# STC SA02765SE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Acme Suspensions LLC, United States - Description: Installation of Acme Stinger tailwheel landing gear shock absorber - Applied: May 4, 2022 - Status date: October 31, 2024 - Product: Aircraft, Small Airplane - Certification basis: Part 23 - Data sheets: [TCDS A-780](https://openairdocs.org/tcds/A-780), [TCDS A-797](https://openairdocs.org/tcds/A-797), [TCDS 1A2](https://openairdocs.org/tcds/1A2), [TCDS A-691](https://openairdocs.org/tcds/A-691), [TCDS A00006SE](https://openairdocs.org/tcds/A00006SE), [TCDS A00053SE](https://openairdocs.org/tcds/A00053SE), [TCDS A22NM](https://openairdocs.org/tcds/A22NM) - Certificate PDF: https://openairdocs.org/files/sha256/39/4d/394db854bd8ffd4712d775279acd9f3f12259a43fb4c382d34865b6a3637ba9a - Approved model list and other attachments: [SA02765SE_AML.pdf](https://openairdocs.org/files/sha256/07/73/0773a13a516aeb7ceb1c961555e92f4e929702df9b95523fb5b75561d80caf72) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149628007220241218143355.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA02765SE ## ADs that name it (0) None. ## Approved models (37) - Aviat Aircraft Inc A-1 ([TCDS A22NM](https://openairdocs.org/tcds/A22NM)) - Aviat Aircraft Inc A-1A ([TCDS A22NM](https://openairdocs.org/tcds/A22NM)) - Aviat Aircraft Inc A-1B ([TCDS A22NM](https://openairdocs.org/tcds/A22NM)) - Aviat Aircraft Inc A-1C-180 ([TCDS A22NM](https://openairdocs.org/tcds/A22NM)) - Aviat Aircraft Inc A-1C-200 ([TCDS A22NM](https://openairdocs.org/tcds/A22NM)) - Cub Crafters Inc. CC19-180 ([TCDS A00053SE](https://openairdocs.org/tcds/A00053SE)) - Cub Crafters Inc. CC19-215 ([TCDS A00053SE](https://openairdocs.org/tcds/A00053SE)) - FS 2002 Corp. PA-14 ([TCDS A-797](https://openairdocs.org/tcds/A-797)) - FS 2003 Corp. PA-12 ([TCDS A-780](https://openairdocs.org/tcds/A-780)) - FS 2003 Corp. PA-12S ([TCDS A-780](https://openairdocs.org/tcds/A-780)) - Piper Aircraft Inc. J3C-40 ([TCDS A-691](https://openairdocs.org/tcds/A-691)) - Piper Aircraft Inc. J3C-50 ([TCDS A-691](https://openairdocs.org/tcds/A-691)) - Piper Aircraft Inc. J3C-50S ([TCDS A-691](https://openairdocs.org/tcds/A-691)) - Piper Aircraft Inc. J3C-65 (Army L-4; L-4A; L-4B (Navy NE-1); L-4H; L-4J (Navy NE-2)) ([TCDS A-691](https://openairdocs.org/tcds/A-691)) - Piper Aircraft Inc. J3C-65S ([TCDS A-691](https://openairdocs.org/tcds/A-691)) - Piper Aircraft Inc. PA-11 ([TCDS A-691](https://openairdocs.org/tcds/A-691)) - Piper Aircraft Inc. PA-11S ([TCDS A-691](https://openairdocs.org/tcds/A-691)) - Piper Aircraft Inc. PA-18 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18-105 (Special) ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18-125 (Army L-21A) ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18-135 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18-150 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18A ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18A-135 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18A-150 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18AS-125 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18AS-135 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18AS-150 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18S ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18S-105 (Special) ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18S-125 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18S-135 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18S-150 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-19 (Army L-18C) ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-19S ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Topcub Aircraft Inc. CC18-180 ([TCDS A00006SE](https://openairdocs.org/tcds/A00006SE)) - Topcub Aircraft Inc. CC18-180A ([TCDS A00006SE](https://openairdocs.org/tcds/A00006SE)) ## 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. (See Continuation Sheet Page 3 of 3 Pages) SA02765SE Acme Suspensions, LLC 3425 Airport Road Maiden, NC 28650 Part * the * Regulations * * * See attached Federal Aviation Administration (FAA) Approved Model List (AML) SA02765SE for approved aircraft models and applicable airworthiness regulations Installation of Acme Stinger tailwheel landing gear shock absorber in accordance with the Master Drawing List as listed in the Approved Model List (AML) and document AA-200-INST Revision IR or later FAA-accepted revision and maintained in accordance with document AA-210 ICA Revision A or later FAA-approved revision. This modification should not be installed on aircraft 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, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this certificate and document AA-210 ICA Instructions for Continued Airworthiness, Revision A or later FAA-approved revision, shall 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. May 4, 2022 October 31, 2024 March 29, 2023 for Acting Manager, Seattle ACO Branch SA02765SE ### SA02765SE_AML.pdf **FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA02765SE FOR** Installation of Acme Stinger tailwheel landing gear shock absorber ISSUE DATE: March 29, 2023 Page 1 of 1 **ITEM AIRCRAFT /** **ROTORCRAFT MAKE** **AIRCRAFT /** **ROTORCRAFT MODEL** **ORIGINAL TC NUMBER** **CERTIFICATION** **BASIS FOR** **ALTERATION** **FAA APPROVED** **AIRCRAFT FLIGHT** **MANUAL SUPPLEMENT** **FAA APPROVED** MASTER DRAWING LIST AML REV DATE Number Revision* Drawing Revision* 1. FS 2003 Corporation PA-12, PA-12S A-780 CAR 3 None AA-200 MDL IR 2. FS 2002 Corporation PA-14 A-797 CAR 3 None AA-200 MDL IR 3. Piper Aircraft, Inc. PA-18, PA-18S, PA-18 "105" (Special), PA-18S "105" (Special), PA-18A, PA-18 "125" (Army L-21A), PA-18S "125", PA-18AS "125", PA-18 "135" (Army L-21B), PA-18A "135", PA-18S "135", PA-18AS "135", PA-18 "150", PA-18A "150", PA-18S "150", PA-18AS "150", PA-19 (Army L-18C), PA-19S 1A2 CAR 3 None AA-200 MDL IR 4. Piper Aircraft, Inc. J3C-40, J3C-50, J3C-50S, J3C-65, J3C-65S, PA-11, PA-11S A-691 CAR 4a None AA-200 MDL IR 5. Topcub Aircraft, Inc. CC18-180, CC18-180A A00006SE 14 CFR Part 23 None AA-200 MDL IR * Or later FAA Approved Revision FAA Approved: For Manager, West Certification Branch AMENDED: REISSUED: October 31, 2024 ## Every issue (3) - October 31, 2024: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/39/4d/394db854bd8ffd4712d775279acd9f3f12259a43fb4c382d34865b6a3637ba9a), [SA02765SE_AML.pdf](https://openairdocs.org/files/sha256/07/73/0773a13a516aeb7ceb1c961555e92f4e929702df9b95523fb5b75561d80caf72) - March 31, 2023: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/46/6e/466e4b72e82fe781f32c38d1899f0d3b68c79a71b92f35a8962608116293c22c), [SA02765SE_AML.pdf](https://openairdocs.org/files/sha256/1d/34/1d3462c97b36e2d1713c9abc3330c51e91170b98c84c57b06e194b7fbaf8b82c) - March 29, 2023: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/46/6e/466e4b72e82fe781f32c38d1899f0d3b68c79a71b92f35a8962608116293c22c), [SA02765SE_AML.pdf](https://openairdocs.org/files/sha256/16/e0/16e0693d60f4f6ab6987cdcd2fd65f443a5921b5beebaad9e68d4868d1b65e9d) --- 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.