970. Measure the bonding resistance between the antenna in the countersunk hole and the aircraft fuselage

2393. Retract the main landing gear

2392. The gas charging valve is on the top of the shock strut of the nose landing gear

2391. Identify the disassembled parts with tags This method will help you during the subsequent assembly procedures

2390. Make match marks on the components that you disconnect/remove to record their connections/positionsThis is important for the subsequent installation procedure

2389. Standardization will enhance safety through uniform interpretation of inspection requirements contained in Continuing Airworthiness Programs prepared in accord with this Specification

2388. A/P stabilizer trim commands occur when there is an elevator deflection command from the autopilot that is beyond the trim threshold and stays for a long time

2387. The airplane general arrangement shall be illustrated with a scale line drawing consisting of plan, side and front views presented in a vertical sequence upon a single page

2386. 持续监控速度指示,直到测试结束。

2385. Be careful with easily damaged parts

2384. Turn the potentiometer carefully