spaschal on DSK3GDR082PROD with CFR

Section 26.21

14 CFR Ch. I (1-1-19 Edition)

of the full-scale fatigue testing and
demonstrating that widespread fatigue
damage will not occur in the airplane
structure.
(5) Holders of either supplemental
type certificates (STCs) or amendments to TCs that increase maximum
takeoff gross weights from 75,000
pounds or less to greater than 75,000
pounds: No later than July 14, 2012.
(6) Applicants for either STCs or
amendments to TCs that increase maximum takeoff gross weights from 75,000
pounds or less to greater than 75,000
pounds: No later than the latest of the
following dates:
(i) July 14, 2012;
(ii) The date the certificate is issued;
or
(iii) The date specified in the plan approved under Section 25.571(b) for completion
of the full-scale fatigue testing and
demonstrating that widespread fatigue
damage will not occur in the airplane
structure.
(7) Applicants for either STCs or
amendments to TCs that decrease maximum takeoff gross weights from
greater than 75,000 pounds to 75,000
pounds or less, if the date of application was after January 14, 2011: No
later than the latest of the following
dates:
(i) July 14, 2012;
(ii) The date the certificate is issued;
or
(iii) The date specified in the plan approved under Section 25.571(b) for completion
of the full-scale fatigue testing and
demonstrating that widespread fatigue
damage will not occur in the airplane
structure.
(d) Compliance plan. Each person
identified in paragraph (e) of this section must submit a compliance plan
consisting of the following:
(1) A proposed project schedule, identifying all major milestones, for meeting the compliance dates specified in
paragraph (c) of this section.
(2) A proposed means of compliance
with paragraphs (b)(1) through (b)(4) of
this section.
(3) A proposal for submitting a draft
of all compliance items required by
paragraph (b) of this section for review
by the responsible Aircraft Certification Service office not less than 60
days before the compliance date speci-

fied in paragraph (c) of this section, as
applicable.
(4) A proposal for how the LOV will
be distributed.
(e) Compliance dates for compliance
plans. The following persons must submit the compliance plan described in
paragraph (d) of this section to the responsible Aircraft Certification Service
office by the specified date.
(1) Holders of type certificates: No
later than April 14, 2011.
(2) Applicants for TCs and amendments to TCs, with the exception of
amendments to TCs specified in paragraphs (e)(4), (e)(5), or (e)(6) of this section, if the date of application was before January 14, 2011 but the TC or TC
amendment was not issued before January 14, 2011: No later than April 14,
2011.
(3) Holders of either supplemental
type certificates or amendments to TCs
that increase maximum takeoff gross
weights from 75,000 pounds or less to
greater than 75,000 pounds: No later
than April 14, 2011.
(4) Applicants for either STCs or
amendments to TCs that increase maximum takeoff gross weights from 75,000
pounds or less to greater than 75,000
pounds, if the date of application was
before January 14, 2011: No later than
April 14, 2011.
(5) Applicants for either STCs or
amendments to TCs that increase maximum takeoff gross weights from 75,000
pounds or less to greater than 75,000
pounds, if the date of application is on
or after January 14, 2011: Within 90
days after the date of application.
(6) Applicants for either STCs or
amendments to TCs that decrease maximum takeoff gross weights from
greater than 75,000 pounds to 75,000
pounds or less, if the date of application is on or after January 14, 2011:
Within 90 days after the date of application.
(f) Compliance plan implementation.
Each affected person must implement
the compliance plan as approved in
compliance with paragraph (d) of this
section.
(g) Exceptions. This section does not
apply to the following airplane models:
(1) Bombardier BD-700.
(2) Bombardier CL-44.
(3) Gulfstream GV.

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