What it approves
Installation of S-TEC system 60 single axis flight guidance system, Model ST-012
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 £tatu of America Bepartment of 'Cransportation— federal atnation administration Supplemental 'Cgpe Certificate SA4244SW S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067W^<!^^^ ^ 3 s^J&e< Civil Air
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3A12 Cessna 172N, 172P installation of S-TEC System 60 Single Axis Flight Guidance System, Model ST-012, according to Bulletin No. 112, Revision 2, dated 8-10-81 and Master Drawing List No. 9225, Revision B, dated 8-10-81, or later FAA approved revision. (28 Volt System) gee continuation Sheet, page 2 of this STC, n/ vrvMfefl ' November 3, 1980 ^«6 ^^«^/. 3/6/81; 9/18/81Revision 2 December 11, 1980 -/atearnftu/u/:
•siu'Jatr€f/<i' ^^ ^^ _ (Signal) . Watson Chief, Engineering and Manufacturing Branch (Title)
FAA font 8 1 1 0-2 ( 1 0-68)
ttnited grata of amtrira Bepartmtnt of tensportation— federal Nation administration Supplemental Ttgpe Certificate(Continuation &heet) SA4244SW Revision 2 Limitations and Conditions :
1. FAA Approved Supplemental Flight Manual P/N 8922, dated 12-11-80 is required for Cessna Model 172N or FAA Approved Supplemental Flight Manual P/N 8922-1 dated March 6, 1981, is required for Cessna Model 172N, S/N 17271034 and BELOW.
2. Pilot1, s Operating Handbook and FAA Approved Airplane Flight Manual Supplement P/N 8942 dated March 6, 1981, is required for Cessna Model 172N, S/N 17271035 and UP and Cessna Model 172P.
3. Compatibility of this modification with other previously approved modifications must be determined by the installer.
FAA FORM 8110-2-1 (1O-69) This certificate may bt transferred in accordance with FAR 21.47.
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.