# STC SA02137AT - Type: Supplemental type certificate - Status: Current, Amended - Holder: Lord Corporation, United States - Description: Installation of the Lord Corporation Nose Wheel Shimmy Damper P/N SE-1051 - Applied: March 16, 2000 - Status date: August 24, 2006 - Product: Aircraft, Single-Engine - Certification basis: Part 3, Part 21 - Data sheets: [TCDS 3A19](https://openairdocs.org/tcds/3A19), [TCDS A13EU](https://openairdocs.org/tcds/A13EU) - Certificate PDF: https://openairdocs.org/files/sha256/d4/cd/d4cdff6a70a3efec022cb2ef121ebb081088e708a57ecf4fe4408633db88d97e - Approved model list and other attachments: [SA02137ATaml.pdf](https://openairdocs.org/files/sha256/b2/e8/b2e83a47e522048920fa208c76263667b544c046700519610aab36765894c03f) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/BE3F0C66977B844F86257204007586E3.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA02137AT ## ADs that name it (0) None. ## Approved models (34) - Reims Aviation S.A. F150 Series ([TCDS A13EU](https://openairdocs.org/tcds/A13EU)) - Reims Aviation S.A. F150G ([TCDS A13EU](https://openairdocs.org/tcds/A13EU)) - Reims Aviation S.A. F150H ([TCDS A13EU](https://openairdocs.org/tcds/A13EU)) - Reims Aviation S.A. F150J ([TCDS A13EU](https://openairdocs.org/tcds/A13EU)) - Reims Aviation S.A. F150K ([TCDS A13EU](https://openairdocs.org/tcds/A13EU)) - Reims Aviation S.A. F150L ([TCDS A13EU](https://openairdocs.org/tcds/A13EU)) - Reims Aviation S.A. F150M ([TCDS A13EU](https://openairdocs.org/tcds/A13EU)) - Reims Aviation S.A. F152 ([TCDS A13EU](https://openairdocs.org/tcds/A13EU)) - Reims Aviation S.A. FA150 Series ([TCDS A13EU](https://openairdocs.org/tcds/A13EU)) - Reims Aviation S.A. FA150K ([TCDS A13EU](https://openairdocs.org/tcds/A13EU)) - Reims Aviation S.A. FA150L ([TCDS A13EU](https://openairdocs.org/tcds/A13EU)) - Reims Aviation S.A. FA152 ([TCDS A13EU](https://openairdocs.org/tcds/A13EU)) - Reims Aviation S.A. FRA150L ([TCDS A13EU](https://openairdocs.org/tcds/A13EU)) - Reims Aviation S.A. FRA150M ([TCDS A13EU](https://openairdocs.org/tcds/A13EU)) - The Cessna Aircraft Company 150 ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - The Cessna Aircraft Company 150 Series ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - The Cessna Aircraft Company 150A ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - The Cessna Aircraft Company 150B ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - The Cessna Aircraft Company 150C ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - The Cessna Aircraft Company 150D ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - The Cessna Aircraft Company 150E ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - The Cessna Aircraft Company 150F ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - The Cessna Aircraft Company 150G ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - The Cessna Aircraft Company 150H ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - The Cessna Aircraft Company 150J ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - The Cessna Aircraft Company 150K ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - The Cessna Aircraft Company 150L ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - The Cessna Aircraft Company 150M ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - The Cessna Aircraft Company 152 ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - The Cessna Aircraft Company 152 Series ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - The Cessna Aircraft Company A150K ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - The Cessna Aircraft Company A150L ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - The Cessna Aircraft Company A150M ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - The Cessna Aircraft Company A152 ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) ## 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 SA02137AT This certificate issued to Part 3 of the Civil Air Regulations. Installation of the Lord Corporation Nose Wheel Shimmy Damper P/N SE-1051 in accordance with Lord Corporation Drawing as listed on AML No. SA02137AT. 1. Lord Corporation Instructions for Continued Airworthiness as listed on AML No. SA02137AT is required for this installation. 