19. Check capacitors for looseness in the magneto cover of the harness assembly and for any physical damage.
The capacitors should be checked for capacitance, series resistance and leakage. Capacitance should be 0.34
to 0.41 microfarads. The use of a Bendix condenser tester, part number 11-1767 -1, -2 or-3 or equivalent
will simplify this test. Replace defective capacitors and torque securing nut to 60-70 inch-pounds.
— Note —
Spring in capacitor outlet may cause an indication of a short to ground if adapter lead
is not used. (Refer to Figure 744.)
IMPULSE COUPLING REMOVAL.
1.
Using heavy gloves or shop cloth, grasp the coupling body firmly to prevent the internal spring from
unwinding suddenly. Pull outward on the coupling body only enough to release it from the cam assembly.
Keep the coupling body close against the cam and allow the body to turn as the spring unwinds. After one
or two turns, the spring coils will wedge against the projections on the body, restraining the spring from
further unwinding.
2.
Look into the hole in body and note the location of the inner eye of spring where it engages with mating
recess in cam hub. Insert a screwdriver under spring end and pry spring eye out of recess. Remove the
body and spring together. Uncoil spring from body and pry spring eye from body recess to disengage
spring.
3.
Thread protective cap of 11-702-1 puller securely on end of shaft. Engage puller over protective cap and
cam assembly with wide jaws of puller hooked under cam assembly as shown in Figure 74-10.
4.
Tighten puller handle to remove coupling from shaft. If coupling does not release with maximum hand
torque at puller handle, apply penetrating thread release compound between coupling and shaft. Then while
puller is still fully tightened, hold tip of hot heavy duty soldering iron in contact with hub of coupling cam
assembly. Solder wetting of the tip at point of contact with the cam hub will assist in heat transfer to the
parts. Retighten puller after about a minute of heat application.
— CAUTION —
DO NOT STRIKE THE PULLER WITH A HAMRNER. IF PULLER IS
STRUCK WITH A HAMMER THE MAIN BEARINGS MUST BE
REPLACED.
5.
Do not tighten puller handle further after coupling cam releases from the shaft. This could damage the
flyweight if the flyweight is caught under the woodruff key. Remove the puller from the shaft. Then while
holding both flyweight tips inward, lift cam from the shaft, and remove woodruff key from rotor shaft.
INSPECTION OF IMPULSE COUPLING.
1.
Check clearance between each flyweight and each stop pin by the following method:
A.
Bend the end of a stiff piece of wire into a right angle, 1/8 inch long maximum.
B.
Hold the magneto as shown in Figure 7411. Pull the heel of the flyweight outward with the fabricated
hooked wire and make certain that a feeler gauge of 0.015 of an inch minimum thickness will pass
between the stop pin and the highest point of the flyweight.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
7 4 - 11 - 0 5
Page 74-13
Revised: May 15, 1989
3G6
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...