# STC SA02763SE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Metal Innovations Inc. dba MII Aero, United States
- Description: Installation of Metal Innovations Inc. C-208B Cargo Pod Alteration
- Applied: September 8, 2020
- Status date: February 25, 2025
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Data sheets: [TCDS A37CE](https://openairdocs.org/tcds/A37CE)
- Certificate PDF: https://openairdocs.org/files/sha256/eb/82/eb82af75a9087feef8d181ef270e53ce2df258000f181761b24e4e74456d097b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187947025220250319142652.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02763SE

## ADs that name it (0)

None.

## Approved models (1)

- 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.

(See Continuation Sheet Page 3 of 4 Pages) (See Continuation Sheet Page 3 of 4 Pages) SA02763SE Metal Innovations, Inc. dba MII Aero 2870 25th Street SE Salem, OR 97302 Part 23 Title 14 Code of Federal Regulations A37CE Textron Aviation Inc.

208B Installation of Metal Innovations Inc. C-208B Cargo Pod Alteration in accordance with MIIDoc00307, Revision B, dated November 21, 2022, or later Federal Aviation Administration (FAA) approved revision. Manufactured in accordance with Master Drawing List MIIDoc00305, Revision C, dated February 3, 2023, or later FAA-approved revision.

Installation is limited to model 208B with cargo pod. Approval of this change in type design applies only to the above listed model aircraft only. This approval should not be extended to other aircraft of this model on which previously approved modifications are incorporated unless it is determined by the installer that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft.

September 8, 2020 April 12, 2023; February 25, 2025 March 1, 2023 for Manager, West Certification Branch

SA02763SE

(See Continuation Sheet Page 4 of 4 Pages) SA02763SE Description of Type Design Change (continued):

Maintained in accordance with Instructions for Continued Airworthiness (ICA), MIIDoc00308, Revision B, dated August 1, 2022, or later FAA accepted revision.

Operated in accordance with Aircraft Flight Manual Supplement (AFMS) MIIDoc00385, Revision A, Dated May 13, 2022, or later FAA approved revision.

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.

Under the provisions of Title 14 Code of Federal Regulations (14 CFR) Section 21.101, the following regulations are applicable to the areas changed or affected by this modification, all other regulations per TCDS A37CE: (14 CFR Part 23, Amendment as shown). A copy of this certificate, ICA and the AFMS must be maintained as part of the permanent records for the modified aircraft.

23-0 23-23 § 23-303 § 23-603 § 23-305 § 23-605 § 23-307 § 23-613 § 23-601 § 23-1557 § 23-609

23-7 23-26 § 23-337 § 23-1529 § 23-561 § 23-611 § 23-625

End SA02763SE Limitations and Conditions (continued):

23-13 23-28 § 23-1589 § 23-301 § 23-473

23-17 23-43 § 23-607 § 23-993 § 23-787 § 23-999

23-21 23-49 § 23-1501 § 23-855(b) § 23-1581

## Every issue (2)

- February 25, 2025: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/eb/82/eb82af75a9087feef8d181ef270e53ce2df258000f181761b24e4e74456d097b)
- March 1, 2023: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/65/3a/653a68b45ed24d1c14d93d1ab2c73191bc7428f58241bf4755a9c64c151b3b65)

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