2. A copy of this Certificate and the FAA Approved Model Li st (AML) No. SA02137AT, issued May 26, 2000, or later FAA approved revisions, must be maintained as part of the permanent records for the modified aircraft. 3. Cessna Models 150G, 150H, 150J thru 150M, A150K thru A150M, 152, A152, 175 thru 175C and Remis Aviation S.A. Models F150G, F150H, F150J thru F150M , F152, FA150K, FA150L, FRA150L, FRA150M and FA152 modified per this STC prior to the amendment date March 17, 2005 are consid ered airworthy. These aircraft mode ls were removed from this STC on March 17, 2005 and were added to STC SA02138AT, amended on August 11, 2006. 4. Compatibility of this design change with previously approved modifications must be determined by the installer. 5. If the holder agrees to permit another pers on to use this certificate to alter the product, the holder shall give the other per son written evidence of that permission. Lord Corporation Mechanical Products Division 2000 West Grandview Blvd. Erie, PA 16514 * * - See attached FAA Approved Model List (AML) No. SA02137AT for a list of approved models and applicable airworthiness regulations. Date of application : March 16, 2000 Date of issuance : May 26, 2000 Date reissued : October 1, 2002 Date amended : March 17, 2005, August 24, 2006 ( Signature) Anthony Socias Manager New York Aircraft Certification Office ( Title) ### SA02137ATaml.pdf **FAA APPROVED MODEL LIST (AML) NUMBER SA02137AT** LORD CORPORATION FOR INSTALLATION OF NOSE WHEEL SHIMMY DAMP ER Issue Date: May 26, 2000 Drawing ITEM **AIRCRAFT MAKE** **AIRCRAFT MODEL** **ORIGINAL TYPE** **CERTIFICATE** **NUMBER NUMBER REVISION NO.** **AND DATE** **INSTRUCTIONS** **FOR CONTINUED** **AIRWORTHINESS** **NUMBER/DATE AML** AMEMDMENT DATE 1 Cessna Aircraft Company 150, 150A 150B, 150C 150D, 150E 150F, 150G 150H, 150J 150K A150K 150L A150L 150M A150M 152 A152 3A19 SE-1051 Revision C dated September 16, 1999 or later FAA approved revision. 2 Reims Aviation S.A. F150G F150H F150J F150K F150M F152 FA150K F150L FA150L FRA150L FRA150M FA152 A13EU SE-1051 Revision C dated September 16, 1999 or later FAA approved revision. Page 1 of 2 **FAA APPROVED MODEL LIST (AML) NUMBER SA02137AT** LORD CORPORATION FOR INSTALLATION OF NOSE WHEEL SHIMMY DAMP ER Issue Date: May 26, 2000 Drawing ITEM **AIRCRAFT MAKE** **AIRCRAFT MODEL** **ORIGINAL TYPE** **CERTIFICATE NUMBER NUMBER REVISION NO. AND DATE** **INSTRUCTIONS** **FOR CONTINUED** **AIRWORTHINESS** **NUMBER/DATE AML** AMEMDMENT DATE 3 Cessna Aircraft Company 150 150A 150B 150C 150D 150E 150F 3A19 SE-1051DL Revision -, dated February 7, 2005 or later FAA approved revision. Lord Bulletin No. SM-6514 Revision -, December 4, 2004 March 17, 2005 FAA Approved:_________________________________________ Anthony Socias M a n a g e r , N e w Y o r k A i r c r a f t C e r t i f i c a t i o n O f f i c e A m e n d m e n t D a t e : M a r c h 1 7 , 2 0 0 5 Page 2 of 2 ## Every issue (2) - August 24, 2006: Amended, Current. [certificate](https://openairdocs.org/files/sha256/d4/cd/d4cdff6a70a3efec022cb2ef121ebb081088e708a57ecf4fe4408633db88d97e), [SA02137ATaml.pdf](https://openairdocs.org/files/sha256/b2/e8/b2e83a47e522048920fa208c76263667b544c046700519610aab36765894c03f) - March 17, 2005: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/28/66/286652e0754e81c30db00f007d2f9413d2cd1d594cfd4e6e54dbeb0b7238181e), [SA02137ATAML.pdf](https://openairdocs.org/files/sha256/d8/5c/d85c2864478014a74f501e032de9e40fc7882aae93474bdb2813d0dfb860e02c) --- 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.