@thesis{thesis,
		author={FERNANDO DA CUNHA SOARES  EMIDIO},
		title ={ANALISIS KEANDALAN BOOSTER PUMP PADA ENGINE PRATT 
AND WHITNEY PT 6A-62 PESAWAT KT - 1B MENGGUNAKAN 
METODE RELIABILITY CENTERED MAINTENANCE (RCM)},
		year={2018},
		url={http://eprints.stta.ac.id/2038/},
		abstract={Reliability is the possibility of a product or system can work in the employment rate in 
the period of time desired and specific operating condition. The metod used in this analysis 
was reliability centered maintenance (RCM) combined with the weibull distribution. The data 
use to calculate the reliability were the data of the damages occuread at the analyzed 
component.
From the result of the calculation using these methods, it could be seen that the 
average boost pump on the engine pratt and whitney PT 6A-62 KT - 1B airplane damaged at 
467,087361 hours with ? value of 2,8089. Based on regulation that ? > 1 means wore out, 
This failure was indicated by increasing the failure rate along the increase of aircraft 
preventive. It could be conducted if the time variable of the component or system was 
analyzed.}
		}