In the description of the airplane＇s Engine, any gear reduction system in the engine shall be described.

The listed technical names are only examples.

Always use these words with their approved meanings.

STE is a living language and needs feedback from the users to improve it on a continuous basis.

Examine the flow control orifice and make sure the restrictor holes are free from blockage and contamination.

Make sure that the AC CONNECTED and NOT IN USE lights on the P36 panel are illuminated.

Components replacement are not available for the landing gear retraction system and the applicable indication system in this recommended list.

Make sure the sealant is continuously squeezed out along the edges of the contact surfaces.

To facilitate troubleshooting, repair of circuits, and replacement of components, an identification and coding system should be used.

The aircraft may be maintained in accordance with the latest information issued by the manufacturer.

The abnormalities to be included in this section shall be determined by the handbook producer.