967. This chapter shall provide that information considered necessary by the manufacturer to properly level the aircraft for any of the various maintenance, overhaul or major repairs which might become necessary during the life of the aircraft

2396. The voltage and current wil show on the alphanumeric display when push one of the pushbotton

2395. The pot life of the mixture is approximately 4 hours

2394. 系统的中用于控制机身内压力的部分。包括控制活门,释压活门,指示器,电门,放大器等项目,如适用。

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