Selected issues rules of weight control aircraft

• Autorzy: Stańczyk P. , Stelmach A.

Identyfikatory

DOI

10.5604/12314005.1216466

• Języki publikacji: EN

Abstrakty

EN

In the era of dynamic development of the sciences, uninterrupted security is a priority for each of the sectors of transport. Flight safety depends on many factors that determine the quality and number of operations performed and functioning air transport system whereas the means of transport which is the aircraft. By factors must be understood as any action case, condition or situation where the existence or non-existence increases the probability of failure of the flight. The technical and organizational complexity of air transport system, a multitude of aviation personnel, the operation of the aircraft in various weather conditions are sources of various factors affecting flight safety. This article presents one of the very important things that must be done before every flight - the balance of the aircraft, which is a way of determining the centre of gravity plane COG, moreover, in the article also describes the weight of the passenger. Exemplified filled sheet loading and balance for Boeing B737-400 with the necessary tables, indexes, aimed at normalizing the data. Presented article is an introduction to the issue of control of the weight of the aircraft, taking into account the mass of passengers and their impact on the respective position of the centre of gravity of the aircraft.

Słowa kluczowe

EN

balancing plane; centre of gravity of the airplane; weight of the load

• Wydawca: Łukasiewicz Research Network - Institute of Aviation ; European Science Society of Powertrain and Transport KONES Poland ; Wydawnictwo Instytutu Technicznego Wojsk Lotniczych
• Czasopismo: Journal of KONES
• Rocznik: 2016
• Tom: Vol. 23, No. 3
• Strony: 495--503
• Opis fizyczny: Bibliogr. 7 poz., rys.

Twórcy

autor

Stańczyk P.

• Warsaw University of Technology, Faculty of Transport Koszykowa Street 75, 00-662 Warsaw, Poland

autor

Stelmach A.

• Warsaw University of Technology, Faculty of Transport Koszykowa Street 75, 00-662 Warsaw, Poland

Bibliografia

• [1] Aircraft weight and balance handbook, FAA Flight Standards Service FAA-H-8083-1A, 2007.
• [2] IATA AHM 516.
• [3] IATA AHM 517.
• [4] IATA AHM 560.
• [5] Manerowski, J., Identyfikacja modeli dynamiki ruchu sterowanych obiektów latających, Wydawnictwo naukowe AKOSN, Warszawa 1999.
• [6] Pilot’s Handbook of Aeronautical Knowlegde, FAA Flight Standards Service FAA-H-8083-25A, 2008.
• [7] Weight control of aircraft, Department of Transport, 1975.

Uwagi

PL

Opracowanie ze środków MNiSW w ramach umowy 812/P-DUN/2016 na działalność upowszechniającą naukę.