CS 26.307(a)(iii) and (c) Damage tolerance data for existing
changes to the FCS
Compliance
with the fatigue and damage tolerance evaluation required by point 26.307
(a)(iii) and (c)
of Part-26 is demonstrated by complying with CS 25.571 Amendment 19 or
subsequent amendment, or with the following:
(a) The fatigue and damage tolerance
evaluation is in accordance with the damage tolerance requirements of the applicable certification
basis, except as provided in point (b) of this CS.
(b) For aeroplanes certified on the basis of
JAR-25 Change 6 or 14 CFR §25.571 Amendment 44 or equivalent, or earlier
amendments, the fatigue and damage tolerance evaluation of the change is in
accordance with JAR-25 Change 7 or 14 CFR §25.571 Amendment 45, or equivalent,
or later amendments, except that residual strength loads may be based upon the
fail-safe load cases of the original certification basis.
[Issue: 26/3]
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