# STC SA8382SW-D

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: S-TEC Corporation, United States
- Description: Installation of S-TEC System 55/55X Two Axis automatic flight guidance system,Model ST-513
- Applied: February 15, 1994
- Status date: October 19, 2001
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A15](https://openairdocs.org/tcds/3A15)
- Certificate PDF: https://openairdocs.org/files/sha256/ca/c0/cac05f4520fd44ea52a45c1abb3761c27518be7a4f8201781272a5ea1e7d9b9b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3D366080706AA4A185256CC20058E76B.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA8382SW-D

## ADs that name it (0)

None.

## Approved models (4)

- Raytheon Aircraft Company A36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Raytheon Aircraft Company A36TC ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Raytheon Aircraft Company B36TC ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Raytheon Aircraft Company F33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15))

## 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.

•Iftmtcb JB>tatrE ®f .America cparimcrtl nf *2Irartsp0riaii0n - Jjjeberal jA&tatton (Esrttftcate SA8382SW-D S-TEC Corporation One S-TEC Way Mineral Wells Municipal Airport Mineral Wells, TX 76067-9236 3A15 Beech F33A- A36> A36TC, and B36TC Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System, Model ST-513, according to Bulletin No. 613, Revision 7, dated 10-04-01 and Master Drawing List No. 92662, Revision G, dated 10-04-01 or later FAA Approved revisions of the above data (28 Volt System).

(See Continuation Sheet, Pages 2 and 3, a part of this STC.)

If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

a fa>H/fit.a/*rj/t td/fr sj a//<>>fwjf /y/ss/tifj/ of//*?

2-15-94 3-11 -94 10-19-01 (Signature) Michael Keirnan DAS Staff Coordinator. DAS 5 SW (Title)

•Hnitch j&atcs ©f Jkmcrtca nf "cHranspnriattrm - ^hcral J\.frtaltntt (Abmttttstrattnn SA8382SW-D Limitations and Conditions (con't.)

1 . Also eligible on models F33A, A36, and A36TC when modified per STC SA153EA (tip tanks).

2. Also eligible on model A36 when modified per STC SA5223NM (turbo-normalizing system).

3. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891048. dated 3-11-94 is required for Beech Models F33A; A36, S/N E-2110 and Below (Except S/N E-1946 and S/N E-2104) and A36TC or later FAA Approved revisions of the above supplement.

4. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891049. dated 3-1 1-94 is required for Beech Model A36, S/N E-1946 and S/N E-2104 and S/N E-21 1 1 and Up or later FAA Approved revisions of the above supplement.

5. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891050. dated 3-11-94 is required for Beech Model B36TC, S/N EA-242, S/N EA-273 Through S/N EA-388 (Except S/N EA-320) or later FAA Approved revisions of the above supplement.

6. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 89105 1, dated 3-1 1-94 is required for Beech Model B36TC, S/N EA-320 and S/N EA-389 & Up or later FAA Approved revisions of the above supplement.

7. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891048. Revision 1, dated 10-20-00 is required for Beech models F33A; A36, S/N E-2110 and below (except S/N E-1946 and S/N E-2104) and A36TC for S-TEC System 55/55X or later FAA Approved revisions of the above supplement.

8. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891049. Revision 1, dated 10-20-00 is required for Beech model A36, S/N E-1946 and S/N E-2104 and S/N E-21 11 and up for S-TEC System 55/55X or later FAA Approved revisions of the above supplement.

9. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891050. Revision 1, dated 10-20-00 is required for Beech model B36TC, S/N EA-242, S/N EA-273 through S/N EA-388 (except S/N EA-320) for S-TEC System 55/55X or later FAA Approved revisions of the above supplement.

10. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891051. Revision 1, dated 10-20-00 is required for Beech model B36TC, S/N EA-320 and S/N EA-389 and up for S-TEC System 55/55X or later FAA Approved revisions of the above supplement.

Any alteration of thie certificate ia punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both.

FAA Form 8110-2-1(10-69) Page 2 of 3 This certificate may be transferred in accordance with FAR 22.47.

•Hmtcb ^tatcs ffif ,A eparhtumt of ^transportation - ^fcbcral Rotation JVhmtnistratton upplemental tEgpe (Esrttftcate e/T SA8382SW-D Limitations and Conditions (con't.)

11. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891048. Revision 2, dated 10-19-01 is required for 1. Beech models F33A; A36, S/N E-21 10 and below (except S/N E-1946 and S/N E-2104) and A36TC and the above models when modified per STC SA153EA (tip tanks); 2. Beech model A36, S/N E-21 10 and below (except S/N E-1946 and S/N E-2104) when modified per STC SA5223NM (turbo-normalizing system) for S-TEC System 55/5 5X or later FAA Approved revisions of the above supplement.

12. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891049. Revision 2, dated 10-19-01 is required for Beech model A36, S/N E-1946 and S/N E-2104 and S/N E-21 11 and up and the above model when modified per STC SA153EA (tip tanks) and/or STC SA5223NM (turbo-normalizing system) for S-TEC System 55/55X or later FAA Approved revisions of the above supplement.

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

FAA Form 8110-2-1(10-69) Page 3 of 3

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number .

to (Name of transferee) (Address of transferee) (Number and street) (City, State, and Z}P 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)

- October 19, 2001: Amended, Current. [certificate](https://openairdocs.org/files/sha256/ca/c0/cac05f4520fd44ea52a45c1abb3761c27518be7a4f8201781272a5ea1e7d9b9b)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.