Piper PA-28-151 User Manual

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Revision 2
Lfunitations
and
Conditions
:
1.
Fl.A Approved
Airplane
Supplenental
Flight
Manual
dated
April
5,
L979,
for
Lycming
0-320-D3G
engine
lnstallation
with
Sensenich
74DM6-O-58
propeller;0R
FAA Approved
Alrplane
Supplpoental Flight Manual
dated
ApriL
24,
1980,
for
Lycoming
0-320-D3G
engine
installation
with either
Senenich
74DM6-0-58,
or
74DM6-0-60 propeller;
OR
FAA
Approved
Airplane
Supple'r'ental Flight
Manual
dated
October
21,
1981,
for
Lycoring
0-320-D2A,
-D28, -DzC,
or
-D3G
engine
installation
with
either
Sensenich 74DM6-0-58, ot
74DM6-0-60
propeller
is
required.
2. Conpatibility
of
this
nodification
with other
previously
approved
uodifications
must
be deterained
by the
installer.
An1,allerattcrt
oJ this
ccrttfuaie
is
punishable
by
afru oJ nol cxcccding t|,000,
or
imfrtscnmtrti
ncl
cxctcdtng
3
yars, or botli
FAA
FoRM 8rrG2-t
(tG69)
This cettifuak nu2 bc
nazstarcd
in ucordante
with FAR 21.47
pecg
2
or
2erces

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)