Structural Testing Of Homebuilt Aircraft
In
Will the seat of the aircraft to be when the wing loading is over, we will any case, the wing supporting fixture
proof tested elastically hold 880 lbs.? again inspect these parts to find out if should provide a sturdy support not
How many builders will allow the there have been some changes in just for the spar bending test but also
Technical Counselor to load the their appearance (hole elongations? for the following torsional test.
seat(s) with 880 Ibs. (each!)? Maybe a bolt/nut looseness?). Figure 2L shows Figure 4 shows, schematically,
call to the designer/plans vendor can a typical wooden spar central fitting how a fixture for a light aircraft could
clarify the matter. Maybe only the (please note the bolts are NOT situ- look. A square box made of house-
wing has been designed for n = 4
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