# STC SA00609DE - Type: Supplemental type certificate - Status: Current, Issued - Holder: Lord Corporation, United States - Description: Installation of a nose whell shimmy damper - Applied: January 2, 2007 - Status date: December 3, 2007 - Product: Aircraft, Large Multi-Engine - Certification basis: Part 21, Part 23 - Data sheets: [TCDS 3A15](https://openairdocs.org/tcds/3A15), [TCDS 3A16](https://openairdocs.org/tcds/3A16), [TCDS A-777](https://openairdocs.org/tcds/A-777), [TCDS A23CE](https://openairdocs.org/tcds/A23CE) - Certificate PDF: https://openairdocs.org/files/sha256/17/07/1707ea26d5a1b70ae4451f132a2a9f10801628224706a1f6d6024cd09dbc63fa - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/84D0187D9A1D797386257442007618ED.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA00609DE ## ADs that name it (0) None. ## Approved models (42) - Raytheon Aircraft Company 35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Raytheon Aircraft Company 35-33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Raytheon Aircraft Company 35-A33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Raytheon Aircraft Company 35-C33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Raytheon Aircraft Company 36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Raytheon Aircraft Company 58 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Raytheon Aircraft Company 58P ([TCDS A23CE](https://openairdocs.org/tcds/A23CE)) - Raytheon Aircraft Company 58TC ([TCDS A23CE](https://openairdocs.org/tcds/A23CE)) - Raytheon Aircraft Company 95-55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Raytheon Aircraft Company 95-A55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Raytheon Aircraft Company 95-B55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Raytheon Aircraft Company 95-C55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Raytheon Aircraft Company 95-C55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Raytheon Aircraft Company A35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Raytheon Aircraft Company A36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Raytheon Aircraft Company A36TC ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Raytheon Aircraft Company B35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Raytheon Aircraft Company B36TC ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Raytheon Aircraft Company C35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Raytheon Aircraft Company D35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Raytheon Aircraft Company D55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Raytheon Aircraft Company D55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Raytheon Aircraft Company E33C ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Raytheon Aircraft Company E35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Raytheon Aircraft Company E55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Raytheon Aircraft Company F33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Raytheon Aircraft Company F33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Raytheon Aircraft Company F33C ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Raytheon Aircraft Company F35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Raytheon Aircraft Company G33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Raytheon Aircraft Company G35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Raytheon Aircraft Company G58 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Raytheon Aircraft Company H35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Raytheon Aircraft Company J35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Raytheon Aircraft Company K35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Raytheon Aircraft Company M35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Raytheon Aircraft Company N35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Raytheon Aircraft Company P35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Raytheon Aircraft Company S35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Raytheon Aircraft Company V35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Raytheon Aircraft Company V35A ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Raytheon Aircraft Company V35B ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) ## What the certificate says This is OCR from the scanned FAA certificate. OCR can misread letters and numbers. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA00609DE This certificate issued to: Lord Corporation 2000 West Grandview Blvd Erie, PA 16514-0039 Part 23of the Federal Aviation Regulations. Original Product -Type Certificate Number: *See attached FAA Approved Model List (AML) Make: No. SA00609DE for list of approved airplane models Model: and applicable airworthiness regulations Description of Type Design Change: Installation of a nose wheel shimmy damper in accordance with Lord Corporation Manufacturing Drawing List SE-1076-MDL, Revision IR, dated June 26, 2007 and Installation Drawing List SE-1076-IDL, Revision IR, dated June 28, 2007, or later Federal Aviation Administration (FAA) approved revisions. 1. Approval of this change in type design applies to the aircraft models listed above 2. The installer must determine whether this design change is compatible with previously approved modifications. 3. A copy of this Certificate and the FAA Approved Model List issued December 3, 2007, Lord Corporation Manufacturing Drawing List SE-1076-MDL, Revision IR, dated June 26, 2007, and Lord Corporation Installation Drawing List SE-1076-IDL, dated June 28, 2007 or later FAA approved revisions must be maintained as part of the permanent records for the modified aircraft. 4. Instructions for Continued Airworthiness Document Number 32-20-06, Revision New, dated June 28, 2007, or later FAA accepted is required for this installation. 5. If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission. Date of Application: January 2, 2007 Date Reissued: Date of Issuance: December 3, 2007 Date Amended: FEDERAL AVIATION By Direction of the Administrator , (Signature) TOMINIST RATIOT Program Manager, Denver Aircraft Certification Office Stephen George (Title) or hoth. **FAA APPROVED MODEL LIST (AML) NO. SA00609DE** LORD CORPORATION For NOSE WHEEL SHIMMY DAMPER INSTALLATION PAGE 1 of 2 REVISIONS Rev. Description of Changes FAA Approval Date Original Release S. George 12/3/07 FAA Approved: Make: 12/6/2007 Small Airplane Program Manager Denver Aircraft Certification Office ANM-100D **FAA APPROVED MODEL LIST (AML) NO. SA00609DE** LORD CORPORATION For NOSE WHEEL SHIMMY DAMPER INSTALLATION PAGE 2 of 2 AIRCRAFT ORIGINAL TYPE CERTIFICATION FAA APPROVED DRAWING* AML MAKE AIRCRAFT MODEL CERTIFICATE BASIS FOR AMDT. NUMBER ALTERATION Number Rev. Date DATE 1 BEECH 58P, 58TC A23CE Part 23, See Type Manufacturing Drawing Revision IR, 12/3/07 Certificate A23CE List SE-1076-MDL 06/26/07 Installation Drawing List Revision IR, 12/3/07 SE-1076-IDL 06/28/07 BEECH 35-33, 35-А33, 35-СЗЗА, Е33С, ЗА15 CAR 3, See Type Manufacturing Drawing Revision IR, 12/3/07 F33, F33A, F33C, G33, H35, Certificate 3A15 List SE-1076-MDL 06/26/07 J35, K35, M35, N35, P35, S35, Installation Drawing List Revision IR, 12/3/07 V35, V35A, V35B, 36, A36, SE-1076-IDL 06/28/07 А36TС, В36TС BEECH 95-55, 95-A55, 95-B55, 95-C55, ЗА16 CAR 3, Part 23, See Manufacturing Drawing Revision IR, 12/3/07 95-C55A, G58, D55, D55A, E55, Type Certificate 3A16 List SE-1076-MDL 06/26/07 58 Installation Drawing List Revision IR, 12/3/07 SE-1076-IDL 06/28/07 4 BEECH 35, A35, B35, C35, D35, E35, A-777 CAR 3, See Type Manufacturing Drawing Revision IR, 12/3/07 F35, G35 Certificate A-777 List SE-1076-MDL 06/26/07 Installation Drawing List Revision IR, 12/3/07 SE-1076-IDL 06/28/07 *or Later FAA Approved Revision Revision New, dated December 3, 2007 ## Every issue (1) - December 3, 2007: Issued, Current. [certificate](https://openairdocs.org/files/sha256/17/07/1707ea26d5a1b70ae4451f132a2a9f10801628224706a1f6d6024cd09dbc63fa) --- 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.