SECTION 6
WEIGHT & BALANCE
PS-POH-1-1-01
Date of issue: 10/03/31
Revision: -
6-6
Max.
T
ake
O
ff weight : 1,320 [lb] (600 [kg])
Max. weight in baggage compartment A+B : 40 [lb] (18 [kg])
Max. weight in wing lockers together : 88 [lb] (40 [kg])
Empty weight C.G. range : 16.54 to 18.90 [in] (420 to 480 [mm]) / 28 to 32 % of MAC
Operating C.G. range : 15.94 to 22.4 4 [in] (405 to 570 [mm]) / 27 to 38 % of MAC
Maximum useful weight:
W
Max Useful
= W
Max Take
O
ff
– W
E
W
Max Useful
= 1,320 [lb] (600 [kg]) – = [lb]/[kg]
This useful weight must be never exceeded!
NOTE: MAXIMUM USEFUL WEIGHT INCLUDING PILOT, PASSENGER, BAGGAGE AND FUEL.
M
T
(M
E
) 100
Aircraft C.G. = ------------ [in/mm] x -------- [%]
W
T
(W
E
) MAC
6.6 Permitted payload range table
NOTE
Actual Permitted payload range table is shown in Section 9, Supplement No. 02.
Registration:
Serial No.:
Date:
By:
Содержание Piper Sport
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