What it approves
Installation of S-TEC system 60 pitch stabilization system, model ST-040 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.
ttnittd $tatt> of America Bepartment of transportation—federal atriation administration Supplemental t^pe Certificate SA4419SW t-St&gu&ia&e-nA/.
Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 ,^,^^^ 3 Civil Air 3A21 Cessna 210L, T210L, 210M, T210M, 210N, T210N : Installation of S-TEC System 60 Pitch Stabilization System, Model ST-040 with optional Autotrim System according to Bulletin No. 143, dated 5/4/81 and Master Drawing List No. 9248, dated 5/4/81, or later FAA approved revision. (28 Volt ystem)
1. Supplemental Tlight Manual for Cessna Models 210L, T210L, 210M, T210M with S-TEC System 60 Pitch Stabilization System. Model ST-040 (28 Volt System) FAA ApprovedP7N 8949 dated 7/15/81 is required.
2. Pilot's OperatirCessna Models 21Model ST-040 (2i Handbook and FAA Approved Airplane Flight Manual Supplement for$.,T210N with SrTEC System 60 Pitch-Stabilization System,/ilt System) FAA Apprbved P/N 8950 dated 7/I5/8I is^7required.
3. Compatibility of this modification with other previously approved modifications must be determined by the installer.
'<CLattt-Mt/i4Cri' 4>&.trl€>.*<aA4A. ^<sr'<aJiSw<t'UtivAfL4i//'fe<rrLiM'->n' vrf^Jjfef/^tvn/wAij/p* da/e'A&'j/l/wmst&e'^A /ad/iAAedd'Us 4h&, 9tc/?fn'riiA Jra/t-r- d dAe f 1981 July 15, 1981 *>/ £ne •^' .e ^ (Signature ) 5on P. Watson Chief, Engineering and Manufacturing Branch (Title)
FAA Fo«M 8II0-2 (10-68)
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.