USING THE AMMETER.
Whether in flight or during ground testing, the ammeter can be used to indicate the general nature of most
electrical problems. The troubleshooting chart is primarily based on the use of the ammeter and assumes that the
user does understand all normal operating modes of the system.
— Note —
When troubleshooting, first use the “ammeter test” and “heat test” to determine which
circuits are involved. Use circuit diagram for assistance to check voltages or
continuity.
HELPFUL TIPS.
1. If the ammeter reading drops to one-third normal current, this indicates that one heater circuit is open.
2. Excess current reading on the ammeter always indicates a power lead is shorted to ground. Thus, when
trouble of this nature is found, it is vital that the grounded power lead be located and corrected.
3. A considerable number of timers that have been returned for repair proved to be fully workable when tested.
Accomplish the test described in “Timer Test” before concluding that the timer is defective.
4. Defective wiring in propeller mounted components may be indicated by normal current readings in ground
checkouts (propellers not rotating) but low current with propellers rotating at cruise RPM.
INSPECTION.
50 HOUR INSPECTION.
1. Lock brakes and operate engines at near takeoff power. Turn deicer system switch ON and observe deicer
ammeter for at least two minutes. Ammeter needle must rest within the shaded band, except for a “flicker,”
approximately every 90 seconds, as the step switch of the timer operates. Any movement of the needle
other than the normal 90 second flicker indicates a short or open that must be located and corrected.
2. With engines stopped, turn deicer switch ON and feel deicers on propellers for proper sequence of heater
operation. The deicers should cycle ON for 90 seconds, then OFF for 90 seconds and repeat. Temperature
rise should be noticeable and each heater should warm for about 90 seconds. Local hot spots indicate
surface damage of deicer heaters requiring replacement of deicer.
3. Remove spinner dome and engine cowling. With assistant observing deicer ammeter and with deice r
switch ON, flex all accessible wiring, particularly the deicer wire harness, leads from slip ring assembly,
and the firewall electrical connectors and their wiring. Any movement of the ammeter needle other than the
“90 second flicker” of cycling indicates a short or open that must be located and corrected.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
3 0 - 6 5 - 0 1
Page 30-31
Revised: May 15, 1989
2E11
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...