# STC SA1602CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Dynamic Aviation Group Inc., United States
- Description: Installation of wing front spar reinforcement kit.
- Status date: February 20, 2008
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/d3/c8/d3c87032c4e666b2e79df427c8eff7dee079af6af2d7f171abd9b945fed0448a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/508B4C13D2DA094A86257471004C4405.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1602CE

## ADs that name it (0)

None.

## Approved models (11)

- Raytheon Aircraft Company 200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company 200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company 200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company 200T ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company A200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company A200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company A200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company B200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company B200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company B200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company 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 and B200T

Install wing front spar reinforcement kit per drawings and data listed by FAA approved copy of Aviadesign, Inc.

Engineering Order E.O.-B-8002.

1) This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of these other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane.

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 that permission.

Date reissued : May 15, 1985; November 21, 2006;

February 20, 2008 Date amended : January 5, 1984

Original signed by Todd Dixon

( Signature) Todd G. Dixon Associate ACO Manager, Electrical Systems & Avionics Wichita Aircraft Certification Office (Title) Date of application : February 22, 1980 Date of issuance : August 20, 1980

## Every issue (1)

- February 20, 2008: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/d3/c8/d3c87032c4e666b2e79df427c8eff7dee079af6af2d7f171abd9b945fed0448a)

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