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TWIN COMANCHE PA-39
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Piper Aircraft Corporation TWIN COMANCHE PA-39 Service Manual
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Contents
Table of Contents
Troubleshooting
Bookmarks
Table of Contents
Table of Contents
Engine Liming Marks
To 30-2000 Incl
Removal of Wheel Brake Disc
Brake System Installation
Brake Master Cylinder Assembly
Brake Cylinder Installation
Engine Cowling and Cowl Flap Rigging
Engine Installation
Schematic Diagram of RSA Fuel Injector System
Removing Spring from Lead Assembly
Contact Spring Inspection
Assembly Tool
Installing Grommet over Lead Assemblies
Removing Frozen Spark Plug
Lead Assembly Installed in Grommet
Wire Doubled over for Installation of Eyelet
Turbo Oil Flow Check
Checking Fuel Gauge
Fuel Strainer Assembly
Landing Gear Retraction System
Main Wheel Assembly . . Serial Nos
Landing Gear up Limit Switch
Engine Cowling and Cowl Flap Rigging
Standard Propeller Installation
Typical Nicks and Removal Methods
Propeller Installation
Propeller Governor
Engine Installation
Fuel Injector
Fuel Injector
Fuel Air Bleed Nozzle
Fuel Air Bleed Nozzle
Impulse Coupling
Assembly Tool
Using Assembly Tool
Measuring Lead Assembly Length
Measuring Wire from Top of Ferrule
Lead Assembly Installed in Grommet
Wire Doubled over for Installation of Eyelet
Magneto Breaker Points
Propeller Governor
Fuel System Schematic (PA-30)
Fuel System Installation
Fuel System Installation (Turbo)
Revised: 1011198 PREFACE
Troubleshooting
Heater Operation (Janitrol)
Heater Safety Limit Switch
13-6. Inspection of Heater and Heater Components
Southwindheater
Removal of Heater
Installation of Heater
Fuel Control Valve
Electrical System
Flame Detector Switch
Igniter
13-26. Service
External Cause
13-32. Electrical Check
Fuel Supply
Check-Out Procedure for an Inoperative Heate
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Table of Contents
2
Landing Gear Retraction System
3
Fuel System Schematic (Pa-30)
4
Heater Operation (Janitrol)
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Table of Contents
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Piper Twin Comanche Service Manual Section Xi11 Heating and Ventilating
691
Table of Contents
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Summary of Contents for Piper Aircraft Corporation TWIN COMANCHE PA-39
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