Piper ARCHER III Pilot Operating Handbook page 176

SECTION 6
WEIGHT AND BALANCE
6.3 AIRPLANE WEIGHING PROCEDURE (continued)
(d) Basic Empty Weight Center of Gravity
(1) The following geometry applies to the PA-28-181 airplane when it
is level. Refer to Leveling paragraph 6.3 (b).
(2) The basic empty weight center of gravity (as weighed including
optional equipment, full oil and unusable fuel) can be determined
by the following formula:
C.G. Arm= N (A)+ (R + L) (8)
Arm --
i-----C. G.
---78.4 ---
E
a
"'
'O
REPORT: VB-2749
6-4
T
Where: T = N + R + L
Level Points
(Fuselage)
LEVELING DIAGRAM
Figure 6-3
PA-28-181, ARCHER
inches
=
A 31.0
=
B 109.7
ISSUED: December 22, 2017
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