EC 155 B1 Eurocopter: analisis reabilitas dan kekritisan mode kegagalan ATA 32 (Landing Gear)

Abstract

Kegiatan perawatan berupa program reliability pada pesawat udara dilakukan untuk menjaga keandalan komponen pesawat serta menjaga kondisi pesawat udara agar tetap laik terbang dan meminimalisir kegagalan yang dapat mengakibatkan penurunan performa pada keseluruhan sistem tersebut. Berdasarkan data deffect report helikopter EC 155 B1 Eurocopter, dilakukan penerapan program reliability dari tahun 2011-2023 dan ditemukan bahwasanya ada beberapa komponen yang mengalami kegagalan pada ATA Chapter 32 (Landing Gear). Penelitian ini menggunakan metode Failure Mode Effect Analysis (FMEA). Hasil dari penelitian menunjukkan program reliability yang diterapkan memiliki faktor defiasi bernilai 3.2 dalam perhitungan dengan interval 12 bulan. Berdasarkan dari data deffect report didapatkan 5 modus kegagalan terkait ATA Chapter 32 (Landing Gear). Dari hasil analisa dengan metode FMEA dari 5 jenis permasalahan terkait ATA Chapter 32 (Landing Gear) didapatkan permasalahan pada Brake Accumulator memiliki nilai RPN paling tertinggi yaitu sebesar 36 dimana menjadi mode kegagalan dengan tingkat kegagalan yang rendah.

Keywords

Helicopter, EC 155 B1 Eurocopter, ATA Chapter 32, FMEA

Full Text:

Article (Bahasa Indonesia)

References

Air Transport Association (America), "Spec 100: Manufacturers' Technical Data", 1956

"System Description Section (SDS) EC155", Eurocopter (Airbus), 2023.

H. Schneider and D. H. Stamatis, "Failure Mode and Effect Analysis: FMEA from Theory to Execution," Technometrics, vol. 38, no. 1, p. 80, Feb. 1996, doi: 10.2307/1268911

"Potential Failure Mode and Effects Analysis (FMEA) Including Design FMEA, Supplemental FMEA-MSR, and Process FMEA", doi: 10.4271/J1739_202101

N. Zhang, S. Yan, Z. Fang, and B. Yang, "Fuzzy GERT model based on z-tag and its application in weapon equipment management," Journal of Intelligent Fuzzy Systems, vol. 40, no. 6, pp. 12503-12519, Jun. 2021, doi: 10.3233/JIFS-201731

Michael A. Brown, Jung-Hua Chang, " Analytical Techniques for Helicopter Component Reliability", American Helicopter Society 64th, Annual Forum, Montreal, Canada, April 29 - May 1, 2008.

L. Iven and Y. Zaidi, "Validation of the safety requirements of the landing gear using fault tree analysis," CEAS Aeronautical Journal, vol. 13, no. 2, pp. 503-520, Mar. 2022, doi: 10.1007/s13272-022-00572-8

Y. Yin, N. Hong, N. Huajin, and Z. Ming, "Reliability Analysis of Landing Gear Retraction System Influenced by Multifactors," Journal of Aircraft, vol. 53, no. 3, pp. 713-724, May 2016, doi: 10.2514/1.C033333

I. NICOLIN and B. A. NICOLIN, "Failure Mode and Effect Analysis for a military nose landing gear project," INCAS BULLETIN, vol. 13, no. 4, pp. 205-212, Nov. 2021, doi: 10.13111/2066-8201.2021.13.4.17

Iven and Y. Zaidi, "Validation of the safety requirements of the landing gear using fault tree analysis," CEAS Aeronautical Journal, vol. 13, no. 2, pp. 503-520, Mar. 2022, doi: 10.1007/s13272-022-00572-8

T. Qian, Z. Yongqiang, L. Yongfei, and P. Bo, "Reliability Analysis on Aircraft Main Landing Gear System Based on Simulation of GERT," 2019 3rd International Conference on Electronic Information Technology and Computer Engineering (EITCE), Oct. 2019, doi: 10.1109/EITCE47263.2019.9094798

Z. Li, X. Li, Y. Jiang, and M. Yuan, "Research on Data Analysis Model of Weapon Equipment Acquisition Information Network," 2020 2nd International Conference on Information Technology and Computer Application (ITCA), Dec. 2020, doi: ITCA52113.2020.00155

R. Rohmat, "Analisis Perawatan Mesin Conveyor Dengan Metode Reliability Centered Maintenance (RCM)," JUSTI (Jurnal Sistem dan Teknik Industri), vol. 3, no. 1, p. 145, Oct. 2022, doi: 10.30587/justicb.v3i1.4761

I. Aditiya, L. R. Pinandhita, and B. D. Adiputra, "Reliability Analysis Of Main Rotor EC 155B1 On Pin Blade And Attach Beams Components Using Markov Analysis," Vortex, vol. 3, no. 1, p. 18, Jan. 2022, doi: 10.28989/vortex.v3i1.1026

Srinath, L.S., "Reliability Engineering", East West Press, New Delhi, India, 2013

http://dx.doi.org/10.28989/jumantara.v3i2.2299

Article Metrics

Abstract view: 109 times
Download     : 55   times

This work is licensed under a Creative Commons Attribution 4.0 International License.

Refbacks

• There are currently no refbacks.