CS 26.302 Fatigue and damage tolerance evaluation
Compliance
with point 26.302 of Part-26 is demonstrated by complying with
CS 25.571 Amendment 19, or subsequent amendment, or with points (a) or (b) of
this CS:
(a) For aeroplane structures certified on the
basis of JAR 25.571 Change 6 or 14 CFR §25.571 Amendment 44 or equivalent, or
earlier amendments, a fatigue and damage tolerance evaluation according to JAR
25.571 Change 7 or 14 CFR §25.571 Amendment 45 or equivalent, or later amendment, exists, except that
residual strength loads may be based upon the fail-safe load cases of the
original certification basis. In addition, the inspection and other procedures
resulting from this evaluation:
(1) are contained in an existing ALS; or
(2) are contained in a supplemental structural
inspection document (SSID) mandated by an airworthiness directive (AD).
In both
cases, the documentation includes the time in flight cycles, flight hours or
another relevant measure by which the actions within the ALS/SSID are
implemented.
(b) For aeroplane structures certified on the
basis of JAR 25.571 Change 7 or 14 CFR §25.571 Amendment 45 or equivalent, or later
amendments: the inspections or other procedures resulting from the DTE
required by that certification basis are included in the ALS.
[Issue:
26/3]
Loading collections...