Piper PA-28-161 User Manual

PIPER AIRCRAFT CORPORATION
PA-28-161, WARRIOR II
SECTION 6
WEIGHT
AND BALANCE
iii
c
z
400
350
300
5 250
~
...
:s:
CJ
w 200
~
c
<
g
150
100
50
10 15 20 25 30
MOMENT/1000 (POUNDS -INCHES)
LOADING GRAPH
Figure 6-13
35
40
ISSUED: AUGUST 13, 1982
REPORT: VB-1180
6-13

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)