STC SA5195SW-D

SStsta Btpartracnt of transportation— Jfttaal atriation administration Supplemental "Cgpc Certificate iSUMrwet*'SA5195SW-D S-TEC Corporation 946 Pegram Mineral Wells, Texas 76067 ^ ,^ rtyr.iJWTH.Md ^^P/ 3 y^ Civil Air 3A12 CESSNA 172M AND 172N Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems, Model ST-183-40/50, according to Bulletin No. 283, Revision 2, dated 8-12-94 and Master Drawing List No. 92211, Revision B, dated 8-12-94 or later FAA Approved revisions of the above data (14 Volt System).

1. Also eligible on Models 172M and 172N When Modified By 180 H.P. Engine Conversion.

2. FAA Approved Supplemental Flight Manual, P/N 89242, dated 8-17-83 is required for S-TEC System 40 or later FAA Approved revisions of the above supplement.

(See Continuation Sheet, Page 2, a part of this STC.)

&~,: 7-29-83 8-17-83 : 5-08-84, 8-22-94, 10-17-94 ' Revision 3 William T. Thomas DAS Staff Coordinator, DAS 5 SW (Title)

TAu artificate may Ar troruferrtd in tccvrJantt milk FAR 21.17.f AA KM * 110-1 (!»-«•)

ttrarrd Scans of 3amra Bepartmcnt of transportation— jf edcral 9LQiacion administration Supplemental t:gpe Certificate(Continuation £heet) SA5195SW-D, Revision 3 Limitations and Conditions (con't.)

3. FAA Approved Supplemental Flight Manual, P/N 89242-1, dated 5-08-84 is required for Cessna Model 172M for S-TEC System 40 or later FAA Approved revisions of the above supplement.

4. FAA Approved Supplemental Flight Manual, P/N 89242-2, dated 8-22-94 is required for Cessna Model 172M And The Above Model When Modified By 180 H.P. Engine Conversion for S-TEC 'System 40 or later FAA Approved revisions of the above supplement.

5. FAA Approved Supplemental Flight Manual, P/N 89243, dated 8-17-83 is required for S-TEC System 50 or later FAA Approved revisions of the above supplement.

6. FAA Approved Supplemental Flight Manual, P/N 89243-1, dated 5-08-84 is required for Cessna Model 172M for S-TEC System 50 or later FAA Approved revisions of the above supplement.

7. FAA Approved Supplemental Flight Manual, P/N 89243-2, dated 8-22-94 is required for Cessna Model 172M And The Above Model When Modified By 180 H.P. Engine Conversion for S-TEC System 50 or later FAA Approved revisions of the above supplement.

8. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89464, dated 5-08-84 is required for Cessna Model 172N for S-TEC System 40 or later FAA Approved revisions of the above supplement.

9. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89464-1, dated 8-22-94 is required for Cessna Model 172N And The Above Model When Modified By 180 H.P. Engine Conversion for S-TEC System 40 or later FAA Approved revisions of the above supplement.

10. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89465, dated 5-08-84 is required for Cessna Model 172N for S-TEC System 50 or later FAA Approved revisions of the above supplement.

11. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89465-1, dated 8-22-94 is required for Cessna Model 172N And The Above Model When Modified By 180 H.P. Engine Conversion for S-TEC System 50 or later FAA Approved revisions of the above supplement.

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

.I'D alteration of this certificate is punishable by a Jim of not exceeding 11,000, or imprisonment not exceeding 3 years, or hn/h.

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