# STC SA02298AK - Type: Supplemental type certificate - Status: Current, Issued - Holder: Tanalian Aviation Inc., United States - Description: Installation of Horizontal Stabilizer Screw-on Leading Edge on Cessna 206 and 207. - Applied: February 21, 2006 - Status date: September 7, 2007 - Product: Aircraft, Single-Engine - Certification basis: Part 21 - Data sheets: [TCDS A4CE](https://openairdocs.org/tcds/A4CE) - Certificate PDF: https://openairdocs.org/files/sha256/68/76/6876452da8cc89cfe6d480b7e93e27c779165c3e40f6ca39cbec640b14cee131 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D2F4F766D9A579D0862573A60074E349.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA02298AK ## ADs that name it (0) None. ## Approved models (27) - Cessna Aircraft Company 206 ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company P206 ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company P206A ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company P206B ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company P206C ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company P206D ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company P206E ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TP206A ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TP206B ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TP206C ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TP206D ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TP206E ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TU206A ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TU206B ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TU206C ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TU206D ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TU206E ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TU206F ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TU206G ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company U206 ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company U206A ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company U206B ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company U206C ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company U206D ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company U206E ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company U206F ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company U206G ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) ## What the certificate says This is OCR from the scanned FAA certificate. OCR can misread letters and numbers. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA02298AK This certificate issued to: Tanalian Aviation Inc. Box 77 Port Alsworth, AK 99653 Certifies that the change in the type design for the following produd with the limitations and conditions therefor as specified hereon meets the airworthiness requirenvent's of Part * ofthe * Poegulations. Original Product Type Certificate Number: * See attached FAA Approved Model List (AML) No SA02298AK for list of approved Make: Cessna airplane models and applicable airworthiness regulations. Description of Type Design Change: Installation of Horizontal Stabilizer Screw-on Leading Edge on Cessna 206 and 207, in accordance with Tanalian Aviation, Inc., Master Data List TA-100-MDL, Revision Org, dated August 17, 2007, or later FAA approved revision. 1) The installer must determine whether this design change is compatible with previously approved modifications. 2) For instructions for continued airworthiness, refer to Tanalian Aviation, Inc., "Instructions for Continued Airworthiness for Installation of Horizontal Stabilizer Screw-on Leading Edge on Cessna 206 and 207, Revision Org, dated August 17, 2007 or later FAA approved revision. 3) If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission. Date of Application: February 21, 2006 Date Reissued: Date of Issuance: September 1, 2007 Date Amended: AVIATION potion of the Administrator 1. Hote Gregory 3. Hole (signature) TOMNISTRATO Manager Anchorage Aircraft Certification Office (Title) 47 Tanalian Aviation, Inc. Amendment Level: Original Page 1 of 1 FAA Approved Model List (AML) No. SA02298AK For the Installation of Installation of Horizontal Stabilizer Screw-on Leading Edge on Cessna 206 and 207 in accordance with Master Data List "TA-100-MDL," dated August 17, 2007 Airplane Make and Model Designation Original Type Certification Certificate Basis Number Cessna 206, P206, P206A, P206B, P206C, P206D, P206E, A4CE CAR 3 U206, U206A, U206B, U206C, U206D, U206E, U206F, A4CE CAR 3 U206G, TP206A, TP206B, TP206C, TP206D, TP206E A4CE CAR 3 TU206A, TU206B, TU206C, TU206D, TU206E, TU206F, A4CE CAR 3 TU206G 207, 207A, T207, T207A A16CE Part 23 Amt. 23-1 through 23-6 -- Nothing Follows - FAA APPROVED: Manager, Anchofage Aircraft Certification Office Federal Aviation Administration Anchorage, Alaska Make: September 7, 2007 ## Every issue (1) - September 7, 2007: Issued, Current. [certificate](https://openairdocs.org/files/sha256/68/76/6876452da8cc89cfe6d480b7e93e27c779165c3e40f6ca39cbec640b14cee131) --- 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.