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All Journal Prosiding SNITP (Seminar Nasional Inovasi Teknologi Penerbangan) Airman
Louis Latif, Hendri
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Aerospace Engineering Education Electrical & Electronics Engineering Engineering Industrial & Manufacturing Engineering Transportation

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Rancangan Model Speed Brake Flaps Tipe Clamsheel sebagai Alat Peraga di Prodi Teknik Pesawat Udara Sekolah Tinggi Penerbangan Indonesia Louis Latif, Hendri; Kuntoaji, Wahyu
Airman: Jurnal Teknik dan Keselamatan Transportasi Vol 3 No 1 (2020): Airman: Jurnal Teknik dan Keselamatan Transportasi
Publisher : Politeknik Penerbangan Makassar

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.46509/ajtk.v3i1.181

Abstract

Seeing the development of technology in the world of aviation at this time felt very rapidly, this must also be accompanied by practical tools that must follow the development of these technologies to support teaching and learning activities. To support teaching and learning activities, therefore the author intends to make modeling of teaching aids speed brake flaps found on an aircraft, and introducing the speed brake flaps system found on an aircraft and can also provide an overview of the flight control system regarding speed brake flaps so that the teaching process can be successful in accordance with the objectives of the syllabus, namely students have the ability to can understand the basic principles of aircraft structure and have the basic ability to perform maintenance, because so far students can only imagine never seeing directly the tools being learned. seed brake is a type of flight control surface used on aircraft to increase drag (drag). This speed brake simulation provides an overview of the operation and mechanism of action of a speed brake. This design was made with a simple system to facilitate operation. In the designer, the method used is the library method using literature books and experimental methods. Because it is only as a prop, the hydraulic pressure needed is low. The hydraulic pressure used to operate the design of this trainer is 90 psi with a load on the mechanical system of 160.83 lbs. The electric current source used to operate the design of this teaching aid is 220V AC to start an electric motor with 1 HP power so that it rotates the gear type hydraulic pump which produces pressurized fluid for operation. It takes a power of 766 Watt to operate the design of these Trainer.
Pengembangan Bahan Ajar Mata Kuliah Aircraft Structure, Equipment and Furnishing Di Politeknik Penerbangan Makassar Louis Latif, Hendri; Nur, Mulyadi; Octavianie, Adhitya; Rossydi, Ahmad
Prosiding SNITP (Seminar Nasional Inovasi Teknologi Penerbangan) Vol. 8 No. 1 (2024): SNITP 2024
Publisher : Politeknik Penerbangan Surabaya

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.46491/snitp.v8i1.1945

Abstract

Pada mata kuliah Aircraft Structure, Equipment and Furnishing di Politeknik Penerbangan Makassar, Instruktur dan Dosen masih menggunakan bahan ajar power point dan buku manual. Hal ini kurang efektif diterapkan untuk pembelajaran. Berdasarkan hasil kueisoner kebutuhan Taruna/I menunjukkan 34,2% atau 12 Taruna/I masih belum memahami dengan baik pembelajaran tersebut. Maka dari itu perlu dilakukan pengembangan bahan ajar untuk menunjang proses pembelajaran aircraft structure yang dimana pada penelitian ini dilakukan pengembangan bahan ajar menggunakan e-modul. E-modul dibuat mengacu kurikum dan silabus Teknologi Pemeliharaan Pesawat Udara Program Diploma III dari Pusat Pengembangan Sumber Daya Manusia Perhubungan Udara. Desain e-modul dilakukan dengan merancang bentuk dan konten e-modul mulai dari cover, introduction, tujuan pembelajaran, materi sampai dengan evaluasi. Berdasarkan hasil kuesioner efektivitas e-modul Aircraft Structure Equipment and Furnishing menunjukkan keseluruhan penilaian kueisioner efektivitas e-modul Aircraft Structure berada pada kriteria Sangat Baik dengan perolehan Skor 4,36 dan Presentase 87.3%. Perolehan penilaian tertinggi diperoleh pada aspek Kelayakan isi dengan Skor 4,39 dan Presentase 87,8% dan penilaian terendah diperoleh pada aspek Desain Tampilan dengan Skor 4,31 dan Presentase 86,2 %.
Co-Authors Kuntoaji, Wahyu Nur, Mulyadi Octavianie, Adhitya Rossydi, Ahmad