Piper Cherokee Arrow II Pilots Operating Manual page 101

ARROW
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
each scale. Deduct the tare, if any, from each reading.
4. EMPTY WEIGHT CENTER OF GRAVITY
Scale Position and Symbol
Nose Wheel (N)
Right Main Wheel (R)
Left Main Wheel (L)
Airplane Empty Weight, as Weighed (T)
a. The following geometry applies to the PA-28R-200 airplane when airplane is
level (See Item 2).
(Fuselage Left Side)
W i n g
Leading Edge
Scale
Reading
*
The datum is 78.4 inches ahead of the
wing leading edge at the intersection of
the straight and tapered section.
REPORT: VB-549 PAGE 5-4
I
MODEL: PA-28R-200
Tare
ISSUED:
MAY
14,1973
REVISED: APRIL 13,1979
Weight