D.C. GENERATION (cont.)
(8) Checking Alternator Belt Tension (cont.)
Chart 3
Prestolite Alternator Belt Tension
C 90 Amp Ford Alternator System (Refer to Figure 16.)
(1) Description
The principal components of the alternator are the front housing, fan and pulley, rear housing and
terminal identification, stator core and coil assembly, rotor core and coil, brushes and holder
assembly and rectifier assembly.
(a) The front housing is a die-cast aluminum part which meets design requirements for a
lightweight, non-magnetic material. This casting incorporates the bosses used to attach the
assembly to its mounting bracket. It also provides the supporting surface for the rotor shaft
front bearing and vendor identification data stamped into the front housing.
The fan and pulley are attached to the rotor shaft with a nut and lock-washer. The forward
end of the shaft is threaded to accept the nut.
(b) The rear housing is also a die-cast aluminum part which supports the rotor shaft rear bearing
and provides mounting bosses for the rectifier assembly. The housing contains the various
electrical connections and openings for cooling airflow. (Refer to Figure 17 for Terminal
identification.)
(c) The stator core and coil assembly consists of a number of steel stampings riveted together to
form the stator core which contains 36 equally spaced vertical slots to accommodate the sta-
tor coil windings. (Refer to Figure 18.)
(d) The rotor core and coil assembly consists of the rotor shaft, two slip rings, two rotor halves
and the coil assembly. The shaft is supported at each end by bearings. The front bearing
(ball-type) is a slip fit on the shaft and is retained in the front housing with a retainer. The
rear bearing (needle-type) is pressed into the rear housing. The slip rings, core and coil
assembly are press-fitted to the shaft with a rotor half enveloping each end of the coil.
The rotor core and coil assembly turns inside the stator core and coil assembly with a very
narrow air gap between the two assemblies, thus developing maximum magneto induction.
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
24-30-00
Page 24-19
Reissued: July 1, 1993
1K19
Torque indicated at
Width of Belt
Condition
alternator pulley
3/8 inch
New
11 to 13 ft-lbs
3/8 inch
Used
7 to 9 ft-lbs
1/2 inch
New
13 to 15 ft-lbs
1/2 inch
Used
9 to 11 ft-lbs
—NOTE—
Higher tension specified for new belts compensates for
initial stretch that takes place as soon as it is operated. Do
not apply higher tensions to previously used belts
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 ...