STC ST04433AT

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder.

FAA Form 8110-2 (5/14) Page 1 of 3

Number: ST04433AT This certificate issued to: Chippewa Aerospace, Inc.

490 Allied Dr.

Conway, SC 29526

Part 25of the Federal Aviation Regulations.

Original Product – Type Certificate Number: A21EA Make: Bombardier Model: CL600-2C10, -2D15, -2D24 Series Description of Type Design:

Installation of Passenger In-Seat Power System in the Bombardier CL600-2C10, CL600-2D15, CL600- 2D24 Series Aircraft in accordance with Chippewa Aerospace Master Drawing List (MDL) No. 601-2454- 01-0001, Rev. 1, Dated August 23, 2018, or later FAA approved revision.

Limitations and Conditions: FAA Approved Airplane Flight Manual Supplement (AFMS) to the Model Bombardier CL600-2C10, CL600-2D15, CL600-2D24 Series Aircraft for the Installation of the Passenger In-Seat Power System in accordance with Chippewa Aerospace Airplane Flight Manual Supplement (AFMS) No. 601-2454-01-1012, Rev. IR, Dated October 04, 2018, or later FAA approved revision, is a required part of this STC. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. (Limitations and Conditions continued on page 3 of 3.)

Date of Application: December 22, 2014 Date Reissued:

Date of Issuance: October 09, 2018 Date Amended:

Signature Title (for) Christina Underwood Manager, Atlanta ACO Branch

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does n ot constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder.

FAA Form 8110-2 (5/14) Page 2 of 3

Transfer the ownership of Supplemental Type Certificate Number: ST04433AT

To (Name and address of transferee)

From (Name and address of grantor)

Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does n ot constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder.

FAA Form 8110-2 (5/14) Page 3 of 3

Number: ST04433AT Instructions for Continued Airworthiness (ICA), Chippewa Aerospace Inc.

Document No. 601-2454-01-0002, Rev. 1, Dated August 23, 2018, or later FAA approved revision, must be made available to the operator at the time of installation.

Certification Basis:

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 the Bombardier CL600-2C10, -2D15, -2D24 Series aircraft is as follows:

a. The type certification basis for Bombardier CL600-2C10, -2D15, -2D24 airplane is shown on TCDS A21EA for parts not changed or not affected by the change.

b. The certification basis for parts changed or affected by the change since the reference date of application, December 22, 2014, is based upon part 25 as amended by Amendment 25-140. 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 25-0 through 25-140 §§ 25.23 §§ 25.301 §§ 25.303 §§ 25.305 §§ 25.307 §§ 25.365 §§ 25.561 §§ 25.562 §§ 25.601 §§ 25.603 §§ 25.605 §§ 25.609 §§ 25.613 §§ 25.625 §§ 25.785 §§ 25.789 §§ 25.791 §§ 25.803 §§ 25.813 §§ 25.815 §§ 25.853 §§ 25.869 §§ 25.899 §§ 25.1301 §§ 25.1307 §§ 25.1309 §§ 25.1316 §§ 25.1317 §§ 25.1353 §§ 25.1357 §§ 25.1431 §§ 25.1525 §§ 25.1529 §§ 25.1541 §§ 25.1581 §§ 25.1583 §§ 25.1585 §§ 25.1587

Regulations at the amendment level in TCDS A21EA §§ 25.571 §§ 25.611

14 CFR Part 26 Regulations Based on 14 CFR §21.101 (g), applicable provisions of 14 CFR Part 26 are included in the certification basis. For a future 14 CFR Part 26 amendments, the holder of this STC must demonstrate compliance with the applicable sections. As of issuance date of this STC, compliance has been found for the following regulations: 14 CFR § 26.11 and 14 CFR § 26.47.

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