Advisory Circular (AC) No. 500-009 Issue 1 - Appendix A

Figure 1 - Proof of Composite Structures - Static Strength (6)
(Ref: FAA AC20-107A)

Figure 2 - Proof of Composite Structures - Damage Tolerance

Note:
See FAA AC 20-107A paragraph 7.2.(5) for Discrete - Source Damage Tolerance Requirements