# STC SA02138AT - Type: Supplemental type certificate - Status: Current, Amended - Holder: Lord Corporation, United States - Description: Installation of Lord Corporation nose wheel shimmy damper part number SE-1051-2/3. - Applied: March 9, 1999 - Status date: August 11, 2006 - Product: Aircraft, Single-Engine - Certification basis: Part 3, Part 21 - Data sheets: [TCDS 3A12](https://openairdocs.org/tcds/3A12), [TCDS 3A17](https://openairdocs.org/tcds/3A17), [TCDS A18EU](https://openairdocs.org/tcds/A18EU), [TCDS A4EU](https://openairdocs.org/tcds/A4EU) - Certificate PDF: https://openairdocs.org/files/sha256/40/79/4079c6f18376db9fc90e65d076a981947146334c22ee48a844445315fb128d13 - Approved model list and other attachments: [SA02138ATaml.pdf](https://openairdocs.org/files/sha256/59/f3/59f34243ea8b124a0f2fa6298ae3fd6c02aaa839e2f1d2c4bf32d75880029205) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/06DCA4EF01E7FAF686257209006CFA8A.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA02138AT ## ADs that name it (0) None. ## Approved models (49) - Reims Aviation S.A. F172D ([TCDS A4EU](https://openairdocs.org/tcds/A4EU)) - Reims Aviation S.A. F172E ([TCDS A4EU](https://openairdocs.org/tcds/A4EU)) - Reims Aviation S.A. F172F ([TCDS A4EU](https://openairdocs.org/tcds/A4EU)) - Reims Aviation S.A. F172G ([TCDS A4EU](https://openairdocs.org/tcds/A4EU)) - Reims Aviation S.A. F172H ([TCDS A4EU](https://openairdocs.org/tcds/A4EU)) - Reims Aviation S.A. F172K ([TCDS A4EU](https://openairdocs.org/tcds/A4EU)) - Reims Aviation S.A. F172L ([TCDS A4EU](https://openairdocs.org/tcds/A4EU)) - Reims Aviation S.A. F172M ([TCDS A4EU](https://openairdocs.org/tcds/A4EU)) - Reims Aviation S.A. F172N ([TCDS A4EU](https://openairdocs.org/tcds/A4EU)) - Reims Aviation S.A. F172P ([TCDS A4EU](https://openairdocs.org/tcds/A4EU)) - Reims Aviation S.A. FR172E ([TCDS A18EU](https://openairdocs.org/tcds/A18EU)) - Reims Aviation S.A. FR172F ([TCDS A18EU](https://openairdocs.org/tcds/A18EU)) - Reims Aviation S.A. FR172G ([TCDS A18EU](https://openairdocs.org/tcds/A18EU)) - Reims Aviation S.A. FR172H ([TCDS A18EU](https://openairdocs.org/tcds/A18EU)) - Reims Aviation S.A. FR172J ([TCDS A18EU](https://openairdocs.org/tcds/A18EU)) - Reims Aviation S.A. FR172K ([TCDS A18EU](https://openairdocs.org/tcds/A18EU)) - The Cessna Aircraft Company 172 ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - The Cessna Aircraft Company 172 Series ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - The Cessna Aircraft Company 172A ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - The Cessna Aircraft Company 172B ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - The Cessna Aircraft Company 172C ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - The Cessna Aircraft Company 172D ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - The Cessna Aircraft Company 172E ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - The Cessna Aircraft Company 172F (USAF T-41A) ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - The Cessna Aircraft Company 172G ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - The Cessna Aircraft Company 172H (USAF T-41A) ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - The Cessna Aircraft Company 172I ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - The Cessna Aircraft Company 172K ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - The Cessna Aircraft Company 172L ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - The Cessna Aircraft Company 172M ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - The Cessna Aircraft Company 172N ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - The Cessna Aircraft Company 172P ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - The Cessna Aircraft Company 172Q ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - The Cessna Aircraft Company 172R ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - The Cessna Aircraft Company 172RG ([TCDS 3A17](https://openairdocs.org/tcds/3A17)) - The Cessna Aircraft Company 172S ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - The Cessna Aircraft Company P172D ([TCDS 3A17](https://openairdocs.org/tcds/3A17)) - The Cessna Aircraft Company R172 Series ([TCDS 3A17](https://openairdocs.org/tcds/3A17)) - The Cessna Aircraft Company R172E (USAF T-41B) ([TCDS 3A17](https://openairdocs.org/tcds/3A17)) - The Cessna Aircraft Company R172E (USAF T-41C) ([TCDS 3A17](https://openairdocs.org/tcds/3A17)) - The Cessna Aircraft Company R172E (USAF T-41D) ([TCDS 3A17](https://openairdocs.org/tcds/3A17)) - The Cessna Aircraft Company R172E Series ([TCDS 3A17](https://openairdocs.org/tcds/3A17)) - The Cessna Aircraft Company R172F (USAF T-41D) ([TCDS 3A17](https://openairdocs.org/tcds/3A17)) - The Cessna Aircraft Company R172G (USAF T-41C) ([TCDS 