217. The engine tachometer system supplies the engine low pressure rotor (N1) and the engine high pressure rotor (N2) speed signals

3146. The discrepancy report should include the following: Continuing Airworthiness Program Inspection Number; Airplane Model and Serial Number; Airplane Hours; Title of Continuing Airworthiness Program Inspection; Location and Description of the Damage; How Detected

3145. 尝试移动驾驶杆

3144. Make sure that the latch is fully engaged

3143. The CAP inspection sets forth manufacturer recommended retirement times for parts or assemblies( ) and FAA required retirement ( ) times for life limited parts or assemblies

3142. Visually examine the assembly to determine extent of damage

3141. Centrifugal force is a force that acts outwardly on any body moving in a curved path Centrifugal force tries to move a body away from the center of its rotation, and this force is opposed by the centripetal force

3140. When the light comes on, set the switch to NORMAL

3139. If you do not do a regular monitoring of the APU oil consumption, do the steps that follow to make sure that the APU oil quantity is sufficient for the flight

3138. 控制杆向前移动必须缓慢而且连续。

3137. 确保近地警告系统是可以操作的