What it approves
Installation of S-TEC system 60 pitch stabilization system, model ST-054 with optional autotrim system
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 £tatts of amtrica Bepartment of transportation—jfederal 2toiation administration Supplemental t^gpe Certificate SA4416SW i-flecttifa^ion^.
Gr*ai>nsa/ tJrveUtet —— S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 -<^^/k^^ Civil Air Beech S35, V35, V35A, V35B and these models when modified by STC SA1035WE (Turbocharged Engine) -— Installation of S-TEC System 60 Pitch Stabilization System, Model ST-054 with optional Autotrim System, according to Bulletin No. 157, dated 5/18/81 and Master Drawing List No. 9251, dated 5/18/81, or later FAA approved revision.
(14 Volt System)
1. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement P/N 8954 dated 7/15/81 is required with or without airplanes modified per STC SA1035WE with S-TEC System 60 Pitch Stabilization System Model ST-054.
2. Compatibility of this modification with other previously approved _ modifications must be determined by the installer.
^ -w May 19, 1981 July 15, 1981 _Sjfdf rv&ldtfssf :
_/ 4>& ftt/tSttSI*t/' {Signature) P. Watson Chief, Engineering and Manufacturing Branch(Title)————————————————————
FAA FOIM 81 10-2 (10-68)
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.