# STC SA01919WI

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Aircraft Structures International Corp, United States
- Description: Installation of Replacement Wing Strut Fitting and Empennage, Empennage Attachments and related Aft Fuselage
Structures
- Applied: October 10, 2017
- Status date: April 22, 2019
- Product: Aircraft
- Certification basis: Part 21
- Data sheets: [TCDS A37CE](https://openairdocs.org/tcds/A37CE)
- Certificate PDF: https://openairdocs.org/files/sha256/30/e8/30e81facf566ac7ff26c0a755426a0ed250e5712134f41f3107dc04e29cdbd57
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/81F5FEC674B40B388625843A00577D6B.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA01919WI

## 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.

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 the property oft h eS T C holder.

FAA Form 8110-2 (5/14) Page 1 of This certificate issued to:

Part of the

Signature

Title Aircraft Structures International Corporation 620 N. Rock Road, Suite 230, #233 Derby, KS 67037 3 SA01919WI Federal Aviation Regulations.23 Installation of Replacement Wing Strut Fitting and Empennage, Empennage Attachments and related Aft Fuselage Structures in accordance with Master Data List (MDL), Document No. 16534000-300, Rev. C, dated 4/22/19, or later FAA Approved revision.

1. This installation should not be incorporated on any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce adverse effect upon the airworthiness of the airplane.

(See continuation sheet page 3) Textron Aviation (Cessna) 208, 208B October 10, 2017 April 22, 2019 A37CE Ben Tyson Program Manager Wichita ACO Branch

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 the property oft h eS T C holder.

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

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

3 SA01919WI

The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property oft h eS T C holder.

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

3 Date Issued:

Limitations and Conditions: (continued from page 1)

2. Model 208, s/n 20800001 and On, and Model 208B, s/n 208B00001 and On, with maximum takeoff and flight weights of 8750 pounds or less.

3. Instructions for Continued Airworthiness (ICA), Document No. 16534000-600, Rev. B, dated 3/13/19, or later FAA accepted revision, must be made available to the operator at the time of installation. The ICA does not change the Textron Aviation ICA limitations. It provides a procedure to reset the inspection requirements for the replacement fittings, thus zeroing the in service hours for the new fittings. Subsequent inspections for fittings installed per the MDL Document No. 16534000-300, Rev.

C, dated 4/22/19, or later FAA Approved revision, will be as defined in the Textron Aviation ICA limitations.

------------ END ----------- SA01919WI

## Every issue (1)

- April 22, 2019: Issued, Current. [certificate](https://openairdocs.org/files/sha256/30/e8/30e81facf566ac7ff26c0a755426a0ed250e5712134f41f3107dc04e29cdbd57)

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