STC SA6027SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
July 18, 1985
Applied
July 12, 1985
Product
Aircraft · Small Airplane
Certification basis
Part 21
Data sheet
TCDS3A21

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 System, Model ST-310-40/50.

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.

Ulrica! grata of SLmcrica Bepartmcnt of Iransportation — jfcdcral 2toiation administration ^Supplemental 'Cgpe Certificate tSUvrrvvvr' SA6027SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 ria* *n ^n* JuJi^ ea*£VP«rrvem/il'4>fiJa AIT £*r*ia*nji4 J&CCMG/ ^i'X&cvi/t/iurn -Qf<-//yJve—zj CESSNA 210D, 210E, 210F AND T210F Installation of S-TEC System 40/50, Single and Two Axis Automatic Flight Guidance System, Model ST-310-40/50, according to Bulletin No. 410, dated 7-5-85 and Master Drawing List No, 92336, dated 7-5-85 and/or later FAA Approved revisions of the above data (14 Volt System).

1, FAA Approved Supplemental Flight Manual, P/N 89617, dated 7-18-85 is required for S-TEC System 40 in Cessna Models 210D, 210E, 210F and T210F and/or later FAA Approved revisions of the above supplement.

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

^-^n^ ^iA^ ^^jijfy'ii^^M^AA^a^/r^'fnM'n'j^^i^/.u^i^i^-' 7-12-85 7-18-85 jhu/J&e- S&&mi0it&foiz&>*->af;^in4' (Signature) Harold W. Holdeman DAS Staff Coordinator-, DAS 5 SW ~ (Title)

TAif cfTtificatt may In transform! in »u»rJana unth FAR 21.47.

fAA haut •! 1O-J (10-61)

3tatu of 2Lntnca Bepartment of fenaportafton— federal Striation administration Supplemental t:gpe Certificate(Continuation £heet) SA6027SW-D Limitations and Conditions (con't)

2. FAA Approved Supplemental Flight Manual, P/N 89618, dated 7-18-85 is required for S-TEC System 50 in Cessna Models 210D, 210E, 210F and T210F 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, .l';i alteration of /his certificate is punishable by a fine oj not exceeding SI,000, or imprisonment not exceeding 3 years, or b»l^ '-A.\ FORM aiio-2-1 (10-69) This ccrtifitatt may be transferred in accordance with 1'AR .7 -l~ PAGE 2 OF 2 PAGES

1 INSTRUCTIONS: The transfer endoncmcn. below may be used .0 notify the appropriate FAA Kegion.1 Office of the transfer of thU Supplemenul Type Certificate.

The FAA will reissue the certificate in the name of the transferee and forward it lo him.

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

(Address of transferee). ( Mumtxr *nt sttttt > (City, Stole, fitd yP ante / from (Name of grantor) (Print or type).

(Address of grantor) (Xumlm fit* artel/ 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 · 4

MakeModelData sheet
Textron Aviation Inc.210D3A21
Textron Aviation Inc.210E3A21
Textron Aviation Inc.210F3A21
Textron Aviation Inc.T210F3A21