SECTION 6
WEIGHT & BALANCE
PS-POH-1-1-01
Date of issue: 10/03/31
Revision: -
6-4
6.4 Operating weights and loading
Max. takeoff weight.............................................
1,320 [lb]
(600 [kg])
Max. landing weight ............................................
1,320 [lb]
(600 [kg])
Max. weight of fuel..............................................
180 [lb]
(82 [kg])
Max. baggage weight in rear fuselage ................
40 [lb]
(18 [kg])
Max. baggage weight in each wing locker ..........
44 [lb]
(20 [kg])
Empty weight (minimum equipment)...................
760 [lb]
(345 [kg)
NOTE
Actual Empty weight is shown in Section 9, Supplement No. 02
Number of seats .................................................
2
Minimum crew ....................................................
1
pilot on the left seat
Minimum crew weight .........................................
95 [lb]
(43 [kg])
Maximum crew weight on each seat
................... 253 [lb] (115
[kg])
6.5 C.G. range and determination
Aircraft C.G. range:
Operating C.G. range..........................................
27 to 38 [%]
of MAC
15.94 to 22.44 [in] (405 to 570 [mm])
of MAC
Empty weight C.G. range
....................................28 to 32 [%]
of MAC
16.54 to 18.90 [in] (420 to 480 [mm])
of MAC
Aircraft C.G. determination:
NOTE
Actual Weight and Balance record is shown in Section 9, Supplement No. 02.
Summary of Contents for Piper Sport
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