![]() ![]() Amendment 33-13, published in the Federal Register dated August 18, 1989, is part of a larger reorganisation of the general U.S. In addition, the following amendments to the United States Code of Federal Regulations, Title 14, Chapter 1, Part 33 are included in the FAR text (left column) for completeness: Chapter 516, Second Edition Subchapter B. the Air Regulation enabling the type approval of aeronautical products and Chapter 511 and This change introduces an amendment to section 533.1 paragraph (b) to refer to: The Canadian standards bear the same number as the FAR equivalent, prefixed by the number “5”, as this chapter contains the standards for Part V of the Canadian Aviation Regulations (CARs). These United States airworthiness standards have been used and adapted as the model for the Canadian standards supplemented by additional airworthiness requirements based on Canadian experience and required for Canadian aviation purposes. The content of this chapter is based on the United States Code of Federal Regulations, Title 14, Chapter I, Part 33 entitled Airworthiness Standards, Aircraft Engines. (b) the word “approved” or “authorised”, when used without an indication of a method of approval or authorisation, is to be interpreted as referring to an approval or an authorisation granted under the Aeronautics Act.(a) The passages giving the Minister power to determine, approve, establish or authorise something without stating criteria for the use of such power are to be interpreted as requiring that the power be used in consideration of two factors only: the airworthiness of the aircraft that is the subject of the determination, approval or authorisation, or on which an aeronautical product that is the subject of the determination, approval or authorisation is to be installed, and the aircraft's level of safety.Last amendment to chapter: 8 Interpretation Provision for Part V Standards Appendix D - Mixed Phase and Ice Crystal Icing Envelope (Deep Convective Clouds).Appendix B - Certification Standard Atmospheric Concentrations of Rain and Hail.Appendix A - Instructions for Continued Airworthiness.533.201 - Design and Test Requirements for Early ETOPS Eligibility.Subchapter G - Special Requirements: Turbine Aircraft Engines.533.99 - General Conduct of Block Tests.533.96 - Engine Tests in Auxiliary Power Unit (APU) Mode.533.95 - Engine-Propeller Systems Tests.533.94 - Blade Containment and Rotor Unbalance Tests.533.91 - Engine System and Component Tests.533.90 - Initial Maintenance Inspection.Subchapter F - Block tests Turbine Aircraft Engines.533.77 - Foreign Object Ingestion - Ice.533.64 - Pressurized Engine Static Parts.Subchapter E - Design and Construction Turbine Aircraft Engines.533.57 - General Conduct of Block Tests.533.53 - Engine System and Component Tests.Subchapter D - Block tests Reciprocating Aircraft Engines.Subchapter C - Design &Construction Reciprocating Aircraft Engines.533.27 - Turbine, Compressor, Fan and Turbosupercharger Rotors Overspeed.533.23 - Engine Mounting Attachments and Structure.Subchapter B - Design &Construction : General.533.8 - Selection of Engine Power and Thrust Ratings.533.7 - Engine Ratings &Operating Limitations.533.5 - Instruction Manual for Installing and Operating the Engine.533.4 - Instructions for Continued Airworthiness.Interpretation Provision for Part V Standards. ![]()
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