Piper PA-28-161 User Manual

PILOT'S OPERATING HANDBOOK LOG OF REVISIONS
Revision
Number and Revised
Code
Pages
Rev. 3 (cont) 7-4
7-10
7-11
8-11,
8-13,
8-14
Rev.4 7-11
(PR850712) 7-22
9-73
thru
9-77
Rev.5
5-22
(PR880715)
8-1,
8-2
9-i
Rev.6 vi
(PR900228)
7-24a&
7-24b
8-2&
8-3
8-11
8-12
Rev. 7 V1
(PR900912)
1-3
2-3
2-3a
REPORT:
VB-1180
vi
FAA Approval
Description of Revisions
Signature and
Date
Revised para. 7. 7.
Revised para. 7.13.
Revised para. 7 .15.
LJ~
Revised para. 8.21.
Ward Evans
June 28, 1984
Revised para. 7 .15
Revised para. 7.26
..p,~~ J
Added Supplement 8
(Aux. Vacuum System) D.H.Trompler
Sept. 23, 1985
Revised fig. 5.23
example.
J~w
Revised para. 8.1.
Added Supplement 8 D.H.Trompler
toT.O.C.
August 11, 1988
Added Rev. 6 to Log of
Revisions.
Added pages. Revised
para. 7.35.
Added
Narco ELT 910 info.
Revised para.
8.3.
J~~.
Revised para's. 8.19 & 8.21.
D. H :rromJer
Revised Fuel Grade Chart.
Mar. 2!2. 1290
Date
Added Rev. 7 to Log of
Revisions.
Revised para.
1.5 (c).
Revised
para. 2.7 G) and (1).
Added para. 2.7 (m). Moved
info. to page 2-3a.
Page added. Info. relocated
from page 2-3.

Piper PA-28-161 Specifications

General

Manufacturer	Piper Aircraft
Model	PA-28-161 Warrior II
Engine	Lycoming O-320-D3G
Horsepower	160 hp
Seating Capacity	4
Wingspan	35 ft (10.7 m)
Length	24 ft 0 in
Maximum Speed	127 knots
Cruise Speed	122 knots
Maximum Takeoff Weight	2, 325 lb (1, 055 kg)
Fuel Capacity	48 US gallons (182 L)