What it approves
Modify of main landing gear assembly, P/N 250-040-451, by addition of gussets at intersection of drag brace and main leg.
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may 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 <f &f June 10, 1976 &„& November 15, 1976 , :«. - 5fa* i *)/<{$* ., (Signature) r^Don P. Watson Chief, Engineering and Manufacturing Branch (Tttle l Any alteration of thit certificate u punishable by a fine of not exceeding SI,000, or imprisonment nnt exceeding 3yrars, or both.
This certi/tiate may br trni5/r"rrl tn affoidartte iwth h'AH 21 *7
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.