*Loading graph is shown with the seats in the fourth notch from the most
forward position. If C.G. falls near the forward or aft limit, occupant seat
positions are important; and moments should be calculated by multiplying
pilot and passenger weight by appropriate arm aft datum (see Figure
6-14), rather than determined by the loading graph.
LOADING GRAPH
Figure 6-15
PIPER AIRCRAFT CORPORATION SECTION 6
PA-38-112, TOMAHAWK WEIGHT AND BALANCE
ISSUED: JANUARY 20, 1978 REPORT: 2126
REVISED: MARCH 1, 1979 6-11
*Loading graph is shown with the seats in the fourth notch from the most
forward position. If C.G. falls near the forward or aft limit, occupant seat
positions are important; and moments should be calculated by multiplying
pilot and passenger weight by appropriate arm aft datum (see Figure
6-14), rather than determined by the loading graph.
LOADING GRAPH
Figure 6-15
PIPER AIRCRAFT CORPORATION SECTION 6
PA-38-112, TOMAHAWK WEIGHT AND BALANCE
ISSUED: JANUARY 20, 1978 REPORT: 2126
REVISED: MARCH 1, 1979 6-11
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