Content, scope and capabilities of different levels of maintenance and repair of aviation gas turbine engines of tactical aviation aircraft

Authors

DOI:

https://doi.org/10.54858/dndia.2025-21-29

Keywords:

aviation gas turbine engine (GTE), maintenance and repair (M&R) system, airworthiness.

Abstract

 

The airworthiness of aviation gas turbine engines (GTEs) used in tactical aviation is sustained through a comprehensive system of maintenance and repair (M&R). The paper investigates the content, scope, and functional capabilities of various M&R levels for aviation GTEs, focusing on a comparative assessment of two approaches: the classical Soviet hierarchical maintenance system applied to engines such as the RD-33, AL-31F, AL-21F-3T, and R-95Sh, and the three-level maintenance model used for Western engines such as the F100-PW-229 and F110-GE-129. The authors provide an analytical evaluation of the work composition at each M&R level, the scale of diagnostic and repair operations, personnel qualification requirements, material and technical support, and spare-parts logistics. It is demonstrated that the three-level maintenance architecture—with a significant role played by field repair units and specialized repair-diagnostic centers—ensures greater flexibility in allocating repair workloads, reduces aircraft downtime, and optimizes resource utilization while maintaining the required level of flight safety.

The paper also considers practical steps for integration, including standardization of technical documentation and terminology, upskilling of engineering and technical personnel, establishment of repair-diagnostic centers, definition of spare-parts requirements and logistics chains, and implementation of resource accounting and repair quality control systems. Recommendations are provided for optimizing cost and time during the transition to a modified M&R system, including phased introduction of diagnostic technologies, centralization of complex repair activities, and delegation of routine servicing tasks to lower echelons. It is emphasized that incorporating operational and maintenance experience from the F100 and F110 engine programs can enhance resource management efficiency and extend the service life of legacy Soviet-designed engines through the implementation of modern diagnostic methodologies and optimized logistics

References

Wong J. S. Whole life cost methods for aero-engine design. University of Southampton. http://eprints.soton.ac.uk/// 2012. 151p.

Kotlarz W., Królik M., Kolasa R. Influence of modular F100-PW-229 engine construction upon the fleet of F-16 aircraft exploitation. Journal of Polish CIMAC. - Gdansk Univercity of Technology. 2012. – p.p 36 – 42.

Технический отчет № 99.193.02 ОТ-88. Организация работ по восстановлению изделий 99В в условиях эксплуатирующих организаций. – Люберцы: в/ч 75360, 1988 – 28 с.

TO 00-25-257-1. Engine Health Management Plus (EHM+) User’s Manual. Instructions for Turbofan Engine model: F100-220. - Pratt&Witney, 2008 – 108 p.

Maletta P. NATO RTO: “Recommended Practices for Monitoring Gas Turbine Engine Life Consumption”, Appendix 1: US Military Engine Tracing and Operational Usage Metods, RTO-TR-28, (AC/323(AVT)TP/22), 2000. – pp. 142–144.

SZRAMA, S. F-16 turbofan engine monitoring system. Combustion Engines. 2019, 177(2), 23 - 35. DOI: 10.19206/CE-2019-205. – pp. 88–95.

Hocko M., Venceľ M., Divok M., Husťák M. General Electric F110-GE-129 Turbofan Engine. Acta Avionica. Volume XXV, 49 – No.2, 2023, DOI: 10.35116/aa.2023.0015. – pp. 102–110.

Davenport O. NATO RTO: “Recommended Practices for Monitoring Gas Turbine Engine Life Consumption”, RTO Technical Report 28, Appendix 2: Maintenance Policies and Procedures, RTO-TR-28, (AC/323(AVT)TP/22), 2000. – pp. 146–161.

NATO RTO Workshop on Life Management Techniques for Aging Engines; Aging Mechanisms and Control, Symposium B: Monitoring and Management of Gas Turbine Fleets for Extended Life and Reduced Costs, Symposium held in Manchester, UK, October 2001, RTO-MP-079(I), 2003. – pp. 153–166.

Engine Management and Tracking System. Southwest Research Institute. San Antonio, Texas. – p. 4.

Engine Structural Integrity Monitoring Requirements. Technical Airworthiness Authority, TAA Advisory 2016-02e, 2016, – рр. 137…155.

Самулєєв В.В. Методичний підхід щодо визначення накопиченої пошкодженості основними деталями ГТД військового призначення. Тези доповідей та виступів Міжнародної науково-практична конференцїя “Перспективи розвитку військової авіації. Кооперація підприємств авіаційної промисловості. – Київ: ДНДІА, 2016. – С. 79 – 80.

James Fellenstein. F100-PW-220/E/229 Engine Life Management Plan and Part Lifing Programs. 8th Israeli Symposium on Jet Engines and Gas Turbines. Nov. 2009, 17 р.

Szrama S., Kadziński A. Hazard identification process in the selected analysis domain of the F100 turbofan engines maintenance system. Combustion Engines. 2017, 171(4), 68-73. DOI: 10.19206/CE-2017-412 p.p 68 – 73.

Правила інженерно-авіаційного забезпечення державної авіації України (ПрІАЗ - 2016). – Київ: 2016 - 590 с.

Методические рекомендации группам диагностики, регламента и анализа авиадвигателей – Люберцы: в/ч 75360,. Вып. № 5300, 1984 - 20 с.

Смирнов Н. Н., Владимиров Н.И., Черненко Ж.С. и др. Техническая эксплуатация летательных аппаратов. – М.: Транспорт, 1990 – 423 с.

Published

2025-12-29

Issue

Section

Advanced technologies for the operation and repair of aircraft and weapons