# STC SA8377SW-D

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: S-TEC Corporation, United States
- Description: Installation of S-TEC System 60 single axis automatic flight guidance system, Model ST-013.
- Applied: December 23, 1993
- Status date: December 30, 1993
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 5A3](https://openairdocs.org/tcds/5A3)
- Certificate PDF: https://openairdocs.org/files/sha256/15/71/1571f16d817438729a47c2f5f0c88dce75baf525af39c8610653151a6d4cc018
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/51949E71323F966B85256CC20058E763.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA8377SW-D

## ADs that name it (0)

None.

## Approved models (2)

- Raytheon Aircraft Company A45 (T-34A) ([TCDS 5A3](https://openairdocs.org/tcds/5A3))
- Raytheon Aircraft Company D45 (T34B) ([TCDS 5A3](https://openairdocs.org/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.

cUBtD Btpartnot of transportation— federal atriation Administration Supplemental "Cgpc Certificate i i<vmi'a«Ji<i»iJ SA8377SW-D S-TEC Corporation 946 Pegram Wolters Industrial Park Mineral Wells, Texas 76067 ClVll Airea*^rarr\ ^ 5 A3 BEECH A45 (T-34A) AND D45 (T-34B) Installation of S-TEC System 60 Single Axis Automatic Flight Guidance System, Model ST-013, according to Bulletin No. 113, Revision 1, dated 12-20-93 and Master Drawing List No. 9276, Revision A, dated 12-20-93 (28 Volt System).

1. Also eligible on the above models when modified by STC SA1450SW or STC SA1864SW (Installation of 285 H.P. Engine).

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

V^A^J0aA^f^*aJttAr<^-a44Aji//*t*'rn*aj^j^*jy*{;£i4n&/* SXamini&Jra&rr- of ZAt 12-23-93 12-30-93 Wi11iam J. Thomas DAS Staff Coordinator. DAS 5 SW(Title) Any alteration of t hit urtificalt it punishable by a fine of not exceeding tl ,000, or imprisonment not exceeding 3 years, or both.

Tka urti/uaie nay tt ttanifmtd in atntdana u»M FAR 21.17.

» AA r i 1 1 1 0- 1 ( 1 0»«(|

Unitzd Statu of 2ncnn Bepartmcnt of Importation— federal aoiation administration Supplemental ITgpe Certificate(Continuation SA8377SW-D Limitations and Conditions (con't.)

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 8986-1, dated 12-30-93 is required for Beech Models A45 (T-34A) and 045 (T-34B) And The Above Models When Modified By STC SA1450SW or STC SA1864SW (Installation of 285 H.P. Engine) 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.

.!•;•, .aura/tun i>f this certificate is punishable by a fint of not exceeding 11,000, or imprisonment not exceeding J years, nr hni FAA FORM «no.2-l (IO-«») Thll certificati may bt tranifrrrtJ m accordant! with, !•',•[K .'/ PAGE 2 OF 2 PACES

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, 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

## Every issue (1)

- December 30, 1993: Issued, Current. [certificate](https://openairdocs.org/files/sha256/15/71/1571f16d817438729a47c2f5f0c88dce75baf525af39c8610653151a6d4cc018)

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