Piper CHEROKEE ARCHER II Pilot Operating Handbook page 19

SECTION I
GENERAL
PIPER AIRCRAFT CORPORATION
PA.2&I8I,
CHEROKEE ARCHER
tr
I.1I
MA)(IMUM
WEIGHTS
(a)
Maximum Takeoff Weight (lbs)
(b)
Maximum Landing Weight (lbs)
(c)
Maximum
Weights
in
Baggage
Compartment
1.13 STAI.IDARD AIRPLAI.IE WEIGIITS*
(a)
Standard
Empty Weight (lbs): Weight
of
a
standard airplane including unusable fuel,
full
operating fluids and
full
oil.
(b)
Maximum Useful Load (lbs): The difference
between the Maximum Takeoff Weight
and
the Standard
Empty
Weight.
I.I5
BAGGAGE
SPACE
(a)
Compartment Volume (cubic feet)
(b)
Entry Width
(inches)
(c)
Entry Height (inches)
I.I7
SPECINC LOADINGS
(a)
Wing Loading (lbs per
sq
ft)
(b)
Power Loading (lbs per
hp)
rThese values
are
Standard Empty
specified.
REFORT: VB-790
t4
and may vary
from
one
and Useful Load
value
aircraft
to
another.
to
be used
for
C.G.
UTILITY
2r30
2130
0
l4l6
I
134
15.0
t4.2
Refer
to
Figure 6-5
for
the
calculations
for
the
aircraft
NORMAL
2550
2550
200
24
)')
20
approximate
Weight
value
ISSUED: JLJNE
18, 1976
REVISED: MAY 23,19t0