Alam, Dipo (2023) ANALISIS KESALAHAN DALAM PERHITUNGAN LETAK CENTER OF GRAVITY TERHADAP VARIABEL TERTENTU PADA PESAWAT BOEING 737-900ER. Thesis thesis, Institut Teknologi Dirgantara Adisutjipto.
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Abstract
Balancing and calculating weight of the aircraft before the aircraft operated is very important in aviation safety, There are many cases of aircraft accidents that occur because the aircraft is not in the right weight condition and is not in a state of equilibrium. Some aircraft are subjected to an aircraft weight and balance process during technical inspections, both in the aircraft maintenance hangar and during operations in the maintenance line. This study discusses the process of determining the center of gravity on the Boeing 737-900ER using the calculation method available in the Weight and Balance Control and Loading Manual Boeing 737-900ER. The research was conducted at the hangar FL-Technics Indonesia and Lion Air terminal 2 located at Soekarno-Hatta Airport, Tangerang, Banten. From the results of calculating the weight and balance of the aircraft, it was found that on long-range flight with full passengers and maximum load cargo, the center of gravity point of aircraft at 37.79%MAC, on medium-range flight with full passengers and maximum load cargo the center of gravity point of aircraft at 31.43%MAC, on short-range flight with full passengers and maximum load cargo the center of gravity point of aircraft at 44.95 %MAC.
Item Type: | Thesis (Thesis) |
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Subjects: | T Technology > T Technology (General) |
Divisions: | Institut Teknologi Dirgantara Adisujtipto > D3 Aeronaitika |
Depositing User: | Mr Dipo alam |
Date Deposited: | 27 Feb 2024 03:12 |
Last Modified: | 27 Feb 2024 03:12 |
URI: | http://eprints.stta.ac.id/id/eprint/1242 |
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