Method of estimation of characteristics losses of aircraft airworthiness

Authors

  • С. А. Ищенко Национальный авиационный университет
  • А. Р. Давидов Национальный авиационный университет

DOI:

https://doi.org/10.18372/2306-1472.7.11266

Abstract

Proposed is a new method of separation of degradation degree of characteristics of engine a&: airplane of a transport aircraft according to the results of interpretation of flight informatics registrated by regular airborne storage during regular flight. Demonstrated is actuality of the proposed method for maintaining airworthiness in accordance with ICAO recommendations. Given are the results of calculations of airplane and engine degradation degree received by means of aircraft Ил-86 flight mathematical model

References

Руководство по организации работ в области летной годности. ИКАО,- Док. 9389- АШ919.

Международный стандарт. Летная годность воздушных судов. Приложение 8 к конвенции о международной гражданской авиации. - Монреаль, 1988.

Ищенко С.А. Методика определения индивидуальных особенностей ВС по данным бортовых систем регистрации полетной информации // Вісник КМУЦА. - 1998. -Вып. 1. - С.88-92.

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How to Cite

Ищенко, С. А., & Давидов, А. Р. (2000). Method of estimation of characteristics losses of aircraft airworthiness. Proceedings of National Aviation University, 7(3-4), 67–72. https://doi.org/10.18372/2306-1472.7.11266

Issue

Vol. 7 No. 3-4 (2000)

Section

AIRPORTS AND THEIR INFRASTRUCTURE

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