SECTION
2
LIMITATIONS
PIPER
AIRCRAFT
CORPORATION
PA-28-161,
WARRIOR
II
SPEED
Design Maneuvering Speed
(VA}
-
Do
not
make full
or
abrupt
control
movements above this speed.
At
2440 LBS. G.W.
At
1531
LBS. G.W.
CAUTION
KIAS
Ill
88
Maneuvering speed decreases at lighter weight
as the effects of aerodynamic forces become
more pronounced. Linear interpolation may
be
used for intermediate gross weights. Maneu-
vering speed should not
be
exceeded while
operating in rough air.
2.5
AIRSPEED
INDICATOR
MARKINGS
MARKING
Red Radial
Lint:
(Never Exceed)
Yellow
Arc (Caution Range
-Smooth
A;r Only)
Green Arc (Normal Operating Range)
White Arc (Flap Down)
2.7
POWER
PLANT
LIMITATIONS
Number
of
Engines
KCAS
108
89
KIAS
160
126
lu
160
50
to I26
44 to
103
(a)
(b)
(c)
(d)
Engine Manufacturer
Engine
Model No.
Lycoming
0-320-D2A
or
0-320-DJG
Engine Operating Limits
(I)
Maximum
Horsepower
(2) Maximum Rotation Speed
(RPM)
(3) Maximum Oil Temperature
160
2700
24SO
F
(e) Oil Pressure
Minimum (n:d line)
Maximum
(red line)
(f)
Fuel
Pres~urc
(g)
Minimum (n:d line)
Maximum
(red line)
Fuel
(AVGAS ONLY)
(minimum
~rade}
REPORT:
VB-ll80
2-2
25
PSI
100
PSI
.5
PSI
g PSI
100
or
IOOLL
Aviation Grade
ISSUED:
AUGUST
13, 1982
REVISED:
JUNE
28, 1984
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