STC SA7813SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
April 21, 1992
Applied
March 31, 1992
Product
Aircraft · Small Multi-Engine
Certification basis
Part 21
Data sheet
TCDS3A10

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 65 two axis automatic flight guidance system, model ST-408.

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.

Btpartnot of Transportation—jfotaal atnation administration Supplemental t^pe Certificate i/uwnvei*'SA7813SW-D % imffifl.fr iiuin.iV, S-TEC Corporation 946 Pegram Welters Industrial Park Mineral Wells, Texas 76067

y.^^^^^&#»t*iy^>«nrf£« ClVll Air 3A10 Cessna 310D, 310E, 310F, 310G, and 310H Installation of S-TEC System 65 Two Axis Automatic Flight Guidance System, Model ST-408, according to Bulletin No. 508, dated 3-30-92 and Master Drawing List No.

92559, dated 3-30-92 and/or later FAA Approved revisions of the above data.

1. Also eligible on Models 310G and 310H When Modified Per STC SA412SO (300 H.P.

Colemill Conversion).

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

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3-31-92 4-21-92 William J. Thomas DAS Staff Coordinator, DAS 5 SW Any alteration ofthit certificate is punishable by a fine of not exceeding SI ,000, or imprisonment not exceeding 3 years, or both.

Ttiu crrtijualt nay Or traruferrtd in ucmdana with FAR 21.47.

FAAFo*»«l!O-l( IO-MI

ttmod £cua «f 3nmn Btpartment of Transportation— federal atiation administration Supplemental ICgpt Certificate(Continuation £hett) SA7813SW-D

2. FAA/DAS Approved Supplemental Flight Manual, P/N 89964, dated 4-21-92 is required for Cessna Models 310D, 310E, 310F, 310G, and 310H and Models 310G and 310H When Modified Per STC SA412SO (300 H.P. Colemill Conversion) and/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.

.I'M alteration of this certificate is punishable by afint af not exceeding SI,OOP, or imprisonment not exceeding 3 years, or hnih.

FAA FORM ano.2.) (10-81) Tint ttrtiftati may at Umiftrrtd in accordant! with I'AK .'/.•/'*.

dumber and street ) ( C.ilv. Slate, and ^IT 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 · 5

MakeModelData sheet
The Cessna Aircraft Company310D3A10
The Cessna Aircraft Company310E (USAF U-3B)3A10
The Cessna Aircraft Company310F3A10
The Cessna Aircraft Company310G3A10
The Cessna Aircraft Company310H3A10