ANALISIS KEBUTUHAN JARAK TINGGAL LANDAS
PESAWAT AIRBUS A320-200 DAN BOEING 737-900ER
DIDASARKAN PADA POTENSI REJECTED TAKE-OFF
DI BANDARA INTERNATIONAL ADISUTJIPTO
YOGYAKARTA
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Institusion
INSTITUT TEKNOLOGI DIRGANTARA ADISUTJIPTO
Author
BAGUS GEDE HARI SUTA MANUABA, IDA
Subject
T Technology (General)
Datestamp
2024-06-20 06:13:58
Abstract :
The need for takeoff distance needed by an aircraft, not only during the take off phase, but also needed for anticipation when the plane experiences a failure of takeoff conditions both due to weather factors, technical factors and other factors, so the takeoff distance is always corrected with the possibility the occurrence of rejected takeoff. When the plane has not reached the speed of V1, the pilot can take rejected takeoff but when the plane exceeds the speed of V1 the pilot is required to go around or continue the takeoff phase. If the pilot forces to take rejected takeoff with a speed exceeding V1, the aircraft is at risk of being out of control or exiting the runway. The method of rejected takeoff calculation using takeoff performance calculation. This calculation is based on aircraft ramp weight which includes the aircraft's empty weight, passenger weight, baggage, cargo and the weight of the fuel carried to carry out flight missions. By knowing ramp weight, takeoff performance calculation can be done to be able to determine aircraft acceleration as a reference for calculating speed V1 and aircraft deceleration which is a reference for calculating the distance of the aircraft when doing rejected takeoff so that it can determine the total takeoff distance on the flight mission. From the analysis of takeoff performance calculations, it is known that aircraft weight, air temperature and wind speed affect the total takeoff distance. With a payload percentage of 90%, Airbus A320-200 aircraft require a total takeoff distance of 1,637 meters while a Boeing 737-900ER requires 1,983 meters. Based on the percentage level of cargo, the takeoff distance of the Boeing 737-900ER aircraft is longer than the Airbus A320-200 aircraft.
The need for takeoff distance needed by an aircraft, not only during the take off phase, but also needed for anticipation when the plane experiences a failure of takeoff conditions both due to weather factors, technical factors and other factors, so the takeoff distance is always corrected with the possibility the occurrence of rejected takeoff. When the plane has not reached the speed of V1, the pilot can take rejected takeoff but when the plane exceeds the speed of V1 the pilot is required to go around or continue the takeoff phase. If the pilot forces to take rejected takeoff with a speed exceeding V1, the aircraft is at risk of being out of control or exiting the runway. The method of rejected takeoff calculation using takeoff performance calculation. This calculation is based on aircraft ramp weight which includes the aircraft's empty weight, passenger weight, baggage, cargo and the weight of the fuel carried to carry out flight missions. By knowing ramp weight, takeoff performance calculation can be done to be able to determine aircraft acceleration as a reference for calculating speed V1 and aircraft deceleration which is a reference for calculating the distance of the aircraft when doing rejected takeoff so that it can determine the total takeoff distance on the flight mission. From the analysis of takeoff performance calculations, it is known that aircraft weight, air temperature and wind speed affect the total takeoff distance. With a payload percentage of 90%, Airbus A320-200 aircraft require a total takeoff distance of 1,637 meters while a Boeing 737-900ER requires 1,983 meters. Based on the percentage level of cargo, the takeoff distance of the Boeing 737-900ER aircraft is longer than the Airbus A320-200 aircraft.
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