# STC SA02546NY - Type: Supplemental type certificate - Status: Current, Issued - Holder: Lord Corporation, United States - Description: Installation of the Lord Corporation Nose Wheel Shimmy Damper Part Number SE-1090-1 - Applied: March 11, 2007 - Status date: July 9, 2008 - Product: Aircraft, Small Multi-Engine - Certification basis: Part 21, Part 23 - Data sheets: [TCDS 3A10](https://openairdocs.org/tcds/3A10), [TCDS 3A25](https://openairdocs.org/tcds/3A25), [TCDS A25CE](https://openairdocs.org/tcds/A25CE), [TCDS A28CE](https://openairdocs.org/tcds/A28CE), [TCDS A7CE](https://openairdocs.org/tcds/A7CE) - Certificate PDF: https://openairdocs.org/files/sha256/35/6f/356f5801b030c8f362acfb63f8b8aa2d3e8ff8a0cff1ab071fbe7252b2d75e1c - Approved model list and other attachments: [02546AML.pdf](https://openairdocs.org/files/sha256/13/a8/13a8c0ddb89e818425920e6de97f8a708b6c410d8cc88b4f2ac469d74bb4d2ed) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2133D9B1DC49AE2A8625749B006A4462.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA02546NY ## ADs that name it (0) None. ## Approved models (45) - Cessna Aircraft Company 310 ([TCDS 3A10](https://openairdocs.org/tcds/3A10)) - Cessna Aircraft Company 310B ([TCDS 3A10](https://openairdocs.org/tcds/3A10)) - Cessna Aircraft Company 310C ([TCDS 3A10](https://openairdocs.org/tcds/3A10)) - Cessna Aircraft Company 310D ([TCDS 3A10](https://openairdocs.org/tcds/3A10)) - Cessna Aircraft Company 310F ([TCDS 3A10](https://openairdocs.org/tcds/3A10)) - Cessna Aircraft Company 310G ([TCDS 3A10](https://openairdocs.org/tcds/3A10)) - Cessna Aircraft Company 310H ([TCDS 3A10](https://openairdocs.org/tcds/3A10)) - Cessna Aircraft Company 310I ([TCDS 3A10](https://openairdocs.org/tcds/3A10)) - Cessna Aircraft Company 310J ([TCDS 3A10](https://openairdocs.org/tcds/3A10)) - Cessna Aircraft Company 310K ([TCDS 3A10](https://openairdocs.org/tcds/3A10)) - Cessna Aircraft Company 310L ([TCDS 3A10](https://openairdocs.org/tcds/3A10)) - Cessna Aircraft Company 310N ([TCDS 3A10](https://openairdocs.org/tcds/3A10)) - Cessna Aircraft Company 310P ([TCDS 3A10](https://openairdocs.org/tcds/3A10)) - Cessna Aircraft Company 310Q ([TCDS 3A10](https://openairdocs.org/tcds/3A10)) - Cessna Aircraft Company 310R ([TCDS 3A10](https://openairdocs.org/tcds/3A10)) - Cessna Aircraft Company 320 ([TCDS 3A25](https://openairdocs.org/tcds/3A25)) - Cessna Aircraft Company 320A ([TCDS 3A25](https://openairdocs.org/tcds/3A25)) - Cessna Aircraft Company 320B ([TCDS 3A25](https://openairdocs.org/tcds/3A25)) - Cessna Aircraft Company 320C ([TCDS 3A25](https://openairdocs.org/tcds/3A25)) - Cessna Aircraft Company 320D ([TCDS 3A25](https://openairdocs.org/tcds/3A25)) - Cessna Aircraft Company 320E ([TCDS 3A25](https://openairdocs.org/tcds/3A25)) - Cessna Aircraft Company 320F ([TCDS 3A25](https://openairdocs.org/tcds/3A25)) - Cessna Aircraft Company 340 ([TCDS 3A25](https://openairdocs.org/tcds/3A25)) - Cessna Aircraft Company 340A ([TCDS 3A25](https://openairdocs.org/tcds/3A25)) - Cessna Aircraft Company 401 ([TCDS A7CE](https://openairdocs.org/tcds/A7CE)) - Cessna Aircraft Company 401A ([TCDS A7CE](https://openairdocs.org/tcds/A7CE)) - Cessna Aircraft Company 401B ([TCDS A7CE](https://openairdocs.org/tcds/A7CE)) - Cessna Aircraft Company 402 ([TCDS A7CE](https://openairdocs.org/tcds/A7CE)) - Cessna Aircraft Company 402A ([TCDS A7CE](https://openairdocs.org/tcds/A7CE)) - Cessna Aircraft Company 402B ([TCDS A7CE](https://openairdocs.org/tcds/A7CE)) - Cessna Aircraft Company 402C ([TCDS A7CE](https://openairdocs.org/tcds/A7CE)) - Cessna Aircraft Company 404 ([TCDS A25CE](https://openairdocs.org/tcds/A25CE)) - Cessna Aircraft Company 406 ([TCDS A25CE](https://openairdocs.org/tcds/A25CE)) - Cessna Aircraft Company 411 ([TCDS A7CE](https://openairdocs.org/tcds/A7CE)) - Cessna Aircraft Company 411A ([TCDS