@thesis{thesis,
		author={Akza AR  Ratika},
		title ={ANALISIS KEANDALAN ALTERNATOR PADA PESAWAT PIPER PA-28-181 ARCHER III},
		year={2023},
		url={http://eprints.stta.ac.id/1040/},
		abstract={The main function of the alternator is to convert the mechanical energy
generated by the aircraft engine into electrical energy that can be used by the aircraft's
electrical system. The alternator also functions as the main source of electricity to
generate the electrical power needed by the aircraft system during flight. Therefore,
maintenance of the alternator must be very concerned so that it is always in airworthy
condition. Based on information data from the mechanic and by looking at the data on
the maintenance record of the Piper PA 28-181 Archer III aircraft at the Indonesian
Aviation College.
The data analysis data on the maintenance record of the Piper PA 28-181
Archer III Aircraft with data processing using Weibull DR-21 Software and also
FMECA (Failure Modes Effects & Criticality Analysis).
The results of the analysis using the Weibull DR-21 Software and also FMECA
(Failure Modes Effects & Criticality Analysis)shows that the level of reliability of each
component has decreased with the Critical Life Time of the alternator component
being 2123,078 Hours.}
		}