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Piper ARCHER II - Page 31

Piper ARCHER II
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SECTION
1
GENERAL
PIPER
AIRCRAFT
CORPORATION
PA-28-181,
ARCHER
II
Moment
Center
of
Gravity
(C.G.)
C.G.
Arm
C.G.
Limits
Usable
Fuel
Unusable
Fuel
Standard
Empty
Weight
Basic
Empty
Weight
_
Payload
Useful
Load
Maximum
Ramp
Weight
REPORT:
VB-1120
The
product
of
the
weight
of
an
item
multi-
plied
by
its
arm.
(Moment
divided
by
a
constant
is
used
to
simplify
balance
calcu-
lations
by
reducing
the
number
of
digits.)
The
point
at
which
an
airplane
would
balance
if
suspended.
Its
distance
from
the
reference
datum
is
found
by
dividing
the
total
moment
by
the
total
weight
of
the
airplane.
The
arm
obtained
by
adding
the
airplane’s
individual
moments
and
dividing
the
sum
by
the
total
weight.
The
extreme
center
of
gravity
locations
within
which
the
airplane
must
be
operated
at
a
given
weight.
Fuel
available
for
flight
planning.
Fuel
remaining
after
a
runout
test
has
been
completed
in
accordance
with
govern-
mental
regulations.
Weight
of
a
standard
airplane
including
unusable
fuel,
full
operating
fluids
and
full
oil.
Standard
empty
weight
plus
optional
equipment.
Weight
of
occupants,
cargo
and
baggage.
Difference
between
takeoff
weight,
or
ramp
weight
is
applicable,
and
basic
empty
weight.
Maximum
weight
approved
for
ground
maneuver,
(It
includes
weight
of
start,
taxi
and
run
up
fuel.)
ISSUED:
JULY
2,
1979

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