What it approves
Installation of S-TEC System 60 two axis automatic flight guidance system model ST-080 with optional automatic electric trim
What the certificate saysOCR
This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA511954-D This certificate issued to: 1. S-TEC Corporation Rt. 4, Blag. 946 Wolters Industrial Complex Mineral Wells, TX 76067 Part 3 of the CiVil Air Kegulations.
Original Product - Type tientificate Numben: ЗА16 Make: ВЕЕСН Model: 58 AND 58A Description of Type Design Change:
Installation of S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-080, with Optional Automatic Electric Trim System according to Bulletin No.
183, Revision 8, dated 5-01-86 and Master Drawing List No. 9295, Revision H, dated 5-01-86 with Optional Flight Director Steering Horizon and/or later FAA Approved revisions of the above data (28 Volt System).
1. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89109-1, dated 11-8-82 is required and/or later FAA Approved revisions of the above supplement.
(See Continuation Sheet, Page 2, a part of this STC.)
Date of Application: 10-05-82 Date Reissued: 4-26-83, 5-31-84, 6-26-84, 5-08-86, Revision 4 Date of Issuance: 11-08-82 Date Amended:
FEDERAL AVIATION By Direction of the Administrator (Signature) DINIS TRATOR DAS Staff Coordinator, DAS 5 SW Harold W. Holdeman
47.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA51195W-D, Revision 4 Limitations and Conditions: (con't)
2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89109-2, dated 6-26-84 is required 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 89109-3, dated 5-08-86 is required 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.
47.
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