Piper PA 28-181 User Manual

SECTION I
Gf,NERAL
PIPER AIRCRAFT
CORPORATION
PA,28-181,
ARCHf,R
rr
1.9 otl,
(a)
Oil Capacrly
(U.S. quaftt
(b)
Oil Specification
(c)
Oil
Viscosill per
Average Anbient
Ternp.
for Starting
(l)
Above 60' F
(2)
30" F to 90'F
(3)
0"F to
70'F
(4)
Below I0'F
8
Refer to
laiest issue
of Lyconing
Service
lnstruction
1014.
Single
Multi
S.A.E.
50
S.A.E. 40 or
50
s.A.E.40
S.A.E..10
S.A.E. l0
S.A.E. 40
or
20w_30
s.A.E.20
S.A_E.20W-to
1.11 MAXIMUM WEIGHTS
REPORT: VB-1120
l-4
\ormal
2558
2550
2550
200
ISSUED:
JULY
2,
REVISf,D:
JI;LY 2l!
(a)
Vaximum Ramp weishr
(lbs.)
(b)
\,aximum
Takeoff weisht
(lbs.)
(c)
Maxirnum Landing weight
(1bs.)
(d)
\'Iaximum Wcights
in BaSSage
Compartmenr
(lbs.)
Utility
2138
2l]0
2130
I.13 STANDARD
AIRPLANE WEIGHTS
Rcfer ro Figure 6-5
ior lhe
Standard Empty
Weigh!
and
the Useful
Load.
1919
1982

Piper PA 28-181 Specifications

General

Manufacturer	Piper Aircraft
Engine	Lycoming O-360-A4M
Horsepower	180 hp
Wingspan	35 ft 6 in (10.82 m)
Height	7 ft 3 in (2.21 m)
Maximum Takeoff Weight	2, 550 lb (1, 157 kg)
Seating	4
Service Ceiling	14, 100 ft
Fuel Capacity	50 US gal (190 L)
Propeller	Fixed Pitch