PENANGANAN DAN ANALISIS KEGAGALAN ANTISKID SYSTEM PADA PESAWAT BOEING 737-800 NEXT GENERATION MENGGUNAKAN METODE FISHBONE DI FL TECHNICS INDONESIA

HELGA CHAERUDIN, MUHAMMAD (2023) PENANGANAN DAN ANALISIS KEGAGALAN ANTISKID SYSTEM PADA PESAWAT BOEING 737-800 NEXT GENERATION MENGGUNAKAN METODE FISHBONE DI FL TECHNICS INDONESIA. Tugas Akhir thesis, Institut Teknologi Dirgantara Adisutjipto.

[img] Text (ABSTRAK)
20060020_ABSTRAK.pdf

Download (138kB)
[img] Text (BAB I)
20060020_BAB 1.pdf

Download (99kB)
[img] Text (DAFTAR PUSTAKA)
20060020_DAFTAR PUSTAKA.pdf

Download (92kB)
[img] Text (FULL SKRIPSI)
20060020.pdf
Restricted to Repository staff only

Download (2MB)

Abstract

During landing, the craft will require a monitoring system that will enable it to maintain a steady speed while maintaining the safety of the crew members. Thus, there is a pesawat braking system that uses hydraulics as its primary means of providing force so that pengereman can be carried out as efficiently as possible; this system is known as the brake system. Integrating this system with other components and systems of the Boeing 737-800 Next Generation is very important for ensuring safe maintenance operations. The fishbone analysis is one of the most effective techniques available for data analysis to identify problems by analyzing the causes of the problems that occur. The purpose of the antiskid system is to ensure that the pesawat does not experience slippage or skidding when doing maintenance. Based on analysis conducted using the fishbone diagram method, there are a few factors that contribute to antiskid failure. Factors such as technology, environmental conditions, landmass aging, and human behavior can affect the anti-skid system's performance. If there are indications of malfunction in the valve catup that corresponds to AMM Aircraft Maintenance Manual Chapter 32–42, Task 801, then the Antiskid maintenance procedure will be carried out. The first step is to apply resistance training to antiskid. Normal resistance between 180 and 200 Ω at 70 ±5°F 21 ±3°C. If the resistance is outside the batas, an antiskid event will occur, necessitating penanganan. Thus, in accordance with the Fault Isolation Manual, the new component's installation and removal must be carried out using the Aircraft Maintenance Manual.

Item Type: Thesis (Tugas Akhir)
Subjects: T Technology > T Technology (General)
Divisions: Institut Teknologi Dirgantara Adisujtipto > D3 Aeronaitika
Depositing User: Mr Muhammad helgacherudin
Date Deposited: 20 May 2024 05:02
Last Modified: 20 May 2024 05:02
URI: http://eprints.stta.ac.id/id/eprint/1752

Actions (login required)

View Item View Item

Downloads

Downloads per month over past year