AMMETER.
The ammeter is mounted in the instrument panel. This instrument measures the output of the alternator into
the entire electrical system including the battery charging demand.
EXTERNAL POWER.
EXTERNAL POWER RECEPTACLE.
The external power receptacle is located on the right side of the nose section. When using external power for
operation of any of the airplane's equipment, the master switch must be ON. To start the engine with external
power proceed as follows:
— CAUTION —
EXTERNAL POWER IS SUPPLIED DIRECTLY TO THE ELECTRICAL
BUS. TURN OFF ALL ELECTRICAL EQUIPMENT BEFORE APPLY I N G
OR REMOVING EXTERNAL POWER.
1. Turn aircraft MASTER SWITCH and all electrical equipment OFF.
2. Connect the RED lead of PEP (Piper External Power) kit jumper cable to the POSITIVE (+) terminal of
external 12 volt battery and the BLACK lead goes to the NEGATIVE (-) terminal.
3. Insert the plug of the jumper cable into the socket located on the aircraft fuselage.
4. Leave MASTER SWITCH OFF and proceed with engine starting technique as follows:
A.
Start engines with the standard technique but after starting both engines reduce power on the left
engine to the lowest possible RPM to reduce sparking. and shut down the right engine.
5. Turn all electrical equipment OFF and remove the jumper cable plug from the aircraft.
6. Turn the aircraft MASTER SWITCH to the ON position and check the alternator ammeter for an
indication of output. Do not attempt any flight if there is no indication of alternator output.
— Note —
For all normal operations using the PEP jumper cables, the master switch should be
OFF, but it is possible to use the ship 's battery in parallel by turning the master switch
ON. This will give longer cranking capabilities, but will not increase the amperage.
— CAUTION —
CARE SHOULD BE EXERCISED BECAUSE IF THE SHIP’S BATTERY HAS
BEEN DEPLETED, THE EXTERNAL POWER SUPPLY CAN BE REDUCED
TO THE LEVEL OF THE SHIP’S BAT T E RY. THIS CAN BE TESTED BY
TURNING THE MASTER SWITCH ON MOMENTA R I LY WHILE THE
STARTER IS ENGAGED. IF CRANKING SPEED INCREASES, THE SHIP’S
B AT T E RY & AT A HIGHER LEVEL THAN THE EXTERNAL POWER
S U P P LY. IF THE BAT T E RY HAS BEEN DEPLETED BY EXCESSIVE
CRANKING IT MUST BE RECHARGED BEFORE THE SECOND ENGINE
IS STA RTED. ALL THE ALT E R N ATOR CURRENT WILL GO TO THE
LOW BAT T E RY UNTIL IT RECEIVES SUFFICIENT CHARGE, AND IT
MAY NOT START THE OTHER ENGINE IMMEDIATELY.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
2 4 - 4 1 - 0 0
Page 24-23
Revised: May 15, 1989
1J11
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...