Federal Aviation Administration September 2, 2009 – Federal Register Recent Federal Regulation Documents
Results 1 - 9 of 9
Airworthiness Directives; SOCATA Model TBM 700 Airplanes
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:
Government/Industry Aeronautical Charting Forum Meeting
This notice announces the hi-annual meeting of the Federal Aviation Administration (FAA) Aeronautical Charting Forum (ACF) to discuss informational content and design of aeronautical charts and related products, as well as instrument flight procedures development policy and design criteria.
Advisory Circular 33.70-1, Guidance Material for Aircraft Engine Life-Limited Parts Requirements
This notice announces the issuance of Advisory Circular (AC) 33.70-1, Guidance Material for Aircraft Engine Life-limited Parts Requirements. This AC provides definitions, guidance, and acceptable methods that may be used to demonstrate compliance with the engine life-limited parts integrity requirements of Sec. 33.70 of Title 14 of the Code of Federal Regulations. Section 33.70 contains requirements applicable to the design and life management of propulsion system life- limited parts including high-energy rotating parts.
Advisory Circular 33-8, Guidance for Parts Manufacturer Approval of Turbine Engine and Auxiliary Power Unit Parts Under Test and Computation
This notice announces the issuance of Advisory Circular (AC) 33-8, Guidance for Parts Manufacturer Approval of Turbine Engine and Auxiliary Power Unit Parts under Test and Computation. This AC provides guidance for developing substantiation data to support the design approval of critical and complex turbine engine and auxiliary power unit (APU) parts produced under parts manufacturer approval. This guidance is for the comparative test and analysis method used to show compliance to the airworthiness requirements under test and computation, per S21.303 of Title 14 of the Code of Federal Regulations (14 CFR). This method supports showing the engine or APU still complies with 14 CFR part 33 and Technical Standard Order (TSO) C77.
Notice of Intent To Rule on Request To Release Airport Property at the Brigham City Municipal Airport, Brigham City, UT
The FAA proposes to rule and invite public comment on the release of land at the Brigham City Municipal Airport under the provisions of Section 125 of the Wendell H. Ford Aviation Investment Reform Act for the 21st Century (AIR 21).
Notice of Intent to Request Approval from the Office of Management and Budget of a New Information Collection Activity, Request for Comments; Aeronautical Chart Point of Sale Survey
The FAA invites public comments about our intention to request the Office of Management and Budget (OMB) to approve a new information collection. Aeronautical Chart Point of Sale Survey data will be used by the Federal Aviation Administration to measure management objectives and analyze customer feedback for ISO-9001.
Airworthiness Directives; BAE Systems (Operations) Limited Model BAe 146-100A and 146-200A Series Airplanes
The FAA is correcting a typographical error in an existing airworthiness directive (AD) that was published in the Federal Register on July 29, 2009. The error resulted in an incorrect AD number appearing in one location of the document. This AD applies to certain BAE Systems (Operations) Limited Model BAe 146-100A and 146-200A series airplanes. This AD requires inspecting for damage of the horizontal stabilizer lower skin and joint plates, and doing related investigative and corrective actions.
Airworthiness Standards; Aircraft Engine Standards Overtorque Limits
This rule will amend the certification standards for aircraft engines to establish requirements for approval of maximum engine overtorque. Specifically, this action will add a new engine overtorque test, amend engine ratings and operating limits, and define maximum engine overtorque for certain turbopropeller and turboshaft engines. The rule will harmonize applicable United States (U.S.) and European standards and simplify airworthiness approvals for import and export of aircraft engines.
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