STC ST06297LA

National Aircraft Interior (NAI) National Limited trading as Generation Global 90 St. Vincent Street Nelson 7010 New Zealand 25*

(*see Page 3)

A21EA Bombardier Inc.

CL-600-2D24 (Regional Jet Series 900) Installation of Passenger Seat Assembly Headrest Dress Covers in accordance with Master Data List MDL 011118, Revision 1, dated 01 February 2019, or later FAA approved revision.

This approval should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previous approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. The approval of this modification applies to the above noted aircraft models only. A copy of this STC must be included in the permanent records of the modified aircraft. If the holder agrees to permit another person to use this certifi cate to alter the product, the holder shall give the other person written evidence of that permission.

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February 13, 2019 May 08, 2019

(Signature) Aviation Safety Manager, Los Angeles ACO Branch (Title)

Transfer the ownership of Supplemental Type Certificate Number

to (Name of transferee)

(Address of transferee) (Number and street)

(City, State, and ZIP Code)

from (Name of grantor) (Print or type)

(Address of grantor) (Number and street)

(City, State, and ZIP Code)

Signature of grantor (In ink):

U.S. GPO 1987-763-289

ST02697LA

Instructions for Continued Air worthiness, ICA 011118, Revision 0, dated 19 December 2018 , or later FAA approved revisions, must be made available to the operator for incorporation into the operator’s maint enance program.

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for modifications and installations to Bombardier Inc. CL-600-2D24 airplanes modified by this change is as follows:

a. The type certification basis is shown in TCDS A21EA Revision 45 for parts not changed or not affected by the change.

b. The certification basis for parts changed or affected by this change as the reference date of application, 13 February 2019 is based 14 CFR part 25 as amended by Amendment 25-145 as stated by the applicant.

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be:

Regulations at the latest amendment 25-1 through 25-145

25.29, 25.301, 25.303, 25.305, 25.307, 25.561(a), (b), (d), 25.562, 25.601, 25.603, 25.608, 25.785,

25.853(a), (c), 25.1529

Regulations at an intermediate amendment None.

Regulations at the amendment level in TCDS A21EA Revision 45 None

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