Piper SENECA III - Page 31

PIPER
AIRCRAFT
CORPORATION
SECTION
I
PA-34-220T,
SENECA
III
GENERAL
Unusable
Fuel
Fuel
remaining
after
a
runout
test
has been
completed
.
in
accordance
with
govern-
mental regulations.
Standard Empty
Weight
of
a
standard
airplane
including
Weight
unusable
fuel,
full
operating
fluids
and
full
oil.
Basic Empty
Standard
empty
weight
plus
optional
Weight
e4uipment.
Payload
Weight
of
occupants,
cargo
and
baggage.
Eseful
Load
Difference
between
takeoff
weight,
or
ramp
weight
if
applicable,
and
basic
empty
weight.
Maximum Ramp
Maximum
weight
approved
for
ground
Weight
maneuver.
(It
includes
weight
of
start,
taxi
and
run
up
fuel.)
Maximum
Maximum
weight
approved
for the
start
of
Takeoff Weight
the
takeoff
run.
Maximum
Maximum
weight
approved
for
the
landing
Landing
Weight
touchdown.
Maximum
Zero
Maximum weight exclusive of usable
fuel.
Fuel
Weight
ISSUED:
JANUARY
8,
1981
REPORT:
VB-1110
1-11