CHART 2103. INSPECTION (IGNITION UNIT)
INSPECTION OF IGNITION UNIT.
Inspect components as directed in Chart 2103 and Figure 21-13.
— Note —
Replace any component that fails to meet checks listed in Chart 2102.
CYCLING SWITCH AND LIMIT (OVERHEAT) SWITCH. (Refer to Figure 21-18)
1. Removal:
A. If the limit switch is damaged or defective, disconnect the three electrical leads from the switch
terminals. Be sure to mark the leads for proper reassembly. (The switch terminals are identified by
numbers “1”,“2” and “3”).
B. Remove the two attaching screws and lift the limit switch and spacers (gaskets) from the
jacket opening.
C. If the cycling switch is damaged or defective, disconnect the electrical leads being sure
to mark them for proper reassembly.
D. Remove the two screws and lift the cycling switch from the jacket opening.
— Note —
No attempt should be made to repair either of these switches. If they do not operate
properly, they should be replaced.
2. Installation: (Refer to Figure 21-18)
A. Install the limit switch and spacers (gaskets) by placing them in position in the heater jacket
opening and installing two screws.
B. Tighten screws securely; then reconnect the electrical leads in accordance with markings made
during disassembly. (Refer to wiring diagram, Figure 21-7)
C. Install the cycling switch (refer to Figure 21-18) by placing it in position in the heater jacket
opening and securing it with the two screws. Tighten screws securely; then reconnect the electrical
leads to their respective terminals as marked during disassembly. (Refer to wiring diagram, Figure
21-7)
Index No.
Nomenclature
Inspection
1
Cover Assembly
Inspect for security of lead assembly to cover.
Ignition cable, grommet, terminal and connector
for carbon tracks, cracks or distortion. Repair
or replace for any of the above conditions.
4
Ignition Coil
Inspect for broken bakelite, carbon tracks, oil
leaks, and dents in coil cover. Replace for any
of the above conditions.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
2 1 - 4 3 - 2 0
Page 21-27
Revised: May 15, 1989
1F18
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...