TM 55-1520-240-23-9
11-187
INSTALL MIXING LINKAGE CONNECTING LINKS
(Continued)
11-187
INSTALL PITCH AND THRUST LINK
48.
Remove nut (105), washers (106 and 107), and
bolt (108) from bellcrank (109).
FLIGHT SAFETY PARTS
This is an installation critical flight
safety part. All aspects of its assembly
and installation must be ensured.
Ensure bearings are properly staked.
Ensure proper attaching hardware
(impedance type bolt, nut, and
washers) is installed including
verification of bolt head orientation,
torque, and installation of cotter pins.
Loose attachments within flight control
primary linkage will degrade aircraft
control. Missing components will
cause loss of control.
49.
Position pitch and thrust link (110) in bellcrank
(109). Install bolt (108), washers (107 and 106),
and nut (105). Do not torque nut at this time.
Remove tag.
50.
Remove nut (111), washers (112 and 113), and
bolt (114) from bellcrank (25).
51.
Position link (110) in bellcrank (25). Install bolt
(114), washers (113 and 112), and nut (111). Do
not torque nut at this time.
52.
Neutral rig first and second stage linkage (Task
11-51).
11-744
