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SECTION 6
PIPER AIRCRAFT CORPORATION
PA-28R-lOI, ARROW
WEIGHT AND BALANCE
6.3 AIRPLANE WEIGHING PROCEDURE (continued)
Scale Position and Symbol
Scale
Reading
Tare
Net
Weight
Nose Wheel
(N)
Right Main Wheel
(R)
left Main Wheel
(l)
Basic Empty Weight. as Weighed (T)
E
a
Ol
'0
WEIGHING FORM
Figure 6-1
(d) Basic Empty Weight Center of Gravity
(I)
The following geometry applies to the PA-28R-201
airplane when it is level. Refer to leveling paragraph
6.3 (b).
N
Level Points
(Fuselage)
- -
~ 1-~
Wing Leading Edge
R
L
The datum is 78.4 inches ahead
+
of the wing leading edge at the
J
intersection of the straight and
tapered section
1 - - - - - - 8
A
=
15.6
B
=
109.7
LEVELING DIAGRAM
Figure 6-3
REPORT: VB-1365
6-4
ISSUED: SEPTEMBER 15,1988
(
(
(
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