# STC SA01744SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Robair Repair, United States
- Description: Installation of forward left and forward right cabin door step assemblies and installation of aft right cargo door cabin step assembly.
- Applied: February 27, 2007
- Status date: April 19, 2007
- 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/sha256/5a/f3/5af32491817db2d7ae0aff411b1e4a3a326a77ca7bb5ca3ce8d635f25798ee78
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/FB08E8E229E85115862572C7005DF659.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01744SE

## 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.

Number SA01744SE

This certificate, issued to Robair Repair LLC 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: Installation of forward left and forward right cabin door step assemblies and installation of aft right cargo door cabin step assembly. These parts are to be manufactured and installed in accordance with Master Drawing List, Robair Document RA-400, Revision IR, dated January 20, 2007, or later FAA approved revision.

Limitations and Conditions : Approval of this change in type design applies only to the aircraft model listed above. This approval should not be extended to other aircraft of this model on which other previously approved modification are incorporated unless it is determined that the relationship between this change and any 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 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.

This certificate and the supporting data, which is th e basis for approval, shall remain in effect until surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator of the Federal Aviation Administration .

Date of application: February 27, 2007 Date reissued:

Date of issuance: March 27, 2007 Date amended: April 19, 2007

Original signed by James Rehrl (Signature) Acting Manager, Seattle Aircraft Certification Office

(Title) FAA FORM 8110-2(10-68)

## Every issue (2)

- April 19, 2007: Issued, Current. [certificate](https://openairdocs.org/files/sha256/5a/f3/5af32491817db2d7ae0aff411b1e4a3a326a77ca7bb5ca3ce8d635f25798ee78)
- March 27, 2007: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/b8/e0/b8e05ebca299eb74ce4d1d032a0c3547f8c7d76b6624f77561891d8a014e1b54)

---
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.