Piper PA-28-151 User Manual

I
2. PROPFT.T ER:
II.
LIMITATIONS
1.
NGINE
LTMIIS:
2. PROPELLM.
LD{I15:
3.
M{GINE
INSTR.I]MENT
I4ARKINGS:
F.A.A.
APPROVED
DATE:
L|/LL/8L
{tF:jiii;:i:b
Lycmrlng
0-320-D2A
or
Lycoming 0-32O-D2B
or
Lyconing O-32O-D2C
or
Lycoming 0-320-D3G
Sensenich
74DM6-0-60
or
Sensenich
74DM6-0-58
Maximum
Continuous:
150 H.P.
-
2550
RPM
Takeoff
(Five (5)
llinutes)
150 H.P.
-
2700
RPM
Static RPM
at
maximum
throttle
setting:
Not
over
2450,
Not under
2350
Diameter:
Maximrmr
=
74
inches
Minimurn
=
72 inches
TACIIOMETERI
Green
Arc
Yellow
Arc
Red
Radial
2200
-
2650
RPM
2650
-
2700 RPM
-
2700
RPM
AIRCRAFT
MODIFICATIONS
INC.
PIPER
CIIEROKEE
MODEL
PA-28-151
SUPPLN,IE{TAL
FL IGIIT
MANUAL
GENEMI.
1.
ENGINE:
III.
PROCEDIJRES
No
Change
IV.
PERFORMANCE
the
perfonnance
of
Lhis
airptane equipped with
a Lycoming
O-320-D2A,
O'32O-D2B'
0-320-D2C,
or
0-320-D3G
engine is
equal
to or better
than
the
original
F.A.A.
approved
perfor:mance.
S.T.C. No.
SA2969SW
Page2of2pages
Woco-Modison
Cooper
Airport
.
P.O.
Box 5249.
Woco, Texos
76708
.
817-752-8384

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)