# STC SA02323AK - Type: Supplemental type certificate - Status: Current, Issued - Holder: Tanalian Aviation Inc., United States - Description: Installation of Horizontal Stabilizer Screw-on Leading Edge. - Applied: May 7, 2008 - Status date: October 20, 2008 - Product: Aircraft, Single-Engine - Certification basis: Part 21 - Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13), [TCDS 3A24](https://openairdocs.org/tcds/3A24), [TCDS 5A6](https://openairdocs.org/tcds/5A6) - Certificate PDF: https://openairdocs.org/files/sha256/d5/38/d5387e940192925b49ed72c86d0af2dec56f74f133dd3362c535e30301eff5f6 - Approved model list and other attachments: [STC certificate.pdf](https://openairdocs.org/files/sha256/f0/59/f059db74235af1137eaebfec90750a522c6032fb5db9572f4da8f02c9c33f298) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D158030FF604BA84862574F80074A9A0.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA02323AK ## ADs that name it (0) None. ## Approved models (26) - Cessna Aircraft Company 180 ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180A ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180B ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180C ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180D ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180E ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180F ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180G ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180H ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180J ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180K ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182A ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182B ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182C ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182D ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182E ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182F ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182G ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 185A ([TCDS 3A24](https://openairdocs.org/tcds/3A24)) - Cessna Aircraft Company 185B ([TCDS 3A24](https://openairdocs.org/tcds/3A24)) - Cessna Aircraft Company 185C ([TCDS 3A24](https://openairdocs.org/tcds/3A24)) - Cessna Aircraft Company 185D ([TCDS 3A24](https://openairdocs.org/tcds/3A24)) - Cessna Aircraft Company 185E ([TCDS 3A24](https://openairdocs.org/tcds/3A24)) - Cessna Aircraft Company A185E ([TCDS 3A24](https://openairdocs.org/tcds/3A24)) - Cessna Aircraft Company A185F ([TCDS 3A24](https://openairdocs.org/tcds/3A24)) ## 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. For the installation of a horizontal stabilizer screw-on leading edge on Cessna 180, 182 and 185 aircraft, in accordance with Tanalian Aviation, Inc., Master Data List TA-110-MDL, Revision (-), dated September 16, 2008, or later FAA approved revision. Approved Model List No. SA02323AK STC issue date: October 30, 2008 Airplane Make and Model Designation Original Type Certificate Number Certification Basis Cessna 180,180A,180B,180C,180D,180E, 180F, 180G, 180H, 180J, 180K 5A6 CAR3 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G 3A13 CAR3 185A, 185B, 185C, 185D, 185E, 185F, A185E, A185F 3A24 CAR3 END FAA Approved: Manager, Anchorage Aircraft Certification Office Federal Aviation Administration Anchorage, Alaska Date: 30 August, 2008 Revision: (-) FAA APPROVED MODEL LIST FOR Tanalian Aviation Inc. Box 77 Port Alsworth, AK 99653 ### STC certificate.pdf United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate _____________________________________________________________________________________________________________________________________ Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. _____________________________________________________________________________________________________________________________________ FAA Form 8110-2(10-68) Page 1 of 1 T his certificate may be transferred in accordance with FAR 21.47. Number SA02323AK This Certificate issued to certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meets the airworthiness requirements of Part * of the * Regulations. Original Product Type Certificate Number: Description of Type Design Change: Installation of Horizontal Stabilizer Screw-on Leading Edge on Cessna 180, 182 and 185 aircraft, in accordance with Tanalian Aviation, Inc., Master Data List TA-110-MDL, Revision:(-), dated September 16, 2008, or later FAA approved revision. Limitations and Conditions: 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 180, 182, 185,” Revision Org, dated August 21, 2008, 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. This certificate and the supporting data which is the 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. Tanalian Aviation Inc. Box 77 Port Alsworth, AK 99653 * See attached FAA Approved Model List (AML) No SA02323AK for list of approved Cessna airplane models and applicable airworthiness regulations. Make: Model: Date of application: May 7, 2008 Date of issuance: October 30, 2008 Date reissued: Date amended: By direction of the Administrator ______________________________________________ ( Signature) Gregory J. Holt Manager Anchorage Aircraft Certification Office ______________________________________________ ( Title) ## Every issue (1) - October 20, 2008: Issued, Current. [certificate](https://openairdocs.org/files/sha256/d5/38/d5387e940192925b49ed72c86d0af2dec56f74f133dd3362c535e30301eff5f6), [STC certificate.pdf](https://openairdocs.org/files/sha256/f0/59/f059db74235af1137eaebfec90750a522c6032fb5db9572f4da8f02c9c33f298) --- 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.