STC SA04221CH

SA04221CH Skandia, Inc.

5000 North Highway 251 Davis Junction, IL 61020 Part 23 the Federal Aviation complete certification basis A24CE Textron Aviation, Inc.

1) FAA Accepted Instructions for Continued Airworthiness, Manual 7806034ICA001, Revision B, dated July 10, 2015, or later FAA accepted revision is required for this modification.

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

(Continued on page 3) 6/27/2014 7/21/2026 6/5/2017 for Jason S. Deutschman Acting Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 3 Installation of Thermal Acoustic Kit in accordance with Skandia, Inc. Master Data List Document Number 7806034MDL001, Revision B, dated May 9, 2017, or later FAA approved revision.

Regulations. See Page 3 for A100-1, 200, 200C, 200CT, 200T, A200, A200C, A200CT, B200, B200C, B200CT, B200GT, B200CGT, B200T, 300, 300LW, B300, B300C

SA04221CH 07/21/26 3

SA04221CH 07/21/26 Limitations and Conditions (continued):

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

Certification Basis:

The certification basis for the changed A100-1, 200, 200C, 200CT, 200T, A200, A200C, A200CT, B200, B200C, B200CT, B200GT, B200CGT, B200T, 300, 300LW, B300, and B300C aircraft as described in this certificate is as follows:

a. The type certification basis for the aircraft is shown on TCDS A24CE for parts not changed or not affected by this change.

b. The certification basis for the parts changed or affected by this change since the reference date of application, June 27, 2014, is shown on TCDS A24CE; with the addition of 14 CFR Part

23.853(d)(3)(ii) Amendment 23-62, and 14 CFR Part 23.856, Amendment 23-62.

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