rubber bushings and insert the bushings into the retainers, rounded long edges first.
F. Place a new gasket on the magneto flange. Install the magneto carefully so the drive coupling lugs
mate with the slots of the drive bushings. Install and snug down the two sets of attaching screws.
Do not tighten at this time.
G. Breaker point opening may be checked by use of a suitable timing light. Tap the magneto case
with a non-marring hammer, counterclockwise (from the rear) to make certain the points are
closed. After the timing light indicates that the points are closed, tap the magneto lightly clockwise
until the points are open. Tighten the magneto attaching nuts.
H. Check timing by backing up crankshaft approximately 5 degrees and tapping gently forward until
the timing light indicates opening of breaker points. If timing is correct, the 20 degree mark
(midway between the 16 and 24 stamped on the crankshaft) will appear in the center of the
inspection hole. The crankshaft has punch marks in 2 degree increments with 16 and 24 at each
end. Tighten the magneto attachment nuts and replace the plug in the inspection hole on top of the
engine.
DISTRIBUTION.
INSPECTION OF HARNESS.
1. Check the lead assemblies for nicks, cuts, mutilated braiding, badly worn section or any other evidence
of physical damage. Inspect the spark plug sleeves for chafing or tears and damaged or stripped threads on
coupling nuts. Check the compression spring to see if it is broken or distorted. Inspect the grommet for tears.
Check all the mounting brackets and clamps to see that they are secure and not cracked.
2. Should a harness problem be suspected, integrity of the harness wiring may be checked using an
ohmmeter, buzzer, or other suitable device such as the Bendix/ECD High Tension Lead Tester Kits, P/N 11-
8950 or 11-8950-1; check each lead for continuity. If continuity does not exist, harness wire is broken and
must be replaced.
3. If an insulation failure is suspected, the condition of the insulation may be determined using the
Bendix 11-8950 and the 11-8950-1 High Tension Lead Tester Kits manufactured by the Electrical Components
Division, The Bendix Corporation, Sidney, New York.
4. Test Unit Preparation:
A. Install two “C” cells in the battery holder in accordance with correct position.
B. Check that red and black leads are open-circuited.
C. Depress PRESS-TO-TEST push-button switch.
D. Insure INDICATOR lamp flashes and GAP fires intermittently as long as PRESS-TO - T E S T
switch is depressed.
E. Interconnect both red and black high voltage leads and again depress PRESS-TO-TEST switch.
INDICATOR lamp only should flash. GAP does not fire.
F. Disconnect black and red leads.
5. Insulation Test:
A. Attach clip of red high voltage test lead to ignition harness lead terminal.
B. Attach black test lead clip to lead ferrule.
C. Depress PRESS-TO-TEST push-button switch.
D. Observe that INDICATOR lamp flashes and GAP fires intermittently as long as PRESS-TO-TEST
switch is held depressed.
E. Whenever INDICATOR lamp flashes and GAP fails to fire, lead under test is defective.
Effectivity
74-21-00
PA-28RT-201T
Page 74-10
December 1, 1978
3D19
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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