# STC SA01602SE

- Type: Supplemental type certificate
- Status: Historical, Amended
- Holder: AeroMech Incorporated, United States
- Description: Group aircraft approval for Reduced Vertical Separation Minimum (RVSM).
- Applied: July 15, 2004
- Status date: November 17, 2006
- Product: Aircraft, Single-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A28CE](https://openairdocs.org/tcds/A28CE)
- Certificate PDF: https://openairdocs.org/files/sha256/a8/a6/a8a648f6ecdfffb5c13565634d3ef2ad7d0d2007e8fa275fc386103a3d12361b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2DEDC1F949E235B3862572E20049F6A8.0001
- DRS record last changed: May 21, 2007
- Page: https://openairdocs.org/stc/SA01602SE

## ADs that name it (0)

None.

## Approved models (2)

- Cessna Aircraft Company 441 ([TCDS A28CE](https://openairdocs.org/tcds/A28CE))
- The Cessna Aircraft Company 441 ([TCDS A28CE](https://openairdocs.org/tcds/A28CE))

## 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.

United States of America Department of Transportation _ Federal Aviation Administration Supplemental Type Certificate Number SA01602SE

This certificate, issued to: AeroMech Incorporated 1616 Hewitt Avenue, Suite 312 Everett, WA 98201

Part 23 of the Federal Aviation Regulations.

Original Product⎯Type Certificate Number: A28CE (Rev. 12) Make: Cessna Model: 441

Description of the Type Design Change: Group aircraft approval for Reduced Vertical Separation Minimum (RVSM) in accordance with AeroMech Document No. AMI-QD-CS-0422 Rev. “B," dated November 13, 2006, or latest FAA approved revision.

Limitations and Conditions: For Class 1 airframes, the Instructions for Initial and Continued Airworthiness, document AMI-IICA-CS-0438A, Rev. “A,” dated April 28, 2006, or latest FAA approved revision, is a required part of this STC.The Airplane Flight Manual Supplement (AFMS) for the Cessna Model 441, AeroMech Document AMI-AFMS-CS-0435A, Rev. “B,” FAA approved November 17, 2006, or latest FAA approved revision, is required on-board for operation of the Class 1 airframes.

For Class 2 airframes, the Instructions for Initial and Continued Airworthiness, document AMI-IICA-CS-0438B, Rev. “new,” dated November 13, 2006, or latest FAA approved revision, is a required part of this STC. The Airplane Flight Manual Supplement (AFMS) for the Cessna Model 441, AeroMech Document AMI-AFMS-CS-0435B, Rev. “new,” FAA approved November 17, 2006, or latest FAA approved revision, is required on-board for operation of the Class 2 airframes.

Descriptive data pertaining to this design change are considered inadequate for duplication on other products.

This approval is limited to Cessna Model 441aircraft only.

A copy of this certificate must be maintained as part of the permanent records of the aircraft. If the holder agrees to permit another person to use this certificate the holder shall give the other person written evidence of the permission.

Date of application: July 15, 2004 Date reissued:

Date of issuance: October 26, 2005 Date amended: May 4, 2006, November 17, 2006

This certificate may be transfe rred in accordance with FAR 21.47.

(Signature)

Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (2)

- November 17, 2006: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/a8/a6/a8a648f6ecdfffb5c13565634d3ef2ad7d0d2007e8fa275fc386103a3d12361b)
- May 4, 2006: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/8e/99/8e9990d498c939ff927daa992300bb80d591da6aa6b606e644a2fc06dc7e2b29)

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