Piper PA-28-180 User Manual

iv
INDEX (continued)
SECTION IV – EMERGENCY PROCEDURES
Page
Introduction
Engine Power Loss During Takeoff
Engine Power Loss In Flight
Power Off Landing
Fire
Loss of Oil Pressure
Loss of Fuel Pressure
High Oil Temperature
Alternator Failure
Engine Roughness
Spins
Open Door
27
27
28
29
30
31
31
32
32
32
33
34
SECTION V – PERFORMANCE CHARTS
Page
Altitude Conversion Chart
Takeoff Distance vs Density Altitude
Rate of Climb vs Density Altitude
Range vs Density Altitude
True Airspeed and RPM vs Density Altitude
Landing Distance vs Density Altitude
Power Setting Table
36
37
38
39
40
41
42
SECTION VI – GENERAL MAINTENANCE
Page
Landing Gear Service
Brake Service
Tire Inflation
Care of Windshield and Windows
Battery Service
Fuel Requirements
Oil Requirements
Fuel System
Care of Air Filter
Leveling and Rigging
Serial Number Plate
44
45
45
46
46
46
47
48
49
49
50

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