# STC SA01657SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Robair Repair, United States
- Description: Fabrication of Robair main landing gear lower support fairing .
- Applied: January 6, 2006
- Status date: March 14, 2006
- 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/sha256/0d/34/0d34ca2b771c8d174d9f1079044c0ce4a4a2a420e44590fc221dadb4ce66626b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4EF4A34C3FFCBFC0862571340058F25E.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01657SE

## ADs that name it (0)

None.

## Approved models (4)

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

Number SA01657SE 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 main landing gear lower support fairing in accordance with Robair Master Drawing List No. RA-300 Revision IR, dated December 15, 2005, or later Federal Aviation Administration (FAA) approved revision. The main landing gear lower support fairings must be installed in accordance with Robair Installation Instructions Document, RA-3000, Revision IR, dated December 15, 2005, 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 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 mai8ntained 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: January 6, 2006 Date reissued:

Date of issuance: March 14, 2006 Date amended:

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

## Every issue (1)

- March 14, 2006: Issued, Current. [certificate](https://openairdocs.org/files/sha256/0d/34/0d34ca2b771c8d174d9f1079044c0ce4a4a2a420e44590fc221dadb4ce66626b)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.