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Standard Specification for Required Product Information to be Provided withWeight-Shift-Control Aircraft
Přeložit název
NORMA vydána dne 1.1.2018
Označení normy: ASTM F2457-05(2018)
Datum vydání normy: 1.1.2018
Kód zboží: NS-805188
Počet stran: 2
Přibližná hmotnost: 6 g (0.01 liber)
Země: Americká technická norma
Kategorie: Technické normy ASTM
The following requirements apply for the manufacture of weight-shift-control aircraft. This specification includes Aircraft Operating Instructions (AOI) and Flight Training Supplement (FTS) requirements for aircraft that were designed and manufactured in accordance with requirements. This specification covers the minimum requirements for information that shall be provided by the manufacturer or seller of new light sport aircraft, engines, or propellers as a part of the initial sale or transfer to the first-end user. The information given shall be included where applicable on the information plate. Each aircraft must include a set of aircraft operating instructions. Each aircraft shall have an MIP document provided for the aircraft that complies with an accepted standard. Each aircraft shall have an FTS that describes features, performance, and procedures unique to that aircraft model.
Keywords:
light sport aircraft, special airworthiness certificate, weight-shift-control aircraft,, ICS Number Code 49.020 (Aircraft and space vehicles in general)
1. Scope |
1.1 The following requirements apply for the manufacture of weight-shift-control aircraft. This specification includes Aircraft Operating Instructions (AOI) and Flight Training Supplement (FTS) requirements for aircraft that were designed and manufactured in accordance with ASTM Standards. 1.1.1 This specification covers the minimum requirements for information that shall be provided by the manufacturer or seller of new light sport aircraft, engines, or propellers as a part of the initial sale or transfer to the first-end user. 1.1.2 This specification does not apply to the sale or transfer of used light sport aircraft, engines, or propellers. 1.2 This specification applies to aircraft seeking civil aviation authority approval, in the form of flight certificates, flight permits, or other like documentation. 1.3 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use. 1.4 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee. |
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