submitted by Wayne County 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). The Detroit Metropolitan Wayne County Airport noise exposure maps were determined by FAA to be in compliance with applicable requirements on March 7, 2006. Notice of this determination was published in the Federal Register on March 21, 2006, Federal Register volume 71, number 54, page 14282.
Airworthiness Directives; Pratt & Whitney (PW) JT9D-7 Series Turbofan Engines; Correction
Document Number: E9-14810
Type: Rule
Date: 2009-06-25
Agency: Federal Aviation Administration, Department of Transportation
The FAA is correcting airworthiness directive (AD) 2009-04-18, which was previously published in the Federal Register. That AD applies to PW models JT9D-7, -7A, -7AH, -7H, -7F, and -7J turbofan engines. The two references to the engine manual in paragraph (h) and in Table 1, are incomplete. This document corrects those references. In all other respects, the original document remains the same.
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