# STC SA3783NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Dynamic Aviation Group Inc., United States
- Description: Installation of upper wing reinforcing kit.
- Applied: March 10, 1988
- Status date: October 2, 2014
- Product: Aircraft, Small/Large Airplane
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/f4/01/f40103b892f1dca673439e11d90f1852673f394df9245f00d49960c9610b5021
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7D84619FF655EAC086257D73004F45C3.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA3783NM

## ADs that name it (0)

None.

## Approved models (23)

- Beechcraft Corporation 1900 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation 1900C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation 200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation 200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation 200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation 200T ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation 300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200 (C-12A) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200 (C-12C) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200C (UC-12B) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (C-12D) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (C-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (FWC-12D) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (RC-12D) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (RC-12G) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (RC-12H) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (RC-12K) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (RC-12P) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (RC-12Q) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation B200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation B200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation B200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation B200T ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))

## 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 Dynamic Aviation Group, Inc.

1402 Airport Rd., PO Box 7 Bridgewater, VA 22812 Part 23 of the Federal Aviation Regulations Original Product Type Certificate Number : A24CE Make : Beech Model : 200, 200C, 200CT, 200T, A200, A200C, A200CT, B200, B200C, B200CT, B200T, 300 , 1900, and 1900C Description of Type Design Change: Installation of upper wing reinforcing kit in accordance with FAA Sealed Aviadesign, Inc. Master Drawing List E. O. –B-8808, dated March 10, 1988, or later FAA approved revision, and FAA Approved Aviadesign, Inc. Flight Test Report dated February 14, 1988.

Limitations and Conditions: The approval of this change in type design applies to basic aircraft of the specified models that are otherwise unmodified. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. 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. A copy of this STC must be included in the permanent records of each airplane modified in accordance with this STC.

Date of application : March 10, 1988

Date of issuance : April 29, 1988

Date reissued : October 2, 2014

(Signature) Supervisor, Technical and Administrative Support Staff Los Angeles Aircraft Certification Office (Title)

Transfer the ownership of Supplemental Type Certificate Number

to (Name of transferee)

(Address of transferee) (Number and street)

(City, State, and ZIP Code)

from (Name of grantor) (Print or type)

(Address of grantor) (Number and street)

(City, State, and ZIP Code)

Signature of grantor (In ink):

U.S. GPO 1987-763-289

## Every issue (1)

- October 2, 2014: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/f4/01/f40103b892f1dca673439e11d90f1852673f394df9245f00d49960c9610b5021)

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