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Abstract
Regional flights in Indonesia, particularly in Kalimantan, play a crucial role in connecting remote areas and supporting local economic activities. This analysis focuses on the maximum number of flight cycles that can be operated by the Cessna 208B turboprop aircraft using various strategies within the commuter route network in Kalimantan. The objective of this research is to calculate the maximum number of flight cycles based on differences in payload influenced by several flight strategies, utilizing the Cessna 208B Information Manual. The research process begins with identifying commuter routes in Kalimantan, collecting data from the Pilot Operating Handbook for the aircraft, fuel consumption, and flight performance at specific altitudes. Among the three strategies identified, the full tank strategy allows the aircraft to carry 1,018 kg of fuel at the start of the flight, with remaining passenger weight from the Maximum Take-Off Weight, resulting in 4 flight cycles. The full passenger strategy, with 11 passengers, allows the aircraft to carry 589 kg of fuel without refueling, yielding 2 flight cycles. By employing a refueling strategy at each airport, the aircraft can carry varying amounts of fuel, resulting in 8 flight cycles. It can be concluded that the refueling strategy is the most optimal, as it generates a higher number of flight cycles. The findings from this study are expected to serve as a foundation for further research on regional aviation in Indonesia, particularly in Kalimantan
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References
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References
. G. T. Alam, M. Arifin, and E. Yuniarti, “Perhitungan Jumlah Maksimum Flight Cycle Tanpa Refueling pada Kondisi Full Tank dan Full Payload pada Jaringan Rute Commuter Pesawat ATR 72,” Jurnal Mahasiswa Dirgantara, 2022.
. G. J. J. Rujigrok, Elements of Airplane Performance. Delft, Netherlands: Faculty of Aerospace Engineering, Delft University of Technology, 1994.
. Federal Aviation Administration (FAA), “Holding Aircraft,” 2016. [Online]. Available: https://www.faa.gov/air_traffic/publications/atpubs/atc_html/chap4_section_6.html [Accessed: Oct. 15, 2024].
. D. A. Saputra, S. Priyanto, I. Muthohar, and M. Bhinnety, “Pengkajian Tingkat Beban Kerja Mental Pilot Pesawat Terbang Dalam Melaksanakan Tahap Fase Terbang (Phase Of Flight),” Jurnal Teknik Sipil, vol. 13, no. 3, pp. 181–189, 2015.
. R. H. Barnard and D. R. Philpott, Aircraft Flight: A Description of the Physical Principles of Aircraft Flight. London, UK: Pearson Education, 2010.
. “Civil Aircraft Payload/Range Envelope,” [Online]. Available: https://www.researchgate.net/figure/Civil-aircraft-payload-range-envelope_fig1_329419708 [Accessed: Oct. 10, 2024].
. Federal Aviation Administration (FAA), Aircraft Weight and Balance Handbook, 2016.
. Y. Nurhayati, “Perhitungan Panjang Landas Pacu Untuk Operasi Pesawat Udara,” Jurnal Penelitian Perhubungan Udara, vol. 38, no. 4, pp. 373–381, 2012.
. N. D. Mustifa, M. I. Irawan, and S. Wahyudi, “Optimasi Saving Cost dari Fuel Tankering dengan Pendekatan Fuzzy Goal Programming: Studi Kasus PT. X,” Jurnal Sains dan Seni ITS, vol. 4, no. 2, pp. A.37–A.42, 2015.
. NASA, “Thrust Specific Fuel Consumption,” 2015. [Online]. Available: https://www.grc.nasa.gov/www/k-12/airplane/sfc.html [Accessed: Oct. 15, 2024].
. Solenta Aviation (Pty) Ltd., Aircraft Technical Notes Cessna 208B Grand Caravan, Dec. 2005.
. Cessna Aircraft Company, Information Manual: Cessna Grand Caravan 208B POH Revision 1, June 2008.
. U.S. Congress, House Committee on Public Works and Transportation, Subcommittee on Oversight and Review, Commuter Air Safety: Hearings, 96th Congress, 2nd Session, Feb. 26–29, 1980.
. R. Johnson and T. Lee, “Operational Efficiency and Fuel Strategy in Aviation,” Journal of Air Transport Studies, vol. 8, no. 3, pp. 78–92, 2021.
