STC SA5392SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Reissued
Status date
December 4, 1985
Applied
May 14, 1985
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS2A3

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 60 two axis automatic flight guidance system, Model ST-319, with optional automatic electric trim 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.

Unfed &tatu of amrrica Bcpartmtnt of Transportation — Jpcdtral atriation administration Supplemental t^ipe Certificate tSbwmwr' SA5392SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 'm4^^&t ' * i> 4f /n* Li VI I Air ia*n& ZJroitc —— •'Tute ficaf^/lumt^ 2 A3 MOONEY M20K ^/^eAfv<fi&(*n, jy^/yiA* -J ^e&i&n 'Ofut'ruxe' :

Installation of S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-319, with Optional Automatic Electric Trim System, according to Bulletin No.

419, Revision 1, dated 9-19-85 and Master Drawing List No. 92326, Revision A, datad 9-19-85 with Optional Flight Director Steering Horizon 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 89602, dated 5-31-85 is required and/or later FAA Approved revisions of the above supplement.

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

5-14-85 ^ut^Li-^.- 12-04-85, Revision 1 ~&^£c- 4f*4L (Signature} Harold W. Holdeman DAS Staff Coordinator, DAS 5 SH (Title)

Tkii crrtificalt may kt IraniftmJ in tccorjana with FAR 21.47.

UA Fow> I110-3 (IO-Ai|

£tatu of Bcpartmcnt of Transportation— federal atriation administration 3upplementali:jipe Certificate(Continuation gheet) SA5392SW-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 89602-1, dated 12-04-85 is required 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.

. I':; .litr-ratiim of this certificate is punishable by a fint oj nnt exceeding SI,000, or imprisonment not exceeding 3 veari. "' A.I ' AA f ORM 8110-2-1 (10-69) This certificate may be transferred in accordance with l-~.-\H -'/ • PAGE 2 OF 2 PAGES

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number .

to (Name of transferee) (Address of transferee) (Number and street) (City, State, and ^JP 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):

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
Mooney International CorporationM20K2A3