Eagle ICA-D212-725, Instructions Manual

Page: 577 / 729

ICA-D212-725 (76)
Page 18 of 21
CHAPTER 76 – ENGINE CONTROLS (76-00-00)
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COPYRIGHT

2007 BY DART AEROSPACE LTD.

THIS DOCUMENT IS PRIVATE AND CONFIDENTIAL AND IS SUPPLIED ON THE EXPRESS CONDITION THAT IT IS NOT TO BE USED FOR ANY PURPOSE OR COPIED OR COMMUNICATED TO ANY
OTHER PERSON WITHOUT WRITTEN PERMISSION FROM DART AEROSPACE LTD.
Revision:
0
Date: 07.05.31
Figure 76-3. Power Lever (N1) Control Rigging (Sheet 3 of 3)
76.3.2 Flight Idle Solenoid
A spring loaded, electrically actuated flight idle
solenoid is installed in the power lever control
system. The plunger of the solenoid is
contacted by a stop assembly to arrest
movement of the control linkage at the proper
start or flight idle speed.
76.3.2.1 Removal – Flight Idle
Solenoid
76.3.2.1.1 Disconnect terminals of wires
from solenoid (19, Figure 76-3) and stow cable
assembly.
NOTE
Tag and identify terminals and
shims for proper installation
upon reassembly.
76.3.2.1.2 Remove four bolts and four
washers securing bracket (21) to base (20) and
structures.