Piper PA-28-161 User Manual

APPLICABILITY
Application of this handbook is limited to the specific Piper PA-28-161
model airplane designated by serial number and registration number on the face
of the title page of this handbook.
This handbook cannot be used for operational purposes unless kept in a
current status.
WARNING
INSPECTION, MAINTENANCE AND PARTS REQUIREMENTS
FOR ALL NON-PIPER APPROVED STC INSTALLATIONS ARE
NOT INCLUDED IN THIS HANDBOOK. WHEN A NON-PIPER
APPROVED STC INSTALLATION IS INCORPORATED ON THE
AIRPLANE, THOSE PORTIONS OF THE AIRPLANE AFFECTED
BY THE INSTALLATION MUST BE INSPECTED IN
ACCORDANCE WITH THE INSPECTION PROGRAM
PUBLISHED BY THE OWNER OF THE STC. SINCE NON-PIPER
APPROVED STC INSTALLATIONS MAY CHANGE SYSTEMS
INTERFACE, OPERATING CHARACTERISTICS AND
COMPONENT LOADS OR STRESSES ON ADJACENT
STRUCTURES, PIPER PROVIDED INSPECTION CRITERIA MAY
NOT BE VALID FOR AIRPLANES WITH NON-PIPER APPROVED
STC INSTALLATIONS.
APPLICABILITY
Application of this handbook is limited to the specific Piper PA-28-161
model airplane designated by serial number and registration number on the face
of the title page of this handbook.
This handbook cannot be used for operational purposes unless kept in a
current status.
WARNING
INSPECTION, MAINTENANCE AND PARTS REQUIREMENTS
FOR ALL NON-PIPER APPROVED STC INSTALLATIONS ARE
NOT INCLUDED IN THIS HANDBOOK. WHEN A NON-PIPER
APPROVED STC INSTALLATION IS INCORPORATED ON THE
AIRPLANE, THOSE PORTIONS OF THE AIRPLANE AFFECTED
BY THE INSTALLATION MUST BE INSPECTED IN
ACCORDANCE WITH THE INSPECTION PROGRAM
PUBLISHED BY THE OWNER OF THE STC. SINCE NON-PIPER
APPROVED STC INSTALLATIONS MAY CHANGE SYSTEMS
INTERFACE, OPERATING CHARACTERISTICS AND
COMPONENT LOADS OR STRESSES ON ADJACENT
STRUCTURES, PIPER PROVIDED INSPECTION CRITERIA MAY
NOT BE VALID FOR AIRPLANES WITH NON-PIPER APPROVED
STC INSTALLATIONS.
REPORT: VB-1180
REVISED: MARCH 1, 2005 iii
REPORT: VB-1180
REVISED: MARCH 1, 2005 iii

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)