Rover 60 Operations Instructions download pdf (Page 28)

Figure 18: Fuel and Water

Figure 19: Main fuel tank location

3.6 General, physical and equipment concerns

The apparatus is associated with high pressures and very high temperatures.

The gas turbine incorporates a temperature control as an overriding

safeguard to high temperatures. This device consists of a temperature

sensing tube that projects into the exhaust stream. It is connected by

capillary tubing to the fuel control unit. Over-loading of the engine results in

increased engine operating temperatures. Should the temperature rise above

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Rover 60 Operations Instructions Page 28