# STC SA4414SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: S-TEC Corporation
- Description: Installation of S-TEC system 60 pitch stabilization system, ST-051 with optional autotrim system
- Status date: May 12, 1982
- Data sheets: 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15, 3A15
- Certificate PDF: https://openairdocs.org/files/sha256/58/6a/586a565d19d9c7c9719ce818369271c72751a6fe3030e3aaea49512fb45e218d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/EE8BA319C05FAF4486257E03006BBBBB.0001
- Page: https://openairdocs.org/stc/SA4414SW

## ADs that name it

None.

## Approved models (12)

- 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)

## 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 amenta Bepartment of transportation—federal aoiation administration Supplemental 'Cgpe Certificate <yKwm&€w SA4414SW S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 v*fytSi&;ebeAjjiawf^*£n^f(>ftc>t*ftM^Jw*>du^M>tJ&^ 3 Civil Air <slea<da£&n&.

3A15 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E33A, E33C, F33, F33C, G33, F33A, S/N CE-315 and Below Installation of S-TEC System 60 Pitch Stabilization System, Model ST-051, with Optional Autotrim System, according to Bulletin No. 154, Revision 1, dated 3/26/82 and Master Drawing List No. 9246, Revision A, dated 3/26/82, or later FAA approved revision. (14 Volt System) See Continuation Sheet, page 2, of this STC.

Jewni<nJa& S&c&nimibfaa&r-dj&e' May 5, 1981 July 14, 1981 May 12, 1982 Revision 1 Don P. Watson /(**'«>">")Acting Chief, Aircraft CertificationDivision - Southwest Region (Title)

This certificate may he transferred in accordance with FAR 21.47.

FAA Fow 8110-2 (10-68)

Hinted &tatu of America Bepartmcnt of transportation— federal SOiation administration upplemental l^jpe Certificate(Continuation £heet) SA4414SW Revision 1 Limitations and Conditions:

1. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement P/N 8952 dated 7/14/81, is required with Models 35-C33, 35-C33A, E33, E33A, E33C, F33, F33C, 633, and F33A, S/N CE-315 and Below with S-TEC System 60 Pitch Stabilization System.

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual P/N 89121 dated 5/12/82, is required for Models 35-33, 35-A33, and 35-B33 with S-TEC System 60 Pitch Stabilization System.

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

FAA FORM siio-2-1 (1O-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, State, and %1P code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, Slate, and £//> code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

## Every issue (1)

- May 12, 1982: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/58/6a/586a565d19d9c7c9719ce818369271c72751a6fe3030e3aaea49512fb45e218d)

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