Piper PA-28-161 Maintenance Manual

PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 6
Nov 30/06
5F18
80-10-00
6. Starter Control Circuit
A. Inspect the control circuit wiring between the battery, solenoid and manual starting switches for
breaks, poor connections and faulty insulation. Tighten all connections and make sure solenoid is
firmly mounted and makes a good ground connection.
B. Check the voltage loss across the switch contacts during normal starting. If loss is in excess of 0.2
volts per 100 amperes, the solenoid should be replaced.
C. If solenoid fails to operate when the manual starting switch is turned on or if it fails to release when
the manual starting switch is released, it should be removed and tested to specifications, if
available. If either opening or closing voltages are not to specifications, or tests cannot be
performed, replace the solenoid.
7. Starting with External P
ower
See 24-40-00.

Piper PA-28-161 Specifications

General

Manufacturer	Piper Aircraft
Model	PA-28-161 Warrior II
Engine	Lycoming O-320-D3G
Horsepower	160 hp
Seating Capacity	4
Wingspan	35 ft (10.7 m)
Length	24 ft 0 in
Maximum Speed	127 knots
Cruise Speed	122 knots
Maximum Takeoff Weight	2, 325 lb (1, 055 kg)
Fuel Capacity	48 US gallons (182 L)