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ANALISIS STRATEGI DAN FEASIBILITY PENGEMBANGAN MRO PEMELIHARAAN ENGINE DI INDONESIA Franciscus, Freddy; Utama, Ericko Chandra
JTK: JURNAL TEKNOLOGI KEDIRGANTARAAN Vol 5, No 1 (2020): Jurnal Teknologi Kedirgantaraan
Publisher : JTK: JURNAL TEKNOLOGI KEDIRGANTARAAN

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (838.257 KB) | DOI: 10.35894/jtk.v5i1.425

Abstract

Bisnis pemeliharaan pesawat terbang di Indonesia masih sangat menarik sejalan dengan pertumbuhan jumlah pesawat terbang yang dimiliki maskapai domestik. Sekitar 65% porsi biaya pemeliharaan pesawat terbang milik maskapai domestik belum terserap MRO Indonesia. Sebagian besar porsi yang belum terserap tersebut adalah klaster pemeliharaan engine dan komponen pesawat terbang, dimana hanya terserap sekitar 10% (USD 100 Juta) dari 75% (USD 750 Juta Th 2017) biaya pemeliharaan engine (35%) dan komponen (45%) pesawat terbang yang dikeluarkan oleh maskapai Indonesia. Dari serapan 10% biaya pemeliharaan engine dan komponen tersebut porsi serapan biaya pemeliharaan engine saja hanya 5% (USD 50 Juta) dari 35% (USD 350 Juta) biaya pemeliharaan engine. Masih ada sekitar 30% (USD 300 Juta) yang merupakan peluang MRO Indonesia untuk mengembangkan capability pemeliharaan engine milik maskapai Indonesia. Dari beberapa tipe engine yang ada di maskapai Indonesia, CFM56-7B yang dipakai pesawat B737-800/900 mempunyai populasi terbanyak yaitu sekitar 450 engine. Hasil analisa feasibility terhadap pengembangan capability MRO engine untuk pemeliharaan CFM56-7B diperoleh hitungan ROI dan Pay Back Periodprogram pengembangan capability engine tersebut masing-masing adalah 24,57% dan 4.4 tahun dan nilai tersebut menunjukkan bahwa strategi pengembangan MRO engine CFM56-7B tersebut feasible.
Analisis Penentuan Komposisi Optimum Kargo Dan Pax Pesawat Boeing 787 - 8 Dan Airbus 330 – 900 Pada Rute Jakarta – Dubai Menggunakan Optimasi Linear Programming Fernando Fransiskus Rotty; Freddy Franciscus; Ericko Chandra
Jurnal Teknologi Kedirgantaraan Vol 6 No 2 (2021): Jurnal Teknologi Kedirgantaraan
Publisher : FTK UNSURYA

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (470.839 KB) | DOI: 10.35894/jtk.v6i2.37

Abstract

Abstract - The need for airplanes is increasing every day, this is due to the increasing number of passengers and cargo shipments from one area to another. Therefore, airlines need to provide optimal, safe, and efficient cargo and passenger transportation services so that the delivery of goods and passengers can run according to correct procedures. Opportunities in the business of transporting passengers and shipping cargo must be utilized properly by each airline by purchasing planes so that the shipping process from one area to another can quickly arrive at its destination. The purpose of this paper is to find the optimum value of the two aircraft between the Boeing 787-8 and the Airbus 330-900 in terms of the effect on the range, operational costs and to find out which aircraft is more profitable for operating costs on the Jakarta - Dubai route, using linear optimization. programming. Based on the results of the analysis that the optimum point for the calculation of linear programming optimization, the Boeing 787-8 aircraft obtained results (Max payload 41,075 kg, Fuel 6,657 kg, Max Fuel 101,323 kg) where these three results become a limitation for airlines to know the maximum usage of payload and fuel compared Airbus 330-900 aircraft obtained results at the point (Max payload 45,000 kg, Fuel 4,728 kg, Max Fuel 111,272 kg) so that the optimization results are obtained, for Boeing 787-8 aircraft with a max payload of 41,075 kg, max pax 359, max cargo 15,945 kg , compared to Airbus 330-900 with a max payload of 45,000 kg, max pax 460, max cargo 12,800 kg, so it can be concluded that the results of linear programming optimization and the calculation of the operational costs of the Boeing 787-8 aircraft are more optimal with a figure of Rp. 1,541,334,803.96 but in terms of revenue the Airbus 330-900 is bigger than the Boeing 787-8.
PENGUKURAN TINGKAT KEBISINGAN PESAWAT CASA 212-200 SAAT GROUND RUN TEST BERDASARKAN VARIASI SUDUT Adam Wahyu Saputra Adam; Mufti Arifin; Ericko Chandra Utama
Jurnal Teknologi Kedirgantaraan Vol 8 No 1 (2023): Jurnal Teknologi Kedirgantaraan
Publisher : FTK UNSURYA

