Refer to Table 7001 for information about how the pivot assembly is made.

If you select abort during the test, the test stops and the CDU shows the test abort page.

The turbine clearance control sensor supplies the EEC with temperature data from the high pressure turbine shroud.

The servo fuel heater attaches to the engine oil/fuel heat exchanger.

The combustor mixes air from the compressors and fuel from the fuel nozzles.

Notes call attention to methods which make the job easier, or provide supplementary or explanatory information.

Record the location and the color of the cables of each bundle which goes through the AC current transformer.

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.