Piper ARCHER II - Page 25

SECTION 1 PIPER AIRCRAFT CORPORATION
GENERAL
PA-28-181,
ARCHER
II
1.9
OIL
(a)
Oil
Capacity
(U.S.
quarts)
8
(b)
Oil
Specification
Refer
to
latest
issue
of Lycoming Service
Instruction 1014.
(c) Oil Viscosity per Average Ambient
Temp. for Starting
Single Multi
(1}
Above
60°F
S.A.E.
50
S.A.E.
40
or
50
(2)
30°F
to
90°F
S.A.E.
40
S.A.E.
40
(3)
O°F
to
70°F
S.A.E.
30
S.A.E.
40
or
20 W-30
(4)
Below
10°F
S.A.E.
20
§.A.E.
20W-30
1.11 MAXIMUM WEIGHTS
Normal Utility
(a) Maximum Ramp Weight (lbs.) 2558 2138
(b)
Maximum
Takeoff
Weight
(Ibs.)
2550
2130
(c)
Maximum
Landing
Weight
(Jbs.)
2550
2130
(d) Maximum Weights in Baggage
Compartment
(lbs.)
200
0
1.13 STANDARD AIRPLANE WEIGHTS
Refer
to
Figure
6-5
for
the
Standard
Empty
Weight
and
the
Useful
Load.
REPORT:
VB-1120
ISSUED:
JULY
2,
1979
1-4
REVISED:
JULY
21,
1982