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REFLECTOR: Horizontal cut on the engine cowl
I have the same question as Carl Hoffman as to where the horizontal cut
line "falls" onto the engine cowl. Can anyone else with a std
wing/original fuselage plane tell us where the trailing edge of the wing
lines up with respect to the aft section of the engine cowl???
Mine is right at the original flange "cut off" on the lower half cowl.
How can you test a circuit breaker and check that it trips at the proper
amperage? What is the typical tollerance?