Piper PA-32-300 User Manual

CHEROKEE
SIX.3OO
GROSS
WEIGHTS
WEIGHTS
Standard
Empty
Weieht
(lbs)
Maximum
Useful
Load
(lbs)
POWER
PLANT
Engine. Lycoming
Rated
Horsepower
Rated
Speed
(rpm)
Bore
(inches)
Stroke
(inches)
Displacement
(cubic
inches)
Compression
Ratio
Dry Weight
(pounds)
''
Propeller
(Standard)
(Optional)*
Propeller Diameter
(inches)
(Standard)
(Optional)
FUEL AND OIL
Fuel Capacity
(inboard) (U.S.
gal)
With
Standard
Auxiliary
(U.S.
gal)
Oil Capacity
(U.S.
qts)
Fuel,
Aviation Grade
(min
octane)
BAGGAGE
Maximum Baggage
(lbs)
Baggage Space
(cubic
ft)
Baggage
Door
Size
(in.)
*Serial
nos.
7440001
3400
2900
t824
1516
(Serial
nos.
7440O0
1
through
7
6
4Q06
5
and 7 64.046:7
through
76400',7r) rO-s4GKlAs
(serial
nos.
7640066,7640072
and
up)
IO-54SKlG5
300
2700
).lz)
4.3',15
541.5
8'7:
I
45'l
HC-C2YK-I
(
) |
847
s-4
or
HC{2YK-r(
)
|
847 5D-4
or
HC-C2YK-I
(
)F/F847
5D-4
HC{2YK-I(
)/847sR4
orHC{2YK-I(
)F/F8475R-0
80
84
1824
to16
50
84
t2
100/l
3o
Forward
100
8
16x22
GENERAL
SPECMCATIONS
REVISED: FEBRUARY 2, 191 6
Aft
100
20
thru 7540188 only

Piper PA-32-300 Specifications

General

Manufacturer	Piper Aircraft
Model	PA-32-300
Engine	Lycoming IO-540-K1A5
Horsepower	300 hp
Seating Capacity	6
Propeller	Constant speed, 2-blade
Wingspan	32 ft 10 in
Length	27 ft 8 in
Maximum Takeoff Weight	3, 400 lbs
Fuel Capacity	84 gallons
Stall Speed	61 mph
Rate of Climb	1, 050 ft/min
Cruise Speed	172 mph