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.35894/jtk.v8i1.70

Abstract

Noise is an unwanted sound, including sound that as a result of side effects from activities such as industrial and transportation activities. The greatest intensity of noise in the aircraft maintenance hangar environment is produced by the operation of the aircraft engine when it is ground or what is often called the Aircraft Ground Run Test. An This study was conducted by taking samples using CASA 212-200 aircraft equipped with a turboprop engine type. The measurement of noise generated by aircraft activity is measured using a tool such as the AS804 Sound Level Meter. This study aims to determine the intensity of aircraft noise when conducting a ground run test which is measured based on variations in the angle of measurement location to the source with a distance of 30 m based on an angular reference of 0o in front of the aircraft nose and 180o is behind the aircraft with a clockwise rotation. The measurement of noise levels is based on three references, namely LAmax, LAmin and LAeq. At idle the variation in the direction of the noise receiver which has the potential to produce the largest LAmax value at an angle (30o) of 97 dB. The lowest LAmin at an angle (180o) and (210o) of 84.6 dB. The largest LAeq at an angle (330o) of 95.3 dB. At the time of max power the variation in the direction of the noise receiver which has the largest potential LAmax value at an angle (45o) of 99.1 dB, the lowest LAmin at an angle (135o) of 94.8 dB. The highest LAeq at an angle (45o) of 97.8 dB.
Analisis Tingkat Kebisingan Pesawat Saat Take-Off Berdasarkan Variasi Tinggi Lintasan di Bandara Halim Perdanakusuma Arindho Andrifa Faturrohman; Mufti Arifin; Ericko Chandra Utama
Jurnal Teknologi Kedirgantaraan Vol 9 No 1 (2024): Jurnal Teknologi Kedirgantaraan
Publisher : FTK UNSURYA

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.35894/jtk.v9i1.97

Abstract

An increase in flight frequency can have a negative impact on the surrounding environment, one of which is high noise levels. Noise can come from full activity, runway stay, movement towards the runway, or aircraft engine testing. Airplane noise during take-off is one of the environmental problems that need attention at airports. The height of the aircraft's trajectory during take-off can affect the noise level generated by the aircraft, but not much research has been conducted to measure the impact of variations in the height of the disturbance on the noise level of aircraft at Halim Perdanakusuma Airport. This study aims to measure the noise level of aircraft during take-off with variations in track height at Halim Perdanakusuma Airport. The method used in this study is to observe 4 aircraft taking off at Halim Perdanakusuma Airport with a research time of 3 days, and the measuring instrument used is a sound level meter. Sound level meters measure noise in dBA units between 30 and 130 dB at a frequency of 20 to 20.000 Hz. Based on the calculation and measurement results obtained, it is known that the maximum height when the measurement is on the second day is at point A of 277 meters, while at point B is 299 meters. While the highestnoise measurement at point A is 93,1 dB while at point B it is 91,5 dB. The measured noise value based on calculations is estimated at 66,2 dB and is still below the Airbus A320 aircraft noise certification for flyover takeoff of 73,7 dB.
Review Mikroalga Sebagai Sumber Bahan Baku Alternatif Bioavtur Ericko C. Utama
Jurnal Teknologi Kedirgantaraan Vol 4 No 1 (2019): Jurnal Teknologi Kedirgantaraan
Publisher : FTK UNSURYA

