
ARMY TM 9-2815-254-24
AIR FORCE TO 38G1-94-2
f.
Check stator as follows:
(1) Connect multimeter to each set of stator leads and check for continuity. Standard stator coil resistance
is 0.402 ohms. If there is no continuity, stator coil is open and stator must be replaced.
(2) Connect multimeter from stator lead to stator frame. If there is continuity, stator core is shorted to ground
and stator must be replaced.
g.
Check rectifier as follows:
(1) Check positive side diodes by connecting multimeter positive test probe to each stator terminal and nega-
tive test probe to BAT terminal. There should be no continuity. Reverse test probes. There should be con-
tinuity.
(2) Check negative side diodes by connecting multimeter positive test probe to each stator terminal and neg-
ative test probe to terminal E. There should be continuity. Reverse test probes. There should be no conti-
nuity.
(3) If any diode is found to be bad, replace rectifier.
3-24.5. Assembly.
a.
When soldering leads, use solder (SN60WRAP2), a 572 to 662°F (300 to 350°C) soldering iron (gun), and
complete each solder joint within 5 seconds. Use long nosed pliers or equivalent to allow for heat dissipation.
b.
Connect regulator (29, FIGURE 3-49) to brush assembly (28) and solder all connections.
c.
Press bolts (27) into brush assembly (28) and regulator (29). Pressure required is 221 Ibs (100 kg).
d.
Connect rectifier (26) to brush assembly (28) and solder all connections.
e.
Connect stator leads to rectifier (26) and solder all connections.
f .
Mate stator (25) with end cover (24) aligning benchmarks.
3-97
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...