STC ST04516NY

FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___

Part of .

IMPORT ST04516NY B/E Aerospace Limited 25 Dunlop Avenue Winnipeg, Manitoba Canada R2X 2V2 25 the Federal Aviation Regulations A21EA-1 Bombardier Inc.

CL-600-2B19 S/N 8080

1. Installation of Complete Custom Aircraft Interior must be accomplished in accordance with B/E Aerospace Limited Modifcation Data Summary G116000 Revision K, dated July 10, 2020, or later TCCA approved revisions.

2. Savannah Air Center, Inc. Airplane Flight Manual Supplement G116090 Revision C, dated June 25,2020, or later TCCA approved revisions, is required as part of this modification.

3. The aircraft is to be maintained in accordance with the Instructions for Continued Airworthiness, Document Number G116075 Revision A, dated June 17, 2013, or later TCCA accepted revisions.

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) 03/12/2020 07/14/2020 Timothy J. Hadsall Acting Manager, New York ACO Branch Compliance and Airworthiness Division Aircraft Certification Service 3

FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___

IMPORT ST04516NY 3

IMPORT ST04516NY Date of Issuance: July 14, 2020

2. This approval is limited to only the installation made in Bombardier Inc. Model CL-600-2B19 S/N 8080. This STC does not permit manufacturing of parts for multiple installations.

3. The "Limitations" section of Savannah Air Center, Inc. Airplane Flight Manual Supplement G116090 Revision C, dated June 25, 2020, or later TCCA approved revisions, is applicable as part of this modification.

4. Mandatory replacement times and/or inspection intervals are defined in the "Airworthiness Limitations" section of the Instructions for Continued Airworthiness, Document Number G116075 Revision A, dated June 17, 2013, or later TCCA accepted revisions.

Certification Basis:

Based on title 14 CFR 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Bombardier Inc. Model CL-600-2B19 S/N 8080 is as follows:

a. The type certification basis for the Bombardier Inc. Model CL-600-2B19 S/N 8080 is as shown on TCDS A21EA-1 for parts not changed or not affected by the change.

b. The type certification basis for the Bombardier Inc. Model CL-600-2B19 S/N 8080 is as shown on TCDS A21EA-1 for parts changed or affected by the change with the following additional requirements:

i. Exemption No. 10422A, dated January 19, 2016, has been granted for 14 CFR

25.813(e), Amendment 25-46.

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