REMOVAL OF MAGNETO.
Before removing the magneto, make sure magneto switches are off.
1. Remove the harness assembly terminal plate from the magneto.
—WARNING—
The magneto is not internally grounded; when the ground lead is
disconnected, the magneto is hot. Removing the harness assembly
terminal plate first and installing them last minimizes the danger
of starting the engine accidentally when the ground lead is
removed from the magneto.
2. Disconnect the ground lead at the magneto.
3. Remove the nuts and washers and draw the magneto from the engine.
TIMING PROCEDURE. (Internal Timing)
1. Remove the cover to the contact(s), distributor block, etc.
2. To internally time the contact assembly of the single-breaker magnetos, proceed as follows:
A. Loosen the nut securing the drive plate to the magneto shaft sufficiently in order to install the
Scintilla 11-8465 Rotor Holding Tool under the nut and flat washer as shown in Figure 74-24.
Tighten the nut securely.
B. Remove the timing inspection plug from the top of the magneto. Turn rotating magneto to proper
neutral position. This position is determined by locating keyways on drive end of magnet shaft at
12 o’clock with respect to nameplate on housing. Tighten adjusting knob of 11-8465 Rotor
Holding Tool until pressure is applied on housing flange preventing magnet from turning.
C. Loosen and rotate cam until cam follower of contact assembly rests on highest point of cam lobe.
Adjust contact assembly to obtain the clearance of 0.016 of an inch. Tighten contact assembly
securing screws to 20-25 inch-pounds.
D. Install the 11-8693 Timing Plate Assembly and the 11-8149 Pointer Assembly of the 11 - 8 1 5 0
Scintilla Timing Kit to breaker compartment of magneto. (Refer to Figure 74-25) Align pointer
assembly with the 0 mark on timing plate. Loosen adjusting knob of 11-8465 Rotor Holding Tool
and turn rotating magnet in normal direction of rotation until pointer indexes with the respective E
gap mark (15° ± 2° ). Tighten adjusting knob of 11-8465 Tool and remove the 11-8149 Pointer
Assembly from magneto. Using a timing light, adjust contact points to just open. This adjustment
shall be made by rotating cam, in opposite direction of rotation until contacts just open. While
holding cam in this exact position, push cam on magnet shaft as far as possible with the fingers.
Extreme care must be exercised in this operation. If cam adjustment is changed in the slightest
degree, the timing of the magneto will be thrown off. Do not drive cam on shaft with a mallet or
other instrument. Tighten the securing screw thereby drawing the cam down, evenly and tightly.
Torque screw to 16-20 inch-pounds. Loosen the 11-8465 Rotor Holding Tool adjusting knob and
return rotating magnet to neutral position. Reinstall the 11-8149 Pointer Assembly over 0 mark on
timing plate. Rotate magnet shaft in normal direction of rotation and check for opening of main
contact points at E gap setting (15° ± 2°).
3. If the distributor block was not removed from the housing, the internal timing may be checked by
turning the magneto in the normal rotation to number one firing position (keyway up and points just opening).
At this position, the reference line on the distributor block should line up between the L and LB marks on the
gear. On single contact magnetos the line should favor the L mark, if possible.
Effectivity
74-11-03
PA-28RT-201
Page 74-26
December 1, 1978
3E11
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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