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John's
* Weight & Balance *
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MM-DD-YYYY |
Hours |
Photos |
Scope of work |
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12-7-2004 |
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Imported Zenith
Weight & Balance Worksheet |
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KIT SERIAL # |
7-4544
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Registration # |
N????? |
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By: |
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Date: |
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ITEM
|
WEIGHT
(pounds)
|
ARM
(mm.)
|
MOMENT |
|
RIGHT MAIN WHEEL |
W
R
=
Scale Reading
|
L =
Measured
|
WR
X LR |
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LEFT MAIN WHEEL |
W
L
= |
L =
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|
NOSE WHEEL |
W = |
L = -
Negative arm |
– |
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COMPUTED CG
EMPTY |
Empty
Weight: |
CG=
Arm to Datum
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Aircraft Moment
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Forward Check:
Add
to the empty weight & aircraft moment items located forward of the
computed empty CG (i.e. Fuel) plus the pilot.
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MOMENT - Forward |
MOMENT - Rear |
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PILOT / PASSENGER
|
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600 *
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WING TANKS
L & R: _10_
Gal. each |
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600
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REAR BAGGAGE
(MAX. 40 Lbs.) |
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1050
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TOTAL
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TWF=
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TWR=
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Gross
Weight: |
Take-Off
Weight: |
*
Depends on seat
position &
individuals’
weight
distribution. |
TMF
= |
TMR
=
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CG
(FWD)
= |
CG
(AFT)
= |
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CG Range: From
280 mm |
to 500 mm. |
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Center of Gravity
(CG) = |
Total Weight (TW)
Total Moment (TM) |
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