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Sihono
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RANCANG BANGUN MAGNETO TESTER BERKECEPATAN 30-3000 RPM DI HANGAR 01 TEKNIK PESAWAT UDARA SEKOLAH TINGGI PENERBANGAN INDONESIA Niko Ardian; Sihono; Amal Fatkhulloh
Langit Biru: Jurnal Ilmiah Aviasi Vol 13 No 01 (2020): Langit Biru: Jurnal Ilmiah Aviasi Vol.13 No.1 [Februari 2020]
Publisher : Politeknik Penerbangan Indonesia Curug

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Abstract

B.IndonesiaPada Program Studi Teknik Pesawat Udara Sekolah Tinggi Penerbangan Indonesia taruna melakukan praktek memasang, membongkar dan menguji magneto. Dalam pengujian magneto, dibutuhkan putaran tertentu yaitu 1000,2000 dan 3000. Pengujian tersebut dilakukan dengan menggunakan alat tester magneto agar mengetahui kondisi magneto dengan indikator percikan konstan. Berdasarkan beberapa identifikasi masalah yang akan menjadi batasan masalah adalah bagaimana merancang magneto tester berkecepatan 30-3000RPM. Dari hasil perhitungan dan perancangan yang telah dilakukan, alat yang dibuat belum mampu mencapai putaran yang diingkinkan. Putaran maksimum yang tercapai adalah 2984 rpm.B.EnglishThe Aircraft Engineering Study Program of Indonesian Civil Aviation Institute, cadets practice installing, managing and restoring magneto. In magneto testing, certain rounds of 1000,2000 and 3000 are required. This test is carried out using a magneto tester in order to know the magneto conditions with a constant spark indicator. Based on several considerations, the problem that will be the limitation of the problem is how to return a magneto tester with a 30-3000 RPM. From the results of calculations and designs that have been carried out, the tools made have not been able to reach the desired rotation. The maximum successful duration is 2984 rpm.
ANALISIS KESALAHAN PENUNJUKAN INDIKATOR TEKANAN BAHAN BAKAR DITINJAU DARI KERUSAKAN TRANSDUCER PADA PESAWAT SOCATA TB-10 DI SEKOLAH TINGGI PENERBANGAN INDONESIA CURUG-TANGERANG Bela Firmantoyo; Sihono
Langit Biru: Jurnal Ilmiah Aviasi Vol 12 No 1 (2019): Langit Biru: Jurnal Ilmiah Aviasi
Publisher : Politeknik Penerbangan Indonesia Curug

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Trainer aircraft type Socata TB-10 is one of the types of aircraft piston engine (engine) used by Indonesian Civil Aviation Institute. The aircraft began to be used for flight training for cadets STPI Airmen Department since August 1997. During operation of the Socata TB-10 aircraft within a certain time there is a mistake appointing fuel pressure indicator on all Socata TB-10 aircraft that existed at Indonesian Civil Aviation Institute Curug-Tangerang. This designation errors either low pressure, high pressure in the run-up both positions, climbing cruising and landing. To support error analysis designation fuel pressure indicator required some theories that the aircraft fuel system TB-10, the designation system fuel pressure, transducer, transducer sensitivity. To solve these problems required transducer calibration test of the fuel components. Testing was conducted at the Indonesian Institute of Sciences Research Center Instrumentation Calibration and Metrology (KIM-LIPI). Based transducer calibration test and results analysis is, the cause of the error designation fuel pressure indicator in terms of damage to the fuel pressure transducer is rated third transducer sensitivity tested had a sensitivity value greater than the allowed value sensitivity (standard). Resulting voltage change corresponding outgoing errors resulting in the appointment of a fuel pressure indicator on the Socata TB-10 aircraft owned by Indonesian Civil Aviation Institute Curug-Tangerang.
KONTRIBUSI METODE PERSEDIAAN BARANG YANG TEPAT TERHADAP KELANCARAN ARUS PEMAKAIAN SUKU-CADANG PESAWAT DI SEKOLAH TINGGI PENERBANGAN INDONESIA CURUG-TANGERANG A. Nugroho Budi; Sihono
Langit Biru: Jurnal Ilmiah Aviasi Vol 12 No 2 (2019): Langit Biru: Jurnal Ilmiah Aviasi
Publisher : Politeknik Penerbangan Indonesia Curug

