# STC SA1751SW - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Mitsubishi Heavy Industries America Inc. - Description: Installation of shoulder harness. - Status date: July 1, 2008 - Data sheets: A10SW, A10SW, A10SW, A10SW, A10SW, A10SW, A10SW, A10SW, A2PC, A2PC, A2PC, A2PC, A2PC, A2PC, A2PC, A2PC, A2PC - Certificate PDF: https://openairdocs.org/files/sha256/e7/50/e75052015296468b61636a4d7ecd0a7c0daac7b20f69f03969e4e873b4427a25 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7D720F7728A6AF5F862574940074B488.0001 - Page: https://openairdocs.org/stc/SA1751SW ## ADs that name it - [AD 2021-07-13](https://openairdocs.org/ad/2021-07-13) (historical): Cabin Equipment/Furnishings ยท Pacific Scientific rotary buckle assembly. Effective May 11, 2021 ## Approved models (17) - Mitsubishi Heavy Industries Ltd. MU-2B (TCDS A2PC) - Mitsubishi Heavy Industries Ltd. MU-2B-10 (TCDS A2PC) - Mitsubishi Heavy Industries Ltd. MU-2B-15 (TCDS A2PC) - Mitsubishi Heavy Industries Ltd. MU-2B-20 (TCDS A2PC) - Mitsubishi Heavy Industries Ltd. MU-2B-25 (TCDS A10SW) - Mitsubishi Heavy Industries Ltd. MU-2B-25 (TCDS A2PC) - Mitsubishi Heavy Industries Ltd. MU-2B-26 (TCDS A10SW) - Mitsubishi Heavy Industries Ltd. MU-2B-26 (TCDS A2PC) - Mitsubishi Heavy Industries Ltd. MU-2B-26A (TCDS A10SW) - Mitsubishi Heavy Industries Ltd. MU-2B-30 (TCDS A2PC) - Mitsubishi Heavy Industries Ltd. MU-2B-35 (TCDS A10SW) - Mitsubishi Heavy Industries Ltd. MU-2B-35 (TCDS A2PC) - Mitsubishi Heavy Industries Ltd. MU-2B-36 (TCDS A10SW) - Mitsubishi Heavy Industries Ltd. MU-2B-36 (TCDS A2PC) - Mitsubishi Heavy Industries Ltd. MU-2B-36A (TCDS A10SW) - Mitsubishi Heavy Industries Ltd. MU-2B-40 (TCDS A10SW) - Mitsubishi Heavy Industries Ltd. MU-2B-60 (TCDS A10SW) ## 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. Part 3 of the CAA Regulations. Description of Type Design Change: Installation of Flight Crew Restraint System on Mitsubishi MU-2B airplanes with Tenryu seats (P/N 037A-91120) in accordance with Master Drawing List MU2-9000, Rev. C, dated August 20, 2003, or with MHI seats (P/N 010A-91101) in accordance with Master Drawing List MU2- 9000M, Rev. B, dated August 19, 2003, or later FAA approved revision. Limitations and Conditions: Compatibility of this design change with previously approved modifications must be determined by the installer. 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. Mitsubishi Heavy Industries, LTD. Licensee: Mitsubishi Heavy Industries America, Inc. 4951 Airport Parkway, Suite 800 Addison, TX 75001 A10SW and A2PC Make : Mitsubishi Model : MU-2B, MU-2B-10, -15, -20, -25, -26, -26A, -30, -35, - 36, -36A, -40, and -60 Date of application: September 11, 1973 Date of issuance : October 30, 1973 Date reissued: 3/13/1986; 8/17/1999; 1/19/2001; 7/1/2008 Date amended: 3/29/1977; 10/16/2003 Rev. 3 ( Signature) Michele M. Owsley Manager, Airplane Certification Office, Southwest Region (Title) SA1923AC-A ADM - 150 FAA Form 8110-2-1(10-69) Page 2 of 2 ## Every issue (1) - July 1, 2008: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/e7/50/e75052015296468b61636a4d7ecd0a7c0daac7b20f69f03969e4e873b4427a25) --- From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.