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.35894/jtk.v4i1.229

Abstract

Tulisan ini menginformasikan tentang kebutuhan sumber alternatif pengganti bahan bakar fosil untuk pesawat (Avtur). Peningkatan kebutuhan energi  terus terjadi dan di sisi lain jumlah energi yang bersumber dari fosil terus menurun, maka perlu dilakukan upaya diversifikasi energi, yaitu upaya pemanfaatan energi alternatif. Berdasarkan Renstra Kementerian ESDM Tahun 2015–2019, cadangan minyak bumi Indonesia sebesar 3,6 miliar barel diperkirakan akan habis dalam 13 tahun mendatang. Menteri Perhubungan (2009–2014) E. E. Mangindaan mengatakan pemanfaatan bahan bakar nabati dan energi terbarukan bagi sektor transportasi secara khusus juga mendorong peningkatan konten lokal baik dari aspek penguasaan riset, teknologi dan aplikasi dari hulu hingga ke hilir di dalam seluruh mata rantai suplai, produksi dan distribusi. Gagasan untuk menggunakan mikroalga sebagai sumber bahan bakar bukanlah hal baru, tetapi sekarang dianggap serius karena kenaikan harga minyak bumi dan lebih penting lagi, masalah yang muncul tentang pemanasan global dan efek rumah kaca yang terkait dengan pembakaran bahan bakar fosil. Kelebihan yang dimiliki oleh mikroalga bila dibandingkan dengan tanaman lainnya yaitu efisiensi fotosintesis yang tinggi, menghasilkan biomassa yang lebih banyak, pertumbuhan lebih cepat, tidak berkompetisi dengan produksi pangan, mengurangi emisi gas rumah kaca, dapat mengubah CO2 menjadi biomassa, mempunyai komponen sampingan selain lipid, dapat menghemat sumberdaya air karena menggunakan air hasil daur ulang, dapat bertahan dalam salinitas yang tinggi, 10-100 kali menghasilkan biodisel dibanding tanaman lain untuk luas yang sama, siklus hidup yang lebih singkat dan sesuai dengan iklim Indonesia.   This paper informs about the need for alternative sources of substitute for fossil fuels for aircraft (Avtur). Increasing energy needs continue to occur and on the other hand the amount of energy sourced from fossils continues to decline, it is necessary to do energy diversification efforts, namely efforts to use alternative energy. Based on the ESDM Ministry Strategic Plan for 2015-2019, Indonesia's oil reserves of 3.6 billion barrels are expected to run out in the next 13 years. The Minister of Transportation (2009-2014) EE Mangindaan said that the use of biofuels and renewable energy for the transportation sector in particular also encouraged the increase of local content both from the mastery of research, technology and applications from upstream to downstream in all supply chains, production and distribution. The idea of ​​using microalgae as a fuel source is not new, but is now taken seriously because of the increase in petroleum prices and more importantly, the problems that arise about global warming and the greenhouse effect associated with burning fossil fuels. The advantages of microalgae compared to other plants are high photosynthetic efficiency, producing more biomass, faster growth, not competing with food production, reducing greenhouse gas emissions, can convert CO2 into biomass, have a side component other than lipids, can save water resources because it uses recycled water, can survive in high salinity, 10-100 times produce biodiesel compared to other plants for the same area, a shorter life cycle and in accordance with Indonesia's climate.
Simulasi Distribusi Manpower Pemeliharaan Maskapai X Dengan Metode Northwest Corner, Least Cost, Dan Vogel’s Approximation Method Mahendra, Moch. Rezza; Arifin, Mufti; Utama, Ericko
Jurnal Mahasiswa Dirgantara Vol. 1 No. 2 (2022): Jurnal Mahasiswa Dirgantara
Publisher : FTK UNSURYA

