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Aircraft Engineering Reference Sheet

Aircraft Engineering Reference Sheet This comprises a pump on each engine either of which draws air through the gyrooperated instruments via a changeover cock dashstarboard and Plessey 215B adjustable relief valves, set to 5 in. Hg. on forward face of each firewall. The suction gauge is on the port side of the dash. If an automatic pilot is fitted, it is connected to the discharge from the port pump, otherwise the pumps exhaust into an oil drain collector box at the bottom of each firewall. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

Aircraft Engineering Reference Sheet

Tonkin, T.
Aircraft Engineering and Aerospace Technology , Volume 22 (3): 2 – Mar 1, 1950
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Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/eb031876
Publisher site
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Abstract

This comprises a pump on each engine either of which draws air through the gyrooperated instruments via a changeover cock dashstarboard and Plessey 215B adjustable relief valves, set to 5 in. Hg. on forward face of each firewall. The suction gauge is on the port side of the dash. If an automatic pilot is fitted, it is connected to the discharge from the port pump, otherwise the pumps exhaust into an oil drain collector box at the bottom of each firewall.

Journal

Aircraft Engineering and Aerospace Technology – Emerald Publishing

Published: Mar 1, 1950

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