SECTION
6
WEIGHT
AND
BALANCE
PIPER
AIRCRAFT
CORPORATION
PA-28-161,
WARRIOR
ll
Arm Aft
Weight Datum
Moment
(Lbs) (Inches)
(ln-Lbs)
Basic Empty Weight
Pilot
and
Front
Passenger
80.5
Passengers (Rear Seats)*
118.1
Fuel (48 Gallon Maximum)
95.0
Baggage* (200 Lbs. Maximum)
142.8
Ramp
Weight (2447 Lbs. Normal,
2027 Lbs. Utility Maximum)
Fuel Allowance
-7
95.0
-665
For
Engine Start, Taxi and Run Up
Total
Loaded Airplane (2440 Lbs. Normal,
2020 Lbs. Utility Maximum)
Totals
must
be
within approved weight and
e.G.
limits. It
is
the responsi-
bility
of
the airplane owner and the pilot to insure that the airplane
is
loaded
properly. The Basic Empty Weight
e.G.
is
noted on the Weight and Balance
Data
Form
(Figure 6-5).
If
the airplane has been altered, refer
to
the Weight·
and
Balance Record for this information.
*Utility Category Operation
- No baggage
or
aft passengers allowed.
WEIGHT AND BALANCE
LOADING
FORM
Figure
6-11
REPORT: VB-1180
6-12
ISSUED: AUGUST 13, 1982
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