624
14 CFR Ch. I (1–1–14 Edition)
§ 26.21
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 max-
imum takeoff gross weights from
greater than 75,000 pounds to 75,000
pounds or less, if the date of applica-
tion 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 ap-
proved under § 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 sec-
tion must submit a compliance plan
consisting of the following:
(1) A proposed project schedule, iden-
tifying all major milestones, for meet-
ing 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 FAA Oversight Office not less
than 60 days before the compliance
date specified 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 sub-
mit the compliance plan described in
paragraph (d) of this section to the
FAA Oversight Office by the specified
date.
(1) Holders of type certificates: No
later than April 14, 2011.
(2) Applicants for TCs and amend-
ments to TCs, with the exception of
amendments to TCs specified in para-
graphs (e)(4), (e)(5), or (e)(6) of this sec-
tion, if the date of application was be-
fore January 14, 2011 but the TC or TC
amendment was not issued before Jan-
uary 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 max-
imum 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 max-
imum 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 max-
imum takeoff gross weights from
greater than 75,000 pounds to 75,000
pounds or less, if the date of applica-
tion is on or after January 14, 2011:
Within 90 days after the date of appli-
cation.
(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.
(4) Gulfstream GV–SP.
(5) British Aerospace, Aircraft Group,
and Societe Nationale Industrielle
Aerospatiale Concorde Type 1.
(6) British Aerospace (Commercial
Aircraft) Ltd., Armstrong Whitworth
Argosy A.W. 650 Series 101.
(7) British Aerospace Airbus, Ltd.,
BAC 1–11.
(8) BAE Systems (Operations) Ltd.,
BAe 146.
(9) BAE Systems (Operations) Ltd.,
Avro 146.
(10) Lockheed 300–50A01 (USAF
C141A).
(11) Boeing 707.
(12) Boeing 720.
(13) deHavilland D.H. 106 Comet 4C.
(14) Ilyushin Aviation IL–96T.
(15) Bristol Aircraft Britannia 305.
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