STC SA00787DE

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate SA00787DENumber:

This certificate issued to: 3S Certification, LLC 9111 E. Douglas, Suite 100 Wichita, KS 67207 BB__.

Make:A37CE Cessna Aircraft CompanyOriginal Product *See Pages 3 & 4 for complete Certification Basis* 7\SH&HUWLILFDWH1XPEHU Model: 208B Description of Type Design Change:

Installation of a replacement Radio Frequency Transparent pod in accordance with FAA approved Master Data List, Document No. 0190-00-9342, Rev. A, dated 6/26/2015, or later approved revision. A copy of this certificate and FAA approved Airplane Flight Manual Supplement, Document No. 0190-00-9322, Rev. A, dated 5/14/2015, or later FAA approved revision, and Instructions for Continued Airworthiness, Document No. 0190-00-9305, Rev. A, dated 01/12/2015 or later FAA accepted revision for the replacement pod installation must be maintained as part of the permanent records for the modified aircraft.

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

(See Continuation Pages 3 & 4)

Date of Application: July 22, 2014 Date Reissued: 09/15/2021 Date of Issuance: June 26, 2015 Date Amended:

Robert C. Jones, Acting Manager Denver ACO Branch Title: Compliance and Airworthiness Division $Q\DOWHUDWLRQRIWKLVFHUWLILFDWHLVSXQLVKDEOHE\DILQHRIQRWH[FHHGLQJRULPSULVRQPHQWQRWH[FHHGLQJ\HDUVRUERWK7KLVFHUWLILFDWHPD\EHWUDQVIHUUHGRUPDGH DYDLODEOHWRWKLUGSHUVRQVE\OLFHQVLQJDJUHHPHQWVLQDFFRUGDQFHZLWK&)53RVVHVVLRQRIWKLV6XSSOHPHQWDO7\SH&HUWLILFDWH 67& GRFXPHQWE\SHUVRQVRWKHUWKDQ WKH67&KROGHUGRHVQRWFRQVWLWXWHULJKWVWRWKHGHVLJQGDWDQRUWRDOWHUDQDLUFUDIWDLUFUDIWHQJLQHRUSURSHOOHU7KH67&¶VVXSSRUWLQJGRFXPHQWDWLRQ GUDZLQJVLQVWUXFWLRQV SURSHOOHUPXVWSURYLGHWKDWSHUVRQZLWKZULWWHQSHUPLVVLRQDFFHSWDEOHWRWKH)$$ 5HI&)5   )$$)RUP  683(56('(635(9,286(',7,21 3DJHRIBBB 4

I United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate SA00787DENumber:

Date oI transfer:

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United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA00787DE Limitations and Conditions Continued:

2. 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 the permission.

3. The FAA has not certified the installation of equipment for which these provisions are intended. You must get additional FAA approval to install any equipment in the pod.

The FAA must evaluate the installation to ensure it complies with the applicable airworthiness standards. Contact the STC holder for further information on future payload design limits and details.

4. Flight into known icing conditions is prohibited when the RF transparent pod is installed under this STC.

5. Installation of the transparent pod, under this STC is limited to aircraft equipped with the Garmin G1000 avionics system and a TKS Ice Protection System.

6. Supplemental Type Certificate (STC) SA02080AK-D must be installed as a prerequisite for this STC Installation.

7. Approval of this change in type design applies to the above model of airplane only, with an existing cargo/baggage pod installed.

Certification Basis:

It was determined that there is no acoustical change in accordance with § 21.93(b)(3)

(iii) as a result of this modification.

Based on 14 CFR Part 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Cessna Model 208B replacement pod installation is as follows:

a) The type certification basis for Cessna 208B is shown on A37CE 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 the application, 07/22/2014, is based upon part 23 as amended by Amendment 23-62. Based on 14 CFR § 21.115 and §21.101, and the FAA policy for significant changes in the FAA Order 8110.48, the certification basis for this modification was determined to be:

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United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA00787DE Certification Basis Continued:

Regulations at the latest amendment 23-0 through 23-62

23.607 Amdt. 23-48, 23.1365(a) Amdt. 23-49.

Regulations at an intermediate amendment

23.335 Amdt. 23-34, 23.441 Amdt. 23-42.

Regulations at the amendment level in TCDS A37CE

23.45, 23.49, 23.51, 23.65, 23.75, 23.77, 23.251, 23.253, 23.301(a)(b)(c), 23.303,

23.305, 23.307(a), 23.321, 23.333, 23.337(a)(b), 23.341, 23.347, 23.471, 23.473,

23.479, 23.481, 23.485(c), 23.493, 23.601, 23.603, 23.605, 23.609, 23.611,

23.613, 23.619, 23.625(a)(b)(c), 23.627, 23.787(a), 23.863(a)(b)(d), 23.867(a)(c),

23.999, 23.1301, 23.1309(a), 23.1431(b), 23.1529, 23.1557(a), 23.1581(a)(b),

23.1589.

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