
ARMY TM 9-2815-254-24
AIR FORCE TO 35G1-94-2
j.
Disconnect rectifier (26) wiring from stator using a soldering gun. Melt the solder (SN60WRAP2)
quickly and use long-nosed pliers or equivalent to allow for heat dissipation.
k.
Disconnect rectifier (26) from brush assembly (28) using a soldering gun. Melt the solder quickly
and use long nosed pliers or equivalent to allow for heat dissipation.
I.
Remove bolts (27) from brush assembly (28).
m. Disconnect brush assembly (28) from regulator (29) using a soldering gun. Melt the solder quickly
and use long nosed pliers or equivalent to allow for heat dissipation.
3-24.4. Inspection/Testing,
a.
Inspect pulley for cracks and wear.
b.
Inspect fan for wear and damaged vanes.
c.
Inspect brushes for wear. Normal length is 0.630 in. (16 mm), wear limit is 0.276 in. (7 mm). If
below wear limit, replace brush assembly.
d.
Check brush spring tension. Ensure they hold brush tight against slip ring. If weak, replace brush
assembly.
e.
Inspect/check rotor assembly as follows:
(1)
(2)
(3)
(4)
Measure OD of slip rings. Standard OD is 1.245 in. (31.6 mm) and useable limit is 1.205 in.
(30.6 mm). If OD is less than limit, replace rotor.
Check slip ring surface for roughness, oil stain, etc. When surface is rough, use abrasive
paper (#400) to smooth roughness. If dirty or oil stained, wipe clean with alcohol soaked
cloth.
Set multimeter for ohms and connect to each slip, ring and check for continuity. Standard
rotor coil resistance is 12.72 ohms. If there is no continuity, rotor coil is open and rotor must
be replaced.
Connect multimeter from one slip ring to shaft. If there is continuity, rotor coil is shorted to
ground and rotor must be replaced.
Change 2 3-95
Summary of Contents for C-240PW-28
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Page 46: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 FIGURE 3 2 Water Pump 3 20...
Page 49: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 FIGURE 3 3 Fuel Filter Assembly 3 23...
Page 52: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 FIGURE 3 4 Fuel lnjectors and Piping 3 26...
Page 60: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 FIGURE 3 7 Fuel Feed Pump and Timer Assembly 3 34...
Page 61: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 FIGURE 3 8 Fuel Injection Pump Assembly 3 35...
Page 82: ...ARMY TM 9 2815 254 24 AlR FORCE TO 36G1 94 2 TABLE 3 1 Fuel Pump Test Specifications 3 56...
Page 98: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 FIGURE 3 39 Oil Piping 3 72...
Page 106: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 FIGURE 3 44 PCV Assembly 3 80 Change 2...
Page 109: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 FIGURE 3 45 Intake and Exhaust Manifolds 3 83...
Page 122: ...ARMY TM 9 2815 264 24 AIR FORCE TO 38G1 94 2 FIGURE 3 49 Alternator Assembly 3 96 Change 2...
Page 126: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 FIGURE 3 50 Front Gear Cover 3 100...
Page 129: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 FIGURE 3 52 Rocker Covet and Arms 3 103...
Page 137: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 FIGURE 3 60 Cylinder Head Assembly 3 111...
Page 185: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 FIGURE 3 107 Flywheel and Housing 3 159...
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Page 216: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 Section 111 MAINTENANCE LEVELTD PARAGRAPHS...
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Page 234: ...PIN 071752 002...