STC SA01437SE

Supplemental type certificate · Rosen Sunvisor Systems LLC

Holder
Rosen Sunvisor Systems LLC · United States
Status
Current · Issued
Status date
August 2, 2004
Applied
January 28, 2004
Product
Aircraft · Single-Engine
Certification basis
Part 21, Part 23
Data sheet
TCDSA12SO

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

The manufacture of a Commander Sunvisor System in accordance with Rosen Sunvisor Systems Drawing List No. 1430000-DL, Revision D, dated July 19, 2004, or later Federal Aviation Administration (FAA) approved revision. The sunvisor system must be installed and maintained in accordance with Rosen Sunvisor Systems Installation and Continued Airworthiness Instructions Document 9050-0143-001, Revision C, dated June 29, 2004, or later FAA approved revision.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate Number SA01437SE 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: A12SO Make: Commander Aircraft Company Model: 112, 112B, 112TC, 112TCA, 114, 114A, 114B, 114TC

Description of the Type Design Change: The manufacture of a Commander Sunvisor System in accordance with Rosen Sunvisor Systems Drawing List No. 1430000-DL, Revision D, dated July 19, 2004, or later Federal Aviation Administration (FAA) approved revision. The sunvisor system must be installed and maintained in accordance with Rosen Sunvisor Systems Installation and Continued Airworthiness Instructions Document 9050-0143-001, Revision C, dated June 29, 2004, or later FAA approved revision.

Limitations and Conditions: Approval of this change in type design applies to the aircraft models listed above only. This approval should not be extended to other 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 effects upon the airworthiness of that aircraft. A copy of this Certificate must be maintained as part of the permanent record 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.

e Date of application: January 28, 2004 Date reissued:

Date of issuance: August 2, 2004 Date amended:

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

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 8

MakeModelData sheet
Commander Aircraft Company112A12SO
Commander Aircraft Company112BA12SO
Commander Aircraft Company112TCA12SO
Commander Aircraft Company112TCAA12SO
Commander Aircraft Company114A12SO
Commander Aircraft Company114AA12SO
Commander Aircraft Company114BA12SO
Commander Aircraft Company114TCA12SO