STC SA4197SW

United $tatu of amenta Bepartment of transportation—jfeieral aviation administration Supplemental "Cuje Certificate SA4197SU S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 ^JwJy^deAt^w.f^^fofittcu'ts^/iw^^ 3 ^J&& Civil Air i/l&zttfa&vnfr.

: 3A13 : Cessna 182P, 182r Installation of S-TEC System 60 Two Axis Flight Guidance System, Model ST-011 with Optional Autotrim System, according to Bulletin No. Ill, Revision 3, dated 7-18-81 and Master Drawing List No. 9216, Revision C, dated 7-18-81 with Optional Flight Director Steering Horizon according to Bulletin No. 120, dated 6-02-80 and Master Drawing List No. 9209, dated 6-02-80, or later FAA approved revision. (14 Volt System) See Continuation Sheet, page 2 of this STC.

>^,<^^ ^w August 18, 1980 ^~^«~/ 5/14/81; 9/9/81 Revision 2 September 9, 1980 L/***,,,*,,*/*/:

(Signatur/7 P. Watson Chief, Engineering and Manufacturing Branch (Title) ~~~

ttnftti £tatts of amtrica Btpartment of transportation— federal aviation administration Supplemental ICgpe Certificate(Continuation Revision 2 Limitations and Conditions:

1. FAA Approved Supplemental Flight Manual P/N 8912 dated 9/9/80 is required with S-TEC System 60 Two Axis Automatic Flight Control System Model ST-011.

2. FAA Approved Supplemental Flight Manual P/N 8912-1 dated 5/14/81 is required with S-TEC System 60 Two Axis Automatic Flight Control System Model ST-011 with or without optional Autotrim System;

or FAA Approved Supplemental Flight Manual P/N 8912-2 dated 9-9-81 is required for Cessna Model 182P and Cessna Model 182$, S/N 18266590 and BELC&7 with S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-011, with or without optional Autotrim System;

or Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement P/N 8973 dated 9-9-81 is required for Cessna Model 182q, S/N 18266591 and UP with S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-011, with or without optional Autotrim System.

3. Compatibility of this modification with other previously approved modifications must be determined by the installer.

FAA FORM 8HO-2-I (10-69) PAGE 2 OF

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