ANALISIS KEANDALAN BOOSTER PUMP PADA PESAWAT KT-IB DENGAN MENGUNAKAN METODE FAULT TREE ANALYSIS

SAMUEL EDEL KOIBUR, FRANKLIN (2020) ANALISIS KEANDALAN BOOSTER PUMP PADA PESAWAT KT-IB DENGAN MENGUNAKAN METODE FAULT TREE ANALYSIS. Skripsi thesis, Institut Teknologi Dirgantara Adisutjipto.

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Abstract

Booster pump is a very important component in airplane, which functions to transfer fuel with a pressure of 20 psi from the tank to the fuel pump, so that the fuel to be channeled to the engine has a stable or regular pressure and flow rate. Failure of the booster pump can cause the plane to fall so that the possibility of the plane having an accident and casualties. This study discusses the reliability of the booster pump on the KT-1B aircraft which includes the booster reliability process using the fault tree analysis method. Aircraft flight regulations cover the safety and reliability of the aircraft being manufactured. The reliability assessment begins with the identification of the system function, failure conditions and failure effects. There are two methods used, the quantitative fault tree analysis method and the qualitative method of the functional hazard assessment. The results showed that the Pf ( Probalility of failure ) based on the failure calculation was 3x10-3 , while the one allocated was 10-1 . So thus the number of booster pump failures can still be accepted.

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