On the base of the relevant as well as available resources, it can be stated that the maintenance flexibility depends on various factors, mainly connected with aircraft structure and maintenance system; such as; units accessibly, part replacement, utilisation of already existing means (power generators, fuel distributors, cranes, jacks etc instead of delivery of new ones), frequency and scope of the aircraft maintenance works and safety at works. A selected group of aircraft was evaluated. All the mentioned factors were implemented into analyses. The matrix evaluation method was used for evaluation and comparison.
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