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返回课程 ASD-STE100（简化技术英语）规则部分Rule 6.6 Make sure that no paragraph has more than six sentences. 规则6.6确保每一段都不超过六句话。

Paragraphs organize a text into logical units and help to hold the reader's attention. If they are too long, then they can no longer do this. Do not put different topics in the same paragraph. And if a paragraph has more than six sentences, then divide it into two smaller paragraphs. Then, your text will be easier to read.


Example in STE:

Description of the fuel manifold (refer to figure 10001)


The fuel manifold (1) has these primary parts:
- Two motorized fuel shut-off valves (referred to in this manual as “shut-off valve”)
- A pressure transducer (2)

- Three fittings (10), (13) and (15).


The shut-off valve operates in the valve body (21). The valve body (21) has:

- An aluminum alloy ball (27)
- A retaining ring (31)
- Two seals (26)

- A spring (25).


The spring (25) holds the ball (27) in position to prevent internal leakage. The preformed packings (18), (2) and (30) are installed on the seals (26), the shaft (28), and in the valve body. They prevent external leakage. The seal (26), on which the spring (25) operates, has the function of a relief valve. It operates when the pressure applied in the opposite direction is more than a set value.


The actuator assembly (4) is of a rotary type. A DC motor, which has a permanent high-speed magnet, supplies power to the actuator. Micro-switches in the actuator de-energize it at the end of travel. They also send signals to the fuel control panel to show the operation condition of the valve. A micro-relay controls the direction of shaft rotation and an electrical connector connects the actuator assembly to the aircraft electrical supply.


The pressure transducer (2) is installed downstream of the shut-off valve (in the RH engine line). The fitting (10) connects the pressure transducer (2) to the fuel manifold (1). A lockwire safeties the pressure transducer (2). The pressure transducer (2) has an electrical connector that connects it to the Fuel Management System of the aircraft.


Three fittings (10), (13) and (15) connect the two shut-off valves and the pressure transducer (2). They attach the fuel manifold (1) to the aircraft structure.


The example has short paragraphs, which give the text a clear structure and make it easy for the reader to understand.

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