Piper Arrow IV Turbo Maintenance Manual page 213

14. Install the hex-head screws through the end shield and into the heatsink assembly. Torque 15 to 25
inch-pounds.
15. Position the stator over the rectifier end shield assembly and place the winding terminals on the
terminal block studs. Press the stator into the end shield, install terminal nuts and torque 11 to 17 inch-pounds.
(Refer to Figure 24-26.)
Route the stator winding leads so that they cannot contact the
rotor or sharp edges of the negative heatsink.
16. Position the rotor and drive end shield assembly over the stator and rectifier end shield assembly.
Align the through bolt holes in the stator, rectifier end shield and drive end shield.
17. Compress the stator and both end shields manually and install through bolts and washers. Torque 25 to
55 inch-pounds.
18. Place field brushes in insulated holders and install in rectifier end shield. Place an insulating washer on
each field brush terminal and install lock washers and attaching screws. Torque 15 to 35 inch-pounds.
19. Slowly rotate the alternator pulley by hand to be sure that rotor fan blades do not contact the stator
winding leads.
20. Install the alternator and adjust the drive belt to specifications.
After installing the alternator on the engine, test the complete
charging system to be certain it is functioning properly.
Figure 24-26. Installation of Negative
EFFECTIVITY:
CHRYSLER ALTERNATOR
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL
—NOTE—
—NOTE—
1I21
Figure 24-27. Installation of Stator
Rectifier Assembly
Revised: July 13, 1983
24-32-14
Page 24-26