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Pengembangan Laboratorium Virtual untuk Pelatihan Perencanaan Pemeliharaan Pesawat Terbang Ahmad Buana Syamra Pratama Rahman; Mufti Arifin; Syarifah Fairuza
Jurnal Mahasiswa Dirgantara Vol. 3 No. 1 (2024): Jurnal Mahasiswa Dirgantara
Publisher : FTK UNSURYA

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.35894/jmd.v3i1.121

Abstract

Perencanaan pemeliharaan pesawat terbang merupakan aspek vital dalam menjaga keselamatan dan keandalan operasional penerbangan. Namun, pelatihan perencanaan pemeliharaan sering kali menghadapi keterbatasan akses terhadap pesawat nyata, kompleksitas prosedur, serta keterbatasan sumber daya laboratorium fisik. Kondisi ini menimbulkan kebutuhan mendesak akan solusi alternatif yang fleksibel, efektif, dan efisien untuk mendukung proses pembelajaran. Penelitian ini bertujuan untuk mengembangkan laboratorium virtual sebagai media pelatihan interaktif dalam perencanaan pemeliharaan pesawat, yang mampu mensimulasikan skenario dunia nyata dan meningkatkan pemahaman peserta terhadap prosedur teknis dan regulasi yang berlaku. Metode penelitian dilakukan melalui pendekatan rekayasa perangkat lunak, yang meliputi tahapan analisis kebutuhan, desain sistem, implementasi, dan evaluasi efektivitas penggunaan laboratorium virtual. Evaluasi dilakukan melalui uji coba terbatas terhadap mahasiswa teknik penerbangan yang mengikuti mata kuliah perencanaan pemeliharaan. Hasil penelitian menunjukkan bahwa laboratorium virtual ini mampu meningkatkan pemahaman konsep secara signifikan, mempercepat proses pembelajaran, serta memberikan pengalaman praktis yang mendekati kondisi operasional di industri penerbangan. Penggunaan laboratorium virtual juga dinilai efisien dalam hal waktu, biaya, dan ketersediaan alat pelatihan. Dengan demikian, pengembangan ini diharapkan dapat menjadi alternatif strategis dalam pendidikan teknik penerbangan yang berorientasi pada praktik dan kebutuhan industri.   Aircraft maintenance planning is a critical component in ensuring the safety and reliability of aviation operations. However, training in maintenance planning often encounters several challenges, including limited access to real aircraft, the complexity of procedures, and constraints in physical laboratory resources. These limitations highlight the urgent need for an alternative learning solution that is flexible, efficient, and capable of simulating real-world conditions. This study aims to develop a virtual laboratory as an interactive training medium for aircraft maintenance planning, designed to enhance learners’ understanding of technical procedures and regulatory compliance. The research was conducted using a software engineering approach, comprising stages of needs analysis, system design, implementation, and usability evaluation. The evaluation involved trial implementation with aerospace engineering students enrolled in a maintenance planning course. The results indicate that the virtual laboratory significantly improves conceptual understanding, accelerates the learning process, and provides practical experience comparable to real-world industry scenarios. Furthermore, the virtual platform proved to be cost-effective and resource-efficient in terms of time, tools, and accessibility. Therefore, this development is expected to serve as a strategic alternative in aviation engineering education, aligning with industry-oriented training needs
Analisis Fuel Leak Repetitive Problem Pada Pesawat Boeing 737 di Maskapai ABC Ahmad Al Muhraj; Mufti Arifin; Erna Shevilia
Jurnal Mahasiswa Dirgantara Vol. 3 No. 1 (2024): Jurnal Mahasiswa Dirgantara
Publisher : FTK UNSURYA

