Piper PA-28-161 User Manual

PIPER AIRCRAFT CORPORATION
PA-28-161, WARRIOR II
SECTION 6
WEIGHT
AND BALANCE
MODEL PA-28-161, WARRIOR II
Airplane Serial Number----------
Registration Number __________ _
Date
_______________________ __
AIRPLANE BASIC
EMPTY WEIGHT
C.G. Arm
Weight
x (Inches Aft = Moment
Item
Actual
Standard Empty Weight* Computed
Optional Equipment
Basic Empty Weight
(Lbs) of Datum) (In-Lbs)
*The standard empty weight includes full
oil capacity and 2.0 gallons of
unusable fuel.
AIRPLANE
USEFUL LOAD- NORMAL CATEGORY OPERATION
(Ramp Weight) -(Basic Empty Weight) = Useful Load
(Normal Category:
(2447 lbs) - (
(Utility Category:
(2027 lbs) - (
lbs.)
=
lbs.) =
· lbs.
lbs.
THIS BASIC EMPTY WEIGHT, C.G. AND USEFUL LOAD ARE
FOR THE AIRPLANE AS LICENSED AT THE FACTORY. REFER
TO APPROPRIATE AIRCRAFT RECORD WHEN ALTERATIONS
HAVE BEEN MADE.
WEIGHT AND BALANCE DATA FORM
Figure 6-5
ISSUED: AUGUST 13, 1982
REPORT:
VB-1180
6-7

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)