# STC SA3831NM

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Raisbeck Engineering, United States
- Description: Installation of improved leading edge consisting of inboard leading edges,deice boots, leading edge ducts, leading edge to nacelle fairing and associated hardware.
- Applied: November 10, 1986
- Status date: April 17, 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/sha256/24/27/2427e0ebed24a98773ac452e3c4f41f411b5c17f9b4676e80ec5197851f9ebba
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/55874061B52573708625743A0072312A.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA3831NM

## 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.

Number SA3831NM

This certificate, issued to Raisbeck Engineering 4411 South Ryan Way Seattle, WA 98178

Part 23 of the Federal Aviation Regulations.

Original Product⎯Type Certificate Number: A24CE Make: Raytheon (Beech) Model: 200, 200C, 200T, 200CT, A200, A200C, A200CT B200, B200C, B200T, B200CT, B200GT, B200CGT

Description of the Type Design Change: Installation of improved leading edge consisting of inboard leading edges, deice boots, leading edge ducts, leading edge to nacelle fairing, and associated hardware in accordance with Raisbeck Engineering Master Drawing List R81-1002, Revision J, dated January 30, 2008, or later FAA-approved revisions.

Limitations and Conditions: This installation must be maintained in accordance with the appropriate Raytheon (Beech) maintenance manual.

Approval of this change in type design applied to the above aircraft models only. This approval should not be extended to other aircraft of this model on which other previously approved modifications have been incorporated unless it is determined 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. A copy of this certificate must be maintained as part of the permanent records for the modified 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.

Date of application: November 10, 1986 Date reissued:

Date of issuance: May 29, 1987 Date amended: May 26, 1993, April 17, 2008

(Signature)

Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (1)

- April 17, 2008: Amended, Current. [certificate](https://openairdocs.org/files/sha256/24/27/2427e0ebed24a98773ac452e3c4f41f411b5c17f9b4676e80ec5197851f9ebba)

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