# STC SA2381SW - Type: Supplemental type certificate - Status: Current, Issued - Holder: Dodd Engr & Welding - Description: Modify of main landing gear assembly, P/N 250-040-451, by addition of gussets at intersection of drag brace and main leg. - Status date: November 15, 1976 - Data sheets: 1A8, 1A8, 1A8, 1A8 - Certificate PDF: https://openairdocs.org/files/sha256/ed/1b/ed1b6db6686f46f0839ec30ca213c6282328675c95446b8ac9513c4acfaa8fab - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/537C236435A3E61685256CC200015D7B.0001 - Page: https://openairdocs.org/stc/SA2381SW ## ADs that name it None. ## Approved models (4) - Helio Aircraft LLC H-250 (TCDS 1A8) - Helio Aircraft LLC H-295 (USAF U10D) (TCDS 1A8) - Helio Aircraft LLC H-395 (USAF L-28A or U-10B) (TCDS 1A8) - Helio Aircraft LLC H-395A (TCDS 1A8) ## 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. United JSmti af anmca Bepartmtnt of Iransportadon -federal atoiadon administration Supplemental TCpe Certificate SA2381SW Project A3508SW-DS MGM-212 Dodd Engineering & Welding Co. 3302 N. Lewis Tulsa, Oklahoma CiVll Air ^^If-aa^a^ifnA'. 'kiuirtjtl ,~%cduf£ —— • Jyfe'l^r&^ifaJt-^'lu-rrdvr 1A8 Helio H-250, H-295, H-395, H-395A ; Modify ^ain ianding sear assembly P/N 250-040-451 by addition of gussets at intersection of drag brace and main leg according to Drawing DW-451 dated July 20, 1976, and Dodd Process Specification Revision A "ited August 10, 1976) or later FAA approved revision. ^WT?/^^^ .tXt/rritniadra/i'r