Piper PA-28-151 User Manual

CHEROKEE
WARRIOR
POWER PLANT
Engine
(Lycoming)
Rated Horsepower
Rated
Speed
(rpm)
Bore
(inches)
Stroke
(
inches)
Displacement
(
cubic
inches)
Compression
Ratio
Dry
Weight
(pounds)
Propeller
McCauley
Sensenich
FUEL AND OIL
Fuel
Capacity
(U.S.
gal)
(standard)
Fuel
Caprcitf'
(U.S.
gal)
Usable
Oil Capacity
(qts)
Fuel. Aviation Grade
Minimum Octane
Specified Octane
Altemate
Fuels
DIMENSIONS
Wing
Span
(ft)
Wing
Area
(sq
ft)
Length
(ft)
Heieht
(ft)
Wing
Loading
(lbs
per
sq
ft)
Power
Loading
(lbs
per
hp)
Propeller
Diameter
(in.)
McCauley
Sensenich
Turning
Radius
BAC'GAGE
Maximum
Baggage
(lbs)
Baggage
Space
(cubic
ft)
Baggage
Door
Size
(in.)
LANDING
GEAR
Wheel
Base
(ft)
Wheel
Tread
(ft)
Tire Pressure
(psi)
Nose
Main
o-320-E3D
rs
2700
5.125
3.875
319.8
7:l
276
rcr60/EGM76s3
74DMGG58
50
48
8
8o/87
80/87
Refer to
Fuel
Requirements,
Section
l0
-
Page I G9
35
170.0
23.8
7.3
13.7
15.5
76
74
t
3.0
Nose
(4
ply
rating)
Main
(4
ply
rating)
200
24
20x22
6.7
10.0
30
24
5.00
x 5
6.00 x
6
GEITIERAL
SPECIFICATIONS
REVISED:
APRIL
16,1976
t-2
Tire
Size

Piper PA-28-151 Specifications

General

Manufacturer	Piper Aircraft
Engine	Lycoming O-320-E3D
Horsepower	150 hp
Wingspan	30 ft 0 in (9.14 m)
Seating Capacity	4
Model	PA-28-151
Height	7 ft 3 in
Cruise Speed	108 knots (124 mph, 200 km/h)
Fuel Capacity	50 US gallons (189 liters)
Maximum Takeoff Weight	2, 325 lb (1, 055 kg)