STC SA5243SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
November 28, 1983
Applied
October 19, 1983
Product
Aircraft · Small Multi-Engine
Certification basis
Part 1, Part 21
Data sheet
TCDSA29CE

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of S-TEC System, 40/50 single and two axis automatic flight guidance systems Model ST-219-40/50.

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 Starts of anmca Btpartment of transportation —jfderal atriation administration Supplemental 'Cgpe Certificate SA5243SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex :

Mineral Wells, TX 76067 \.Jevru/,cf>n£u£*>nA &^4cj£edAe*e*>n-*n4^jA**i4*wf>v>^^ 23 ^J&v Federal Aviation isf&2A&c&&f>nA,, A£ :? L t BEECH 76 Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems, Model ST-219-40/50, according to Bulletin No. 319, dated 9-13-83 and Master Drawing List No. 92246, dated 9-13-83 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 89340, dated 11-28-83 is required for S-TEC System 40 and/or later FAA Approved revisions of the above supplement.

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

"Aj sM*~*j*i'A *, 44 /(r/t/r'ft^^sS jiy, M* ££dmvrUjlJr<l/&r-MjSl» 10-19-83 11-28-83 (Signature) Harold W. Holdeman DAS Staff Coordinator. DAS 5 SW (TitU)

TAit certificate may bt traufrmc in tenrtotttt with FAR 21.47.

FAA tavi II1O-2 (1O-6*1

•Hnitrfl &tatu of SLmcrica Bepartmtnt of ^Transportation— federal atriation administration Supplemental t:jjpe Certificate(Continuation £heet) SA5243SW-D Limitations and Conditions (con't)

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89341, dated 11-28-83, is required for S-TEC System 50, and/or later FAA Approved revisions of the above supplement.

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

FAA FORM 8110-2-1 (IO-69) This certificate may be tranrj'crred in acemdanrt with FAR i'1.47.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number .

to (Name of transferee).

(Address of transferee). (Number and street) (City, State, and Z.IP code) from (Name of grantor) (Print or type).

(Address of grantor) (Number and street) (City, State, and ^IP code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

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

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 1

MakeModelData sheet
Beechcraft Corporation76A29CE