# STC SA5182SW-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: S-TEC Corporation, United States
- Description: Installation of S-TEC System 60 pitch stabilizer system Model ST-065 with optional automatic electric trim system.
- Applied: April 28, 1983
- Status date: February 16, 1994
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS 5A3](https://openairdocs.org/tcds/5A3)
- Certificate PDF: https://openairdocs.org/files/sha256/ef/90/ef9045e911c7b202860b02868e4b875fdfba375a6eaf788fa262b1497f7cf608
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8EF82B07F70E9FB986257EC80068AB96.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA5182SW-D

## ADs that name it (0)

None.

## Approved models (2)

- Beechcraft Corporation A45 (Military T-34A; B-45) ([TCDS 5A3](https://openairdocs.org/tcds/5A3))
- Beechcraft Corporation D45 (Military T-34B) ([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.

Btpartmnit of Transportation—federal atriation administration Supplemental "Cgpt Certificate SA5182SW-D S-TEC Corporation 946 Pegram Wolters Industrial Park Mineral Wells, Texas 76067 J»»H5^i^.<5t^^^.o»i«»«i*-t»v,^t.*-<^4»J<z^ \^ J%^^Li**ux>r&j*i£^**e^u4ir*Tnen&jafC%»r£ Civil Air ifatim 5A3 BEECH A45 (T-34A) and D45 (T-34B) Installation of S-TEC System 60 Pitch Stabilization System, Model ST-065, with Optional Automatic Electric Trim System, according to Bulletin No. 168, Revision 2, dated 1-24-94 and Master Drawing List No. 9277, Revision B, dated 1-24-94 or later FAA Approved revisions of the above data (28 Volt System).

1. Also eligible on Beech Models A45 (T-34A) and D45 (T-34B) When Modified By STC SA1450SW or STC SA1864SW (Installation of 285 H.P. Engine).

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

•~<M^^*r*ZL/&<^-^in&J^^y^for£rt^J^^ £Zc/mintt 4-28-83 7-15-83 : 2-16-94, Revision 1 WilTTam 3. Thomas DAS Staff Coordinator, DAS 5 SW (Title)

This tertijuatt may tt IraiafrrrtJ in acnraana with FAR 21.17.

f AA FOM> 111»-1 (10-*«|

ttnurd Starts of GUnmra ©eparrmcnt of Transportation— .federal aoiation administration Supplemental ITgpe Certificate(Continuation 3heet) SA5182SW-D, Revision 1 Limitations and Conditions (con't.)

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 8987-1, dated 7-15-83 is required for Beech Models A45 (T-34A) and D45 (T-34B) And The Above Models When Modified By STC SA1450SW (Installation of 285 H.P. Engine) or later FAA Approved revisions of the above supplement.

3. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 8987-2, dated 2-16-94 is required for Beech Models A45 (T-34A) and D45 (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.

4. Compatibility of this modification with other previously approved modifications must be determined by the installer.

alifTittiun of this certificate is punishable by a fine of not exceeding 11,000, or imprisonment not exceeding 3 years, or h<>/h.

FORM 8HO-Z-1 (lo-6») THit ctrtifcatt may bi tram/and in accordant! witk FAR .'/.•/" 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, Stale, and <7P 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):

U.S. GOVERNMENT PRINTING OFFICE : 1966 OF —205-579

## Every issue (1)

- February 16, 1994: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/ef/90/ef9045e911c7b202860b02868e4b875fdfba375a6eaf788fa262b1497f7cf608)

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