Piper PA-28-161 User Manual

SECTION 6
WEIGHT AND BALANCE
WEIGHT
vs
C.G. ENVELOPE
2440 M~X. GROSS WT.
PIPER AIRCRAFT CORPORATION
PA-28-161, WARRIOR II
89 90
NORMALCATEGORY ~--~--~~~~~~--r-~
86
,., Ill
\---1----+--+--+--1----+--+----+---1---1 a,--~- 1 BOO
t: .
~ i
~--+--1----t- -+----1r- --t---t--1--f--f :-- !:2-1700
"- w
c:r ~
~~~~~-+--+-~~~~~----~-1600
<[
....
!1.
\--\.--+-f-------l--l--.f--t----1--+--1-----!;-, 500
<[
':.G. LOCATION (INCHES AFT DATUM)
REPORT: VB-1180
6-14
C.G. RANGE AND WEIGHT
Figure 6-15
ISSUED: AUGUST 13, 1982

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)