ASTM F2425 REV A Standard Specification for Continued Airworthiness System for Weight-Shift-Control Aircraft
Данный раздел/документ содержится в продуктах:
- Техэксперт: Машиностроительный комплекс
- Картотека зарубежных и международных стандартов
- ASTM F3060 REV A Standard Terminology for Aircraft
- ASTM F2245 Standard Specification for Design and Performance of a Light Sport Airplane
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- ASTM F2245 Standard Specification for Design and Performance of a Light Sport Airplane
- 49.020
- ASTM F2972 Standard Specification for Light Sport Aircraft Manufacturer’s Quality Assurance System
- ASTM F3060 REV B Standard Terminology for Aircraft
- ASTM F2972 Standard Specification for Light Sport Aircraft Manufacturer’s Quality Assurance System
- ASTM F2930 Standard Guide for Compliance with Light Sport Aircraft Standards
- ASTM F2295 Standard Practice for Continued Operational Safety Monitoring of a Light Sport Aircraft
- ASTM F2930 Standard Guide for Compliance with Light Sport Aircraft Standards
- ASTM F3035 Standard Practice for Production Acceptance in the Manufacture of a Fixed Wing Light Sport Aircraft
- ASTM F3060 Standard Terminology for Aircraft
- Картотека зарубежных и международных стандартов
ASTM International
Standard Specification for Continued Airworthiness System for Weight-Shift-Control Aircraft
N F2425 REV A
Annotation
The following continued airworthiness requirements apply for the manufacture of weight-shift-control aircraft and their qualification for possible certification.
This specification applies to aircraft seeking civil aviation authority approval, in the form of flight certificates, flight permits, or other like documentation.
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 and health practices and determine the applicability of regulatory requirements prior to use.
Автоматический перевод:
Стандартная спецификация для поддержавшей летную годность системы для самолета управления изменения веса
Следующий поддержал летную годность, требования просят производство самолета управления изменения веса и их квалификации для возможной сертификации.
Эта спецификация применяется к самолету, ища одобрение управления гражданской авиации, в форме сертификатов полета, разрешений на полет или другого как документация.