3A17](https://openairdocs.org/tcds/3A17)) - The Cessna Aircraft Company R172G (USAF T-41D) ([TCDS 3A17](https://openairdocs.org/tcds/3A17)) - The Cessna Aircraft Company R172G Series ([TCDS 3A17](https://openairdocs.org/tcds/3A17)) - The Cessna Aircraft Company R172H (USAF T-41D) ([TCDS 3A17](https://openairdocs.org/tcds/3A17)) - The Cessna Aircraft Company R172J ([TCDS 3A17](https://openairdocs.org/tcds/3A17)) - The Cessna Aircraft Company R172K ([TCDS 3A17](https://openairdocs.org/tcds/3A17)) ## 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 SA02138AT This certificate issued to Lord Corporation Mechanical Products Division 2000 West Grandview Blvd. Erie, PA 16514 Part 3 of the Civil Air Regulations. Original Product -- Type Certificate Number : * *See attached FAA Approved Model List (AML) No. SA02138AT for a list of approved models and applicable airworthiness regulations. Installation of the Lord Corporation Nose Wheel Shimmy Damper P/N SE-1051-2 in accordance with Lord Corporation Drawing as listed on AML No. SA02138AT. 1. Lord Corporation Instructions for Continued Airworthiness as listed on AML No. SA02138AT is required for this installation. 2. A copy of this Certificate and the FAA Approved Model List (AML) No. SA02138AT, issu ed May 26, 2000 or later FAA approved revisions, must be maintained as part of the permanent records for the modified aircraft. 3. Compatibility of this design change with previously approved modifications must be determined by the installer. 4. If the holder agrees to permit another pers on to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. Date of application : March 9, 1999 Date of issuance : May 26, 2000 Date reissued : October 1, 2002 Date amended : August 11, 2006 ( Signature) Anthony Socias Manager New York Aircraft Certification Office (Title) ### SA02138ATaml.pdf **FAA APPROVED MODEL LIST (AML) NUMBER SA02138AT** **LORD CORPORATION FOR** **INSTALLATION OF NOSE WHEEL SHIMMY DAMPER** Original 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 172, 172A, 172B, 172C, 172D, 172E, 172F, 172G, 172H, 172I, 172K, 172L, 172M, 172N, 172P, 172Q, 172R, 172S 3A12 SE-1051 Revision C dated September 16, 1999 or later FAA approved revision. 2 Cessna Aircraft Company P172D, R172K 3A17 SE-1051 Revision C dated September 16, 1999 or later FAA approved revision. August 11, 2006 Page 1 of 4 **FAA APPROVED MODEL LIST (AML) NUMBER SA02138AT** **LORD CORPORATION FOR** **INSTALLATION OF NOSE WHEEL SHIMMY DAMPER** Original Issue Date: May 26, 2000 Drawing ITEM **AIRCRAFT MAKE** **AIRCRAFT MODEL** **ORIGINAL TYPE** **CERTIFICAT E NUMBER NUMBER REVISION NO. AND DATE** **INSTRUCTIONS** **FOR CONTINUED** **AIRWORTHINESS** **NUMBER/DATE AML** AMEMDMENT DATE 3 Reims Aviation S.A F172D,F172E, F172F, F172G, F172H, F172K, F172L, F172M, F172N, F172P A4EU SE-1051 Revision C, dated September 16, 1999 or later FAA approved revision. 4 Reims Aviation S.A FR172E FR172F FR172G FR172H FR172J FR172K A18EU SE-1051 Revision C, dated September 16, 1999 or later FAA approved revision. Page 2 of 4 **FAA APPROVED MODEL LIST (AML) NUMBER SA02138AT** **LORD CORPORATION FOR** **INSTALLATION OF NOSE WHEEL SHIMMY DAMPER** Original 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 5 Cessna Aircraft Company 150G, 150H, 150J, 150K, 150L, 150M, 152, A152, A150K, A150L, A150M 3A19 SE-1051DL Revision A, dated March 22, 2005 or later FAA approved revision. Lord Bulletin No. SM-6514 Revision -, December 4, 2004 August 11, 2006 6 Reims Aviation S.A. F150G, F150H, F150J, F150K, F150L, F150M, F152, FA150K, FA150L, FRA150L, FRA150M, FA152 A13EU SE-1051DL Revision A, dated March 22, 2005 or later FAA approved revision. Lord Bulletin No. SM-6514 Revision -, December 4, 2004 August 11, 2006 7 Cessna Aircraft Company 175, 175A, 175B, 175C 3A17 SE-1051DL Revision A, dated March 22, 2005 or later FAA approved revision. Lord Bulletin No. SM-6514 Revision -, December 4, 2004 August 11, 2006 Page 3 of 4 **FAA APPROVED MODEL LIST (AML) NUMBER SA02138AT** **LORD CORPORATION FOR** **INSTALLATION OF NOSE WHEEL SHIMMY DAMPER** Original 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 8 Cessna Aircraft Company 182B, 182C, 182D 3A13 SE-1051DL Revision A, dated March 22, 2005 or later FAA approved revision. Lord Bulletin No. SM-6514 Revision -, December 4, 2004 August 11, 2006 FAA Approved: Anthony Socias Manager, New York Aircraft Certification Office Original Issue Date: May 26, 2000 Date of Amendment: August 11, 2006 Page 4 of 4 ## Every issue (1) - August 11, 2006: Amended, Current. [certificate](https://openairdocs.org/files/sha256/40/79/4079c6f18376db9fc90e65d076a981947146334c22ee48a844445315fb128d13), [SA02138ATaml.pdf](https://openairdocs.org/files/sha256/59/f3/59f34243ea8b124a0f2fa6298ae3fd6c02aaa839e2f1d2c4bf32d75880029205) --- 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.