SECTION
1
GENERAL
PIPER
AIRCRAFT
CORPORATION
PA-28-161,
WARRIOR
ll
1.9
OIL
(a) Oil Capacity (U.S. quarts)
(b) Oil Specification
(c) Oil Viscosity per Average Ambient
Temp. for Starting
(1) Above 60°F
(2) 30°F
to
90°F
(3) 0°F
to
70°F
(4) Below 10°F
1.11
MAXIMUM
WEIGHTS
(a) Maximum Takeoff Weight (lbs)
(b) Maximum Ramp Weight (lbs)
(c) Maximum Landing Weight (lbs)
(d) Maximum Weight in Baggage
Compartment (lbs)
8
Refer to latest issue
of
Lycoming Service
Instruction
1014.
Single
S.A.E. 50
S.A.E.
40
S.A.E. 30
S.A.E. 20
Normal
2440
2447
2440
200
Multi
S.A.E. 40 or 50
S.A.E.
40
S.A.E. 40 or
20W-30
S.A.E. 20W-30
Utility
2020
2027
2020
0
1.13 STANDARD
AIRPLANE
WEIGHTS
Refer
to
Figure
6-5 for the Standard Empty Weight and the Useful
Load.
1.15
BAGGAGE
SPACE
(a) Compartment Volume (cubic feet
(b) Maximum Ramp Weight (lbs)
(c) Maximum Landing Weight (lbs)
1.17
SPECIFIC
LOADINGS
(a) Wing Loading (lbs per sq ft)
(b) Power Loading (lbs per hp)
REPORT:
VB-1180
1-4
24
22
20
14.4
15.3
ISSUED: AUGUST 13, 1982
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