ANALISA DAN PENANGANAN TERJADINYA SLOW RESPON
ENGINE SYSTEM CFM 56-3 PADA PESAWAT BOEING 737-
300 TRI MG PT. MULYA SEJAHTERA TECHNOLOGY
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Institusion
INSTITUT TEKNOLOGI DIRGANTARA ADISUTJIPTO
Author
WAHYU DUANTO, DEPANO
Subject
T Technology (General)
Datestamp
2024-04-25 03:54:15
Abstract :
The fuel system is the most important fuel system on an airplane when flying to deliver fuel to the combustion chamber and also to cool the oil temperature while at altitude. The problem that occurs on the Boeing 737-300 TRI-MG aircraft at Hangar hall e PT Mulya Sejahtera Technology Bandung is a problem with the fuel system, indicated by the appearance of a slow response to the high pressure compressor (N2) when rotating during take off at the airport. These problems can affect the flight performance of the aircraft. In this study, the direct observation method was used to observe and analyze the handling of the Boeing 737-300 TRI-MG aircraft at Hangar hall e PT Mulya Sejahtera Technology Bandung. In addition, this study also uses the fault tree analysis method to obtain the root cause of the failure of the Boeing 737-300 TRI- MG fuel system The results of the research on the problems of the Boeing 737-300 TRI-MG Fuel system are problems with the fuel filter, fuel pump, and fuel distribution system. These problems were solved by performing troubleshooting referring to AMM Boeing 777-300, AMM Boeing 737-300 task 30-00-41 for trouble shooting, AMM Boeing 737-300 task 73-11-01 for removal and installation of fuel pump and AMM Boeing. 737-300 task 73-11-02 for removal and installation of fuel filters. By using the fault tree analysis method.
The fuel system is the most important fuel system on an airplane when flying to deliver fuel to the combustion chamber and also to cool the oil temperature while at altitude. The problem that occurs on the Boeing 737-300 TRI-MG aircraft at Hangar hall e PT Mulya Sejahtera Technology Bandung is a problem with the fuel system, indicated by the appearance of a slow response to the high pressure compressor (N2) when rotating during take off at the airport. These problems can affect the flight performance of the aircraft. In this study, the direct observation method was used to observe and analyze the handling of the Boeing 737-300 TRI-MG aircraft at Hangar hall e PT Mulya Sejahtera Technology Bandung. In addition, this study also uses the fault tree analysis method to obtain the root cause of the failure of the Boeing 737-300 TRI- MG fuel system The results of the research on the problems of the Boeing 737-300 TRI-MG Fuel system are problems with the fuel filter, fuel pump, and fuel distribution system. These problems were solved by performing troubleshooting referring to AMM Boeing 777-300, AMM Boeing 737-300 task 30-00-41 for trouble shooting, AMM Boeing 737-300 task 73-11-01 for removal and installation of fuel pump and AMM Boeing. 737-300 task 73-11-02 for removal and installation of fuel filters. By using the fault tree analysis method.
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