Assessment of Aircraft Engine Blade Inspection Performance Using Attribute Agreement Analysis

被引:4
|
作者
Aust, Jonas [1 ]
Pons, Dirk [1 ]
机构
[1] Univ Canterbury, Dept Mech Engn, Christchurch 8041, New Zealand
关键词
human cognitive performance; aviation safety; visual inspection; aero engine maintenance; measurement systems analysis; attribute agreement analysis; inspection accuracy; consistency; repeatability; reproducibility; reliability; human factors; AUTOMATED VISUAL INSPECTION; AVIATION MAINTENANCE; RELIABILITY; QUALITY; KAPPA;
D O I
10.3390/safety8020023
中图分类号
R1 [预防医学、卫生学];
学科分类号
1004 ; 120402 ;
摘要
Background-Visual inspection is an important element of aircraft engine maintenance to assure flight safety. Predominantly performed by human operators, those maintenance activities are prone to human error. While false negatives imply a risk to aviation safety, false positives can lead to increased maintenance cost. The aim of the present study was to evaluate the human performance in visual inspection of aero engine blades, specifically the operators' consistency, accuracy, and reproducibility, as well as the system reliability. Methods-Photographs of 26 blades were presented to 50 industry practitioners of three skill levels to assess their performance. Each image was shown to each operator twice in random order, leading to N = 2600 observations. The data were statistically analysed using Attribute Agreement Analysis (AAA) and Kappa analysis. Results-The results show that operators were on average 82.5% consistent with their serviceability decision, while achieving an inspection accuracy of 67.7%. The operators' reproducibility was 15.4%, as was the accuracy of all operators with the ground truth. Subsequently, the false-positive and false-negative rates were analysed separately to the overall inspection accuracy, showing that 20 operators (40%) achieved acceptable performances, thus meeting the required standard. Conclusions-In aviation maintenance the false-negative rate of <5% as per Aerospace Standard AS13100 is arguably the single most important metric since it determines the safety outcomes. The results of this study show acceptable false-negative performance in 60% of appraisers. Thus, there is the desirability to seek ways to improve the performance. Some suggestions are given in this regard.
引用
收藏
页数:24
相关论文
共 50 条
  • [1] Inspection of Aircraft Engine Components using Induction Thermography
    Genest, Marc
    Li, Gang
    [J]. 2018 IEEE CANADIAN CONFERENCE ON ELECTRICAL & COMPUTER ENGINEERING (CCECE), 2018,
  • [2] Evaluation of Influence Factors on the Visual Inspection Performance of Aircraft Engine Blades
    Aust, Jonas
    Pons, Dirk
    Mitrovic, Antonija
    [J]. AEROSPACE, 2022, 9 (01)
  • [3] Structural Analysis and Optimization of a Composite Fan Blade for Future Aircraft Engine
    Coroneos, Rula M.
    Gorla, Rama Subba Reddy
    [J]. INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2012, 29 (03) : 131 - 164
  • [4] PHASE PORTRAITS IN THE ANALYSIS OF AN AIRCRAFT ENGINE PERFORMANCE
    Kowalski, Miroslaw
    Jankowski, Antoni
    Cwik, Dariusz
    [J]. 7TH INTERNATIONAL CONFERENCE INTEGRITY-RELIABILITY-FAILURE (IRF2020), 2020, : 775 - 784
  • [5] R-function analysis of the thermally stressed state of an aircraft engine blade
    Rvachev, VL
    Shevchenko, AN
    Sizova, ND
    [J]. INTERNATIONAL APPLIED MECHANICS, 1996, 32 (02) : 117 - 121
  • [6] TOPTIG Robot Welding Technology and Welding Joint Performance Research of the Aircraft Engine Blade
    Shen, Hongyuan
    Chen, Huabin
    [J]. Shanghai Jiaotong Daxue Xuebao/Journal of Shanghai Jiaotong University, 2016, 50 : 114 - 116
  • [7] Performance Analysis of an Aircraft Gas Turbine Engine using Particle Swarm Optimization
    Choi, Jae Won
    Sung, Hong-Gye
    [J]. INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2014, 15 (04) : 434 - 443
  • [8] POD assessment using real aircraft engine components
    Fahr, A
    Forsyth, DS
    [J]. REVIEW OF PROGRESS IN QUANTITATIVE NONDESTRUCTIVE EVALUATION, VOLS 17A AND 17B, 1998, : 2005 - 2012
  • [9] Assessment of the Effect of Cleanliness on the Visual Inspection of Aircraft Engine Blades: An Eye Tracking Study
    Aust, Jonas
    Mitrovic, Antonija
    Pons, Dirk
    [J]. SENSORS, 2021, 21 (18)
  • [10] Conjectural bifurcation analysis of the contact-induced vibratory response of an aircraft engine blade
    Batailly, Alain
    Legrand, Mathias
    Millecamps, Antoine
    Garcin, Francois
    [J]. JOURNAL OF SOUND AND VIBRATION, 2015, 348 : 239 - 262