Technical data

13773-001
4-00
Page 331 July 2001
C. Structural Limitations
The certification requirements of FAR 23.573 require that the composite airframe structure, cabin,
wing, empennage their carry thru, and attaching structure whose failure would be catastrophic must be
designed to damage tolerant criteria. Damage tolerant certification for the selected airframe life of
4350 flight hours has been established for all of the affected parts with no special structural limitations
or inspections.