# STC SA4085SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: S-TEC Corporation
- Description: Installation of S-TEC System 60 single axis automatic flight guidance system model ST-001.
- Status date: July 7, 1982
- Data sheets: 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15
- Certificate PDF: https://openairdocs.org/files/sha256/0b/0e/0b0e1b178a0dd9ec3917bcbbb1467a2fb5b156d09cbd6689c7681d6a7e42d1a3
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D9565CF8D96D0CC086257DF60055A414.0001
- Page: https://openairdocs.org/stc/SA4085SW

## ADs that name it

None.

## Approved models (22)

- Beechcraft Corporation 35-33 (TCDS 3A15)
- Beechcraft Corporation 35-A33 (TCDS 3A15)
- Beechcraft Corporation 35-B33 (TCDS 3A15)
- Beechcraft Corporation 35-C33 (TCDS 3A15)
- Beechcraft Corporation 35-C33A (TCDS 3A15)
- Beechcraft Corporation E33 (TCDS 3A15)
- Beechcraft Corporation E33A (TCDS 3A15)
- Beechcraft Corporation E33C (TCDS 3A15)
- Beechcraft Corporation F33 (TCDS 3A15)
- Beechcraft Corporation F33A (TCDS 3A15)
- Beechcraft Corporation F33C (TCDS 3A15)
- Beechcraft Corporation G33 (TCDS 3A15)
- Beechcraft Corporation H35 (TCDS 3A15)
- Beechcraft Corporation J35 (TCDS 3A15)
- Beechcraft Corporation K35 (TCDS 3A15)
- Beechcraft Corporation M35 (TCDS 3A15)
- Beechcraft Corporation N35 (TCDS 3A15)
- Beechcraft Corporation P35 (TCDS 3A15)
- Beechcraft Corporation S35 (TCDS 3A15)
- Beechcraft Corporation V35 (TCDS 3A15)
- Beechcraft Corporation V35A (TCDS 3A15)
- Beechcraft Corporation V35B (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.

United States of America BcpartmEnt of transportation— jpederal aviation administration Supplemental t;gpe Certificate SA4085SW S-TEC Corporation Bout* 4, Building 946 Wolters Industrial Complex Mineral Wells, Texas 76067 stSi&^£y^i&de&4Jg^ <^ 3 Civil Air 3A15 Beech

35-33. 35-A33, 35-B33, 35-C33. 35-C33A,3, H35, J35. K35, M35, H35.W5. S35,tV35when modified by STC SA1035WE(Turbocl Installation of S-TEC System 60 Single Axis Automatic Flight Guidance System, Model ST-001 according to Bulletin Mo. 101, Revision 6, dated 3-26-82 and Master Drawing List No. 9202, Revision F, dated 3-26-82; or later FAA approved revision. (14 Volt System) See Continuation Sheet, page 2, of this STC.

September 28, 1979 February 22, 1980 ^ J&4^ S^c^n^rud^afe^^J 3/13/80; 4/11/80; 11/19/80;

7/7/82 Revision 4 P. WatBou Manager, Aircraft Certification DivisionSouthwest Region ~~~~~~~~~"~

**FAA FOKM 8110-2 (10-68)**

United £tatzs of America Bepartmtnt of transportation— Jpederal HOiation administration Supplemental ICgpe Certificate(Continuation £httt) SA4085SW Revision 4 Limitations and Conditions :

1. Pilot's Operating Handbook and PAA Approved Airplane Flight Manual Supplement P/N 8901 dated February 22, 1980, is required for Beech Models V35, V35A, V35B.

2. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement, P/N 8901-1, dated March 13, 1980, is required for Beech Models 35-C33, 35-C33A, E33, E33A, E33C, F33, F33A, F33C, G33, V35, V35A, V35B.

3. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement P/N 8901-2 dated April 11, 1980, is required for Beech Models 35-033, 35-C33A, E33, E33A, E33C, F33, F33A, F33C, G33, H35, J3§, K35, M35, N35, P35, S35, V35, V35A, V35B.

4. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement P/N 8901-3 dated November 19, 1980, is required for Beech Models 35-C33, 35-C33A, E33, E33A, E33C, F33, F33A, F33C, G33, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B; and S35, V35, V35A, V35B when modified by STC SA1035WE (Turbocharged Engine.)

5. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89120, dated 7/7/82, is required for Beech Models 35-33, 35-A33, and 35-B33.

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

FAA FORM sno-2-1 (10-69) 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, Slate, and ^IP cade) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and ^1P code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

## Every issue (1)

- July 7, 1982: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/0b/0e/0b0e1b178a0dd9ec3917bcbbb1467a2fb5b156d09cbd6689c7681d6a7e42d1a3)

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