Airlines are also starting to use wide body aircraft such as the Airbus A330-900 Neo. For regular flights, the average plane used is a narrow body, while for Hajj and Umrah it is a wide body. Therefore the airport needs to prepare the capacity and area of the apron area to serve wide body aircraft such as the A330-900 Neo which are currently used by Lion Air and Garuda Indonesia airlines. The research method used in this study is Simple Linear Regression, whereby this method is obtained for the calculation results of forcasting the number of aircraft movements in 2023 at Adi Soemarmo International Airport, Boyolali for arrivals is 17,636 aircraft movements and departures are 17,627 aircraft movements, so the total of the total movement of these aircraft is 34,903 aircraft. The results of data analysis and processing of the number of parking stands in the apron area of Adi Soemarmo Boyolali International Airport in 2023 during peak hours are 12 parking stands for narrow body aircraft and 3 parking stands for wide body aircraft. So that the minimum area required for the apron of Adi Soemarmo Boyolali International Airport in 2023 to accommodate Narrow Body and Wide Body aircraft is 100,788.355 m 2 .
Penentuan biaya manhours dan material 24 yearly inspection pada pesawat Bae 146 – RJ85 tidak hanya memprediksi langsung, tetapi dengan melihat referensi dokumen pesawat serta menyesuaikan dengan proyek perawatan pesawat yang akan dilakukan. Metode penelitian yang digunakan adalah pendekatan kuantitatif deskriptif, karena penelitian dengan memperoleh data yang berbentuk angka. Subjek dan objek penelitian ini adalah mengenai perhitungan efektifitas dan efisiensi biaya manhour dan biaya material pada 24 yearly inspection pada pesawat BAe 146 – RJ85. Pengumpulan data menggunakan metode wawancara, observasi dan studi perpustakaan. Setelah dilakukan perhitungan dan analisis didapatkan jumlah manhours dan material yang digunakan diperoleh USD 336.565,01. Waktu pengerjaan 24 yearly inspection pada Pesawat Bae 146 – RJ85 adalah 91 Hari Kerja.
An Anti-icing system is a system that aims to prevent the formation of ice when the plane is in the air. The formation of ice in aircraft is of great concern because an airplane flight will pass through the atmosphere, which will experience the formation of the ice at a certain altitude. The formation of such ice will cause a hazard to the aircraft. So that the ice protection system, namely the anti-icing system, is very concerned so that it is always in a serviceable condition. In this study, direct observation and fault tree analysis were used to determine the cause of failure of the Boeing 737-800 NG anti-ice system engine and anti-icing cowl inlet. The results of the analysis using the fault tree analysis method obtained essential events, namely: actuator fails, electrical connector disconnected, Control Selenoid Trouble, Regulator Trouble, Sense Line Connector Trouble, Engine Fault, Engine Control Trouble, Engine Duct Trouble, Panel Buttom Problem, EICAS Module Problem, No Source Electricity, Negative Electrical Source, Wiring Problem.
An Anti-icing system is a system that aims to prevent the formation of ice when the plane is in the air. The formation of ice in aircraft is of great concern because an airplane flight will pass through the atmosphere, which will experience the formation of the ice at a certain altitude. The formation of such ice will cause a hazard to the aircraft. So that the ice protection system, namely the anti-icing system, is very concerned so that it is always in a serviceable condition. In this study, direct observation and fault tree analysis were used to determine the cause of failure of the Boeing 737-800 NG anti-ice system engine and anti-icing cowl inlet. The results of the analysis using the fault tree analysis method obtained essential events, namely: actuator fails, electrical connector disconnected, Control Selenoid Trouble, Regulator Trouble, Sense Line Connector Trouble, Engine Fault, Engine Control Trouble, Engine Duct Trouble, Panel Buttom Problem, EICAS Module Problem, No Source Electricity, Negative Electrical Source, Wiring Problem.
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