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FAR 23 Simplified Load Criteria

FAR 23 Simplified Load Criteria

FAR 23 Simplified Load Criteria

(OP)
Hi:
I looking for help in this matter:

In my horizontal tail load calculation I have decided to use Appendix "A" chapter A23:11
 
c)Surface loading conditions. Each surface loading condition must be investigated as follows:

(1) Simplified limit surface loadings for the horizontal tail, vertical tail, aileron, wing flaps, and trim tabs are specified in figures 5 and 6 of this appendix.

The question is : The "Average Surface Loading" obtained via fig. A5 is all I need? or I must add to the Balancing Loads.

Best regards.  
 

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