INSTALLATION AND REMOVAL
61-00-75
Propeller Owner’s Manual
175
Page 3-46
Rev. 1 Jun/11
(b) From the engine side of the bulkhead, insert the
attaching bolts through the bulkhead and into the
start lock units.
(c) Install the washers and locking nuts (Table 3-1)
on the propeller side of the start lock to secure the
attaching bolts and the bulkhead.
(4) Lubricate the specified shaft O-ring (Table 3-1) with
engine oil and install it on the engine flange.
WARNING 1
: TO FACILITATE BOXING AND SHIPPING
OF THE PROPELLER, THE PISTON NUT
MAY HAVE BEEN REMOVED TO PERMIT
ROTATION OF THE BLADES BEFORE
PACKAGING.
WARNING 2
: MAKE SURE THE SLING IS RATED UP TO
800 POUNDS (363 KG) TO SUPPORT THE
WEIGHT OF THE PROPELLER ASSEMBLY
DURING INSTALLATION.
CAUTION
:
WHEN INSTALLING THE PROPELLER
ON THE AIRCRAFT, DO NOT DAMAGE
THE ICE PROTECTION SYSTEM
COMPONENTS, IF APPLICABLE.
(5) With a suitable crane hoist and sling, carefully move the
propeller assembly to the aircraft engine mounting flange
in preparation for installation.
CAUTION
:
USE CARE TO AVOID SCRAPING
ALUMINUM FROM THE BORE OF THE
SPINNER BULKHEAD. SCRAPINGS
COULD BECOME WEDGED BETWEEN
THE FLANGES.
(6) Align the threaded holes of the propeller flange with the
bolt holes in the engine flange, and align the dowel pins
in the propeller flange with the dowel pin holes in the
engine flange.
OBSOLETE PROPELLER MODELS. SEE COVER PAGE
WARNINGS AND SERVICE BULLETIN HC-SB-61-331