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.35894/jmd.v3i1.122

Abstract

Masalah kebocoran bahan bakar pada mesin pesawat merupakan aspek krusial dalam menjaga keselamatan penerbangan dan efisiensi operasional. Penelitian ini bertujuan untuk menganalisis penyebab dan dampak kebocoran bahan bakar yang terjadi secara berulang, serta memberikan solusi untuk mengurangi frekuensi dan dampak kebocoran tersebut. Metodologi penelitian yang digunakan mencakup pengumpulan data dari insiden sebelumnya, termasuk data pilot report Maskapai ABC tahun 2018-2020, menganalisis penyebab akar masalah, serta simulasi kondisi operasi. Penelitian ini bertujuan untuk mengidentifikasi pola dan faktor yang berkontribusi terhadap masalah kebocoran. Dengan ini, keselamatan penerbangan dapat ditingkatkan dan kebocoran bahan bakar dapat diminimalisirkan. Dari hasil penelitian, ditemukan enam registrasi pesawat yang mengalami kebocoran bahan bakar berulang, salah satunya mengalami kebocoran bahan bakar berulang sebanyak tiga kali. Kebocoran tersebut disebabkan oleh berbagai faktor, yaitu keausan material, kesalahan dalam proses pemasangan, dan tidak adanya tindakan permanen. Adapun langkah-langkah yang dapat meminimalisir terjadinya kebocoran bahan bakar berulang seperti, melakukan inspeksi lebih sering pada komponen sistem bahan bakar, dan melakukan penggantian komponen berdasarkan rekomendasi pabrikan atau interval waktu yang sesuai meskipun komponen tidak menunjukkan tanda-tanda kerusakan.   The issue of fuel leaks in aircraft engines is a critical aspect of ensuring flight safety and operational efficiency. This thesis aims to analyze the causes and impacts of recurring fuel leaks, as well as provide solutions to reduce the frequency and impact of these leaks. The research methodology includes data collection from previous incidents, including pilot reports from ABC Airlines between 2018 and 2020, analyzing the root causes of the issues, and simulating operational conditions. It is hoped that this study will identify patterns and factors contributing to the fuel leak problems. In turn, this will contribute to improving flight safety and minimizing fuel leaks. The research findings identified six aircraft registrations that experienced recurring fuel leaks, one of which had repeated fuel leaks three times. These leaks were caused by various factors, including material wear, installation errors, and the lack of permanent corrective actions. Steps to minimize recurring fuel leaks include more frequent inspections of the fuel system components and replacing components according to manufacturer recommendations or suitable time intervals, even if the components show no signs of damage.
Pendampingan Pengembangan Komponen Instrument Terpadu (KIT) Fisika Terbang untuk SMK Penerbangan Mufti Arifin; Endah Yuniarti; Syarifah Fairuza
JURNAL Comunità Servizio : Jurnal Terkait Kegiatan Pengabdian kepada Masyarakat, terkhusus bidang Teknologi, Kewirausahaan dan Sosial Kemasyarakatan Vol. 6 No. 2 (2024): OKTOBER
Publisher : Lembaga Penelitian dan Pengabdian kepada Masyarakat (LPPM), Univesitas Kristen Indonesia

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.33541/cs.v6i2.6427

Abstract

The lack of adequate physics laboratory facilities for conducting flight physics practicums in Aviation Vocational High Schools has been a significant obstacle in the learning process. Due to these limitations, students' understanding of the physics concepts underlying aviation principles has been suboptimal. To address this issue, community service activities have focused on enhancing the capacity of teachers at Gutama Aviation Vocational High School to design and implement physics practicums. Through the creation and utilization of Integrated Instrument Kits (KIT) for flight physics, it is hoped that teachers can provide more concrete and engaging learning experiences for students. With the successful development of 5 KITs, teachers now have the skills to design a variety of practical activities that meet the needs of their students. Additionally, the provided mentorship has equipped teachers with a deep understanding of physics concepts relevant to the aviation industry. It is hoped that the success of this activity can improve the quality of physics education at Gutama Aviation Vocational High School, encourage teachers to be more innovative in developing additional KITs, and prepare graduates who are more competent in the field of aviation.
Analysis of The Removal and Installation Stages of The RR Trent 700 Engine on an Airbus A330 Aircraft Using The Critical Path Method Husaini, Fahdli Zulfikar; Mufti Arifin; Muhammad Hadi Widanto
Jurnal Teknologi Kedirgantaraan Vol 10 No 2 (2025): Jurnal Teknologi Kedirgantaraan
Publisher : FTK UNSURYA

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.35894/jtk.v10i2.245

Abstract

The lifting of the Restriction of Community Activities (PPKM) in January 2023 was the beginning of the aviation industry in Indonesia starting to rise marked by the emergence of new Maintenance Repair and Operations (MRO). Limited hangar space at MRO is a challenge in scheduling aircraft maintenance, setting the order of task cards that have been submitted by the airline and must be done in the maintenance project will be an illustration of how long this project will be done. MP item number 7122410504 contains Detailed Inspection of Aft Engine Mount Fail-Safe link is a maintenance job that can be done after the removal of Engine. The engine removal and installation process often takes more time and effort, potentially causing delays in the overall maintenance time. The purpose of this research is to make efficiency in the removal and installation process of the RR Trent 700 engine using the critical path method. The critical path method in analysing the stages of work in the maintenance process aims to identify and optimise resource allocation, so that maintenance time can be minimised and overall efficiency can be improved. The results showed that the application of the critical path method in the stages of engine removal and installation work resulted in a time efficiency of about 1,655 Hours so that the delay in work on the critical path became the main factor affecting the total duration of the engine removal and installation process.
Analisis Efektifitas Laboratorium Manajemen Pemeliharaan Virtual Berdasarkan Tutorial Virtual surya wijaya, Andi; Mufti Arifin; Erna Shevilia Agustian
Jurnal Mahasiswa Dirgantara Vol. 4 No. 1 (2025): Jurnal Mahasiswa Dirgantara
Publisher : FTK UNSURYA

