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goes above 400 foot-pounds, annunciator light must extinguish.
(2.) To check auto ignition system,move condition lever past idle detent. With ignition switch in AUTO, ensure amber annunciator light is illuminated.
Switch
(Pressure)
Governor

Auto Ignition Installation 
Figure401 
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PIPER AIRCRAFT
PA-42-720(AdvancedTrainer)

MAINTENANCEMANUAL

Air
A. General
Three separate bleed air systems are provided:
Onesystem provides air for bearing compartment sealing.
A second system providescooling air.
The third system provides air for the compressor bleed valve and airframe services.

Refer to Pratt and Whitney Maintenance Manual, p/n 3034342, Chapter 75 for information on the air system.
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PA-42-720 (Advanced Trainer)
MAINTENANCE MANUAL

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CHAPTER 76 -ENGINECONTROLS
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Engine Controls 1 Descriptionand Operation 1
76-10-00

Power Lever Control Cable 1 Storageand Handling 1 Removal of Power Lever Control Cable 3 Installation of Power Lever Control Cable 4 Engine Control AdjustmentsPrior To First Run 8 Rigging of Rear Linkage, Fuel Control Unit, and Propeller Control Cam Assembly 8 PowerLevel Control Installation 15 Front End Rigging 15 Condition (Start Control) Lever Rigging 16 Propeller Control Rigging 17 EngineRun Adjustments 20 Preparing For Initial Start and Run 20 First Engine Run 21 Engine Running Adjustments 25 Dry Engine Motoring Run 34 Wet Engine Motoring Run 34 Engine Performance Check 36 Engine Data Plate Speed Check 36 Feather Stop Adjustment 36 General 36 External Feather Stop Adjustment 36
EFFECTIVITY:
040-999
CONTENTSan 10/90
PIPER AIRCRAFT
PA-42-720 (Advanced Trainer)
MAINTENANCE MANUAL
　
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