# STC SA01285SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Rosen Sunvisor Systems LLC, United States
- Description: The manufacture of a Cirrus sunvisor system
- Applied: July 2, 2003
- Status date: October 27, 2003
- Product: Aircraft, Single-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A00009CH](https://openairdocs.org/tcds/A00009CH)
- Certificate PDF: https://openairdocs.org/files/sha256/85/ac/85acae9dcbc911421d73e87d06d13d470b7edfa867ec470b5f484284e911545d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C108D1D26EC5422586256DE400590166.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA01285SE

## ADs that name it (0)

None.

## Approved models (2)

- Cirrus Design Corporation SR20 ([TCDS A00009CH](https://openairdocs.org/tcds/A00009CH))
- Cirrus Design Corporation SR22 ([TCDS A00009CH](https://openairdocs.org/tcds/A00009CH))

## 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 SA01285SE

This certificate, issued to: Rosen Sunvisor Systems, LLC.

86365 College View Road Eugene, OR 97405

Part 23 of the Federal Aviation Regulations.

Original ProductType Certificate Number: A00009CH Make: Cirrus Design Corporation Model: SR20, SR22

Description of the Type Design Change: The manufacture of a Cirrus sunvisor system in accordance with Rosen Sunvisor Systems, LLC. Master Drawing List No. 1740000-DL, Revision B, dated August 13, 2003, or later FAA approved revision. The sunvisor system must be installed and maintained in accordance with Rosen Sunvisor Systems, LLC. Installation and Continued Airworthiness Instructions Document 9050-0174-001, Revision A, dated August 5, 2003, or later FAA approved revision.

Limitations and Conditions: Approval of this change in type design applies to the aircraft models listed on the AML only. This approval should not be extended to other aircraft of these models 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 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: July 2, 2003 Date reissued:

Date of issuance: October 27, 2003 Date amended:

(Signature) Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (1)

- October 27, 2003: Issued, Current. [certificate](https://openairdocs.org/files/sha256/85/ac/85acae9dcbc911421d73e87d06d13d470b7edfa867ec470b5f484284e911545d)

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