D.C. GENERATION (cont.)
(5) Service Procedures
Since the alternator and regulator are designed for use on only one polarity system, the following
pre- cautions must be observed when testing or servicing the electrical system. Failure to observe
these precautions will result in serious damage to the electrical equipment.
(a) Disconnect battery before connecting or disconnecting test instruments (except voltmeter) or
before removing or replacing any unit or wiring. Accidental grounding or shorting at the regulator,
alternator, ammeter or accessories, will cause severe damage to units and/or wiring.
(b) Alternator must not be operated on open circuit with the rotor winding energized.
(c) Do not attempt to polarize alternator. No polarization is required. Any polarization attempt
may result in damage to alternator, regulator or circuits.
(d) Grounding of alternator output terminal may damage the alternator and/or circuit and
components.
(e) Reversed battery connections may damage rectifiers, wiring or other components of the
charging system. Check battery polarity with a voltmeter before installing. Most aircraft are
negative ground.
(f) If a booster battery or fast charger is used, its polarity must be connected correctly to prevent
damage to the electrical system components.
(6) Overhaul of Alternator
Complete disassembly may not be required when repairing the alternator, . 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, use only the required operations.
(a) Disassembly of Alternator
1 Remove two Number 10-24 screws holding brush holder assembly in slip ring end head.
Remove t brush and holder assembly from end head.
2 Remove safety wire from through bolts. Hold pulley with a strap wrench and remove
pulley nut. Pulley must be removed with a puller. Remove fan, woodruff key and spacer
from shaft.
3 Remove four through bolts and tap drive end head lightly to separate drive end head and
rotor, as a unit, from stator and slip ring end head.
4 Remove nuts, lock washers, flat washers and insulators from output and auxiliary termi-
nal studs. Note carefully the correct assembly of insulator washers and bushings. Using
special tools shown in Figure 6, support the end head and press out the three negative
rectifiers. End head can now be separated from stator assembly.
5 Use a hook type or impact type bearing puller, as shown in Figure 5, to remove slip ring
end bearing and grease seal. Do not remove bearing unless replacement is necessary.
— 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.
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
24-30-00
Page 24-12
Reissued: July 1, 1993
1K12
Summary of Contents for PA-32R-301T SARATOGA S
Page 26: ...CHAPTER 4 AIRWORTHINESS LIMITATIONS 1C1 ...
Page 29: ...CHAPTER 5 TIME LIMITS MAINTENANCE CHECKS 1C4 ...
Page 53: ...CHAPTER 6 DIMENSIONS AND AREAS 1D6 ...
Page 64: ...CHAPTER 7 LIFTING AND SHORING 1D21 ...
Page 68: ...CHAPTER 8 LEVELING AND WEIGHING 1E1 ...
Page 72: ...CHAPTER 9 TOWING AND TAXIING 1E5 ...
Page 76: ...CHAPTER 10 PARKING AND MOORING 1E9 ...
Page 80: ...CHAPTER 11 REQUIRED PLACARDS 1E13 ...
Page 92: ...CHAPTER 12 SERVICING 1F1 ...
Page 126: ...CHAPTER 20 STANDARD PRACTICES AIRFRAME 1G17 ...
Page 127: ...THIS PAGE INTENTIONALLY LEFT BLANK ...
Page 139: ...CHAPTER 21 ENVIRONMENTAL SYSTEMS 1H5 ...
Page 188: ...CHAPTER 22 AUTOFLIGHT 1J7 ...
Page 193: ...CHAPTER 23 COMMUNICATIONS 1J12 ...
Page 203: ...CHAPTER 24 ELECTRICAL POWER 1J22 ...
Page 263: ...CHAPTER 25 EQUIPMENT FURNISHINGS 2A13 ...
Page 269: ...CHAPTER 27 FLIGHT CONTROLS 2A20 ...
Page 332: ...CHAPTER 28 FUEL 2D11 ...
Page 363: ...CHAPTER 29 HYDRAULIC POWER 2E18 ...
Page 404: ...CHAPTER 30 ICE AND RAIN PROTECTION 2G16 ...
Page 470: ...CHAPTER 32 LANDING GEAR 3A13 ...
Page 550: ...CHAPTER 33 LIGHTS 3D24 ...
Page 562: ...CHAPTER 34 NAVIGATION AND PITOT STATIC 3E12 ...
Page 582: ...CHAPTER 35 OXYGEN 3F8 ...
Page 604: ...CHAPTER 37 VACUUM 3G6 ...
Page 616: ...CHAPTER 39 3G18 ELECTRIC ELECTRONIC PANELS MULTIPURPOSE PARTS ...
Page 620: ...CHAPTER 51 STRUCTURES 3G22 ...
Page 636: ...CHAPTER 52 DOORS 3H14 ...
Page 650: ...CHAPTER 55 STABILIZERS 3I4 ...
Page 662: ...CHAPTER 56 WINDOWS 3I16 ...
Page 670: ...CHAPTER 57 WINGS 3I24 ...
Page 688: ...CHAPTER 61 PROPELLER 3J18 ...
Page 704: ...CHAPTER 70 STANDARD PRACTICES ENGINES 3K10 ...
Page 708: ...CHAPTER 71 POWER PLANT 3K14 ...
Page 737: ...CHAPTER 73 ENGINE FUEL SYSTEM 4A13 ...
Page 749: ...CHAPTER 74 IGNITION 4B1 ...
Page 783: ...CHAPTER 77 ENGINE INDICATING 4C11 ...
Page 793: ...CHAPTER 78 EXHAUST 4C21 ...
Page 801: ...CHAPTER 79 OIL 4D5 ...
Page 805: ...CHAPTER 80 STARTING 4D9 ...
Page 819: ...CHAPTER 81 TURBINES 4D23 ...
Page 833: ...CHAPTER 91 CHARTS WIRING DIAGRAMS 4E13 ...