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All Journal JURNAL INTEGRASI Jurnal Teknologi dan Riset Terapan (JATRA) Jurnal Pengabdian kepada Masyarakat Politeknik Negeri Batam
James Siregar
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Aerospace Engineering Computer Science & IT Economics, Econometrics & Finance Electrical & Electronics Engineering Engineering Mechanical Engineering Other

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Journal : JURNAL INTEGRASI

 1 
RANCANG BANGUN SIMULASI PERGERAKAN HIGH LIFT DEVICE PADA PESAWAT lalu giat juangsa putra; James Siregar; Dedy Syarif Qusyairi
JURNAL INTEGRASI Vol 12 No 2 (2020): Jurnal Integrasi - Oktober 2020
Publisher : Politeknik Negeri Batam

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.30871/ji.v12i2.2204

Abstract

The most high lift device modifying, for small airplanes and large, is the wing flap. Flaps can be installed on the leading edge or trailing edge (only for large airplane) aircraft. To make a simulator, the design and also the drive system are needed which will form the movement as in the real flap. As a driving mode, the system which designed on this flap simulator will use an electronic system. By using a servo motor as a drive and Arduino as a microcontroller that will be programmed according to the planned movement. The flap simulator can produce angles formed on servo motors such as 5º, 14º, 19º, 25º and 30º its moving flaps on flap level 0, 1, 2, 3 and 4 in extend and retract movement modes.
Identifikasi Penyebab Terjadinya Landing Gear Indication Tidak Berfungsi Normal pada Pesawat Boeing 737-900 ER Mohamad Alif Dzulfiqar; Nabila Ayu Saputri; Nova, Muhammad Andi; James Siregar; Lalu Giat Juangsa Putra; Nur Rafia Dija; Meilani Mandhalena
JURNAL INTEGRASI Vol. 17 No. 1 (2025): Jurnal Integrasi - April 2025
Publisher : Pusat Penelitian dan Pengabdian Masyarakat Politeknik Negeri Batam

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.30871/ji.v17i1.9510

Abstract

The Boeing 737-900 ER aircraft has a system called landing gear indication which in its application uses a proximity sensor that is useful in providing information about the position of the landing gear. However, this system can experience problems where if the landing gear indication does not function, the pilot cannot obtain information from the instrument that ensures the position of the landing gear. The purpose of this study is to identify problems that often occur in the landing gear indication system on the aircraft. The analysis was carried out using the Root Cause Analysis (RCA) method with the Fishbone Diagram approach. From the identification results, it was found that the main cause was a problem with the proximity switch sensor experiencing corrosion and changes in position which caused the signal reading to be inaccurate. For this reason, it is necessary to replace components and adjust the sensor position so that the system can run properly.
Co-Authors Abda Abda Abulija Maskarai Annisa Fyona Ari Wibowo Arif Wahyu Budiarto Asrafi Asrafi Aulia Fajrin Billi Aldin Sumadireja Budi Baharudin Dedy Syarif Qusyairi Dicky Reza Prawira Dija, Nur Rafia Domi Kamsyah Fauzun Atabiq Fedia Restu Hanifah Widiastuti Hendra Saputra Ihsan Saputra Irwanto Zarma Putra Kartika Kartika Lalu Giat Juangsa Putra Meida Perwira Antartika Meilani Mandhalena Mohamad Alif Dzulfiqar Mufti Fathonah M Mufti Fathonah Muvariz Muhammad Andi Nova Muhammad Ismail Muhammad Nurhidayat Muhammad Syafei Gozali Nabila Ayu Saputri Naufal A Prasetyo Naufal Abdurrahman Prasetyo Nidia Yuniarsih Nidia Yuninarsih Nova, Muhammad Andi Nugroho Pratomo Ariyanto Nur Fitria Pujo Leksonowati Nur Rafia Dija Nurman Pamungkas Nurul Laili Arifin Nurul Laili Arifin Nurul Ulfah Rahman Hakim Rizky Pratama Hudhajanto Saiful Akhyar Lubis Sapto Wiratno Satoto Widodo Widodo Wowo Rossbandrio Yattawuri Arinta Timur Yogantara Yogantara