936、当进行每一步的活门测试时,确保没有泄漏,没有腐蚀,没有生锈并且在整个程序结束后再次确认。

611 THE HYDRAULIC FLUID FLOW OPENS THE VALVE.

610 THE FLAG()INTO VIEW.

609 ()THE ENG INE.

608 ITHE CONTROL UNIT IS INSTALLED AFT OF THE FLIGHT COMPARTMENT.

607 The”General Specification”part contains technical publication guidance applicable to the preparation of all Maintenance Manuals.

606 That portion of the system which uses magnetic gyroscopic and inertia forces. Includes items such as gyro horizons, directional gyros, magnetic compasses, and magnetic heading systems.turn and bank, amplifiers, servos, and flight director, etc.

605 That portion of the system which is used to dissipate static electricity.

604 That portion of the system used to induct and distribute air. Includes equipment rack cooling systems and items such as blowers, scoops, ducting, inlets, check valves, etc. Does not include valves which are part of pressurization and temperature control.

603 That portion of the system that uses radio/radar beam, directional and vertical gyro,Pitot static and manually induced inputs to the system to automatically control yaw, pitch and roll of the aircraft. This includes power source devices, interlocking devices and amplifying,computing,integrating,controlling,actuating, indicating and warning devices such as computers,servos, control panels, indicators, warning lights, etc.

602 That portion of the system and its controls which supply cooled air to the cabin.Includes items such as the cooling unit,indicating systems related to the cooler operation, etc.,as applicable. Does not include temperature control and indicating systems.