(d) Center of Gravity
(1) The following geometry applies to the PA-38-112 airplane
when it is level. Refer to Leveling paragraph 6.3 (b).
LEVELING DIAGRAM
Figure 6-3
(2) The empty weight center of gravity (as weighed including
optional equipment, full oil and operating fluids) can be
determined by the following formula:
C.G. Arm = N (A) + (R + L) (B) inches
T
Where: T = N + R + L
SECTION 6 PIPER AIRCRAFT CORPORATION
WEIGHT AND BALANCE PA-38-112, TOMAHAWK
REPORT: 2126 ISSUED: JANUARY 20, 1978
6-4
(d) Center of Gravity
(1) The following geometry applies to the PA-38-112 airplane
when it is level. Refer to Leveling paragraph 6.3 (b).
LEVELING DIAGRAM
Figure 6-3
(2) The empty weight center of gravity (as weighed including
optional equipment, full oil and operating fluids) can be
determined by the following formula:
C.G. Arm = N (A) + (R + L) (B) inches
T
Where: T = N + R + L
SECTION 6 PIPER AIRCRAFT CORPORATION
WEIGHT AND BALANCE PA-38-112, TOMAHAWK
REPORT: 2126 ISSUED: JANUARY 20, 1978
6-4
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