CHART 2401. TROUBLESHOOTING (ALTERNATOR)
Trouble
Cause
Remedy
ALTERNATOR (cont)
Output indicated on ammeter
High resistance connections
Check visually for loose
does not meet minimum
in field or output circuit.
binding posts at the various
values specified in alternator
junction points in system,
system test procedure. (cont.)
alternator battery post, lugs
on ammeter, connections at
voltage regulator, circuit
breaker, etc., (See wiring
schematic.) Examine crimped
terminal ends for signs of
deterioration at crimp or strands of
broken wire at crimp. Tighten
any loose binding posts or replace
bad wire terminals.
Open rectifier.
If any of the six rectifiers
pressed into the rear bell
housing of the alternator
open up internally, it will
result i a definite limitation
on the current that can be
drawn from the alternator.
After having checked the previous
causes of low output it can be
assumed that a faulty rectifier exists.
See Paragraph titled Inspection
and Testing of Components.
Field circuit breaker trips.
Short circuit in field circuit.
Disconnect field wiring at
terminal of alternator. Turn
on master switch. If breaker
continues to trip, proceed to
disconnect each leg of field
circuit, working from the
alternator towards the circuit
breaker until breaker can be
reset and will hold. Replace
component or wire which was
isolated as defective. (See
wiring schematic.)
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
2 4 - 0 2 - 0 0
Page 24-04
Revised: May 15, 1989
1I16
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...