Piper PA-28-161 User Manual

Paragraph
No.
TABLE OF CONTENTS
SECTION 5
PERFORMANCE
Page
No.
5.1 General . . . . . . . . • . . • . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5·1
5.3 Introduction- Performance and Flight Planning....... 5-l
5.5 Flight Planning Example . . . . . • . . . . . . . . . . . . . . . . . . . . . 5·3
5. 7 Performance Graphs . • . . . . . . . . . . . • . • . . . . • . . . . . . . . . . 5-9
List
of Figures .•.•................•.. : . . . . . . . . . 5-9
REPORT: VB-1180
5-i

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)