This article reads the options for further quality improving of training for aviation personnel in higher education insti-tutions of the Russian Federation via introduction of innovative forms and methods of modernization of educational pro-cess in accordance with international educational standards of new generation.

The article considers methodological aspects of software processes management of the airworthiness of the aircraft, solving problems of the formation and correction of flexible programs of the airworthiness of the aircrafts taking into ac-count the actual operating conditions and the technical condition of the airline fleet.

Based on the reliability theory schemes of justifying the volume and structural principles of periodic maintenance (repair) of civil aircraft depending on operational conditions meeting the requirements on the failure-free operation, aircraft durability and flight safety are considered.

The article discusses aircraft fail-safe model formation aspects, the key tasks of reliability control and flight safety are pointed out together with failure mode effects and criticality analysis.

The paper deals with modeling of the processes of maintenance and repair of aircraft. The role of information in im-proving the effectiveness of maintenance systems is described. The methodology for functional modelling of maintenance processes is given. A simulation model is used for modelling possible changes.

This article deals with the assessment model of the quality of preventive maintenance of the means of radiotechnical flight support and telecommunications which is based on the evaluation of the availability while minimizing the discount-ed value of the analyzed processes.

A mathematical model of the processes of maintenance of aircraft engineering as a closed service system shoving their probability-statistic characteristics is constructed.

The article deals with the classical approaches to solving analytical problems associated with determining the value of diagnostic information introduced as different functional parameters of aviation equipment object.

This article considers efficiency assessment of the maintenance of onboard systems of aircraft based on suggested «ideal» model with a set of parameters, criteria and evaluation function.

The article describes a method of statistical modelling form the required amount of spare resource by the criterion of performance assurance of aircraft functionale systems for a long term operation. The calculations and the results of the statistical modelling are given.

This article describes an algorithm parameter optimization method for the diagnosis of GTD in order to devide zones of efficiency. The autor focuses on the retional combination of methods of mathematical analysis and statistics and de-veloping an algorithm that allows to optimize the use of mathematical methods by longitudinal data collection and ma-chine learning.

The article is devoted to the organization of ensuring problem how to obtain the uniformity of measurements at in-teragency testing of new generation of tribodiagnostics of aircraft GTE on the example of the x-ray spectrum analyzers. The article provides a synthesis of the obtained in testing results of measuring the concentration of products of wear pro-cess taking place in working oils, as well as recommendations and conclusions.

This article analyzes the international requirements being taken in to account when building a system of aviation specialists training whose activities are related to the sphere of aircraft airworthiness and aviation safety. The content of normative and technical documentation is considered, provisions related to the international standards requirements and a set of documents on the certification of aviation specialists training are analyzed.

The article considers the problem how to improve the evaluation of the efficiency of scientific-pedagogical activity of scientists working in dissertation councils with the help of integrated indicator of the effectiveness evaluation of scientific and pedagogical activity on the basis of a number of private indicators application.

This article discusses the pre-conditions for aircraft ground icing, the dynamics of traffic increase in the Russian avia-tion, the urgency of the problem and the ways and methods of it is solution and improvement of aircraft anti-icing protec-tion.

The article considers the ways of development and maintainance of training materials complex on the basis of the computerized training system. The basic types of test questions are defined and the technology of their formation in ac-cordance with subject matter of the training program of the course studied is presented. The article includes the technology of test questions development to be used in the laboratory work to find the reasons for hydraulic circuit failures on board Il-96-300.

Article considers methods of formation and argumentation of rough landing criteria based on the on-board MSRP-A-02 recorder data with an example of IL-76TD with PS-90A-76 gas-turbine engines. The volume of reliable information development on aircraft in-flight parameters and its maximum load factors on landing with different degree of roughness has been defined. The results of load quantity simulation have been analyzed.

The articles provides the results of the research on the development of the load condition mode selection for acceler-ated testing of the hydraulic system pipelines durability, taking into account the results of zero loading technique providing the adequacy to the actual process of leading to fatigue cracks and material destruction.

The article considers the physical nature of the ultrasonic cleaning of small-capillary filtering elements of hydraulic and fuel systems of modern aircraft. The physical nature of filtering elements cleaning processes is the influence of the detergent liquid of gas bubbles in the oscillation frequency the unilateral gas diffusion on effectiveness of and on the flow of the filtering elements viscoplastic contamination layer.

Considers new methods to improve the fuel efficiency in opperation of civil aircraft, based on the reduction ground work time of aircraft engines, reducing take-off weight. Experimental data and assessment of these methods.

The article shows algorithm of solving problems in calculating work of force applied to the floating point in a solid. A theorem proof is provided calculating power of such a force. The use of the theorem and its consequence is shown on some examples.

The article presents a method of screening caps crew of engine rotors. In the absence of data on the amount of elon-gation for coupling bolts after a few repairs, a method of fault detection through caps crew on the magnitude of its reduc-tion.

The article is devoted to the methodology of metrological assurance during of operational test of the new-gen ground-based automated control of system. On the example of ATE-200, designed to measure the parameters (to diagnose) onboard means of control and other aircraft equipment. The basic test results have been summarized and presented.