Piper ARCHER II - Page 129

SECTION
6
__
PEPER
AIRCRAFT
CORPORATION
WEIGHT
AND
BALANCE
:
;
PA-28-181,
ARCHER
I
Arm
Ait
Weight
Datum
ent
(Lbs)
(Inches)
_({In-Lbs)
Basic
Emply
Weight
Meili
PAP
S\
9
50G
¢-
Pilot
and
Front
Passenger
a
|
80.5
Passengers
(Rear
Seats)*
118.1
Fuel
(48
Gallon
Maximum)
:
“
*
95.0
Baggage
(200
Lbs:
Maximum)*
wD
142.8
Ramp Weight (2558 Lbs. Norfnal, -
2138 Lbs. Utility Maxi )
Fuel
Allowance
.
For
Engine
_
Taxi
and
Run
Up.
-8
95)
-760
Tak Weight (2550.Lbs. Normal,
30 Lbs. Utility Maximum)
Totals
must
be
within
approved
weight
and.
ce
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
C.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
rear
passengers
allowed.
WEIGHT AND BALANCE LOADING FORM
Figure 6-11
REPORT:
VB-1120
-
ISSUED:
JULY
2,
1979
6-10
REVISED:
FEBRUARY
2,
1990