Modifications completed prior to January 31, 2007: Installation of Honeywell engine Model LTS 101-600A-3A, in accordance with Soloy Document EHDA-199-B, Revision 1, dated February 16, 2005, and maintained in accordance with Maintenance Manual Supplement EHDA-197-B Revision 2, dated February 18, 2005, or later FAA approved revision. Modifications completed after to January 31, 2007: Installation of Honeywell LTS101-600A-3A engine, in accordance with Soloy Master Drawing List 920-100, Revision N/C, dated February 28, 2007, or later FAA approved revisions, and maintained in accordance with Maintenance Manual Supplement S2042H, Revision 0, dated December 4, 2006, or later FAA approved revisions.
Modifications completed prior to January 31, 2007: Installation of Honeywell engine Model LTS 101-600A-3A, in accordance with Soloy Document EHDA-199-B, Revision 1, dated February 16, 2005, and maintained in accordance with Maintenance Manual Supplement EHDA-197-B Revision 2, dated February 18, 2005, or later FAA approved revision. Modifications completed after to January 31, 2007: Installation of Honeywell LTS101-600A-3A engine, in accordance with Soloy Master Drawing List 920-100, Revision N/C, dated February 28, 2007, or later FAA approved revisions, and maintained in accordance with Maintenance Manual Supplement S2042H, Revision 0, dated December 4, 2006, or later FAA approved revisions.
Please contact modification supplier for further details.
STC Status: Amended
STC Date: 05/04/11
Responsible Office: Seattle Aircraft Certification Office (ANM-100S), Tel: (425) 917-6400
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