# STC SA5347SW-D

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: S-TEC Corporation
- Description: Installation of S-TEC System 60 single axis automatic flight guidance system, Model ST-240.
- Status date: October 10, 1984
- Data sheets: A20CE
- Certificate PDF: https://openairdocs.org/files/sha256/65/c4/65c48edf1c66b869c05cb638e449e9a810d39caf0e78f15ec81c1f5e5687efe1
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6B372F4EBF0DA75F85256CC200122888.0001
- Page: https://openairdocs.org/stc/SA5347SW-D

## ADs that name it

None.

## Approved models (1)

- Cessna Aircraft Company 177RG (TCDS A20CE)

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

Uiritrd £tatrs of ararrica department of transportation — ^federal 2toiation administration Supplemental l^pe Certificate tyKttrrvv&r SA5347SW-D

- S-TEC Corporation Rt. 4, Bldg, 946 Wolters Industrial Complex Mineral Wells, TX 76067 eaM*/r*r 23 4& /&e. Air A20CE JtaA»: CESSNA 177RG &i&n ~lsia-nja« :

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 89522, dated 10-10-84 is required for Cessna Model 177RG, S/N 177RG0787 and Below and/or later FAA Approved revisions of the above supplement.

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

9-2-84 10-10-84 <&r^n4>n&l^^ (Signature) Harold W. Holdeman DAS Staff Coordinator, DAS5 SU _-^__ This certificate "vi> h.- fa«.;ftrrtJ in lumrdanct with FAR 21.47.

fX' FO--I 31 10-2 (IO-68)

tlnittd £tatts of SLrnmra Bcpartment of Transportation—federal atriation administration 3upplemtntal *Cgpt Certificate(Continuation £heet) SA5347SW-D Limitations and Conditions (con't)

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89523, dated 10-10-84 is required for Cessna Model 177RG, S/N 177RG0788 through S/N 177RG1266 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.

:' ,:ri af this itrtifefate is punishable by a fine of not exceeding SI. 000, or impTitanmen'. nut exceeding J yenn, <•' ''•• ai 10-2.1 (10-69) 7 An cntificate n::n V Ir-i-^'errfJ in atc->rJ,inci mil: i'AU .7 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 QP 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):

## Every issue (1)

- October 10, 1984: Issued, Current. [certificate](https://openairdocs.org/files/sha256/65/c4/65c48edf1c66b869c05cb638e449e9a810d39caf0e78f15ec81c1f5e5687efe1)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.