Specifications

CHEROKEE
SD(.300
A.
SECTION
I
LIMITATIONS
The
following Iimitations
must be observed
in the operation of this airplane:
ENGINE
Lycomins
IO'540-KIA5
(Serial
nos.
7440001
through 7640A65
and
7640067
through
764007t)
Lycoming
IO'54GKlG5
(Serial
nos. 7640066,7640A7 2
and
up)
ENGINE
LMITS
For
all
operations
2700 RPM,300 HP
FUEL
100/130
minimum aviation
grade
fuel
PROPELLER
Hartzell HC{2YK-l
18475D4
or HC{2YK-I(
)184754
or
HC{2YK-I(
Low
pitch
stop 13.5'
t
.2o
,
hieh
pitch
stop 34'
I
I'
Maximum
diameter
80
inches, minimum diameter
78.5
inches
OPTIONAL
PROPELLER
(Ser.
nos.
7440001
through 7540188
only)
Hartzell HC-C2YK-I(
)/8475R{
or HC{2YK-1(
)F/F8475R-0
Low
pitch
stop 12.4'
!
.2o
,
high
pitch
stop 29'
t
1'
Maximum
diameter
84
inches,
minimum
diameter
82.3 inches
POWER
INSTRT'MENTS
OIL TEMPERATURE
Green Arc
(Normal
Operating
Range)
)F/F847sD4
75'F
to 245"
F
245"F
B.
c.
D.
FAA
APPROVED
MAY 14,
1913
REVISED:
FEBRUARY
2. 197 6
Red Line
(Maximum)
OIL PRESSURE
Green Arc
(Normal
Operating
Range)
Yellow
Arc
(Caution
Range)
Red Line
(Minimum)
Red Line
(Maximum)
FUEL
PRESSURE
Green Arc
(Normal
Operating Range)
Red Line
(Minimum)
Red Line
(Maximum)
Yellow Arc
(Idle
Range)
TACHOMETER
Green Arc
(Normal
Operating Range)
Red Line
(Maximum
Continuous Power)
60
PSI to
90
PSI
25
PSI to
50
PSI
25 PSI
90
PSI
l8
PSI
to
4'0
PSI
I8
PSI
4.0 PSI
l2
PSI
to
18
PSI
500 to
2700 RPM
27OO RPM
REFORT:
vB-562
PAGE 3-1
MODEL:
PA-32-300