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Quantifying human-centric uncertainty in aircraft maintenance

Published online by Cambridge University Press:  29 August 2025

D. Yiannakides*
Affiliation:
School of Sciences and Engineering, University of Nicosia, Nicosia, Cyprus
D. Drikakis
Affiliation:
School of Sciences and Engineering, University of Nicosia, Nicosia, Cyprus
C. Sergiou
Affiliation:
Department of Computer Science and Engineering, European University Cyprus, Nicosia, Cyprus
*
Corresponding author: D. Yiannakides; Email: yiannakides@gmail.com
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Abstract

Human-centric uncertainty remains one of the most persistent yet least quantified sources of risk in aviation maintenance. Although established safety frameworks such as SMS (safety management system), STAMP (Systems-Theoretic Accident Model and Processes), and FRAM (Functional Resonance Analysis Method) have advanced systemic oversight, they fall short in capturing the dynamic, context-dependent variability of human performance in real time. This study introduces the uncertainty quantification in aircraft maintenance (UQAM) framework – a novel, predictive safety tool designed to measure and manage operational uncertainty at the task level. The integrated uncertainty equation (IUE) is central to the model, a mathematical formulation that synthesises eight empirically derived uncertainty factors into a single, actionable score. Using a mixed-methods design, the research draws on thematic analysis of 49 semi-structured interviews with licensed maintenance engineers, followed by a 12-month field validation across four distinct maintenance tasks. Results demonstrate that the IUE effectively distinguishes between low, moderate and high-risk scenarios while remaining sensitive to procedural anomalies, diagnostic ambiguity and environmental complexity. Heatmap visualisations further enable supervisory teams to identify dominant uncertainty drivers and implement targeted interventions. UQAM enhances predictive governance, supports real-time decision-making and advances the evolution of next-generation safety systems in high-reliability aviation environments by embedding quantitative uncertainty metrics into existing safety architectures.

Information

Type
Research Article
Creative Commons
Creative Common License - CCCreative Common License - BYCreative Common License - NCCreative Common License - SA
This is an Open Access article, distributed under the terms of the Creative Commons Attribution-NonCommercial-ShareAlike licence (https://creativecommons.org/licenses/by-nc-sa/4.0/), which permits non-commercial re-use, distribution, and reproduction in any medium, provided the same Creative Commons licence is used to distribute the re-used or adapted article and the original article is properly cited. The written permission of Cambridge University Press or the rights holder(s) must be obtained prior to any commercial use.
Copyright
© The Author(s), 2025. Published by Cambridge University Press on behalf of Royal Aeronautical Society
Figure 0

Figure 1. The system safety engineering process components based on STAMP. Adapted from Ref. (66).

Figure 1

Figure 2. A display of FRAM. A hexagon representing a function, with the six aspects of input (I), output (O), preconditions (P), resources (R), control (C), and time (T). In public domain [41].

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Figure 3. The procedural steps of the literature review.

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Figure 4. Percentage distribution by publication type.

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Figure 5. The sources arranged by themes.

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Table 1. Gap domains in uncertainty modeling

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Table 2. The interviews outline

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Figure 6. The mixed method research approach.

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Table 3. Primary dimensions of operational uncertainty in aircraft maintenance

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Figure 7. Thematic map of uncertainty in maintenance tasks.

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Figure 8. The UQAM process.

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Table 4. Risk categories and recommended actions based on uncertainty score

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Figure 9. Factor contribution heatmap: engine oil changes.

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Figure 10. Factor contribution heatmap: lubrication.

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Figure 11. Factor contribution heatmap: freewheel inspection.

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Table 5. Uncertainty observations, thresholds, and key contributors per task

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Table 6. Sensitivity of IUE Score to input factors (baseline $U = 9.27$)

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Figure 12. Factor contribution heatmap: driveshaft inspection.

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Figure 13. UQAM potential integration into STAMP.

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Figure 14. UQAM potential integration into FRAM.

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Figure 15. Reshaping the SMS with UQAM.

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Table B1. The 73 studies included in the analysis for the research gap identification