PENENTUAN WEIGHT AND BALANCE PADA PESAWAT
BOEING 737-800 NG DAN AIRBUS A320 MENGGUNAKAN
LOAD TRIMSHEET DAN EXCEL LOADSHEET di PT.LION
AIR BANDAR UDARA INTERNASIONAL JUANDA
SURABAYA 2021
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Institusion
INSTITUT TEKNOLOGI DIRGANTARA ADISUTJIPTO
Author
Harry Kurniawan, Fajar
Subject
T Technology (General)
Datestamp
2024-08-02 04:25:58
Abstract :
The calculation of the weight and balance of an aircraft that is carried out accurately according to the standards set by IATA (International Air Transport Association) is a top priority for aircraft security and the safety of passengers and the aircraft itself during flight. Center of gravity (CG) is a point that is assumed to be the center of concentration of the total weight of the aircraft, CG must be located within a certain limit for flight safety. Where in this case, several methods are used in the process of this thesis including by conducting research at PT. Lion Air Juanda Surabaya by taking data related to load sheets, conducting interviews with workers in the airport operations section to find out how to fill in load sheets and to know how to calculate load sheet. In this case the payload distribution process on the load control unit before making the Boeing 737-800 NG and Airbus A320 loadsheets where the total traffic load calculation for Boeing produces a value of 2411 Kg and Airbus produces a value of 8527 Kg. The conventional manual loadsheet by filling in the data directly on a paper form performs calculations and plots the final data results into a chart for the Boeing manual loadsheet looking for MACCG using the water fall technique and the results obtained are MACZFW = 20.2%, MACTOW = 22.7%, while Airbus is looking for MACCG with table index and the results obtained MACZFW = 29.3%, MACTOW = 28.8%
The calculation of the weight and balance of an aircraft that is carried out accurately according to the standards set by IATA (International Air Transport Association) is a top priority for aircraft security and the safety of passengers and the aircraft itself during flight. Center of gravity (CG) is a point that is assumed to be the center of concentration of the total weight of the aircraft, CG must be located within a certain limit for flight safety. Where in this case, several methods are used in the process of this thesis including by conducting research at PT. Lion Air Juanda Surabaya by taking data related to load sheets, conducting interviews with workers in the airport operations section to find out how to fill in load sheets and to know how to calculate load sheet. In this case the payload distribution process on the load control unit before making the Boeing 737-800 NG and Airbus A320 loadsheets where the total traffic load calculation for Boeing produces a value of 2411 Kg and Airbus produces a value of 8527 Kg. The conventional manual loadsheet by filling in the data directly on a paper form performs calculations and plots the final data results into a chart for the Boeing manual loadsheet looking for MACCG using the water fall technique and the results obtained are MACZFW = 20.2%, MACTOW = 22.7%, while Airbus is looking for MACCG with table index and the results obtained MACZFW = 29.3%, MACTOW = 28.8%
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