8.
Check the capacitors for looseness in the magneto cover of the harness assembly and for any physical
damage. Using a Bendix 11-1767-1, -2 or -3 condenser tester or equivalent, check capacitors for
capacitance, series resistance and leakage. Capacitance shall be 0.34 to 0.41 microfarads.
9.
Check magneto to engine timing per instructions given in the following paragraph.
10. Check action of impulse coupling. With the ignition switch off, observe breaker cam end of r.otor while
manually cranking the engine through a firing sequence. The rotor should alternately stop and then (with an
audible snap) be rotated rapidly through a retard firing position. If impulse action is not correct, remove the
magneto for overhaul.
MAGNETO INSTALLATION AND TIMING PROCEDURE. (Timing Magneto to Engine)
1.
Installation of the magneto to the engine may be accomplished without removal of the cover from the
magneto. Also, the magneto cover has switch terminal outlets for the right and left sides of the magneto
located in the center of the harness lead outlet sections of the cover.
2.
The magneto incorporates a built-in pointer and a degree wheel with sufficient reference to assist the
mechanic in magneto timing procedures. Printed upon the rotating magnet are marks to indicate magneto
neutral and magneto “E” gap (8°). (Refer to Figure 74-5.) Also included are retard angle references of 15,
20 and 25 degrees. These marks are set up for either clockwise (R) or counterclockwise (L) rotation of the
magneto as viewed from the magneto drive end. The timing tooth of the large distributor gear is marked
with red paint. (Refer to Figure 74-6.)
3.
When correctly timed internally, a magneto will have the timing teeth of the large distributor gears
approximately centered in the timing windows, the R or L (“E” gap) mark on the rotor in alignment with the
pointer and both main breaker points opening, all occuring simultaneously. These three references, “E” gap,
painted teeth and point opening, are all used when timing the magneto to the engine.
4.
Remove the spark plug from the No. 1 cylinder and turn the crankshaft in the direction of normal rotation
until the compression stroke is reached.
5.
Continue turning the crankshaft until the 23° advance timing mark is in alignment with the small hole
located on the top face of the starter housing at the two o’clock position. (Refer to Figure 74-3.)
6.
Install the magneto-to-engine gasket on the magneto flange.
— WARNING —
DO NOT AT TACH HARNESS SPARK PLUG ENDS TO THE SPARK PLUGS
UNTIL AN MAGNETO TO ENGINE TIMING PROCEDURES AND
MAGNETO-TO-SWITCH CONNECTIONS ARE ENTIRELY COMPLETED
— Note —
The use of a timing light, unit Part No. 11-9110 or 11-9110-1 will simplify the timing
procedure. This unit is availablefrom theBendix Corporation, Sidney, New Yo r k
13838.
It is recommended that short adapter leads be fabricated to facimate connecting the
timing light unit to the switch outlet terminals of the cover. (Refer to Figure 74-4.)
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
7 4 - 11 - 0 2
Page 74-05
Revised: May 15, 1989
3F22
PIPER AIRCRAFT
Summary of Contents for SEMINOLE PA-44-180
Page 38: ...CHAPTER DIMENSIONS AND AREAS 1B14...
Page 49: ...CHAPTER LIFTING AND SHORING 1C1...
Page 53: ...CHAPTER LEVELING AND WEIGHING 1C5...
Page 58: ...CHAPTER TOWING AND TAXIING 1C10...
Page 62: ...CHAPTER PARKING AND MOORING 1C14...
Page 65: ...CHAPTER REQUIRED PLACARDS 1C17...
Page 70: ...CHAPTER SERVICING 1C22...
Page 98: ...CHAPTER STANDARD PRACTICES AIRFRAME 1E2...
Page 108: ...CHAPTER ENVIRONMENTAL SYSTEM 1E12...
Page 189: ...CHAPTER AUTOFLIGHT 1H21...
Page 192: ...CHAPTER COMMUNICATIONS 1H24...
Page 202: ...CHAPTER ELECTRICAL POWER 1I10...
Page 228: ...CHAPTER EQUIPMENT FURNISHINGS 1J12...
Page 233: ...CHAPTER FIRE PROTECTION 1J17...
Page 238: ...CHAPTER FLIGHT CONTROLS 1J24...
Page 304: ...2A18 CHAPTER FUEL...
Page 325: ...2B17 CHAPTER HYDRAULIC POWER...
Page 357: ...2D1 CHAPTER ICE AND RAIN PROTECTION...
Page 414: ...CHAPTER LANDING GEAR 2F13...
Page 479: ...2I6 CHAPTER LIGHTS...
Page 488: ...2I16 CHAPTER NAVIGATION AND PITOT STATIC...
Page 503: ...2J7 CHAPTER OXYGEN...
Page 524: ...2K6 CHAPTER VACUUM...
Page 535: ...2K19 CHAPTER ELECTRICAL ELECTRONIC PANELS AND MULTIPURPOSE PARTS...
Page 546: ...INTENTIONALLY LEFT BLANK PA 44 180 180T AIRPLANE MAINTENANCE MANUAL 2L6 PIPER AIRCRAFT...
Page 547: ...2L7 CHAPTER STRUCTURES...
Page 582: ...CHAPTER DOORS 3A18...
Page 593: ...CHAPTER STABILIZERS 3B8...
Page 604: ...CHAPTER WINDOWS 3B22...
Page 611: ...CHAPTER WINGS 3C10...
Page 624: ...CHAPTER PROPELLER 3D1...
Page 643: ...CHAPTER POWER PLANT 3D21...
Page 667: ...CHAPTER ENGINE FUEL SYSTEM 3F1...
Page 681: ...CHAPTER IGNITION 3F16...
Page 712: ...CHAPTER ENGINE INDICATING 3H1...
Page 730: ...CHAPTER EXHAUST 3H19...
Page 734: ...CHAPTER OIL 3I1...
Page 743: ...CHAPTER STARTING 3I11...
Page 755: ...CHAPTER TURBINES 3J1...