Piper PA-28-161 User Manual

SECTION 8 PIPER AIRCRAFT CORPORATION
HANDLING, SERV & MAINT PA-28-161, WARRIOR II
REPORT: VB-1180 ISSUED: AUGUST 13, 1982
8-1a REVISED: MARCH 1, 2005
SECTION 8 PIPER AIRCRAFT CORPORATION
HANDLING, SERV & MAINT PA-28-161, WARRIOR II
REPORT: VB-1180 ISSUED: AUGUST 13, 1982
8-1a REVISED: MARCH 1, 2005
8.1 GENERAL (CONTINUED)
WARNING
Use only genuine PIPER parts or PIPER approved parts
obtained from PIPER approved sources, in connection with the
maintenance and repair of PIPER airplanes.
Genuine PIPER parts are produced and inspected under
rigorous procedures to insure airworthiness and suitability for
use in PIPER airplane applications. Parts purchased from
sources other than PIPER, even though identical in appearance,
may not have had the required tests and inspections performed,
may be different in fabrication techniques and materials, and
may be dangerous when installed in an airplane.
Additionally, reworked or salvaged parts or those parts obtained
from non-PIPER approved sources, may have service histories
which are unknown or cannot be authenticated, may have been
subjected to unacceptable stresses or temperatures or may have
other hidden damage not discernible through routine visual or
nondestructive testing. This may render the part, component or
structural assembly, even though originally manufactured by
PIPER, unsuitable and unsafe for airplane use.
PIPER expressly disclaims any responsibility for malfunctions,
failures, damage or injury caused by use of non-PIPER
approved parts.
8.1 GENERAL (CONTINUED)
WARNING
Use only genuine PIPER parts or PIPER approved parts
obtained from PIPER approved sources, in connection with the
maintenance and repair of PIPER airplanes.
Genuine PIPER parts are produced and inspected under
rigorous procedures to insure airworthiness and suitability for
use in PIPER airplane applications. Parts purchased from
sources other than PIPER, even though identical in appearance,
may not have had the required tests and inspections performed,
may be different in fabrication techniques and materials, and
may be dangerous when installed in an airplane.
Additionally, reworked or salvaged parts or those parts obtained
from non-PIPER approved sources, may have service histories
which are unknown or cannot be authenticated, may have been
subjected to unacceptable stresses or temperatures or may have
other hidden damage not discernible through routine visual or
nondestructive testing. This may render the part, component or
structural assembly, even though originally manufactured by
PIPER, unsuitable and unsafe for airplane use.
PIPER expressly disclaims any responsibility for malfunctions,
failures, damage or injury caused by use of non-PIPER
approved parts.

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)