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.
Scale
Scale Position and Symbol
Reading
Tare
Weight
Nose Wheel
(N)
Right Main Wheel
(R)
Left Main Wheel
(L)
Airplane Empty Weight, as Weighed (T)
4.
EMPTY WEIGHT CENTER OF GRAVITY
a.
The following geometry applies to the PA-28R-200 airplane when airplane
is level (See Item 2).
----C.G. ARM---,M
---- 78.4*-----i�
N
A
----B------
A =
B =
REPORT:
VB-334 PAGE S-4
MODEL: PA-28R-200
Level Points
R+L
(Fuselage Left Side)
Wing Leading Edge
*
The datum is 78.4 inches ahead of the
wing leading edge at the intersection of
the straight and tapered section.
ISSUED: October 14, 1971
REVISED: APRIL 10, 1979
N16422 POH
