TM55-2840-251-23
Section II FUEL CONTROL LINKAGE
6-2 FUEL CONTROL LINKAGE
This task covers:
a.
Removal (6-2-1)
b.
Inspection (6-2-2)
c.
Installation (6-2-3)
d.
Adjustment (6-2-4)
INITIAL SETUP
Applicable Configurations:
All
Tools:
None
Materials:
None
Personnel Required:
68B Powerplant Mechanic
66G Aircraft Inspector
6-2-1 REMOVAL
Refer to TM55-1510-209-23 or
TM55-1510-215-23.
6-2-2 INSPECTION
1. Visually inspect for:
- Broken or missing
cotterpins
- Elongated bolt holes in
clevis
- Cracked clevis
- Bent or damaged control
rods.
2. If any damage is found refer
to TM55-1510-209-23 or
TM55-1510-215-23.
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