STC ST04492NY

FAA Form 8110-2 (4/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___

Part of .

IMPORT ST04492NY Flying Colours Corporation 901 Airport Road Peterborough, Ontario, Canada K9J 6X6 25 the Federal Aviation Regulations.

A21EA-1 Bombardier Inc.

CL-600-2B19 S/N 8110

1. Installation of Complete Custom Aircraft Interior must be accomplished in accordance with ACS-NAI Ltd. Modification Data Summary H708000 Revision H, dated May 8, 2020 or later TCCA approved revisions.

2. Flying Colours Corporation Airplane Flight Manual Supplement H188091, Revision A, dated May 7, 2020, or later TCCA approved revisions, is required as part of this installation.

3. The aircraft is to be maintained in accordance with the Instructions for Continued Airworthiness, Document Number, H708075, Revision C, dated September 9, 2014, 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) December 3, 2019 June 8, 2020 Anthony E. Gallo, Acting Manager New York ACO Branch Compliance and Airworthiness Division 3

FAA Form 8110-2 (4/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___

IMPORT ST04492NY ST04492NY 3

FAA Form 8110-2 (4/20) Page ___ of ___

IMPORT ST04492NY Date of Issuance: June 8, 2020

2. You cannot use descriptive data about this design change to duplicate other products. This approval is limited to only the installation made in Bombardier Inc. Model CL-600-2B19 S/N 8110. This STC does not permit manufacturing of parts for multiple installations.

3. The "Limitations" section of Flying Colours Corporation Airplane Flight Manual Supplement H188091, Revision A, dated May 7, 2020, or later TCCA approved revisions, is applicable as part of this installation.

4. Mandatory replacement times and/or inspection intervals are defined in the "Airworthiness Limitations" section of the Instructions for Continued Airworthiness, Document Number, H708075, Revision C, dated September 9, 2014, 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 8110 is as follows:

a. The type certification basis for the Bombardier Inc. Model CL-600-2B19 S/N 8110 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 8110 is as shown on TCDS A21EA-1 for parts changed or affected by the change with the following additional requirements:

i. Exemption No. 17321, dated April 4, 2017, has been granted for 14 CFR 25.813(e), Amendment 25-46.

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