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Piper PA-28-161 Maintenance Manual

Piper PA-28-161
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PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 1
Nov 30/062F3
24-50-00
ELECTRICAL LOAD DISTRIB
UTION
Component Loads
See Chart 1.
Duty Cycle Circuit / Circuit
Cont. Inter. Equipment Breaker (Amps) Optional
X Alternator Field 5 2.3
X Anti-Collision (Strobe) 5 3.5
X Auxiliary Vacuum Pump 20 5.0 X
X Cabin Dome Light 5 0.3
X Cockpit Flood Light 5 0.3
X Electric Clock - Negl. X
X Engine Gauge 3 0.2
X Fuel Pump 5 5.0
Instr. Panel/Switch Lights 7.5
X Panel Lights - 0.8
X Switch Lights - 0.8
X Landing Light 5 3.6
X Master Contactor - 0.5
X Pitot Heat 7.5 6.0 X
X Position (Nav) Lights 5 4.0
X Primer Valve - 0.4
X Radio Lights 5 0.5
X Recognition Lights 5 3.0 X
X Starter - 175.0
X Starter Contactor - 0.74
X Turn & Bank 5 0.3
Avionics (See Mfg's Installation Manual.)
CHART 1
ELECTRICAL SYSTEM COMPONENT LOADS

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Piper PA-28-161 Specifications

General IconGeneral
ManufacturerPiper Aircraft
ModelPA-28-161 Warrior II
EngineLycoming O-320-D3G
Horsepower160 hp
Seating Capacity4
Wingspan35 ft (10.7 m)
Length24 ft 0 in
Maximum Speed127 knots
Cruise Speed122 knots
Maximum Takeoff Weight2, 325 lb (1, 055 kg)
Fuel Capacity48 US gallons (182 L)

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