STC ST04715NY

IMPORT ST04715NY Bombardier Aerospace 400 Cote-Vertu Road West Dorval, Quebec Canada H4S 1Y9 Part 25 Title 14 Code of Federal Regulations T00003NY Bombardier Inc.

BD-700-1A10

1. Installation of Occupancy of Aft Cabin Divans must be in accordance with B/E Aerospace Modification Data Summary M704000, Revision B, dated February 22, 2022 or later Transport Canada Civil Aviation (TCCA) approved revision.

2. Maintenance must be in accordance with Bombardier Instructions for Continued Airworthiness (ICA) BAS67057142, Revision B, dated October 19, 2021 or later TCCA accepted revision.

(See Description of Type Design Change on Page 3 of 3)

1. The installer must determine whether this design change is compatible with previously approved modifications.

(See Limitations and Conditions Continued on Page 3 of 3) January 13, 2021 March 23, 2022 Anthony E. Gallo Manager, International Validation Branch (AIR-730) Compliance & Airworthiness Division Aircraft Certification Service (AIR) 3

IMPORT ST04715NY ST04715NY 3

IMPORT ST04715NY Date of Issuance: March 23, 2022

Description of Type Design Change (continued)

3. Operation must be in accordance with B/E Aerospace Supplemental Airplane Flight Manual M704090, Revision B, TCCA approved February 22, 2022 or later TCCA approved revision.

2. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

3. This approval is limited to only the installation made in Bombardier Inc. Model BD-700-1A10 Serial No. 9014.

4. Complete custom aircraft interior installation certified under STC No. ST02997NY must be installed concurrently with the installation of this approval.

5. The "Limitations" section of B/E Aerospace Supplemental Airplane Flight Manual M704090, Revision B, TCCA approved February 22, 2022 or later TCCA approved revision is applicable as part of this installation.

6. This interior configuration has not been certified for ditching.

Certification Basis:

Based on 14 CFR § 21.115 and § 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48, the certification basis for this modification to the Bombardier Inc. Model BD-700-1A10 is as follows:

a. The type certification basis for the Bombardier Inc. Model BD-700-1A10 as shown on TCDS T00003NY for parts not changed or not affected by the change.

b. The type certification basis for the Bombardier Inc. Model BD-700-1A10 as shown on TCDS T00003NY for parts changed or affected by the change in addition to:

• Equivalent Level of Safety (ELOS) to the requirements of 14 CFR §§ 25.811(d)(1) and 25.811(d)(2) per TAD ELOS Memo ST6814NY-T-C-1 dated June 20, 2011.

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