SECTION 9
SUPPLEMENTS
PS-POH-1-1-01
Revision: -
Date of issue: 10/03/31
4 of 14
WEIGHT & BALANCE RECORD
Rearward C.G. Check
of PiperSport aircraft S/N : P1001001
REARWARD C.G.
WEIGHT
[lb]
ARM
[in]
MOMENT
(WEIGHT x ARM)
EMPTY AIRCRAFT
853.60
--------
14,460.91
PILOT
190.08
27.56
5,238.60
PASSENGER
190.08
27.56
5,238.60
BAGGAGE
COMPARTMENT - A
33.00
51.58
1,702.14
BAGGAGE
COMPARTMENT - B
6.60
70.87
467.74
WING LOCKERS
24.42
23.62
576.80
FUEL TANKS
0.0
7.09
0.0
TOTAL
W
T
=1,297.78
[lb]
M
T
= 27,684.80
TAKEOFF WEIGHT
1,297.78
[lb]
CG= 21.33
[in]
36.1
[%] MAC
NOTE: MINIMUM FUEL QUANTITY IN WING TANKS FOR 30MINUTE FLIGHT (22.2LB=3.7US GAL) IS SUBTRACTED
FROM MTOW (1,320LB). MOST REARWARD C.G. CALCULATION IS DONE WITH ZERO FUEL QUANTITY
(AFTER FUEL DEPLETION).
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
Serial No.: P1001001
Date: 2010-03-02
By: Otakar Hrabinec
Summary of Contents for Piper Sport
Page 2: ...Date of issue 10 03 31 Revision PS POH 1 1 01 ii Intentionally left blank ...
Page 4: ...Revision PS POH 1 1 01 Date of issue 10 03 31 iv Intentionally left blank ...
Page 6: ...Revision PS POH 1 1 01 Date of issue 10 03 31 vi Intentionally left blank ...
Page 14: ...Revision PS POH 1 1 01 Date of issue 10 03 31 xiv Intentionally left blank ...
