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ALBERT'S WEB SITE
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Date:  8-4-2009
Number of Hours:  1.00
Manual Reference:  None
Brief Description:  FIRST ENGINE RUN on aircraft

Ran engine with gas line from can to fuselage fitting. 93 oct.
Oil Pressure 42 lbs
Oil temp rising
Fuel pressure 4 lbs engine runnuing (3 lbs static)
CHT risine. (Both Cyls)
Alternator 14 Volts (12 volts static)
Idle speed 1100 rpm. Tach works on both ignition systems
Switching from #2 to #1 ignition O.K.
Switching from #2 to #1 Fuel pump-, no prssure..
Carb heat O.K.
Slight vibration in airframe. Quick check of prop pitch shows 1/2 degree out.

To Do,
Redo prop pitch to get 9 degrees both blades.
Correct #1 Fuel pump problem.
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