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Inventories is not only considered a burden because it is wasteful, but at the same time it can also be considered as wealth that can be immediately disbursed in the form of product activities. The problem is focused on the current situation for the service and management of contributions and distribution of training aircraft parts that have an impact on the smooth flight training. With the existing problems the writer tries to solve the problem, in the current condition in the warehouse. As a result, these items cannot be obtained instantly, but a grace period is needed to get or find a location, a non-systemic numbering system using a computer. With a manual system, the easiest way to do it is done. Still using the document paper form as a control tool. The limitation is even lacking in responding to the importance of the warehouse planning and management system so that training time is a bit hampered by time. In the research opportunity that we raised on the method of contributing to the smooth flow of usage of restricted aircraft parts without evaluating energy and budget, so it is expected to make a single step change in the system of goods contribution to cut the time and the right inventory.
RANCANGAN TURBIN EKSPANSI TIPE RADIAL SATU TINGKAT DENGAN MASSA ALIRAN UDARA INPUT SEBESAR 0,245 KG/S Ego Widoro; Sihono
Langit Biru: Jurnal Ilmiah Aviasi Vol 13 No 02 (2020): Langit Biru: Jurnal Ilmiah Aviasi Vol.13 No.2 [Juni 2020]
Publisher : Politeknik Penerbangan Indonesia Curug

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Abstract

B.Indonesia Penggunaan turbin sangat luas, sesuai dengan fungsinya turbin didisain dalam bentuk khusus untuk dapat melakukan fungsinya tersebut, salah satunya turbin dapat digunakan sebagai turbin ekspansi pada air cycle machine yang digunakan sebagai sistem pendingin udara di kabin pesawat terbang. Perancangan turbin radial satu tingkat sebagai turbin ekspansi yang mudah dan murah biaya produksinya serta memiliki efisiensi yang tinggi. Perancangan ini diawali dengan menghitung parameter disain awal dan dilanjutkan dengan tahapan perancangan mendisain impeler turbin, nosel inlet turbin dan scroll turbin. Parameter disain turbin yang diperoleh dari perhitungan mencakup parameter non dimensional dan dimensional. B.English The utility of turbine is very wide, according to the function of turbine designed in special form to be able to perform this function, one of which the function is the turbine can be used as expansion turbine on air cycle machine that used as air cooling system in aircraft cabin. The design of a single stage radial turbine as an expansion turbine with easy and inexpensive production and high efficiency. This design begins with calculating the initial design parameters and continued with the design steps of designing the turbine impeller, inlet turbine nozzles and turbine scroll. Turbine design parameters derived from calculations include non-dimensional and dimensional parameters.
PROSES DAN PENYEBAB TERJADINYA KOROSI PADA PESAWAT TERBANG Sihono; Sukahir
Langit Biru: Jurnal Ilmiah Aviasi Vol 2 No 4 (2009): Langit Biru: Jurnal Ilmiah Aviasi
Publisher : Politeknik Penerbangan Indonesia Curug

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KONSEP SISTEM MANAJEMEN PERAAWATAN PERALATAN ELEKTRONIKA DAN LISTRIK BANDARA Ibnu Hermawan; Sihono
Langit Biru: Jurnal Ilmiah Aviasi Vol 2 No 5 (2009): Langit Biru: Jurnal Ilmiah Aviasi
Publisher : Politeknik Penerbangan Indonesia Curug

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RANCANGAN TURBIN EKSPANSI TIPE RADIAL SATU TINGKAT DENGAN MASSA ALIRAN UDARA INPUT SEBESAR 0,245 KG/S Ego Widoro; Sihono
Langit Biru: Jurnal Ilmiah Aviasi Vol 13 No 02 (2020): Langit Biru: Jurnal Ilmiah Aviasi Vol.13 No.2 [Juni 2020]
Publisher : Politeknik Penerbangan Indonesia Curug

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

Abstract

B.Indonesia Penggunaan turbin sangat luas, sesuai dengan fungsinya turbin didisain dalam bentuk khusus untuk dapat melakukan fungsinya tersebut, salah satunya turbin dapat digunakan sebagai turbin ekspansi pada air cycle machine yang digunakan sebagai sistem pendingin udara di kabin pesawat terbang. Perancangan turbin radial satu tingkat sebagai turbin ekspansi yang mudah dan murah biaya produksinya serta memiliki efisiensi yang tinggi. Perancangan ini diawali dengan menghitung parameter disain awal dan dilanjutkan dengan tahapan perancangan mendisain impeler turbin, nosel inlet turbin dan scroll turbin. Parameter disain turbin yang diperoleh dari perhitungan mencakup parameter non dimensional dan dimensional. B.English The utility of turbine is very wide, according to the function of turbine designed in special form to be able to perform this function, one of which the function is the turbine can be used as expansion turbine on air cycle machine that used as air cooling system in aircraft cabin. The design of a single stage radial turbine as an expansion turbine with easy and inexpensive production and high efficiency. This design begins with calculating the initial design parameters and continued with the design steps of designing the turbine impeller, inlet turbine nozzles and turbine scroll. Turbine design parameters derived from calculations include non-dimensional and dimensional parameters.
RANCANGAN TURBIN EKSPANSI TIPE RADIAL SATU TINGKAT DENGAN MASSA ALIRAN UDARA INPUT SEBESAR 0,245 KG/S Ego Widoro; Sihono
Langit Biru: Jurnal Ilmiah Aviasi Vol 13 No 02 (2020): Langit Biru: Jurnal Ilmiah Aviasi Vol.13 No.2 [Juni 2020]
Publisher : Politeknik Penerbangan Indonesia Curug

