406.Any adjustments/tests that are necessary as part of installation or reactivation procedures shall be in the text in proper sequence( )

531.The cover title and applicable airplane designation shall be prominently displayed on the cover or spine [or both] of the Handbook( )

530.Pushing the ENG FIRE P/BSW [ ] the engine fire extinguishing bottles firing system ( )

529.Each electrical system has a code to identify it( )

528.The airflow passes turbine and depletes energy, in addition to the colder air that bypassed the engine core, produces a force when exiting the nozzle that acts to propel the engine, and therefore the airplane, forward ( )

527.This manual includes procedures such as periodic engine running, control or drainage of fluid systems, static grounding, etc( )

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

525.If you press abort during the test, the test will stop and the TEST ABORT will display on the monitor ( )

524.The rules of construction followed in the preparation of this Specification are the same as generally used by the FAA in the preparation of its rules( )

523.Do these two steps at the same time( )

522.It has a single shaft and operates at a constant speed ( )