ANALISIS MAXIMUM TAKEOFF WEIGHT B737 BERDASARKAN KONDISI RUNWAY, CUACA DAN AIRFIELD DI BANDAR UDARA ADISUTJIPTO YOGYAKARTA

PERMADI ADI PARTA, KETUT (2020) ANALISIS MAXIMUM TAKEOFF WEIGHT B737 BERDASARKAN KONDISI RUNWAY, CUACA DAN AIRFIELD DI BANDAR UDARA ADISUTJIPTO YOGYAKARTA. Skripsi thesis, Institut Teknologi Dirgantara Adisutjipto.

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Abstract

Boeing 737 aircraft has flight capability characteristics that is determined by design specifications and operational specifications. The Limitation of operational capability to be the maximum limit when the aircraft is operated. The intended limitation is that the aircraft will experience a takeoff performance change in the maximum weight of the aircraft including maximum takeoff weight and load capacity. So that this research is carried out on variables that affect flight performance, temperature effects and find out whether airlines operating Boeing 737 exceeds limits that are affected by airport conditions. To determine the maximum take-off weight using the line drawing method in the Flight Planning and Performance Manual chart (FPPM B737-300, B737-400, B737-800NG and B737-900ER), it used data from research results in the form of secondary data such as airport specification data, wind data, air temperature data and the passenger movement data used Boeing 737 aircraft operating in Yogyakarta Adisutjipto Airport. From the analysis, it was found that Boeing 737 experienced a decrease in flight performance caused by several variables in the form of a short runway, high air temperatures and wind conditions in a tail wind state. So by knowing the limitation, there is no airline that exceeds the limits of Yogyakarta Adisutjipto Airport.

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