Piper PA-28-161 Maintenance Manual

PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 2
Nov 30/06
1E18
6-00-00
1. Leading Par
ticulars
and Principal Dimensions
CHART 1 (Sheet 1 of 2)
LEADING PARTICULARS AND PRINCIPAL DIMENSIONS
MODEL PA-28-161 - WARRIOR III
ENGINE
Manufacturer Textron Lycoming
Model O-320-D3G
FAA Type Certificate 274
Rated Horsepower 160
Rated Speed:
Full Throttle 2700 RPM
Oil, SAE Number See Table II-II
Oil Sump Capacity 8 U.S. qts
Fuel, Aviation Grade, Specified Minimum Octane 100LL, 100/130
Fuel Pump Drive Plunger
Carburetor, Marvel-Schebler MA-4SPA
Magnetos Slick
Left 4371
Right 4370
Spark Plugs (Shielded) & Spark Plug Gap Setting Refer to latest Lycoming
Service Instruction No. 1042.
Firing Order 1-3-2-4
Tachometer Drive, Ratio to Crankshaft 0.5:1
Starter:
Electrosystems, 28 Volt MHB4016
Alternator:
Electrosystems, (70 Amp) ALU-8421LS
Alternator Voltage Regulator, Lamar B-00331-2
Alternator Control, Lamar B-00368-2
PROPELLER TWO BLADE
Fixed Pitch:
Manufacturer Sensenich
Model 74 DM6-0-60
Diameter 74 in
Diameter, Minimum 72 in
FUEL SYSTEM
Main Tanks Two (One in each wing)
Capacity (each) 25 U.S. gal.
Unusable Fuel (each tank) One U.S. gal.
Total Fuel Onboard 50 U.S. gal.
Total Unusable Fuel Two U.S. gal.

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)