TM-9-2920-242-35

STARTER, ENGINE ELECTRICAL, ASSEMBLY MODEL 1113943, 1113904 AND 1113944

TECHNICAL MANUAL; DIRECT SUPPORT, GENERAL SUPPORT AND DEPOT MAINTENANCE INCLUDING REPAIR PARTS

SEPTEMBER 1964

  TM-9-2920-242-35 - Page 39 of 110

Section IV. ASSEMBLY
28. GENERAL
a. The assembly procedures are covered in
the following paragraphs of this section. Ref-
erence should be made during assembly and
installation to the exploded views in the disas-
sembly section for the proper relationship and
position of components.
b. Apply thread sealer to pole shoe screws,
pipe plugs, and solenoid relay mounting screws
before assembly.
c. An oil hole must be drilled in the lever
housing, commutator end plate, and drive hous-
ing sleeve bearing after installation. If any
sleeve bearings are replaced, they must be
reamed or burnished to the dimensions speci-
fied in the "Sizes and fits of new parts" column
of the wear limits (par. 41e) after installation
in housings, end plate, or clutch sleeve.
29. LUBRICATION
The lubricants listed in Table II should be
available for use during assembly. Table II lists
the lubricant, the part to which it is to be ap-
lied, and the method of application. Make cer-
tain that these instructions are performed dur-
ing assembly.
30. ASSEMBLY OF FRAME ASSEMBLY
Note. The key letters shown below in paren-
theses refer to figure 19 except where other-
wise indicated.
a. Install terminal stud insulator bushing (D)
on field coil terminal stud and position field coil
(C) in frame (A). Install insulator (B) and two
insulations (G) between frame and field coils.
b. Position each of four pole shoes (E), in
turn, on coil inside frame align mating holes and
secure each pole shoe with two pole shoe screws
(refer to step 2, fig. 18). Coat threads of pole
shoe screws with a suitable thread sealer be-
fore installation.
TABLE II. Lubrication Instructions
Par. ref.
Point of lubrication
Lubricant
Instructions
32a
Clutch and armature splines.
GREASE, AIRCRAFT
Coat splines.
and
and INSTRUMENT (GL).
35c
32b,
Felt wicks and felt plugs.
LUBRICATING OIL,
Soak wick and
33b,
INTERNAL COMBUS-
plugs until
and
TION ENGINE (OE 10)
saturated.
34
32a
Clutch sprags.
LUBRICATING OIL,
Lightly coat
INTERNAL COMBUS-
sprags.
TION ENGINE (OE 10)
35b
Clutch shell (shift lever contact surface).
GREASE, AIRCRAFT
Coat surface.
and INSTRUMENT (GL).
32b,
Preformed packings and gaskets.
GREASE, GENERAL
Lightly coat
32c,
PURPOSE, medium
preformed
and
grade.
packings and
35c
gaskets.
3 0


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