Installation of an engine inlet mounting enhancement to increase the mounting flange service life in accordance with Fairchild Aircraft Inc. Drawing No. SATA716G0001, Rev. IR dated 05/19/2000, including Engineering Order A-2 dated 07/30/2001, or later FAA approved revision.

Installation of a corporate/executive interior in accordance with Fairchild Aircraft Incorporated Engineering Change Package (ECP) 3000, Revision AN, dated 8/26/1999, or later FAA approved revision.