A7CE](https://openairdocs.org/tcds/A7CE)) - Cessna Aircraft Company 414 ([TCDS A7CE](https://openairdocs.org/tcds/A7CE)) - Cessna Aircraft Company 414A ([TCDS A7CE](https://openairdocs.org/tcds/A7CE)) - Cessna Aircraft Company 421 ([TCDS A7CE](https://openairdocs.org/tcds/A7CE)) - Cessna Aircraft Company 421A ([TCDS A7CE](https://openairdocs.org/tcds/A7CE)) - Cessna Aircraft Company 421B ([TCDS A7CE](https://openairdocs.org/tcds/A7CE)) - Cessna Aircraft Company 421C ([TCDS A7CE](https://openairdocs.org/tcds/A7CE)) - Cessna Aircraft Company 425 ([TCDS A7CE](https://openairdocs.org/tcds/A7CE)) - Cessna Aircraft Company 441 ([TCDS A28CE](https://openairdocs.org/tcds/A28CE)) - Cessna Aircraft Company T310Q ([TCDS 3A10](https://openairdocs.org/tcds/3A10)) - Cessna Aircraft Company T310R ([TCDS 3A10](https://openairdocs.org/tcds/3A10)) ## 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 SA02546NY This certificate issued to Part * of the * Regulations. Installation of the Lord Corporation Nose Wheel Shimmy Damper Part Number SE-1090-1 in accordance with Lord Corporation Drawing and Instructions for Continued Airworthiness as listed on AML No. SA02546NY issued July 9, 2008. 1. A copy of this Certificate and the FAA Approved Model List (AML) No. SA02546NY, issued July 9, 2008 must be maintained as part of the permanent records for the modified aircraft. 2. The installer must determine whether this design change is compatible with previously approved modifications. 3. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission. LORD Corporation 2000 West Grandview Blvd Erie, PA 16514-0039 Make: * Model: * Date reissued: (Signature) Anthony Socias Manager New York Aircraft Certification Office (Title) * See Attached FAA Approved Model List (AML) No. SA02546NY for list of approved airplane models and applicable airworthiness regulations. Date of application: March 11, 2007 Date of issuance: July 9, 2008 ### 02546AML.pdf **FAA APPROVED MODEL LIST (AML) NO. SA02546NY** **LORD CORPORATION FOR** INSTALLATION OF NOSE WHEEL SHIMMY DAMPER Page 1 of 1 Original Issue Date: July 09, 2008 ITEM AIRCRAFT MAKE AIRCRAFT MODEL TCDS CERTIFICATION BASIS FAA APPROVED DRAWINGS INSTRUCTIONS FOR CONTINUED AIRWORTHINESS AML AMENDMENT DATE 1 Cessna Aircraft Company 310, 310B, 310C, 310D, 310F, 310G, 310H, 310I, 310J, 310K, 310L, 310N, 310P, T310P, 310Q, T310Q, 310R, T310R 3A10 CAR 3 dated November 1, 1949 Installation Drawing List SE-1090- IDL Revision IR, Dated November 9, 2007 Lord Bulletin No. SM-6528, Revision B, March 4, 2008 2 Cessna Aircraft Company 320, 320A, 320B, 320C, 320D, 320E, 320F, 340, 340A 3A25 CAR 3 dated May 15, 1956 Installation Drawing List SE-1090- IDL Revision IR, Dated November 9, 2007 Lord Bulletin No. SM-6528, Revision B, March 4, 2008 3 Cessna Aircraft Company 401, 401A, 401B, 402, 402A, 402B, 402C, 411, 411A, 414, 414A, 421, 421A, 421B, 421C, 425 A7CE CAR 3 dated May 15, 1956 Installation Drawing List SE-1090-IDL Revision IR, Dated November 9, 2007 Lord Bulletin No. SM-6528, Revision B, March 4, 2008 4 Cessna Aircraft Company 404, 406 A25CE FAR Part 23 Installation Drawing List SE-1090-IDL Revision IR, Dated November 9, 2007 Lord Bulletin No. SM-6528, Revision B, March 4, 2008 5 Cessna Aircraft Company 441 A28CE FAR Part 23 Installation Drawing List SE-1090-IDL Revision IR, Dated November 9, 2007 Lord Bulletin No. SM-6528, Revision B, March 4, 2008 FAA Approved: _______________________________ Anthony Socias Manager, New York Aircraft Certification Office ## Every issue (1) - July 9, 2008: Issued, Current. [certificate](https://openairdocs.org/files/sha256/35/6f/356f5801b030c8f362acfb63f8b8aa2d3e8ff8a0cff1ab071fbe7252b2d75e1c), [02546AML.pdf](https://openairdocs.org/files/sha256/13/a8/13a8c0ddb89e818425920e6de97f8a708b6c410d8cc88b4f2ac469d74bb4d2ed) --- 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.