# STC SA01206SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Robair Repair, United States
- Description: Fabrication of Robair middle gear leg fairing assembly
- Applied: February 24, 2003
- Status date: April 18, 2003
- Product: Aircraft, Single-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A16CE](https://openairdocs.org/tcds/A16CE)
- Certificate PDF: https://openairdocs.org/files/sha256/3b/92/3b920500a6b4e533d31d9e6f2df21c073c6b73fa7214a073e5ced7b83c25deed
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D82FEFA25ECF66AB862576E00075A728.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA01206SE

## ADs that name it (0)

None.

## Approved models (4)

- Cessna Aircraft Company 207 ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- Cessna Aircraft Company 207A ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- Cessna Aircraft Company T207 ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- Cessna Aircraft Company T207A ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))

## 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 SA01206SE This certificate, issued to Robair Repair 6381 NW Aileron Court Silverdale, WA 98383 Part 23 of the Federal Aviation Regulations.

Original Product⎯Type Certificate Number: A16CE Make: Cessna Aircraft Company Model: 207, 207A, T207, T207A

Description of the Type Design Change: Fabrication of Robair middle gear leg fairing assembly in accordance with Robair Master Drawing List No. RA-200, Revision IR, dated March 20, 2003, or later Federal Aviation Administration (FAA) approved revision. The middle gear leg fairings must be installed in accordance with Robair Installation Instructions Document RA-2000, Revision Original Issue, dated December 1, 2002, 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. This is a direct replacement part, and the FAA has determined that FAR 43 is adequate to insure Continued Airworthiness of this modification.

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: February 24, 2003 Date reissued:

Date of issuance: April 18, 2003 Date amended:

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

## Every issue (1)

- April 18, 2003: Issued, Current. [certificate](https://openairdocs.org/files/sha256/3b/92/3b920500a6b4e533d31d9e6f2df21c073c6b73fa7214a073e5ced7b83c25deed)

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