What it approves
Installation of S-TEC system 60 pitch stabilization system Model ST-047 with optional autotrim system
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 States or Zlmmca Bcpartment of transportation federal aviation administration Supplemental l^gpe Certificate iSl&nttta&o-nA'.
SA4389SW S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 v-£foJyfadefa:pwfi^J^^(>&c>urt<^/ircic^^
• 4&e'Mivw(rr£njsneAA//> Civil Air 3 A 13 Cessna 182P, 182Q : Installation of S-TEC System 60 Pitch Stabilization System, Model ST-047 with Optional Autotrim System according to Bulletin No. 150, Revision 1, dated 7-18-81 and Master Drawing List No. 9262, Revision A, dated 7-18-81, or later FAA approved revision. (14 Voit System) gee Continuation Sheet, page 2 of this STC.
{ 27, 1981 June 19, 1981 October 2, 1981 Revision 1 ar at/if f (Signature) Don P. Watson Chief, Engineering and Manufacturing Branch (Title)
FAA FOKM 81 10-2(10-68)
United grata of arnica Bepattment of transportation— federal 3lOiation administration upplemental tigpe Certificate(Continuation £hect) SA4389SW Revision 1 Limitations and Conditions:
1. FAA Approved Supplemental Flight Manual P/N 8960 dated June 19, 1981, or FAA Approved Supplemental Flight Manual P/N 8960-1 dated October 2, 1981, is required for Cessna Model 182P and Cessna Model 182Q, S/N 18266590 and BELOW.
2. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement P/N 8975 dated October 2, 1981, is required for Cessna Model 182Q, S/N 18266591 and UP.
3. Compatibility of this modification with other previously approved modifications must be determined by the installer.
FAA FORM 8HO-2-1 (10-69) This certificate may he transferred in accordance with FAR 21.47.
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ADs that name this STC · 0
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