Piper PA-28-161 User Manual

PIPER AIRCRAFT CORPORATION
PA·28·lfil, WARRIOR U
1.3 ENGINES
(a) Number of Engines
(b) Engine Manufacturer
(c) Engine Model Number
(d) Rated Horsepower
(e) Rated Speed (rpm)
(t) Bore (inches)
(g) Stroke (inches)
(b) Displacement (cubic inches)
(i) Compression Ratio
(J) Engine Type
1.5 PROPELLERS
(a) Number of Propellers
(b) Propeller Manufacturer
(c) Model
(d) Number of Blades
(e) Propeller Diameter (inches)
(1) Maximum
(2) Minimum
(f) Propeller Type
1.7 FUEL
AVGASONLY
(a) Fuel Capacity (U.S. gal) (total)
(b) Usable Fuel (U.S. gal) (total)
(c)
Fuel
(1) Minimum Octane
(2) Alternate Fuel
ISSUED: AUGUST 13,1982
REVISED: SEPTEMBER 12, 1990
SECTION 1
GENERAL
1
Lycoming
0-320-D2A or
0-320-D3G
160
2700
5.125
3.875
319.8
8.5:1
Four Cylinder, Direct Drive,
Horizontally Opposed,
Air Cooled
Sensenich
74DM6-0-60 or I
74DM6-0-58
2
74
72
Fixed Pitch
50
48
100 Green or 1 OOLL Blue
Aviation Grade
Refer
to Fuel Requirements,
Section 8 - Handling, Servicing
and Maintenance.
REPORT: VB-1180
1-3

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)