# STC SA3067NM

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Rosen Sunvisor Systems LLC, United States
- Description: Installation of monorail sun visor system.
- Applied: May 20, 1985
- Status date: July 15, 2004
- Product: Aircraft, Single-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/29/39/2939c3b8096a1706ff484edf7fb16bb68e6a30c49e32370098d4e8d85e6e5d22
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1F6D173307BD054986256EE80073D90C.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA3067NM

## ADs that name it (0)

None.

## Approved models (20)

- 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 A100-1 (U-21J) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company A200 (C-12A) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company A200C (UC-12B) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company A200CT (C-12D) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company A200CT (C-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company A200CT (FWC-12D) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company A200CT (RC-12D) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company A200CT (RC-12G) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company A200CT (RC-12H) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company A200CT (RC-12K) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company A200CT (RC-12P) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company A200CT (RC-12Q) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company B200C (C-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company B200C (C-12R) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company B200C (UC-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company B200C (UC-12M) ([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 SA3067NM

This certificate, issued to Rosen Sunvisor Systems 86365 College View Road Eugene, OR 97405

Part 23 of the Federal Aviation Regulations.

Original ProductType Certificate Number: A24CE Make: Raytheon Model: 200, 200C, 200CT, 200T, A100-1 (U-21J), A200 (C-12A, C-12C), A200C (UC-12B), A200CT (C-12D, FWC-12D, C-12F, RC-12D, RC-12G, RC-12H, RC-12K, RC-12P, RC-12Q), B200C (C-12F,. UC-12M, C-12R, UC-12F)

Description of the Type Design Change: Installation of monorail sunvisor system in accordance with FAA approved Rosen Sunvisor Systems, Drawing List RBKA-00DL, Revision N/C, or later FAA approved revision.

Limitations and Conditions: The approval of this change in type design applies basically to the above model aircraft only. This approval should not be extended to aircraft of this model on which other previously approved modifications are 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 the aircraft. The resulting interior arrangement, along with the required placarding has not been evaluated and is not part of this STC. A copy of this Certificate and FAA approved Rosen Sunvisor Systems Drawing List Number RBKA-00DL, shall be maintained as part of the permanent records of 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: May 20, 1985 Date reissued: March 24, 2003 Date of issuance: July 16, 1985 Date amended: March 24, 2003, July 15, 2004

(Signature)

Acting Manager, Seattle Aircraft Certification Office ( Title)

## Every issue (1)

- July 15, 2004: Amended, Current. [certificate](https://openairdocs.org/files/sha256/29/39/2939c3b8096a1706ff484edf7fb16bb68e6a30c49e32370098d4e8d85e6e5d22)

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