ANALISIS KEGAGALAN WINDSHIELD BOEING 737-800NG MENGGUNAKAN METODE FAILURE MODE EFFECTS AND CRITICALITY ANALYSIS
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Institusion
INSTITUT TEKNOLOGI DIRGANTARA ADISUTJIPTO
Author
Rizki Mahendra, Bagus
Subject
T Technology (General)
Datestamp
2024-02-27 02:07:27
Abstract :
Windshield is an important component in operating an airplane, the condition of the windshield can affect the pilot's vision to see the situation outside the aircraft, precisely in front of the aircraft. windhiseld failure can propagate so that there is the potential for other failures that can jeopardize flight safety. for this reason, identification of the potential risk of failure on the windshield should be done. This research aims to analyze the occurrence of failures in the Windshield. This research using Failure Mode Effect and Criticality Analysis method. where this method uses two analyses, namely Failure Mode Effect Analysis (FMEA) and Criticality Analysis (CA). This method identifies potential failures and determines the criticality of a failure mode. The results of the analysis can determine the Risk Priority Number value that occurs in Delamination with an RPN value of 294, which indicates that this component is a component that has the highest level of risk of occurrence. criticality analysis results show the Crack failure mode has the highest level of criticality with a value of Cm 99 and Cr 990
Windshield is an important component in operating an airplane, the condition of the windshield can affect the pilot's vision to see the situation outside the aircraft, precisely in front of the aircraft. windhiseld failure can propagate so that there is the potential for other failures that can jeopardize flight safety. for this reason, identification of the potential risk of failure on the windshield should be done. This research aims to analyze the occurrence of failures in the Windshield. This research using Failure Mode Effect and Criticality Analysis method. where this method uses two analyses, namely Failure Mode Effect Analysis (FMEA) and Criticality Analysis (CA). This method identifies potential failures and determines the criticality of a failure mode. The results of the analysis can determine the Risk Priority Number value that occurs in Delamination with an RPN value of 294, which indicates that this component is a component that has the highest level of risk of occurrence. criticality analysis results show the Crack failure mode has the highest level of criticality with a value of Cm 99 and Cr 990
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