ANALISIS KEANDALAN KOMPONEN BRAKE ASSY
PADA PESAWAT G 120 TP-A GROB DENGAN
METODE DISTRIBUSI WEIBULL
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Institusion
INSTITUT TEKNOLOGI DIRGANTARA ADISUTJIPTO
Author
CHANDRA ABDURRAHMAN S, DWI
Subject
T Technology (General)
Datestamp
2024-07-23 06:44:20
Abstract :
Brake Assy Reliability on G 120 TP-A Grob Aircraft owned by The Indonesian Air Force uses the Rolls Royce M-250/B17F series engine operates as a turboprop. Where the G 120 TP-A Grob aircraft is one of the training aircraft operated since 2013 by the Indonesian Air Force which is used as a Basic Training and Advanced Training aircraft. Therefore, So there is a need for research and evaluation of the level of aircraft reliability during operation, especially the Brake Assy component which is most frequently used experienced failure. The method for analyzing the reliability of Brake Assy components is by using the Weibull distribution method. The first step to take is collect damage data, then carry out calculations with the aim of knowing the failure rate, failure rate, and maintenance effectiveness of the system to be analyzed. From the results of the analysis of the reliability calculations of the Brake Assy components on G 120 TP-A Grob aircraft can be seen that the average of these components will function until failure at 418 hours 57 minutes and the best maintenance effectiveness for degraded brake assembly components gradual with a value (?) > 1 (1.723993992) is a type of wear failure (wear out). The level of reliability of brake assembly components has decreased As the hours of use increase, the effectiveness of the treatment carried out will increase is preventive maintenance.
Brake Assy Reliability on G 120 TP-A Grob Aircraft owned by The Indonesian Air Force uses the Rolls Royce M-250/B17F series engine operates as a turboprop. Where the G 120 TP-A Grob aircraft is one of the training aircraft operated since 2013 by the Indonesian Air Force which is used as a Basic Training and Advanced Training aircraft. Therefore, So there is a need for research and evaluation of the level of aircraft reliability during operation, especially the Brake Assy component which is most frequently used experienced failure. The method for analyzing the reliability of Brake Assy components is by using the Weibull distribution method. The first step to take is collect damage data, then carry out calculations with the aim of knowing the failure rate, failure rate, and maintenance effectiveness of the system to be analyzed. From the results of the analysis of the reliability calculations of the Brake Assy components on G 120 TP-A Grob aircraft can be seen that the average of these components will function until failure at 418 hours 57 minutes and the best maintenance effectiveness for degraded brake assembly components gradual with a value (?) > 1 (1.723993992) is a type of wear failure (wear out). The level of reliability of brake assembly components has decreased As the hours of use increase, the effectiveness of the treatment carried out will increase is preventive maintenance.
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