# STC SA4133SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: S-TEC Corporation
- Description: Installation of S-TEC system 60-1 single axis automatic flight guidance system model ST-002
- Status date: April 9, 1982
- Data sheets: 3A15, 3A15, 3A15, 3A15, 3A15
- Certificate PDF: https://openairdocs.org/files/sha256/03/35/0335bff437db0512aa5bf58461d537df86300c011999a461ca6c589745c39efb
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B9CE1FDB5E5A8F2286257DF800662796.0001
- Page: https://openairdocs.org/stc/SA4133SW

## ADs that name it

None.

## Approved models (5)

- Beechcraft Corporation A36 (TCDS 3A15)
- Beechcraft Corporation A36TC (TCDS 3A15)
- Beechcraft Corporation F33A (TCDS 3A15)
- Beechcraft Corporation F33C (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 gtatcs or 3mmca Bcpartmtnt of transportation—federal 2toiation administration Supplemental t^gpe Certificate SA4133SW S-TEC Corporation Rt. 4, Bldg. 946 Welters Industrial Complex Mineral Wells, Texas 76067 Vf^^wfit£c*&ima'Jv>weuic£M>i£n. ^A&£rnt£a£*:>7iA.4ind*>c>na<£4>riA J^i£*^ied^4v^4ivi//tnee&-<£wJa4&€WTdritaM 3 j&J&C' Civil Air <sle*a*&ui&&nA,.

Gp*ain>a/ ^froau^ —— <-*vufic-~&e&£tftca&'<yiMrn0et* : 3A15 F33A, F33C, V33B, A36, A36TC Installation of S-TEC System 60 Single Axis Automatic Plight Guidance System, Model ST-002, according to Bulletin No. 102, Revision 3, dated 12-28-81 and Master Drawing List No. 9203, Revision C, dated 12-28-81, or later FAA approved revision. (28 Volt System) gee Continuation Sheet, page 2, of this STC.

April 30, 1980 .SS^wnW.- April 9, 1982 ^ Revision 1 29, 1980 yi ~ij" ^ * I (Signature) Acting cfile?" Aircraft Certification Southweat Region—————

FAA Font 8110-2 (1O-68)

ttnitrd £tattt of amcrica Bepartment of transportation— federal 2Mation administration Supplemental TCjipe Certificate(Continuation SA4133SW Limitations and Conditions: Revision 1

1. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement P/N 8903 dated 5- 29" 80 is required for Beech Models F33A, F33C, V35B, and A36 with S-TEC System 60 Single Axis Automatic Flight Control System, ST-002; OR Supplement to Pilot's Operating EaHbook and/or FAA Approved Airplane Flight Manual, P/N 89106, dated 4-9-82 for Beech Models F33A and F33C with S-TEC System 60 Single Axis Automatic Flight Guidance System, ST-002.

2. Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual P/N 8903-1 dated 4-9-82 is required for Beech Models V35B, A36, and A36TC with S-TEC System 60 Single Axis Automatic Flight Guidance System, ST-002, and using Roll Servo 0106-R9.

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

FAA FORM 8110-z-i (1O-69) PAGE £ OF 2*AGES

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) 1 Number and street) (City, Slate, and ^1P code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) ( City, Stale, and ^IP code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

## Every issue (1)

- April 9, 1982: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/03/35/0335bff437db0512aa5bf58461d537df86300c011999a461ca6c589745c39efb)

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