Piper Warrior III - INDEX

PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 1
Nov 30/06
1B1
INDEX
3-IN-1 Engine Instrument
Calibration: 4K18
A
Access Plates and Panels: 1E22
Accident/Incident Reporting: 1A12
Aerofiche Grid Code: 1A11
Aileron
Control System
Bellcrank: 2H10
Rigging: 2H13
Control Column
Assembly: 2H3
Rigging and Adjustment: 2H11
Troubleshooting: 2H2
Control Wheel: 2H7
Ailerons
Balancing: 4H13
Installation: 4H12
Air Filter
Servicing: 1I8
Airspeed Indicator: 3G14
Airworthiness
Directives (AD’s): 1C15
Instructions: 1A9
Limitations: 1C7
Altimeter: 3G12
Annunciator: 3D1
Description and Function: 3D1
Attitude Indicator (ADI): 3H1
Avionics - See also Instruments
Cooling Blower: 3K6
Instrument Panel: 3J18
B
Battery - See Electrical
Bearings
Installing Rod End Bearings:
1J10
Brakes
Adjustment: 3E15
Conditioning: 3E15
Hand/Parking Brake Master
Cylinder: 3E18
Lining Tolerances: 3E15
Parking Brake: 1G11
System
Draining: 1I4
Filling: 1I4
System Installation: 3E19
Toe Brake Cylinder: 3E21
Wheel Brakes: 3E16
Repair: 3E15
Buttock Lines: 1E21
C
Cabin
Heat: 2C15
Ventilation: 2C9
Cable Tension vs. Ambient Temp.:
2G9
Carburetor: 4K11
Heat: 3C7
Ice Detection System: 4J21
Functional Check: 4J21
Testing: 4J23
Chapter/Section Index Guide:
1A17
Circuit Breaker Panel: 3J19
COM/NAV/GPS
GNS-430: 3I1
Configuration: 3I2
Post Installation Setup: 3I1
Maintenance: 3I1
Consumable Materials: 5G15
Control Cable Inspection: 2G12
Cable Fittings 100 Hour Special
Inspection: 2G15
Control Column Assembly: 2H3
Conversion Tables
Decimal Conversions: 5G9
Drill Sizes: 5G13
Metric (in. to mil): 5G12
Temperature Conversion: 5G10
Torque: 5G7
Weights and Measures: 5G11
Corrosion
Control: 4C11
Removal: 4C13
Types: 4C12
D
Decals: 1G21
Definitions - Important Terms:
1C19
Dimensions - Principal: 1E18
Dimmer Control Modules: 3J18
Directional Gyro: 3H11
Doors
Baggage: 4E3
Tool: 4E4
Cabin: 4D21
Lubrication Chart: 1I23
Snubber Seals: 4D22
Installation: 4D23
E
EFIS
Avidyne Entegra: 3H3
Component Locator: 3H4
Mag/OAT Sensor: 3G15
Maintenance
DAU - Data Acquisition
Unit: 3H7
MFD - Multifunction
Display: 3H5
PFD - Primary Flight
Display: 3H5
Wiring Harness Installation:
3H10
Electrical
Alternator: 2D18
Belt Tension: 2E4
Service Precautions: 2D17
Test: 2E3
Troubleshooting: 2D21
Battery: 2E12
Charging: 2E15
Hydrometer reading: 2E17
Troubleshooting: 2E14
Components
Equipment Listing: 3J23
Locator Illustration: 3J24
Electrical System
Description and Operation:
2D15
Load Distribution: 2F3
Troubleshooting: 2D15
External Power: 2F1
Overvoltage Relay Check: 2E21
Schematics
Alternator Power: 5H13
Ammeter: 5H13, 5H14, 5J15
Annunciator: 5I7
Antenna Coupler: 5J11
Auxiliary Vacuum Pump: 3J4
Avionics Master Switch: 5H9,
5I4
Battery Switch: 5H19
Clock: 5I5
Data Acquisition Unit (DAU):
5I11, 5J15
Emergency Locator
Transmitter (ELT): 5I11
Engine Gauge, 3-IN-1: 5J17
Engine Hour Meter: 5I5
Exhaust Gas Temperature:
5J15
External Power: 5H19, 5I17