Piper cherokee WARRIOR - ENGINE AND PROPELLER LIMITATIONS; Engine Operating Limits

CHEROKEE
WARRIOR
SECTION I
LIMITATIONS
The following limitations must be observed in the operation of this airplane:
A. ENGINE
Lycoming O-320-E3D
ENGINE
LIMITS
For
all operations 2700 RPM, 150 HP
B.
FUEL
80187
octane aviation
fuel minimum
grade
C.
PROPELLER
Sensenich 74DM6, maximum
diameter
74 inches. Minimum diameter 72 inches. Static
RPM
at
maximum
permissible
throttle setting:
Not
over
2375,
not under
2275. No
additional
tollerance
permitted.
McCauley lcl60/EGM7653, maximum diameter
76 inches. Minimum diameter 74.5
inches.
Static
RPM
at maximum
permissible
throttle setting:
Not over 2400,
not
under
2300.
No
additional tollerance
permitted.
D. POWER INSTRUMENTS
OIL TEMPERATURE
FAA
APPROVED
JULY
25,1973
REVISED:
APRIL 16.1976
Green Arc
(Normal
Operating
Range)
Red
Line
(Maximum)
OIL PRESSURE
Green Arc
(Normal
Operating Range)
Yellow
Arc
(Caution
Range)
Rcd
Line
(Mininrum)
l(c:tl
l.inc
(
Mirxirnurrr)
FUEL
PRESSURE
Green
Arc
(NormalOperating
Range)
Red
Line
(Minimum)
Red
Line
(Maximum)
TACHOMETER
Green Arc
(NormalOperating
R*g.)
Red
Line
(Maximum
Continuous
Power)
75'F
to
245'F
245"F
60 PSI tO 90 PSI
25 PSI
to 60
PSI
25
PSI
()0
I'sl
.5
PSI
to 8
PSI
.5 PSI
8 PSI
500 to 2700
RPM
27OO
RPM
REPORT: VB-573
PAGE 3-l
MODEL:
PA-28-151