Leveling Diagram - Piper SENECA III Pilot's Information Manual

SECTION 6
PIPER
AIRCRAFT
CORPORATION
WEIGHT AND BALANCE
PA-34-220T,
SENECA III
(d)
Basic Empty
Weight Center
of Gravity
(l)
The following geometry applies to the PA-34-220T
airplane
when
it is level Refer to Leveling parag.raph 6.3
(b).
C.
G.
ARM
78.4*--
Level
Points
(Fuselage Left Side
Below Window)
/
N
R
+ L
A
*The datum is
78,4
inches
ahead
of the
BA
05
38
wing
leading edge at the
inboard edge of
the mboard fuel tank.
LEVELING
DIAGRAM
Figure 6-3
(2)
The basic
empty weight center of
gravity
(as
weighed
including
optional equipment, full
oil and unusable fuel) can be deter-
mined by the following formula:
C.G. Arm
=
N (A)
+
(R
+
L) (B)
inches
T
Where:T=N+R+L
REPORT: VB-Ill0
ISSUED: JANUARY
8,
1981
6-4