Show Abstract | Download Original | Original Source | Check in Google Scholar

Abstract

Pemeliharaan pesawat udara sangat penting dilakukan. Dimana pada saat ini pesawat udara sebagai salah satu alat transportasi yang digunakan oleh masyarakat. Hal tersebut membutuhkan manpower untuk kegiatan pemeliharaan terjadwal dan tidak terjadwal. Salah satu kegiatan pemeliharaan terjadwal adalah A04-Check yang membutuhkan jumlah manpower cukup banyak untuk pemeliharaannya. Pada maskapai X mempunyai manpower yang terbatas dan harus mengirimkan manpower tersebut ke bandara- bandara pemeliharaan yang kekurangan manpower. Simulasi distribusi manpower dibutuhkan untuk mencari solusi untuk mengirimkan manpower dengan mencari biaya yang minmum. Pusat bandara pemeliharaan pada simulasi adalah Bandara Soekarno-Hatta (CGK), Bandara Juanda (SUB) dan Bandara Sultan Hasanuddin (UPG). Simulasi pada penelitian menggunakan data pemeliharaan A04-Check pesawat ATR 72- 600 sebagai dasar referensi melihat banyaknya pekerjaan jumlah manhour dan perkiraan jumlah manpower yang dibutuhkan pada saat pemeliharaan. Pada penelitian menggunakan metode transportasi solusi awal yaitu: Metode Northwest Corner, Least Cost, dan Vogel’s Approximation Method. Metode transportasi adalah metode yang digunakan untuk permasalahan pengiriman barang dengan mencari biaya yang minimum. Pada simulasi ini metode transportasi digunakan untuk mencari solusi agar maskapai X bisa meminimalkan biaya operasional pengiriman manpower ke setiap bandara pemeliharaan yang dibutuhkan. Biaya dengan metode Northwest Corner mendapatkan solusi biaya sebesar 4718 USD atau Rp.68.920.779,90, sedangkan pada metode Least Cost memperoleh biaya sebesar 3451 USD Atau Rp.50.412.380,55 , dan pada metode Vogel’s Approximation Method memperoleh biaya sebesar 2884 USD atau Rp.42.129.616,20. Sehingga alokasi pengiriman manpower yang paling hemat adalah metode Vogel’s Approximation Method.
Pelatihan Penyusunan Modul Praktikum Fisika Pada Guru SMK Gutama Jakarta dengan Memanfaatkan Artificial Intelligence Sari, Rafika Arum; Mufti Arifin; Syarifah Fairuza; Ade Julizar; Ericko Chandra Utama
Jurnal Bakti Dirgantara Vol. 2 No. 1 (2025): Jurnal Bakti Dirgantara
Publisher : Universitas Dirgantara Marsekal Suryadarma

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.35968/h7saky24

Abstract

Peningkatan kualitas pembelajaran sains di Sekolah Menengah Kejuruan (SMK) merupakan tantangan yang mendesak, terutama dalam pengembangan modul praktikum yang relevan dan aplikatif. Kegiatan Pengabdian Kepada Masyarakat (PKM) ini dilaksanakan oleh Program Studi Teknik Penerbangan Universitas Dirgantara Marsekal Suryadarma sebagai respons terhadap kebutuhan guru dalam menyusun modul fisika yang inovatif dan sesuai dengan perkembangan teknologi. Tujuan dari PKM ini adalah memberikan pelatihan kepada guru-guru SMK Gutama Jakarta untuk menyusun modul praktikum fisika secara mandiri dengan memanfaatkan kecerdasan buatan (AI), khususnya melalui pemanfaatan ChatGPT. Kegiatan dilaksanakan pada bulan Desember 2024 dan diikuti oleh 7 guru bidang sains. Metode yang digunakan meliputi survei awal untuk pemetaan kebutuhan, pemaparan materi tentang pemanfaatan AI dalam pendidikan, serta praktik langsung penyusunan modul bertema kesetimbangan gaya dengan bimbingan instruktur. Hasil evaluasi melalui angket menunjukkan bahwa 66,7% peserta memberikan respon yang sangat positif terhadap pelatihan ini. Temuan ini menunjukkan bahwa teknologi AI, seperti ChatGPT, dapat menjadi solusi praktis dan efektif dalam mendukung guru menyusun modul praktikum yang kontekstual dan sesuai kebutuhan pembelajaran di lapangan.   Improving the quality of science education in vocational high schools (SMK) remains an urgent challenge, particularly in the development of relevant and applicable practicum modules. This community service program (PKM) was conducted by the Aeronautical Engineering Study Program at Universitas Dirgantara Marsekal Suryadarma in response to the need for teachers to independently develop innovative physics practicum modules aligned with current technological advancements. The primary objective of this PKM was to train science teachers at SMK Gutama Jakarta in utilizing artificial intelligence (AI), specifically ChatGPT, for the independent development of physics practicum modules. The activity was conducted in December 2024 and involved seven science teachers. The method included a preliminary needs assessment survey, presentation of AI applications in education, and hands-on practice in developing a practicum module on the topic of force equilibrium, guided by instructors. Evaluation results obtained through post-training questionnaires revealed that 66.7% of participants responded very positively to the training. These findings indicate that AI-based tools, such as ChatGPT, can serve as practical and effective solutions for assisting teachers in creating contextual and field-relevant practicum modules.
Analisis Strategi Dan Feasibility Pengembangan MRO Pemeliharaan Engine Di Indonesia Freddy Franciscus; Ericko Chandra Utama
Jurnal Teknologi Kedirgantaraan Vol 5 No 1 (2020): Jurnal Teknologi Kedirgantaraan
Publisher : FTK UNSURYA

