TY  - JOUR
AB  - This comprises a pump on each engine either of which draws air through the gyro‐operated instruments via a change‐over cock (dash‐starboard) 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.
VL  - 22
IS  - 3
SN  - 0002-2667
DO  - 10.1108/eb031876
UR  - https://doi.org/10.1108/eb031876
AU  - Tonkin T.
PY  - 1950
Y1  - 1950/01/01
TI  - Aircraft Engineering Reference Sheet: 6—Short Sealand
T2  - Aircraft Engineering and Aerospace Technology
PB  - MCB UP Ltd
SP  - 87
EP  - 88
Y2  - 2024/04/25
ER  -