ANALISIS TREND KERUSAKAN STRUKTUR PESAWAT TERBANG BOEING 737 CLASSIC SERIES (STUDI KASUS PADA PESAWAT TERBANG BOEING 737 CLASSIC SERIES, PT GMF AERO ASIA)

RAYNORTH SIREGAR, ABRAHAM (2019) ANALISIS TREND KERUSAKAN STRUKTUR PESAWAT TERBANG BOEING 737 CLASSIC SERIES (STUDI KASUS PADA PESAWAT TERBANG BOEING 737 CLASSIC SERIES, PT GMF AERO ASIA). Skripsi thesis, Institut Teknologi Dirgantara Adisutjipto.

	Text (ABSTRAK) 07050043_ABSTRAK.pdf Download (129kB)
	Text (BAB I) 07050043_BAB I.pdf Download (129kB)
	Text (DAFTAR PUSTAKA) 07050043_DAFTAR PUSTAKA.pdf Download (59kB)
	Text (FULL SKRIPSI) 07050043.pdf Restricted to Repository staff only Download (4MB)

Abstract

The service life of an aircraft includes the entire life of components, systems and aircraft structure during the flight operational cycle. Within its useful life operation of an aircraft, a decrease in aircraft structural performance occurs as a result accumulation of damage caused by environmental factors, fatigue structure / fatigue, and accident / accident damage. The phenomenon of structural damage becomes special attention in aircraft maintenance management, so methods are needed corrective measures to determine the relationship between aircraft service life and damage structure during flight operations, and can estimate how much The trend of damage that occurs is related to the aircraft's lifespan. In analyzing trends in aircraft structural damage, there are three stages, namely determining related attributes, validating data using related attributes, as well as processing and data analysis. Analyze trends in aircraft structural damage using "data analysis" in Ms.Excel 2007 software with parameters of one independent variable "X" (predictor) and one dependent variable "Y" (response), namely flying hours (total hours) or flying cycles (total cycle) as an independent variable and one dependent variable, namely the amount of damage (total damage). The research results show that there is an interactive relationship between number structural damage (total damage) with aircraft service life (total hours / total cycle), namely there was an increase in the number of structural damages due to the influence of increasing flying hours for each aircraft sub series, and conversely there is a decrease in the number of structural damage due to the influence of increasing flight cycles for each aircraft sub series.

Actions (login required)

View Item

Downloads