CS 26.301 Compliance plan for (R)TC holders and applicants
Compliance
with point 26.301 of Part-26 is demonstrated when a compliance
plan exists that includes the following:
(a) a project schedule identifying all the major milestones for meeting the compliance dates as specified in points 26.302 to 26.309 of Part-26, as applicable;
(b) a proposed means of compliance with the applicable requirements as specified in points 26.302 to 26.309 of Part-26, including as appropriate, methods and procedures for:
(1) performing the damage tolerance evaluation
(DTE) of baseline structure, modified structure and published repairs;
(2) identifying the aeroplane structural
configuration to be evaluated;
(3) identifying widespread fatigue damage
(WFD)-susceptible structure;
(4) identifying the source of engineering data
that will be used to perform the required evaluations;
(5) performing the WFD evaluation of
structure;
(6) establishing a limit of validity (LOV) and
plans for distribution upon approval (including incorporation of the LOV into
the (airworthiness limitation section) ALS);
(7) identifying and developing the maintenance
actions required to support the LOV;
(8) developing a baseline corrosion prevention
and control programme (CPCP);
(9) establishing a process to ensure the
continuing structural integrity programme remains valid;
(10) establishing the list of fatigue-critical
baseline structures (FCBSs);
(11) developing the repair evaluation guidelines
(REGs);
(c) a plan for submitting a draft of all the
required compliance items for review by EASA not less than 60 days before the
applicable compliance date.
[Issue:
26/3]
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