Piper PA-28-161 Maintenance Manual

PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 5
Nov 30/06
5F17
80-10-00
B. Stall-Torque Test
To see if the starter is producing its rated cranking power:
(1) Make test connections and set-up as shown in Figure 2.
(2) See specifications in Chart 2.
C. If torque and current are not within specifications, overhaul or replace the starter.
No Load Current Test
Figure 1
Stall Torque Test
Figure 2
Model MHB-4016
Brush Tension
Min. 32 oz.
Max. 40 oz.
No-Load Test (75°F)
Volt 20
Max. Amps 35
Min. RPM 1300
Stall Torque Test
Amps 260
Min. Torque, Ft.-Lbs. 27
Approx. Volts 14
CHART 2
STARTER SERVICE TEST SPECIFICATIONS

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)