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Extended diversion time operations, configuration, maintenance and procedures (CMP) standard. The particular aeroplane configuration minimum requirements including any special inspection, hardware life limits, master minimum equipment list (MMEL) constraints, and maintenance practices found necessary to establish the suitability of an airframe-engine combination for extended diversion time operation.
Equivalent level of safety. As used in type certification, a finding where literal compliance with a specific airworthiness requirement cannot be demonstrated but compensating factors exist in the type design that can be shown to provide a level of safety equivalent to that intended by the certification basis.
Failure condition. The effect on the aircraft and its occupants, both direct and consequential, caused or contributed to by one or more failures, considering relevant adverse operational or environmental conditions.
Instructions for continued airworthiness. A set of descriptive data, maintenance planning and accomplishment instructions, developed by a design approval holder in accordance with the certification basis for the product, providing operators with the necessary information for development of their own maintenance programme and accomplishment instructions.
Latent failure. A failure that is not detected and/or enunciated when it occurs.
Life-limited part. Any part for which a retirement time, service life limitation, part retirement, retirement life limitation or life limitation exists, and is permanently removed from service when its operating limit (hours, cycles or calendar time) is exceeded.
Major modification. In respect of an aeronautical product for which a Type Certificate has been issued, a change in the Type Design that has an appreciable effect, or other than a negligible effect, on the mass and balance limits, structural strength, powerplant operation, flight characteristics, reliability, operational characteristics, or other characteristics or qualities affecting the airworthiness or environmental characteristics of an aeronautical product.
Minor modification. A modification other than a major modification.
Propulsion system. A system consisting of an engine, all ancillary parts installed on the engine, and all other equipment utilized to provide those functions necessary to sustain, monitor and control the power/thrust output of any one engine following installation on the airframe.
Special conditions of airworthiness. The technical requirements added to the certification basis as a consequence of novel or unusual design feature(s) that exists in a type design and the absence or inadequacy of the applicable airworthiness standards to provide a basis for the certification of such features.
Type design. The set of data and information necessary to define a product type for the purpose of airworthiness determination to any later product of the same type.
PART II.— AIRWORTHINESS ORGANIZATION:
STRUCTURE AND RESPONSIBILITIES OF STATES
CHAPTER 1. AIRWORTHINESS RESPONSIBILITIES OF THE STATE
1.1 The Convention on International Civil Aviation
1.1.1 The Convention on International Civil Aviation was signed in Chicago in 1944, and it created the International Civil Aviation Organization (ICAO), which in 1947 became a specialized Organization of the United Nations. The Convention focuses on international civil aviation. It does not necessarily apply to domestic operations, but provides an accepted model for the regulation of civil aviation, and it is sensible for States to have one set of rules that cover both domestic and international aviation. Thus the ICAO Standards apply to international aviation and have a de facto application to domestic aviation.
1.1.2 Article 5 of the Convention provides for all Contracting States, subject to specific conditions, to allow aircraft from other Contracting States to make flights into or across the territory of all Contracting States, unless engaged in scheduled international air services, and to make stops for non-traffic purposes, without prior approval of the Contracting State.
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本文链接地址:适航手册 AIRWORTHINESS MANUAL(6)