Electrical System Component Load - Piper PA-44-180 SEMINOLE Maintenance Manual

CHART 9109. ELECTRICAL SYSTEM COMPONENT LOAD (Sheet 1 of 2)
DUTY 1 CYCLE 2
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1
CONTINUOUS
2
INTERMITTENT
PIPER AIRCRAFT
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
EQUIPMENT
ALTERNATOR FIELD (2)
STARTER SOLENOID (LEFT
AND RIGHT)
CIGAR LIGHTER(ACCESSORY)
STARTER
FUEL PUMP (LEFT)
FUEL PUMP (RIGHT)
ENGINE GAGES (LEFT)
ENGINE GAGES (RIGHT)
HYDRAULIC PUMP
LANDING GEAR CONT. & WARN.
LANDING GEAR SOLENOID
GEAR DOWN LIGHTS (3)
GEAR UNSAFE LIGHT
GEAR WARN HORN
MASTER CONTACTOR
COMBUSTION HEATER
PITOT HEAT
STALL WARNING HORN
ELECTRIC TURN & BANK
PITCH TRIM
LANDING LIGHT (PA-44-180, S/N'S
44-7995001 THRU 44- 8195026, AND
PA-180T, S/N'S 44-8107001 AND UP)
LANDING LIGHT - 2 BULBS.
(PA-44-180, S/N' 4495001 AND UP)
AVIONICS LIGHTS
INSTRUMENT PNL. LIGHTS
FLOOD LIGHTS
RED FLOOD
DOME LIGHT
POSITION LIGHTS
4B19
CKT.- (AMPS)
BKR.
5 5.0 EA
10 10.0
— 8.0
— 175.0
8 0.5
8 0.5
5 appx. 1.0
5 appx. 1.0
25 25.0
5 —
— 0.8
— Total 0.3
— 0.08
— 0.4
— 0.6
15 13.0
15 13.2
5 0.4
5 0.5
5 5.0
10 8.0
15 14.0
Varies on
5 Avionics
Instls.
10 2.5
5
— 1.0
— 0.6
10 7.3
91-23-00
Page 91-24
Revised: June 20, 1995
OPT.