Leveling Diagram - Piper Cheyenne IIXL PA-31T2 1981 Pilot Operating Handbook

SECTION 6
WEIGHT AND BALANCE
PIPER AIRCRAFT CORPORATION
PA-31
T2,
CHEYENNE II XL
(d) Center of Gravity
(I)
The following geometry applies to the PA-31 T2 airplane
when it is level. Refer to Leveling paragraph 6.3 (b).
£
MAIN SPAR
LEVELING PROVISIONS
Longitudinal - Right side of fuselage nose
Stations 24.35 & 56.25
Lateral - Level across 2 center seat rails
LEVELING DIAGRAM
Figure 6-3
(2) C.G. Arm of airplane as weighed
x
REPORT: 2272
6-4
(137
+
15) - (127.6) (N) =
T
Inches Aft of Datum
ISSUED: APRIL 22, 1981