Refer to the appropriate manufacturer＇s Service Manual.

Fault isolation provides the information used to identify, locate and correct any fault that is predicted to occur on the airplane.

Excessive HP fuel supplies, other than that for actuator control and metered fuel to the combustor, is returned to the LP system via the spill valve.

All Supplements may be issued to all owners of the airplane model covered by the Handbook. This method is recommended as minimizing errors of distribution, and also informs owners of the availability of systems and equipment.

Make sure the work area is clean and clear of tools and other items and all access panels are closed.

The slow moving, high pressure air from the compressor is fed into the combuster where it is mixed with a highly flammable fuel and ignited.

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

The engine anti-icing system is used to eliminate and prevent the formation of ice by bleed air in all parts of engine, excluding power plant cowling which is covered under Chapter 30.

The emergency procedures check list should be in concise, abbreviated form designed to remind pilots of items to check without providing details concerning the operation of any system.

Definitions should be worded as simply as possible and must conform with the use of the defined terms in the Handbook.

If the wheel temperature increases to more than 177 deg., the core of the fusible plug melts and the tire deflates.