# STC SA5116SW-D

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: S-TEC Corporation, United States
- Description: Installation of S-TEC System 60 two axis automatic flight guidance system model ST-132 with optional autotrim system.
- Applied: October 26, 1982
- Status date: June 26, 1995
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A17EU](https://openairdocs.org/tcds/A17EU)
- Certificate PDF: https://openairdocs.org/files/sha256/c3/49/c349870757be2adf6b2fa78609186f10ac8ef4bd451a9c7f953453feb4746b61
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F0DD52B5A300A3D785256CC2001226B6.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA5116SW-D

## ADs that name it (0)

None.

## Approved models (8)

- B-N Group Ltd. BN-2A-2 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-20 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-26 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-6 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-8 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2B-20 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2B-26 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2T ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))

## 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.

Btpartranit of transportation— jfdlnal atriation administration Supplemental t^pc Certificate SA5116SW-D «/* S-TEC Corporation 946 Pegram Mineral Wells, TX 76067 t*n 23 Federal Aviation A17EU Britten Norman BN-2A-2, BN-2A-8, BN-2A-20, BN-2A-26, BN-2B-20, BN-2B-26, BN-2T, and BN-2A-6 Installation of S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-132 with Optional Autotrim System according to Bulletin No. 232, Revision 7, dated 6-15-95 and Master Drawing No. 92152, Revision G, dated 6-15-95 with Optional Flight Director/Steering Horizon or later FAA Approved revisions of the above data (28 Volt System).

1. Only eligible on Model BN-2A-6 When Mod. Nos. NB/M/430 and NB/M/631 Are Installed.

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

.-. 10-26-82 11-03-82 ^^^t»,4^ 10-01-90, 6-26-95, Revision 2 William J. Thomas DAS Staff Coordinator. DAS 5 SW (Title)

Tkil trrtificate may *r Irani/errtJ in ttnrmwtt u*tk FAR 21.17.

fAA feM> •! 10-1 (IO-M)

fbtitol 3cata of SUatnta Bepartmait of Transportation— .federal Station administration Supplemental HCgpe Certificate(Continuation £heet) SA5116SW-D, Revision 2 Limitations and Conditions (con't.)

2. FAA Approved Supplement to CAA or FAA Approved Airplane Flight Manual for Britten Norman Model BN-2T, P/N 89168, dated 11-03-82 or later FAA Approved revisions of the above supplement.

3. FAA Approved Supplement to CAA or FAA Approved Airplane Flight Manual for Britten Norman Model BN-2T, P/N 89168-1, dated 10-01-90 or later FAA Approved revisions of the above supplement.

4. FAA Approved Supplement to CAA or FAA Approved Airplane Flight Manual for Britten Norman Models BN-2A-2, BN-2A-8, BN-2A-20, BN-2A-26, BN-2B-20, and BN-2B-26, P/N 89170, dated 11-03-82 or later FAA Approved revisions of the above supplement.

5. FAA Approved Supplement to CAA or FAA Approved Airplane Flight Manual for Britten Norman Models BN-2A-2, BN-2A-8, BN-2A-20, BN-2A-26, BN-2B-20, and BN-2B-26, P/N 89170-1, dated 10-01-90 or later FAA Approved revisions of the above suoplement.

6. FAA Approved Supplement to CAA or FAA Approved Airplane Flight Manual for Britten Norman Models BN-2A-2, BN-2A-8, BN-2A-20, BN-2A-26, BN-2B-20, and BN-2B-26; and BN-2A-6 When Mod. Nos. NB/M/430 and NB/M/631 Are Installed, P/N 89170-2, dated 6-26-95 or later FAA Approved revisions of the above supplement.

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

Am alteration of this certificaU is punishable by a fin* of not exceeding SI,000, or imprisonment not exceeding 3 years, or bnih.

PAA FOWM •iiu-2-1 (10.M) This catifcatt may bt trantfirrid in accordant! with FMl ,'l.-l~ PAGE 2 OF 2 PAGES

## Every issue (1)

- June 26, 1995: Amended, Current. [certificate](https://openairdocs.org/files/sha256/c3/49/c349870757be2adf6b2fa78609186f10ac8ef4bd451a9c7f953453feb4746b61)

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