PERENCANAAN PREVENTIVE MAINTENANCE MENGGUNAKAN METODE RELIABILITY PADA ELECTRICAL SISTEM AUXILIARY POWER UNIT BOEING 737-500
Keywords:
Failure, Reliability, Weibull Distribution, Maintenance Schedule, Auxiliary power unitAbstract
The electrical system Auxiliary Power Unit on the Boeing 737-500 aircraft often experiences operational failure due to damage to the components in the system, this incident causes significant operational losses so that an appropriate maintenance method is needed to eliminate the factors that cause failure in the Electrical system Auxiliary Power Units. The purpose of this study is to plan preventive maintenance activities on the Electrical Auxiliary Power Unit system so that part damage that causes failure can be handled properly. The reliability method is calculated using the Weibull probability distribution so that the critical operating time limit is obtained on the Electrical Auxiliary Power Unit system. From the calculation results, the critical operational limit for the Electrical Auxiliary Power Unit system is 271 flight cycle with the main damage being the start relay component, with maintenance activities in the form of inspection, repair, testing and cleaning activities.
References
Ilham, 2016. “Lubrication System Pada Auxiliary Power Unit ( Apu ),” Lubr. Syst. Pada Aux. Power Unit ( Gtc P85 129 Pesawat Boeing 737 300/400/500, vol. 3, no. 1, pp. 41–56, 2016.
C. E. Ebeling, 1997. “Intro to Reliability & Maintainability Engineering.” p. 486.
W. Zimmer, 1999. “An Introduction to Reliability and Maintainability Engineering,” J. Qual. Technol., vol. 31, no. 4, pp. 464–466, doi: 10.1080/00224065.1999.11979954.
P. Tarigan, E. Ginting, and I. Siregar, 2013. “Perawatan Mesin Secara Preventive Maintenance Dengan Modularity Design Pada Pt. Rxz,” J. Tek. Ind. USU, vol. 3, no. 3, pp. 35–39.
F. Setiawan, E. Sofyan, and D. M. C. Putra, 2020. “Analisis Reliability Sistem Starter Valve Untuk Merencanakan Aktivitas Maintenance Pada Pesawat Boeing 737 Next Generation Di …,” Tek. STTKD J. Tek. …, vol. 6, no. 02, pp. 92–103, 2020, [Online]. Available:
https://jurnal.sttkd.ac.id/index.php/ts/article/vi ew/272.
B. S. P. SUSANTO, 2017. “Penjadwalan Waktu Optimum Maintenance Dengan Metode Reliability Centered Maintenance (Rcm),” p. 4, [Online]. Available: chrome- extension://efaidnbmnnnibpcajpcglclefindmkaj
/viewer.html?pdfurl=https%3A%2F%2Feprints. umm.ac.id%2F36022%2F3%2Fjiptummpp-gdl- bagussusil-48581-3- babii.pdf&clen=1637397&chunk=true.
Cyrilus, 2012. “Analisis Terhadap Starter Motor Auxiliary Power Unit 85 / 129E Saat on Pada Pesawat Boeing 737-300 / Pk-Yvw,” Anal. Terhadap Start. Mot. Aux. Power Unit 85/129E Saat Pada Pesawat Boeing 737, vol. 2, no. 2, pp. 15–18.
H. Munawir, R. M. Ulfa, and M. Djunaidi, 2020. “Analisa Risiko Kegagalan Terhadap Downtime Pada Line Crank Case Menggunakan Metode Failure Mode Effect Analysis,” pp. 149–156.
M. R. Rasindyo, Kusmaningrum, and Y. Helianty, 2015. “Analisis Kebijakan Perawatan Mesin Cincinnati Dengan Menggunakan Metode Reliability Centered Maintenance Di PT. Dirgantara Indonesia,” J. Online Inst. Teknol. Nas., vol. 03, no. 1, pp. 400–410.
Aircraft Maintenance Manual (AMM). Rev 15 Oktober 2019. ATA 80 Engine Starting. Chicago Amerika. Boeing 737-600/700/800/900.
F. Setiawan, E. Sofyan, and M. Hadi, 2021. “JOURNAL OF APPLIED MECHANICAL
ENGINEERING AND RENEWABLE ENERGY (JAMERE), "Perencanaan Preventive Maintenance Ram Air Actuator pada Pesawat Boeing 737 Next Generation Menggunakan Metode Reliability Di PT . GMF Aeroasia”, vol. 1, no. 2, pp. 53–62, 2021.