Landing Gear is the structure of the doors used to enclose the landing gear compartments. If the doors are made as an integral structure they could be shown only in chapter 32.

A fire can be due to excessive overheat or flammable fluid leaks and can endanger the aircraft safety.

When the preset threshold is reached, the smoke detector triggers a warning via the Cabin Intercommunication Data System.

This controller is applicable to all systems. Thus, it can also control thermal oil heaters.

During the approach to the runway, deviation pointers in the course indicators show the pilot in which direction the aircraft must go.

NOTE: During the subsequent test, you get the cracking pressure when the fuel flow from the CROSS FEED port is more than 5 cc/minute.

It is not necessary to remove the nameplate (33) from the flange (27).

The gyroscope will become stable after approximately 15 seconds.

During the soldering procedure, wear a protective shield.

Lavatories includes items such as mirrors, seats, cabinets, dispensing equipment, etc., if furnished as manufacturer-designated standard equipment.

The “Detail Requirements” part provides for a uniform method of arranging and identifying specific subject material.