Federal Aviation Administration June 21, 2010 – Federal Register Recent Federal Regulation Documents

Airworthiness Directives; Robert E. Rust, Jr. Model DeHavilland DH.C1 Chipmunk 21, DH.C1 Chipmunk 22, and DH.C1 Chipmunk 22A Airplanes
Document Number: 2010-14989
Type: Proposed Rule
Date: 2010-06-21
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for all Robert E. Rust, Jr. Model DeHavilland DH.C1 Chipmunk 21, DH.C1 Chipmunk 22, and DH.C1 Chipmunk 22A airplanes. This proposed AD would require a one-time inspection of the flap operating system for an unauthorized latch plate design installation. This proposed AD results from a report of a latch plate failing in service that was not made in accordance with the applicable de Havilland drawing. We are proposing this AD to detect and correct unauthorized latch plate design installation, which could result in an un-commanded retraction of the flaps. This failure could lead to a stall during a landing approach.
Airworthiness Directives; GA 8 Airvan (Pty) Ltd Models GA8 and GA8-TC320 Airplanes
Document Number: 2010-14986
Type: Proposed Rule
Date: 2010-06-21
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for the products listed above that would revise an existing AD. 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: Inspection of a high time aircraft has revealed cracks in the Horizontal Stabilizer rear spar splice plate and inboard main ribs around the area of the Horizontal Stabilizer rear pivot attachment. Additionally, failure of some attach bolts in service may be due to improper assembly. This amendment is issued to include an applicability matrix (Table 1, page 2) in the compliance section of the service bulletin for improved clarity. The
Existence of Proposed Airworthiness Design Standards for Acceptance Under the Primary Category Rule; Orlando Helicopter Airways (OHA), Inc., Models Cessna 172I, 172K, 172L, and 172M
Document Number: 2010-14975
Type: Proposed Rule
Date: 2010-06-21
Agency: Federal Aviation Administration, Department of Transportation
This notice announces the existence of and requests comments on the proposed airworthiness design standards for acceptance of the OHA, Inc., Models Cessna 172I, 172K, 172L, and 172M airplanes under the regulations for primary category aircraft.
Approval of Noise Compatibility Program for Buckeye Municipal Airport, Town of Buckeye, AZ
Document Number: 2010-14971
Type: Notice
Date: 2010-06-21
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) announces its findings on the noise compatibility program submitted by the Town of Buckeye under the provisions of 49 U.S.C. 47501 et seq. (formerly the Aviation Safety and Noise Abatement Act, hereinafter referred to as ``the Act'') and 14 Code of Federal Regulations (CFR) Part 150 (hereinafter referred to as ``Part 150''). On September 22, 2008, the FAA determined that the noise exposure maps submitted by the Town of Buckeye under Part 150 were in compliance with applicable requirements. On May 13, 2010, the FAA approved the Buckeye Municipal Airport noise compatibility program. All of the recommendations of the program were approved.
Airworthiness Directives; CFM International, S.A. CFM56-5, -5B, and -7B Series Turbofan Engines
Document Number: 2010-14819
Type: Rule
Date: 2010-06-21
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for CFM International, S.A. CFM56-5, -5B, and -7B series turbofan engines. This AD requires removing from service, nine stage 3 low-pressure turbine (LPT) disks, identified by serial number (S/N). This AD results from the discovery of a material nonconformity requiring removal of the disk before the certified disk life of certain stage 3 LPT disks. We are issuing this AD to prevent uncontained failure of the stage 3 LPT disk and damage to the airplane.
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