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.

Please contact modification supplier for further details.

STC Status: Reissued
STC Date: 04/06/04
Responsible Office: Ft. Worth Airplane Certification Office (ASW-150), Tel: (817) 222-5150

Dornier Luftfahrt GmbH

• 328-100