STC SA5346SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
October 10, 1984
Applied
September 2, 1984
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDSA13CE

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 single axis automatic flight guidance system, Model ST-240.

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 £tatu of ammea Bepartmcnt of transportation —federal 3toiation administration Supplemental Ttgpe Certificate SA5346SW-D Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 jn nae-A-n &^ £3 4>£.&ie Air faAi tai A 1 3 C E CESSNA 111, 177A AND 177B <3ruinj&e' .

Installation of S-TEC System 60 Single Axis Automatic Flight Guidance System, Model ST-240, according to Bulletin No, 340, dated 8-31-84 and Master Drawing List No. 92289, dated 8-31-84 and/or later FAA Approved revisions of the above data (14 Volt System).

1. FAA Approved Supplemental Flight Manual, P/N 89520, dated 10-10-84 is required for Cessna Models 177, 177A and 177B, S/N 17702313 and Below and/or later FAA Approved revisions of the above supplement.

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

9-02-84 10~10-84 SijtdrniniA&id&r-MfJ/ie' (Signature) Harold W. Holdeman DAS Staff Coordinator. DAS 5 SU___

This certiftcati may be transferred in accordant with FAR 21.47.

FAA Fo«« SM0-2(10-48)

United &tatts of amrrira Btpartmtnt of transportation — Jfedcral SOiation administration Supplemental t^pe Certificate(Continuation £heet) SA5346SW-D Limitations and Conditions (con't)

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89521, dated 10-10-84 is required for Cessna Model 177B, S/N 17702314 through S/N 17702672 and/or later FAA Approved revisions of the above supplement,

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

!• , ,:.''- i:i!:-iri nj this (trtificate is punishable by a fine nj not exct'-hnv SIJ/OO, or im^i'.-ir.ritr.' nut exaedins, 3 \f<in, "' '"'/'' ' A.- roRM aiio-2.1 (10-69) 7/i,j certificate ma-, be iran*Jt"tJ in accordance ittth IM< -I I ' PAGE 2 OF 2

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number _ to (Name of transferee) (Address of transferee) (Number and street) (City, Slate, and ^IP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and ZIP 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 · 3

MakeModelData sheet
Cessna Aircraft Company177A13CE
Cessna Aircraft Company177AA13CE
Cessna Aircraft Company177BA13CE