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.35894/jmd.v4i1.68

Abstract

Maintenance management is a series of activities that include planning, organizing, program implementation, and control methods for maintenance activities. This study aims to determine whether maintenance management practices can be implemented effectively through a hybrid training method (virtual and offline) that utilizes a maintenance management laboratory. The research stages include understanding the data that must be inputted by technical records, how to read and fill out maintenance logs, and designing virtual tutorials which are then tested on aviation engineering students. In using the virtual tutorial, students input data, calculate aircraft life utilization based on Time Since New (TSN) or Cycle Since New (CSN), and calculate the life of aircraft components with the same parameters. Based on the results of testing the AFML tutorial on 10 aviation engineering students, it was found that 96% of them were able to answer the evaluation questions correctly, with 8 students answering perfectly and 2 students reaching 80% success rate. These results show that the virtual tutorial developed is quite effective and useful in improving students' understanding of maintenance management, especially in the use and analysis of AFML data.
Rancang Bangun Alat Peraga Simulasi Kerja Spoiler Pada Pesawat Terbang Al Farabi, Awfa Azka; Mufti Arifin; Evi Endarti
Jurnal Mahasiswa Dirgantara Vol. 4 No. 1 (2025): Jurnal Mahasiswa Dirgantara
Publisher : FTK UNSURYA

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.35894/jmd.v4i1.80

Abstract

Spoiler is one of the components that has an important role in an airplane. This component serves to slow down the speed of an aircraft both in the air and on the ground. However, due to its classification as part of secondary flight control, its understanding is often limited to the general public as a braking device on an aircraft without paying attention to the complexity of its functions and mechanisms. Therefore, the design of this spoiler simulation is expected to help in understanding the work simulation of a spoiler on an aircraft. This tool is designed with a simple working system using a syringe and hose as a simple depiction of the hydraulic system performance on the aircraft, which is also equipped with a series of electrical systems consisting of arduino, servo and microswitch as a support system for this tool so that it can describe the difference in performance between flight spoiler (speed brake) and ground spoiler. The wing structure of this tool is made of thermoplastic material (PLA) and mica plastic, so that it can make it easier to see how this tool can work. This tool is also equipped with a lever that is duplicated as the original according to the aircraft. Based on the design and assembly that has been done, this tool is proven to work successfully in accordance with its respective functions.
Co-Authors AA Sudharmawan, AA Adam Wahyu Saputra Adam Ade Julizar Ade Julizar Afid Nurul Anwar Afifah, Atik Ahmad Akmal Said Ahmad Al Muhraj Ahmad Buana Syamra Pratama Rahman Al Farabi, Awfa Azka Alimin, Edy Karyadi amat chaeroni Ananda Rafi Rijalul Awwal Aprila Sakti K Arindho Andrifa Faturrohman Ayu Martina Bayu Wicaksono Belnov, Syaddad Husaini Borris Y Maningka Budi Aji Warsiyanto Chintya Rahmawati Cynthia Rahmawati Daniel Frederick Romulus Ginting Dhimas Ilyas Ramadhani Dhimas Dwiki Fahreza Andreanto Endah Yuniarti, Endah Erna Shevilia Erna Shevilia Agustian Evi Endarti Fadli Hidirsyah fahmins Fairuza, Syarifah Fara Vania Utami FORTUNE JR OMBUH Freddy, Franciscus Gunawan, Gia Aviani Husaini, Fahdli Zulfikar Imron Rosadi Israq Mifan Junaidi K, Aprilia Sakti Kanda Anantariyanto Alam Tasti Miranda Saputra Muchammad Furqon Muchaddats Muhamad Jayadi Muhammad Hadi Widanto Muhammad Kevin Bilhaq Muhammad Umar Abdulloh NUR HIDAYAH NINGSIH, Nur Hidayah Ningsih PANGGIH JOGO MUSTIKO Paramaharta, Izhar Rabeta, Bismil Rafika Arum Sari Raihan Maulana Yahya Reynaldo Mulya Tedja Riskha Agustianingsih Rizwan Maulana Rosalie, Rhea Anggun Said, Ahmad Akmal Saiful Latif, Saiful Sari, Rafika Arum sausan, Misk Sausan Ghina Septian, Diaz Shevillia Agustian, Erna Simon Sindhu H Sofyan, Mohamad Fauzan Somadi, Ridho Misbahudin surya wijaya, Andi Suwardi, Arie Prasetya Syaiful Rifki T. Dikatama Utama, Ericko Chandra venza, Venza Fawwaz Tsulatsa Victory Rumagit, Jodia Vita Kartika Wicaksono , Paulus Hilman