OVERHAUL OF ALTERNATOR.
When repairing the alternator, complete disassembly may not be required. In some cases it will only be
necessary to perform those operations which are required to effect the repair. However, in this section, the
complete overhaul is covered step-by-step to provide detailed information on each operation. In actual service
practice, these operations may be used as required.
DISASSEMBLY OF ALTERNATOR.
1. Remove the two Number 10-24 screws holding the brush holder assembly in the slip ring end head.
Remove the brush and holder assembly from the end head.
2. Remove the safety wire from the through bolts.
3. On PA-28RT-201 hold the pulley with a strap wrench and remove the pulley nut. The pulley must be
removed with a puller. Remove the fan, woodruff key and spacer from the shaft.
4. Remove the four through bolts and tap the drive end head lightly to separate the drive end head and
rotor, as a unit, from the stator and slip ring end head.
5. Remove the nuts, lockwashers, flat washers and insulators from the output and auxiliary terminal
studs. Note carefully the correct assembly of the insulator washers and bushings. Using the special tools shown
in Figure 24-30, support the end head and press out the three negative rectifiers. The end head can now be
separated from the stator assembly.
6. To remove the slip ring end bearing and grease seal, it will be necessary to have a hook type or impact
—NOTE—
The inner race of the slip ring end bearing is pressed onto the
rotor shaft. When bearing replacement is necessary, always
replace the complete bearing assembly, including the inner race.
7. On PA-28RT-201 models to remove the drive end head from the rotor shaft, use a puller that grips on
the bearing retainer plate as shown in Figure 24-31. Do not attempt to remove by supporting the end head and
pressing on the shaft, as this may result in distortion of the end head of stripping of the retainer plate screws.
Remove the three retainer plate screws and press the bearing out of the end head. (Refer to Figure 24-32.) On
PA-28RT-201T models support the drive end head and carefully press out the rotor assembly. Remove the three
retainer plate screws and press the bearing from the end head. (Refer to Figure 24-32.)
INSPECTION AND TESTING OF COMPONENTS.
Upon completion of the disassembly, all parts should be cleaned and visually inspected for cracks, wear or
distortion and any signs of overheating or mechanical interference.
1. Rotor: The rotor should be tested for grounded or shorted windings. The ground test can be made with
test probes, connected in series with a 110-volt test lamp, an ohmmeter or any type of continuity tester. (Refer
to Figure 24-33.) There must not be any continuity between the slip rings and the rotor shaft or poles. To test
for shorted turns in the rotor windings, connect a voltmeter, ammeter and rheostat as shown in Figure 24-34, or
use an ohmmeter. Rotor current draw and resistance are listed in the Alternator Service Test Specifications
paragraph. Excessive current draw or a low ohmmeter reading indicates shorted windings. No current draw or
an infinite ohmmeter reading would indicate an open winding.
24-33-06
EFFECTIVITY:
Page 24-30
PRESTOLITE ALTERNATOR
Revised: July 13, 1983
1J1
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL
Summary of Contents for Arrow IV
Page 18: ...CHAPTER AIRWORTHINESS LIMITATIONS 1A18...
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Page 22: ...CHAPTER TIME LIMITS MAINT CHECKS 1A22...
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Page 40: ...CHAPTER DIMENSIONS AND AREAS 1B16...
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Page 53: ...CHAPTER LIFTING AND SHORING 1C5...
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Page 57: ...CHAPTER LEVELING AND WEIGHING 1C9...
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Page 62: ...CHAPTER TOWING AND TAXIING 1C14...
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Page 66: ...CHAPTER PARKING AND MOORING 1C18...
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Page 70: ...CHAPTER REQUIRED PLACARDS 1C22...
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Page 77: ...CHAPTER SERVICING 1D5...
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Page 110: ...CHAPTER STANDARD PRACTICES AIRFRAME 1E14...
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Page 117: ...CHAPTER ENVIRONMENTAL SYSTEM 1E21...
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Page 169: ...CHAPTER AUTO FLIGHT 1H1...
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Page 176: ...CHAPTER COMMUNICATIONS 1H8...
Page 185: ...CHAPTER ELECTRICAL POWER 1H17...
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Page 233: ...CHAPTER FLIGHT CONTROLS 1J17...
Page 297: ...CHAPTER FUEL 2A18...
Page 320: ...CHAPTER HYDRAULIC POWER 2B17...
Page 355: ...CHAPTER LANDING GEAR 2D4...
Page 418: ...CHAPTER LIGHTS 2F19...
Page 430: ...CHAPTER NAVIGATION AND PITOT STATIC 2G7...
Page 444: ...CHAPTER OXYGEN SYSTEM 2G21...
Page 464: ...CHAPTER VACUUM SYSTEM 2H17...
Page 473: ...CHAPTER ELECTRICAL ELECTRONIC PANELS AND MULTI PURPOSE PARTS 2I2...
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Page 477: ...CHAPTER STRUCTURES 2I6...
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Page 496: ...CHAPTER DOORS 2J1...
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Page 505: ...CHAPTER STABILIZERS 2J10...
Page 514: ...CHAPTER WINDOWS 2J19...
Page 519: ...CHAPTER WINGS 2J24...
Page 550: ...CHAPTER PROPELLER 3A18...
Page 565: ...CHAPTER STANDARD PRACTICES ENGINE 3B9...
Page 568: ...CHAPTER POWER PLANT 3B12...
Page 592: ...CHAPTER ENGINE FUEL AND CONTROL 3C12...
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Page 611: ...CHAPTER IGNITION 3D7...
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Page 655: ...CHAPTER ENGINE INDICATING 3F16...
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Page 664: ...CHAPTER EXHAUST 3G1...
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Page 669: ...CHAPTER OIL SYSTEM 3G6...
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Page 673: ...CHAPTER STARTING 3G10...
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Page 688: ...CHAPTER TURBINES 3H1...
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Page 694: ...CHAPTER 91 CHARTS AND WIRING DIAGRAMS 3H7...
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