Propeller Owner's Manual
136
INSTALLATION AND REMOVAL
61-00-36
Page 3-21
Rev. 2 Feb/17
(4) Install the composite spinner bulkhead over the installed
spacers “A”, wave washers “B”, and washers “C” on the
hub clamping bolts.
(a) Refer to Table 3-3 for part numbers.
(b) Refer to Figure 3-5 for orientation and location.
(5)
Install a flat washer “D” on the hub clamping bolts, over
the composite spinner bulkhead. Refer to Figure 3-5 and
Table 3-3.
(6) Install a self-locking spinner mounting nut “E” on each
of the hub clamping bolts used to mount the spinner
bulkhead.
(a) The self-locking nut may be removed from a new or
newly overhauled propeller and reinstalled to permit
spinner bulkhead installation on the propeller before
initial propeller installation on the aircraft.
(b) Removal and reinstallation of the self-locking nut
from an in-service propeller is not permitted.
1 A self-locking nut that is removed from an
in-service propeller must be discarded and
replaced with a new self-locking nut.
CAUTION:
A MINIMUM OF ONE THREAD OF THE
HUB CLAMPING BOLT MUST BE VISIBLE
AFTER THE SPINNER MOUNTING NUT
IS INSTALLED.
(7) Torque each self-locking nut “E” in accordance with
Table 3-1 and Figure 3-1.
(a) When the spinner bulkhead is installed, there must
be no less than one thread of the hub clamping bolt
exposed beyond the spinner mounting nut “E”.