Section 21.49

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

name and address of the transferee, and
the anticipated date of the transfer.
(c) For a type certificate transfer in
which the State of Design is changing,
a type certificate may only be transferred to or from a person subject to
the authority of another State of Design if the United States has an agreement with that State of Design for the
acceptance of the affected product for
export and import. Each transferor
must notify the FAA before such a
transfer in a form and manner acceptable to the FAA. This notification
must include the applicable type certificate number; the name, address, and
country of residence of the transferee;
and the anticipated date of the transfer.
(d) Before executing or terminating a
licensing agreement that makes a type
certificate available to another person,
the type certificate holder must notify
the FAA in writing. This notification
must include the type certificate number addressed by the licensing agreement, the name and address of the licensee, the extent of authority granted
the licensee, and the anticipated date
of the agreement.
[Doc. No. FAA-2006-25877, Amdt. 21-92, 74 FR
53386, Oct. 16, 2009; Doc. No. FAA-2018-0119,
Amdt. 21-101, 83 FR 9169, Mar. 5, 2018]

Section 21.49

Availability.

The holder of a type certificate must
make the certificate available for examination upon the request of the FAA
or the National Transportation Safety
Board.
[Doc. No. 5085, 29 FR 14564, Oct. 24, 1964, as
amended by Doc. No. 8084, 32 FR 5769, Apr. 11,
1967]

spaschal on DSK3GDR082PROD with CFR

Section 21.50 Instructions for continued airworthiness
and
manufacturer-s
maintenance manuals having airworthiness limitations sections.
(a) The holder of a type certificate
for a rotorcraft for which a Rotorcraft
Maintenance Manual containing an
 - Airworthiness Limitations -  section
has been issued under Section 27.1529 (a)(2) or
Section 29.1529 (a)(2) of this chapter, and who
obtains approval of changes to any replacement time, inspection interval, or
related procedure in that section of the
manual, must make those changes

available upon request to any operator
of the same type of rotorcraft.
(b) The holder of a design approval,
including either a type certificate or
supplemental type certificate for an
aircraft, aircraft engine, or propeller
for which application was made after
January 28, 1981, must furnish at least
one set of complete Instructions for
Continued Airworthiness to the owner
of each type aircraft, aircraft engine,
or propeller upon its delivery, or upon
issuance of the first standard airworthiness certificate for the affected
aircraft, whichever occurs later. The
Instructions for Continued Airworthiness must be prepared in accordance
with SectionSection 23.1529, 25.1529, 25.1729, 27.1529,
29.1529, 31.82, 33.4, 35.4, or part 26 of this
subchapter, or as specified in the applicable airworthiness criteria for special
classes of aircraft defined in Section 21.17(b),
as applicable. If the holder of a design
approval chooses to designate parts as
commercial, it must include in the Instructions for Continued Airworthiness
a list of commercial parts submitted in
accordance with the provisions of paragraph (c) of this section. Thereafter,
the holder of a design approval must
make those instructions available to
any other person required by this chapter to comply with any of the terms of
those
instructions.
In
addition,
changes to the Instructions for Continued Airworthiness shall be made available to any person required by this
chapter to comply with any of those instructions.
(c) To designate commercial parts,
the holder of a design approval, in a
manner acceptable to the FAA, must
submit:
(1) A Commercial Parts List;
(2) Data for each part on the List
showing that:
(i) The failure of the commercial
part, as installed in the product, would
not degrade the level of safety of the
product; and
(ii) The part is produced only under
the commercial part manufacturer-s
specification and marked only with the
commercial part manufacturer-s markings; and

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