# STC SA4587SW

- 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-013.
- Status date: January 22, 1982
- Data sheets: 5A3, 5A3
- Certificate PDF: https://openairdocs.org/files/sha256/a6/0a/a60a7ec2d77fce9e75de9e58f6c462097de66aad2ba64269089a3bba0683c089
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5F19D05DE7F1E9F885256CC2000E3D55.0001
- Page: https://openairdocs.org/stc/SA4587SW

## ADs that name it

None.

## Approved models (2)

- Beechcraft Corporation A45 (Military T-34A; B-45) (TCDS 5A3)
- Beechcraft Corporation D45 (Military T-34B) (TCDS 5A3)

## 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.

United $tatt* or Bmrrica ©epartment of transportation—federal Htoiadon administradon Supplemental t^pe Certificate SA4587SW Project A5607SW-DSFKP-130 S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 ^<^^/i^xj4l«j?*zy^.<$ie^fe(^*W^^ Civil Air Beech A45 (T-34A) and D45 (T-34B) and these models when modified by STC SA1450SW(285 H.P.Engine) nja*< .' Installation of S-TEC System 60 Single Axis Automatic Flight Guidance System, Model ST-013, according to Bulletin No. 113, dated 10-01-81 and Master Drawing List No. 9276, dated 10-01-81, or later FAA approved revision.

(28 Volt System) — FAA Approved Airplane Flight Manual Supplement, P/N 8986 dated 1-22-82, is required for Beech Models A45 (T-34A) and D45 (T-34B) and the Above Models When Modified by STC SA1450SWlInstalla tion of 285 Iff ,EngincOLwlth S-TEC System60 Single Axis Automatic Flight Guidance System, Model ST-013 Compatibility of this modification with other previously approved modifications must be determined by the Installer.

^ -u< October 28, 1981 January 22, 1982 -J *i _ / a __ P. WatsonActing Chief, Aircraft Certification Division ^^ (Title)

This certificate may be transferred in accordance with FAR 21 AT.

FAA FouM 81 10-2 (10-68)

## Every issue (1)

- January 22, 1982: Issued, Current. [certificate](https://openairdocs.org/files/sha256/a6/0a/a60a7ec2d77fce9e75de9e58f6c462097de66aad2ba64269089a3bba0683c089)

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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.