INSTALL MIXING LINKAGE CONNECTING LINKS
INSTALL UPPER OUTBOARD LINK.
If upper outboard link (29) is a replacement,
loosen nut (30). Turn rod end (31) 90º to rod end
(32). Torque nut to 350 inch-pounds.
Insert link (29) through access hole (33) from aft
side. Remove bolt (34), washers (35 and 36),
and nut (37).
Do not torque nut at this time. Remove tag.
FLIGHT SAFETY PARTS
This is an installation critical flight
safety part. All aspects of its assembly
and installation must be ensured.
Ensure that both rod end jam nuts are
installed and torqued.
Ensure that the rivet through the fixed
rod end bearing is secure.
Ensure larger diameter bore rod end
bearing is facing aft.
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.
Position link (29) in bellcrank (11). Install bolt
(34), washers (35 and 36), and nut (37).
Remove nut (38) and washer (39) from bolt (40).
Raise bolt (40) from bellcrank (41). Position link
(29) in bellcrank.
Install bolt (40), washer (39), and nut (38). Do
not torque nut at this time.