Piper PA-28-180 User Manual

iii
INDEX
SECTION I – SPECIFICATIONS
Page
Performance
Weights
Power Plant
Fuel and Oil
Baggage
Dimensions
Landing Gear
1
2
2
2
2
3
3
SECTION II – DESIGN INFORMATION
Page
Engine and Propeller
Structures
Landing Gear
Control Systems
Fuel System
Electrical System
Heating and Ventilating System
Cabin Features
6
6
7
7
8
10
11
13
SECTION III – OPERATING INSTRUCTIONS
Page
Preflight
Starting Engine
Warm-Up
Ground Check
Take-Off
Climb
Stalls
Cruising
Approach and Landing
Stopping Engine
Engine Power Loss
Ground Handling and Mooring
Weight and Balance
Operating Tips
16
17
18
18
19
20
20
20
21
22
23
23
23
23

Piper PA-28-180 Specifications

General

Manufacturer	Piper Aircraft
Model	PA-28-180
Engine	Lycoming O-360-A4A
Horsepower	180 hp
Seating Capacity	4
Wingspan	30 ft (9.1 m)
Height	7 ft 3 in
Service Ceiling	14, 300 ft
Maximum Takeoff Weight	2, 400 lbs
Fuel Capacity	50 US gal (190 L)
Rate of Climb	720 ft/min
Cruise Speed	140 mph