Piper PA-28-161 Maintenance Manual

PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 2
Nov 30/06
1B2
INDEX
Electrical (continued)
Schematics (continued)
Fresh Air Blower: 5H7
Fuel Flow: 5J16
Fuel Pressure: 5J17
Fuel Primer: 5H23
Fuel Pump: 5H14, 5H23
Fuel Quantity: 5I1, 5J5, 5J15
GMA 340: 5H11
Grounds: 5H15
Landing Light: 5H14
Lift Detector: 5H21
Lights
Annunciator Lights: 5I8
Flood Lights: 5I15, 5I17
Landing Lights: 5J3, 5J5
Navigation Lights: 5J1, 5J5
Overhead Lights: 5I11
Panel Lights: 5I19
Radio Lights: 5I18
Recognition Lights: 5J4
Strobe Lights: 5J1
Switch Lights: 5I21
Low Voltage Monitor: 5H13, 5I4
Mag/OAT: 5J7
Magnetos: 5H14
Multi-Function Display
(MFD): 5J11
Oil Pressure: 5J16, 5J17
Oil Temperature: 5J15, 5J17
Passenger Interphone: 5H11
Pitot Heat: 5I3
Primary Flight Display (PFD):
5J10
Radio Master Switch: 5H9
Stall Warning: 5H21, 5I11
Standby Alternator: 5H17
Standby Attitude Indicator:
5J12
Starter: 5H14, 5I22, 5J19
Tachometer: 5J15
Terminal Blocks: 5H15
Turn and Bank Indicator: 5J9
Standby Alternator: 2E5
Troubleshooting: 2E6
Static Discharging
Bonding Straps: 2D7
Static Wicks: 2D7
Symbols: 5H2
Voltage Regulator: 2E20
Testing: 2E20
Voltage Regulator Check: 2E20
Wire Coding: 5H1
Electrical Bonding: 4D11
Resistance Index: 4D12
Electrical System
Servicing: 1I10
Electronic Flight Instrument
System - See EFIS
ELT: 2F17
Artex ELT 110-4: 2F17
Battery: 2F17
Testing: 2F18
Wiring Schematic: 2F19
Empennage
Installation: 4E24
Repair: 4E23
Engine
Controls
Adjustment: 4K13
Mixture: 4K12
Throttle: 4K12
EGT Probe Installation: 5E3
Exhaust - See Exhaust System
Fuel
Carburetor: 4K11
Idle Mixture: 4K11
Idle Speed: 4K12
Primer: 4K7
Hour Meter: 5I5
Installation: 4J12
Instruments
EGT Gauge: 5E1
Troubleshooting: 5E1
Oil Pressure: 5F1
Oil Temperature: 5F3
Calibration: 5F4
Troubleshooting: 5F3
Tachometer: 5D23
Troubleshooting: 5D23
Lubrication
Changing Oil: 1H23
Chart: 1I22
Oil Filter: 1H24
Oil Screen: 1H23
Oil Sump: 1H23
Mount: 4J17
Corrosion Inspection: 4J18
Oil Cooler: 5E23
Primer: 4K7
Removal: 4J11
Serial Number Location: 1E17
Engine (continued)
Starter: 5F13
Bench Tests: 5F16
Cranking Tests: 5F16
Service Test Specifications:
5F17
Troubleshooting: 5F14
Using External Power: 5F18
Static RPM Test: 4J5
Timing Marks: 5C9
Troubleshooting: 4I23
Exhaust System
100 Hour Inspection: 5E13
Inspection Points: 5E14
F
Fiberglass Repair - See Repairs -
Fiberglass
Flaps
Control System
Installation: 2I21
Rigging and Adjustment: 2I22
Troubleshooting: 2I19
Installation: 4H12
Torque Tube/Push Rod
Inspection: 2I24
Flareless Tube Assemblies: 1J15
Flight Controls
Ailerons - See Aileron
Cable Tension: 2G10
Control Cable Inspection: 2G12
Description and Operation: 2G7
Flaps - See Flaps
Lubrication Chart: 1I20
Rudder - See Rudder
Stabilator - See Stabilator
Standard Practices &
Procedures: 2G8
Surface Travel: 2G10
Fluid Line Identification: 1J12
Fuel System: 2J12
Draining
Entirely: 1H23
Moisture: 1H22
Electric Fuel Pump: 2K3
Testing: 2K4
Engine Primer: 4K7
Filling: 1H22
Fuel Pressure Gauge: 4K17
Calibration: 4K18
Troubleshooting: 4K17
Fuel Quantity Indication
Calibration: 2K12

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)