SISTEM PENDUKUNG KEPUTUSAN UNTUK MENGHITUNG
KESETIMBANGAN DALAM MENENTUKAN KELAYAKAN TERBANG
PESAWAT MA-60 MERPATI NUSANTARA AIRLINES DENGAN
MENGGUNAKAN METODE ANALYTICAL HIERARCHY PROCESS
(AHP)
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Institusion
INSTITUT TEKNOLOGI DIRGANTARA ADISUTJIPTO
Author
SINUHAJI, YASHINTA
Subject
Q Science (General)
Datestamp
2024-08-02 04:27:14
Abstract :
Merpati Nusantara Airlines is one of the largest airlines in Indonesia that has been established since September 6, 1962. Many systems in this airline that still use the system manually or not computerized so that tends to cause the risk of a very big mistake and fatal. One of them is the manual calculation in the determination of loading on MA-60 aircraft which required precision and drain the time that much in the process. So it is necessary a system that is able to help the airlines in the determination of cargo to create equilibrium on the MA-60 aircraft. In this study the results of the calculation system that has been created has been compared with the results of calculations manually and get the difference in the percentage of MAC (% MAC) of 0.1% to 2%. A value of 0.1 to 3% is stated within the tolerance limit of Mean Aerodynamical Chord on MA-60 aircraft. From the calculations that have been done, Analytical Hierarchy Process (AHP) method can not be used in this equilibrium calculation because it will produce a much different output with the purpose of calculating equilibrium and determining the feasibility of flying. For the calculation using AHP method, the value of consistency ratio is <0.1, ie -0.69 with the value of consistency ratio of each alternative below 10% (<0.1), ie 0 which means consistent in the calculation
Merpati Nusantara Airlines is one of the largest airlines in Indonesia that has been established since September 6, 1962. Many systems in this airline that still use the system manually or not computerized so that tends to cause the risk of a very big mistake and fatal. One of them is the manual calculation in the determination of loading on MA-60 aircraft which required precision and drain the time that much in the process. So it is necessary a system that is able to help the airlines in the determination of cargo to create equilibrium on the MA-60 aircraft. In this study the results of the calculation system that has been created has been compared with the results of calculations manually and get the difference in the percentage of MAC (% MAC) of 0.1% to 2%. A value of 0.1 to 3% is stated within the tolerance limit of Mean Aerodynamical Chord on MA-60 aircraft. From the calculations that have been done, Analytical Hierarchy Process (AHP) method can not be used in this equilibrium calculation because it will produce a much different output with the purpose of calculating equilibrium and determining the feasibility of flying. For the calculation using AHP method, the value of consistency ratio is <0.1, ie -0.69 with the value of consistency ratio of each alternative below 10% (<0.1), ie 0 which means consistent in the calculation
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