# STC SA4240SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: S-TEC Corporation
- Description: Installation of S-TEC system 60 two axis automatic flight guidance system, Model ST-018 with optional autotrim system
- Status date: November 2, 1981
- Data sheets: 3A15, 3A15, 3A15
- Certificate PDF: https://openairdocs.org/files/sha256/31/e5/31e5298ef2a8a3c2fec5677feac214c5e6cc519b824ceedd2b2d3c27b784e783
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/73B4AB987C73883D86257DF90059DC86.0001
- Page: https://openairdocs.org/stc/SA4240SW

## ADs that name it

None.

## Approved models (3)

- Beechcraft Corporation A36 (TCDS 3A15)
- Beechcraft Corporation A36TC (TCDS 3A15)
- Beechcraft Corporation F33A (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 amrrica Bepartment of transportation—federal atnation administration Supplemental 'Cgpe CertificateProject A5521SW-DS SA4240SW FKP-130 S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 JA&Ju^ie'ded4cbn^wjA&fi&^ Civil Air 3A15 Beech A36, F33A, A36TC installation of S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-018 with Optional Autotrim System according to Bulletin No. 118, Revision 2, dated 10-22-81 and Master Drawing List No. 9220, Revision B, dated 10-22-81 and Optional Flight Director/Steering Horizon according to Bulletin No. 120 Revision 3 dated 5-21-81 and Master Drawing List No. 9209, Revision C, dated 5-21-81, pr later FAA approved revision.

(28 Volt System) See Continuation Sheet, page 2, of this STC.

«^,<^ November 4, 1980 December 5, 1980 10/26/81; 11/2/81 Revision 2 -S & ._„ P. Watsonbting Chief, Aircraft Certification Division (Title)

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

ttnitrd £tatu of Bepartment of transportation— federal aviation administration Supplemental t:jipe Certificate(Continuation £htet) SA4240SW Revision 2 Limitations and Conditions:

1. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement P/N 8918 dated December 5, 1980, is required for Models A36 and F33A with S-TEC System 60 Automatic Flight Guidance System, Model ST-018 without optional autotrim system; OR Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement P/N 8918-1 dated October 26, 1981, is required for Models A36 and F33A with S-TEC System 60 Automatic Flight Guidance System, Model ST-018 with or without optional autotrim system; OR Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement P/N 8918-2 dated November 2, 1981, is required for Models A36, F33A, and A36TC with S-TEC System 60 Automatic Flight Guidance System, Model ST-018 with or without optional autotrim system.

2. Compatibility of this modification with other previously approved modifications must be determined by the Installer.

**FAA FORM 8HO-2-1 (10-69) PAGE 2 OP 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 2JP code) 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)

- November 2, 1981: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/31/e5/31e5298ef2a8a3c2fec5677feac214c5e6cc519b824ceedd2b2d3c27b784e783)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.