# STC SA01538SE - Type: Supplemental type certificate - Status: Current, Amended - Holder: Dynamic Propeller, United States - Description: Incorporation of bushing on carburetor hot air box control arm - Applied: February 24, 2005 - Status date: September 15, 2015 - Product: Aircraft, Small Airplane - Certification basis: Part 21 - Data sheets: [TCDS 3A19](https://openairdocs.org/tcds/3A19), [TCDS 3A12](https://openairdocs.org/tcds/3A12), [TCDS 5A6](https://openairdocs.org/tcds/5A6), [TCDS 3A13](https://openairdocs.org/tcds/3A13) - Certificate PDF: https://openairdocs.org/files/sha256/e6/fa/e6faa6a653b9c4efb7edd9c863b60ba5a413e1c24dfba9971ff4285e58385bd1 - Approved model list and other attachments: [SA01538SE_AML.pdf](https://openairdocs.org/files/sha256/c9/d4/c9d421b9dcd2a7e29c4aaa05bca78c81a12bc3afaf2339b442b0943b36e5b3e2) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/697E3084806E718F86257EC200687EF1.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA01538SE ## ADs that name it (0) None. ## Approved models (50) - Cessna Aircraft Company 152 ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company 172 ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172A ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172B ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172C ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172D ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172E ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172F (USAF T-41A) ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172G ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172H (USAF T-41A) ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172I ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172K ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172L ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172M ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172N ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172P ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172Q ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172R ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172S ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - 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 182H ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182J ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182K ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182L ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182M ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182N ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182P ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182R ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company A152 ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Cessna Aircraft Company R182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company T182T ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company TR182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) ## 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 SA01538SE This certificate, issued to Dynamic Propeller LLC 341 Lisa Lane Pasco, WA 99301 Part * of the * Regulations. Original ProductType Certificate Number: * See attached Federal Aviation Administration (FAA) Make: Approved Model List (AML) SA01538SE for approved Model: aircraft models and applicable airworthiness regulations Description of the Type Design Change: Incorporation of bushing on carburetor hot air box control arm in accordance with Dynamic Propeller Installation Instructions No. 7000, Revision A, dated February 24, 2005, or later FAA-approved revision. Limitations and Conditions: Approval of this change in type design applies to the aircraft models listed on AML SA01538SE only. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer that the relationship between this change and any of those other previously approved modifications, will produce no adverse effect upon the airworthiness of that aircraft. A copy of this certificate must be maintained as part of the permanent records for 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. Date of application: February 24, 2005 Date reissued: December 10, 2014 Date of issuance: April 27, 2005 Date amended: (Signature) Manager, Seattle Aircraft Certification Office (Title) ### SA01538SE_AML.pdf **FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA01538SE FOR** INSTALLATION OF BUSHING ON THE CONTROL ARM OF THE CARBURETOR HOT AIR BOX ISSUE DATE: April 27, 2005 Page 1 of 1 **ITEM AIRCRAFT MAKE** **AIRCRAFT MODEL ORIGINAL TC NUMBER** **CERTIFICATION** **BASIS FOR** **ALTERATION** **FAA APPROVED MASTER** **DRAWING LIST** AML REV DATE Drawing Revision* 1. Cessna 172, 172A, 172B, 172C, 172D, 172E, 172F, 172G, 172H, 172I, 172K, 172L, 172M, 172N, 172P, 172R 3A12 CAR 3 70DL Revision B, 10/25/06 9/XX/15 2. Cessna 172R, 172S 3A12 FAR 23 70DL Revision B, 10/25/06 9/XX/15 3. Cessna 152, A152 3A19 CAR 3 7000 Kit DP8 Revision A, 2/24/05 9/XX/15 4. Cessna 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, 180K 5A6 CAR 3 7000 Kit DP8 Revision A, 2/24/05 9/XX/15 5. Cessna 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182R R182, TR182, T182T 3A13 CAR 3 7000 Kit DP8 Revision A, 2/24/05 9/XX/15 * Or later FAA Approved Revision FAA Approved: Manager, Seattle Aircraft Certification Office AMENDED: September 15, 2015 REISSUED: December 10, 2014 ## Every issue (3) - September 15, 2015: Amended, Current. [certificate](https://openairdocs.org/files/sha256/e6/fa/e6faa6a653b9c4efb7edd9c863b60ba5a413e1c24dfba9971ff4285e58385bd1), [SA01538SE_AML.pdf](https://openairdocs.org/files/sha256/c9/d4/c9d421b9dcd2a7e29c4aaa05bca78c81a12bc3afaf2339b442b0943b36e5b3e2) - December 10, 2014: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/e6/fa/e6faa6a653b9c4efb7edd9c863b60ba5a413e1c24dfba9971ff4285e58385bd1), [SA01538SE_AML.pdf](https://openairdocs.org/files/sha256/7c/e5/7ce52ce523b9c74c5dc641dfc9e80e25888f38a7e8681a258763e38a5c415183) - April 27, 2005: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/fe/d4/fed41d106ef93d3a8c0b623e826dcdf8d5670086c382a7c7ea781cefde531f4d), [SA01538SEAML.pdf](https://openairdocs.org/files/sha256/2a/d0/2ad07ce6a501de08ed595488581ef349984578e9d2d3c28a9f4a3785d5874e8e) --- 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.