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Old 11-29-2006, 09:22 PM
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garnt.piper garnt.piper is offline
 
Join Date: Mar 2005
Location: Australia
Posts: 152
Default Rolling G

Conventional wisdom, which comes from FAR Pt23 I believe, is 2/3 maximum symmetrical g with full aileron deflection at Va.

re. earlier discussion, I have a finite element analysis of my G-200 wing which shows the highest stresses at about 40% span.
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Grant Piper
SAAA #727 (TC)
RV-4 VH-PIO ~600hrs
G-200 VH-OVR ~250hrs
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