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.35894/jtk.v5i1.282

Abstract

The aircraft maintenance business in Indonesia is still very attractive along with increasing number of aircraft on Indonesia airlines. As much as 65% of the aircraft maintenance costs of domestic airlines that have not been absorbed by MRO Indonesia. Most of the unabsorbed portions are aircraft engine and component maintenance clusters which only absorb about 10% (USD 100 Million) of 75% (USD 750 Million Th 2017) engine maintenance costs (35%) and aircraft components (45%), issued by Indonesian airlines. From the 10% uptake of engine maintenance costs and components, the portion of engine maintenance maintenance uptake is only 5% (USD 50 Million) of 35% (USD 350 Million) engine maintenance costs. There is still around 30% (USD 300 Million) which is an opportunity for MRO Indonesia to develop the engine maintenance capability of Indonesian airlines. Based on several types of aircraft engines in Indonesian airlines, CFM56-7B used by B737-800/900 which has the largest population of around 450 engines. From the feasibility analysis on the development of the capability of the MRO engine for maintenance of the CFM56-7B, the ROI and Pay Back Period / PBP calculations for the capability engine development program are 24.57% and 4.4 years respectively. The ROI and PBP show that the CFM56-7B MRO engine development strategy is feasible.
Pengukuran Kebisingan Pesawat Udara dengan Memasukan Frekuensi Kebisingan di Sekitar Bandara Halim Perdana Kusuma Raihan Sakti Pratama; Mufti Arifin; Imron Rosadi; Ericko Utama
Jurnal Mahasiswa Dirgantara Vol. 4 No. 2 (2025): Jurnal Mahasiswa Dirgantara
Publisher : FTK UNSURYA

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.35894/jmd.v4i2.104

Abstract

The high usage of air transportation today is driven by the community's need for faster and more efficient mobility. However, the impact of using aircraft cannot be ignored, especially in terms of noise pollution caused by aircraft engines. Halim Perdana Kusuma Airport, which was originally designed for military activities, has become a commercial airport since 2014 in an effort to reduce flight density at Soekarno-Hatta Airport. This study aims to measure aircraft noise around Halim Perdana Kusuma Airport by including frequency. Measurements were carried out using a dB meter application downloaded on a mobile phone and a Sound Level Meter, both during flight activity and without flight activity in surrounding settlements. The results of this study indicate that noise in dBA can be measured with a Sound Level Meter, while frequency can be measured with a smartphone that has a dB meter application installed. The highest frequency measured during aircraft take-off activity at Halim Perdana Kusuma Airport peaked at 7716 Hz to 7834 Hz, when the noise reached its highest point. From this research, it can be concluded that the higher the frequency The higher the frequency the smaller ∆LA, meaning the dBA is getting closer to the sound pressure level.