Aircraft Systems: Details of the Fuel, Electrical, Hydraulic, Air Conditioning and Pressurization, Ice Protection and Oxygen Systems and their Mode of Operation
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 September 1963
Abstract
TEN THOUSAND AND NINETY gallons of usable fuel are carried in six integral type tanks, three in each wing, the individual tank capacities per wing being: No. 1 Tank (Inner) 2,865 gallons, No. 2 Tank (Centre) 1,750 gallons, No. 3 Tank (Outer) 430 gallons. Each tank is equipped with two booster pumps mounted in canisters which permit pump replacement without draining the tanks.
Citation
(1963), "Aircraft Systems: Details of the Fuel, Electrical, Hydraulic, Air Conditioning and Pressurization, Ice Protection and Oxygen Systems and their Mode of Operation", Aircraft Engineering and Aerospace Technology, Vol. 35 No. 9, pp. 265-271. https://doi.org/10.1108/eb033784
Publisher
:MCB UP Ltd
Copyright © 1963, MCB UP Limited