# STC SA02465AK

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Aero Twin Inc, United States
- Description: Installation of Aero Twin, Inc., DFS8T seats
- Applied: July 1, 2015
- Status date: December 4, 2015
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A37CE](https://openairdocs.org/tcds/A37CE)
- Certificate PDF: https://openairdocs.org/files/sha256/75/67/7567581420bf580ecba6f42dcab3416e392dfaae204f73545b39b8604e8b1a6f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/24557F65C48CFDCE86257F17006EEA8A.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02465AK

## ADs that name it (0)

None.

## Approved models (2)

- Textron Aviation Inc. 208 ([TCDS A37CE](https://openairdocs.org/tcds/A37CE))
- Textron Aviation Inc. 208B ([TCDS A37CE](https://openairdocs.org/tcds/A37CE))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

This certificate issued to Aero Twin, Inc.

2403 Merrill Field Drive Anchorage, AK 99501

Part 23 of the Civil Air Regulations

Original Product – Type Certificate Number: A37CE Make: Textron Aviation Inc.

Model : 208 and 208B

Installation of Aero Twin, Inc., DFS8T seats in Textron Aviation Inc. model 208 and 208B aircraft in accordance with Aero Twin, Inc., Master Data List, Document Number DFS8-208-MDL, Original Issue, dated December 4, 2015, or later FAA approved revision.

1. The compatibility of this design change with previously approved modifications must be determined by the installer.

2. If the holder agrees to permit another person to use this design approval to alter the product, the holder shall give the other person written evidence of that permission.

3. Instructions for Continued Airworthiness, Aero Twin, Inc. Document Number DFS8-208-ICA, Original Issue, dated June 30, 2015, or later FAA accepted revision is a required part of this modification.

4. Airplane Flight Manual Supplement (AFMS), Aero Twin Document Number DFS8-208-AFMS, Original Issue, dated December 4, 2015, or later FAA approved revision is a required part of this modification.

(Limitations and Conditions continued on page 2)

Date of application: July 1, 2015 Date reissued:

Date of issuance: December 4, 2015 Date amended:

Number By direction of the Administrator

(Signature) August A. Asay Manager, Anchorage Aircraft Certification Office

(Title)

FAA FORM 8110-2-1(10-69) PAGE 2 of 2 PAGES

SA02465AK

Limitations and Conditions (cont’d):

5. DFS8T seat installation in model 208 is compliant with Title 14, Code of Federal Regulations (14 CFR) section 23.562 when installed per the alternate seating configuration shown in figure 6.3 of Aero Twin AFMS Document Number DFS8-208-AFMS, Original Issue, dated December 4, 2015, or later FAA approved revision.

6. DFS8T seat installation in model 208B is compliant with 14 CFR 23.562 when installed per the standard seating configuration shown in figure 6.2 of Aero Twin AFMS Document Number DFS8-208-AFMS, Original Issue, dated December 4, 2015, or later FAA approved revision.

## Every issue (1)

- December 4, 2015: Issued, Current. [certificate](https://openairdocs.org/files/sha256/75/67/7567581420bf580ecba6f42dcab3416e392dfaae204f73545b39b8604e8b1a6f)

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