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

Abstract

B.Indonesia Penggunaan turbin sangat luas, sesuai dengan fungsinya turbin didisain dalam bentuk khusus untuk dapat melakukan fungsinya tersebut, salah satunya turbin dapat digunakan sebagai turbin ekspansi pada air cycle machine yang digunakan sebagai sistem pendingin udara di kabin pesawat terbang. Perancangan turbin radial satu tingkat sebagai turbin ekspansi yang mudah dan murah biaya produksinya serta memiliki efisiensi yang tinggi. Perancangan ini diawali dengan menghitung parameter disain awal dan dilanjutkan dengan tahapan perancangan mendisain impeler turbin, nosel inlet turbin dan scroll turbin. Parameter disain turbin yang diperoleh dari perhitungan mencakup parameter non dimensional dan dimensional. B.English The utility of turbine is very wide, according to the function of turbine designed in special form to be able to perform this function, one of which the function is the turbine can be used as expansion turbine on air cycle machine that used as air cooling system in aircraft cabin. The design of a single stage radial turbine as an expansion turbine with easy and inexpensive production and high efficiency. This design begins with calculating the initial design parameters and continued with the design steps of designing the turbine impeller, inlet turbine nozzles and turbine scroll. Turbine design parameters derived from calculations include non-dimensional and dimensional parameters.
Pengaruh Media Permainan Tebak Kata Dalam Meningkatkan Minat Belajar Bahasa Arab Siswa Kelas V Mi Al Iman Sorogenen Tahun Ajaran 2023/2024 Syukmi Muniratul Kamalia; Sihono; Banat Su'adini Sabrina
Mahira: Journal of Arabic Studies & Teaching Vol. 2 No. 2 (2024)
Publisher : Pendidikan Bahasa Arab Fakultas Ilmu Tarbiyah dan Keguruan UIN Sunan Kalijaga Yogyakarta

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.14421/mahira.2024.22.05

Abstract

This study aims to analyze the effect of using the word-guessing game as an instructional medium on the Arabic learning interest of fifth-grade students at MI Al Iman Sorogenen in the 2023/2024 academic year. The research employed an experimental method with a pretest-posttest control group design. All 20 students of the fifth grade were involved as research subjects. Data were collected through observation, interviews, questionnaires, and documentation, and were then analyzed descriptively using SPSS version 25. The results revealed that there was no significant effect of the word-guessing game on increasing students’ interest in learning Arabic, as indicated by a significance value of 0.104 (p > 0.05). These findings suggest that further investigation into instructional media innovations is necessary to enhance students’ interest in learning Arabic at the elementary school level.
Analisis Buku Fun Learning Jago Bahasa Arab Basic 1 (Tinjauan Kelayakan Isi, Penyajian, Bahasa dan Kegrafikan) Rianda Ayu Ritnaning Tias; Sihono
Mahira: Journal of Arabic Studies & Teaching Vol. 2 No. 2 (2024)
Publisher : Pendidikan Bahasa Arab Fakultas Ilmu Tarbiyah dan Keguruan UIN Sunan Kalijaga Yogyakarta

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.14421/mahira.2024.22.06

Abstract

The selection and use of appropriate textbooks is very important in supporting the effectiveness of learning, especially at the primary education level. The number of textbooks on the market with various qualities requires an objective evaluation of the feasibility of textbooks. This study aims to analyze the feasibility of the Fun Learning Jago Arabic Basic 1 book based on four aspects of assessment from BSNP, namely content, presentation, language, and graphics. This research uses a qualitative approach of library research with data collection through document analysis and semi-structured interviews with the author of the book. The results showed that the book obtained an average score of 3.41 (good) for content eligibility, 3.22 (good) for presentation, 3.41 (good) for language, and 3.76 (excellent) for graphics. The book excels in visual design, integration of audio-visual media, and presentation of contextualized and fun material for children. However, shortcomings were found in grammatical accuracy, presentation structure, and completeness of supporting elements such as SK-KD and glossary. In conclusion, this book is feasible to be used as Arabic teaching materials in elementary schools with a note of improvement on several aspects to increase learning effectiveness.
Co-Authors A. Nugroho Budi Amal Fatkhulloh Banat Su'adini Sabrina Bela Firmantoyo Ego Widoro Ibnu Hermawan Niko Ardian Rianda Ayu Ritnaning Tias SUKAHIR Syukmi Muniratul Kamalia