Piper cherokee WARRIOR Pilots Operating Manual page 54

CHEROKEE WARRIOR
b.
Level airplane (see diagram) deflating nose wheel tire, to center bubble on
level.
3.
WEIGHING - AIRPLANE EMPTY WEIGHT
a.
With the airplane level and brakes released, record the weight shown on
c'ach scale. Deduct the tare. if any' from each reading'
4.
EMPTY WEIGHT CENTER OF GRAVITY
a.
The following geometry applies to the PA-28-l5l airplane when airplane is
level (See Item 2).
C. G. Arm
Level Points
(Fuselage)
7 8 . 4
Wing Leading Edge
R + L
The clatunt is 78.4 inches ahead
of the wing leading edge at the
intersection of the straight and
tapered section.
A -
B -
REPORT: vB-s35 PAGE 54
M O D E L : P A - 2 8 - l 5 l
ISSUED: IvtAY 14, 1973
R E V I S E D : A P R l l . 6 . t , r 7 9
Scale Position and SYmbol
Scale
Reading
Tare
N e t
Weight
Nose Wheel
(N)
Rieht Main Wheel
(R)
Left Main Wheel
(L)
Airplane Empty Weight, as Weighed (T)