PIPER
AIRCRAFf
CORPORATION
PA-28-161,
WARRIOR
II
(h) Number of Propellers
(i)
Propeller Manufacturer
G)
Propeller
Model
(k) Propeller Diameter
Minimum
Maximum
(1)
74DM6-0-60 Propeller Tolerance
(static
rpm
at
maximum
permissible
throttle setting, Sea Level, ISA)
N01E
SECTION
2
LIMITATIONS
1
Sensenich
74DM6-0-60 or I
74DM6-0-58
72IN.
74
IN.
Not above
2430
RPM
Not
below
2330
RPM
Refer to
the
airplane maintenance
manual
for
test
procedure
to
determine approved static rpm
under
non
standard conditions.
(m)
74DM6-0-58
Propeller Tolerance
(static
RPM
at
maximum
permissible
throttle setting, Sea Level, ISA)
N01E
Not
above
2465
RPM
Not
below
2365
RPM
Refer to
the
airplane maintenance
manual
for
test
procedure
to
determine approved static rpm
under
non
standard conditions.
2.9
POWER
PLANT
INSTRUMENT
MARKINGS
(a)
Tachometer
Green
Arc
(Normal
Operating Range)
Red
Line
(Maximum
Continuous Power)
(b) Oil Temperature
Green
Arc
(Normal
Operating Range)
Red
Line
(Maximum)
ISSUED: AUGUST 13, 1982
REVISED:
SEYfEMBER
12, 1990
500
to
2700
RPM
2700RPM
REPORT: VB-1180
2-3
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