ANALISIS KEANDALAN BOOSTER PUMP PADA ENGINE PRATT
AND WHITNEY PT 6A-62 PESAWAT KT - 1B MENGGUNAKAN
METODE RELIABILITY CENTERED MAINTENANCE (RCM)
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Institusion
INSTITUT TEKNOLOGI DIRGANTARA ADISUTJIPTO
Author
FERNANDO DA CUNHA SOARES, EMIDIO
Subject
T Technology (General)
Datestamp
2024-06-25 04:22:33
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.
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.
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