ALTERNATOR SYSTEM (CHRYSLER).
BENCH TESTING ALTERNATOR.
ROTOR FIELD COIL CURRENT DRAW. (Refer to Figure 24-3.)
1. Connect a jumper wire between one field terminal of the alternator and the positive terminal of a fully
charged battery.
2. Connect the test ammeter positive lead to the other field terminal of the alternator and the test ammeter
negative lead to the battery negative terminal.
3. While watching the test ammeter, slowly rotate the alternator rotor by hand.
A. Field coil draw should be 4.5 to 6.5 amperes at 12-volts.
—NOTE—
A low rotor coil draw is an indication of high resistance in the
field coil circuit (brushes, slip rings or rotor coils). A higher rotor
coil draw indicates possible shorted rotor coil or grounded rotor.
B. No reading indicates an open rotor or defective brushes.
TESTING ALTERNATOR INTERNAL FIELD CIRCUIT.
To test the alternator internal field circuit for a short circuit to ground, proceed as follows:
1. Remove the ground brush and place one test probe of a 110-volt test lamp to the field terminal. Attach
the remaining test probe to a machined surface at one of the alternator end shields. The test lamp should not
light. (Refer to Figure 24-4.)
2. Should the test lamp light, proceed as follows:
A. Remove the insulated brush assembly.
B. Remove the three through bolts and separate the two end shield assemblies.
C. Touch one of the test lamp probes to one of the slip rings and the remaining test probe to the rotor
shaft. The lamp should not light. A lighted test lamp indicates a grounded rotor assembly and will
require replacement of the rotor. If the test lamp does not light, a ground condition exists in the
insulated brush assembly. The brush assembly has either been improperly assembled or was
damaged and has short circuited through to ground. Inspect brush holder and insulated washer and
replace if damaged.
—NOTE—
The stack of parts attaching the insulated brush holder assembly
to the end shield must always be installed in the following
sequence: Insulated brush holder, “FLD” terminal, insulating
washer, lock washer and attaching screw.
24-32-03
EFFECTIVITY:
Page 24-14
CHRYSLER ALTERNATOR
Revised: July 13, 1983
1I9
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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