STC SA6078SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Amended
Status date
April 17, 1998
Applied
September 3, 1986
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDSA1CE

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of S-TEC system 65 two axis automatic flight guidance system, Model ST-371.

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.

fatea/fo 3Hnttc& plates ©f of (Her ttf teats SA6078SW-D S-TEC Corporation One S-TEC Way Mineral Wells Municipal Airport Mineral Wells, TX 76067-9236 A ICE BEECH C23 AND C24R Installation of S-TEC System 65 Two Axis Automatic Flight Guidance System, Model ST-371, according to Bulletin No. 471, Revision 1, dated 4-15-98 and Master Drawing List No. 92386, Revision A, dated 4-15-98 with Optional Flight Director/Steering Horizon or later FAA Approved revisions of the above data (28 Volt System).

1. FAA Approved Supplemental Flight Manual, P/N 89684, dated 9-17-86 is required for Beech Model C23 or later FAA Approved revisions of the above supplement.

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

If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

a/tt/dd* <ltf/yn?l6f/t.p affftif (ft/ltf/t a) ttiv dai4/& /til / ei a; fattti&tadieti da fa tii c/a/t/^wfatt ; 9-03-86 .• 9-17-86

e)f eflpf/!' ftsi/t/ 4-17-98, Revision 1 Stfp deies-tic/i ey William J. Thomas DAS Staff Coordinator, DAS 5 SW (Title)

•IHmteb: ^tatca (0f of tEranspnrlatttm - ,3fcfreral ^frtalttm JVhmmtstraiton (Eerttftcate ((Emttmuatitm J^fyeet)

t./t iWMwfo SA6078SW-D, Revision 1 Limitations and Conditions (con't.)

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89685, dated 9-17-86 is required for Beech Model C24R or later FAA Approved revisions of the above supplement.

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

1 INSTRUCTIONS: The iranifcr endowment below may be u*d to notify the appropriate FAA Kegion.l Office of the tranifer of thU Supplemental Type Certificate.

The FAA will reiuue the certificate in the name of the transferee and forward it to him.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee).

(Address of transferee). I.,Vum*<r tnd Oral) from (Name of grantor) (Print or type).

(Address of grantor) tlrulj Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

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 · 2

MakeModelData sheet
Beechcraft CorporationC23A1CE
Beechcraft CorporationC24RA1CE