ANALISIS RELIABILITY FUEL SYSTEM UNTUK PESAWAT TM - 13
Total View This Week0
Total View This Week0
Institusion
INSTITUT TEKNOLOGI DIRGANTARA ADISUTJIPTO
Author
LEONETO DE DEUS A. ALMEIDA, ROGER
Subject
T Technology (General)
Datestamp
2024-06-25 03:39:48
Abstract :
uel system is an essential system in aircraft used to drain fuel from the tank to the engine. The failure of the fuel system can cause the plane to have an accident, such as crash and death. This research discussed the reliability of the fuel system on the TM-13 aircraft which included the process of fuel system reliability. In flight regulations airplanes included the safety and reliability of aircraft produced. The reliability assessment began by identifying the system functions, the failure conditions, and the lack of success. There were two methods used; quantitative methods in the form of fault tree analysis and qualitative methods in the form of functional hazard assessment. The results showed the probability of the total failure of the fuel system capability on the TM-13 aircraft was 6.6580x10-10. The probability of this failure was smaller than functional hazard assessment, 1x10-9. Because of the probability of the failure, the fuel system on the TM-13 aircraft has met the requirements. Thus, the architecture of the TM-13 aircraft fuel system is safe to use
uel system is an essential system in aircraft used to drain fuel from the tank to the engine. The failure of the fuel system can cause the plane to have an accident, such as crash and death. This research discussed the reliability of the fuel system on the TM-13 aircraft which included the process of fuel system reliability. In flight regulations airplanes included the safety and reliability of aircraft produced. The reliability assessment began by identifying the system functions, the failure conditions, and the lack of success. There were two methods used; quantitative methods in the form of fault tree analysis and qualitative methods in the form of functional hazard assessment. The results showed the probability of the total failure of the fuel system capability on the TM-13 aircraft was 6.6580x10-10. The probability of this failure was smaller than functional hazard assessment, 1x10-9. Because of the probability of the failure, the fuel system on the TM-13 aircraft has met the requirements. Thus, the architecture of the TM-13 aircraft fuel system is safe to use
Download
book
BibTex
Latex, Jabref
cloud_download
Original Resource
url resource Institution
