INSTALL COCKPIT CONTROL TRANSFER BELLCRANKS
Clean shaft (3). Use cloth (E120).
Insert shaft (3) about 3 inches through inboard
side of support (6), hollow end outboard.
FLIGHT SAFETY PARTS
This is an installation critical flight
safety part. All aspects of its assembly
and installation must be ensured at
each joint connection and mounting to
Ensure that all bushings are properly
installed (including orientation) in
each input and output clevis of the
Ensure bellcrank hub bearings are
serviceable and properly installed.
Ensure stop bolts are correctly
installed and adjusted.
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.
Do not drive shaft through bellcranks.
Damage to bellcranks and bearings
Slide pitch transfer bellcrank (8) on outboard end
of shaft (3), arm (9) aft, and arm (10) down, until
bottomed. Top of support (6) must be between
two bolts (11).