Piper PA-28-161 User Manual

PIPER AIRCRAFT CORPORATION
PA-28-161, WARRIOR II
ISSUED: AUGUST 13, 1982 REPORT: VB-1180
vi-a
REVISED: JUly 17, 2015
Revision FAA Approval
Number and Revised Description of Revisions Signature and
Code Pages Date
PIlOT’S OPERATING hANDBOOk lOG OF REVISIONS
Rev. 7 (cont) 2-3b Page added.
7-2 Revised para. 7.5.
8-3 Revised para. 8.5. D. H. Trompler
Oct. 8, 1990
Date
Rev. 8 iii Added Warning and moved
(PR050301) info. to page iv.
iv Moved info. from page iii.
vi-a Added Rev. 8 to L of R.
3-5 Revised para. 3.3.
3-13 Revised para. 3.23.
3-14 Corrected Issued date.
7-11 Revised para. 7.15.
8-1 Moved info. to page 8-1b and
revised para. 8.1.
8-1a Added page and
revised para. 8.1.
8-1b Added page and moved info.
from pages 8-1 and 8-2.
8-2 Moved info. to page 8-1b and Linda J. Dicken
revised para. 8.3. March 1, 2005
Rev. 9 ii Added copyright info.
(PR150717) vi-a Added Rev. 9 to L of R.
2-8 Revised Para. 2.25.
8-1b Revised Para. 8.1.
Eric A. Wright
July 17, 2015

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)