STC SA5295SW-D

*aniced Scaces of Slamerica Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA5295SW-D This certificate issued to: S-TEC Corporation Rt. 4, Blag. 946 Wolters Industrial Complex Mineral Wells, TX 76067 Part 3 of the CIVIl Air Regulations.

Original Product -Type tentificate Number: SAb Make: CESSNA Model: 180K Description of Type Design Change:

Installation of S-TEC System 60 Single Axis Automtic Flight Guidance System Model ST-028, according to Bulletin No. 131, Revision 2, dated 11-28-83 and Master Drawing List No. 9227, Revision B, dated 11-28-83 and/or later FAA Approved revisions of the above data, (28 Volt System).

1. Eligible on the above model when modified per STC SA1705WE (Internal Tip Tanks) and/or STC SA1435WE (Robertson STOL) Landplane or Floatplane.

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

Date of Application: 12-29-83 Dato missued:

Date of Issuance: . 4-2-84 Date Amended:

FEDERAL AVIATION By Direction of the Administrator Hall No. Itlden (Signature) TOMINIST ALO DAS Staff Coordinator, DAS 5 SW Harold W. Holdeman (Title)

17.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) SA5295SW-D Number Limitations and Conditions: (con't) FAA Approved Supplemental Flight Manual, P/N 8928-1, dated 4-2-84 is required for Cessna Model 180K S/N 18053000 and below and the above model when modified per STC SA1705WE (Internal Tip Tanks) and/or STC SA1435WE (Robertson STOL) Landplane or Floatplane, and/or later FAA Approved revisions of the above supplement.

3. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 8932-1, dated 4-2-84 is required for Cessna Model 180K S/N 18053001 and on the above model when modified per STC SA1705WE (Internal Tip Tanks) and/or STC SA1435WE (Robertson STOL) Landplane or Floatplane, and/or later FAA Approved revisions of the above supplement.

4. Compatability of this modification with other previously approved modifications must be determined by the installer.

FAA FORM 8110-2. 1 (10-69)

PAGEZ OF LPAGES

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U.S. GOVERNMENT PRINTING OFFICE : 1966 OF ~205-579