SECTION 9
SUPPLEMENTS
PS-POH-1-1-01
Revision: -
Date of issue: 10/03/31
12 of 14
Blank form of Weight & Balance record
ITEM
WEIGHT
[lb/kg]
ARM
[in/mm]
MOMENT
(WEIGHT x ARM)
RIGHT MAIN
WHEEL
W
R
=
L
R
=
LEFT MAIN
WHEEL
W
L
=
L
L
=
NOSE WHEEL
W
N
=
L
N
=
-
negative arm
-
AIRCRAFT EMPTY C.G.
COMPUTED
C.G. EMPTY
Empty weight:
W
E
=
[lb/kg]
C.G.=
[in/mm]
[%]MAC
Aircraft moment:
M
E
=
NOTE:
EMPTY WEIGHT INCLUDING OIL, COOLANT AND HYDRAULIC FLUID.
MAXIMUM FUEL QUANTITY IN WING TANKS (180.62LB =30.1US GAL / 82.1KG=114L) IS USED FOR MOST FORWARD
C.G.CALCULATION.
MINIMUM FUEL QUANTITY IN WING TANKS FOR 30 MINUTE FLIGHT (22.2LB=3.7US GAL / 10.1KG=14L) IS
SUBTRACTED FROM MTOW (1,320LB / 600KG). MOST REARWARD C.G. CALCULATION IS DONE WITH ZERO FUEL
QUANTITY (AFTER FUEL DEPLETION).
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 ...
