SECTION 9
SUPPLEMENTS
PS-POH-1-1-01
Revision: -
Date of issue: 10/03/31
3 of 14
WEIGHT & BALANCE RECORD
Forward C.G. Check
of PiperSport aircraft S/N : P1001001
FORWARD C.G.
WEIGHT
[lb]
ARM
[in]
MOMENT
(WEIGHTxARM)
EMPTY AIRCRAFT
853.60
--------
14,460.91
PILOT
88.00
27.56
2,425.28
PASSENGER
0.0
27.56
0.0
BAGGAGE
COMPARTMENT - A
0.0
51.58
0.0
BAGGAGE
COMPARTMENT - B
0.0
70.87
0.0
WING LOCKERS
0.0
23.62
0.0
FUEL TANKS
180.62
7.09
1,280. 60
TOTAL
W
T
=1,122.22
[lb]
M
T
= 18,166.78
TAKEOFF WEIGHT
1,122.22
[lb]
C.G.= 16.19
[in]
27.4
[%] MAC
NOTE: MAXIMUM FUEL QUANTITY IN WING TANKS (180.62LB =30.1US GAL) IS USED FOR MOST FORWARD
C.G.CALCULATION.
Max.
T
ake
O
ff weight : 1,320 [lb]
Max. weight in baggage compartment A+B : 40 [lb]
Max. weight in wing lockers together : 88 [lb]
Operating C.G. range : 15.94 to 22.44 [in] / 27 to 38 [%] of MAC
M
T
100
Aircraft C.G. = -------- [in] x -------- [%]
W
T
MAC
2010-03-02
Summary of Contents for Piper Sport
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