What it approves
Installation of S-TEC system 60 pitch stabilization system, ST-051 with optional autotrim system
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may 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):
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 12
| Make | Model | Data sheet |
|---|---|---|
| Beechcraft Corporation | 35-33 | 3A15 |
| Beechcraft Corporation | 35-A33 | 3A15 |
| Beechcraft Corporation | 35-B33 | 3A15 |
| Beechcraft Corporation | 35-C33 | 3A15 |
| Beechcraft Corporation | 35-C33A | 3A15 |
| Beechcraft Corporation | E33 | 3A15 |
| Beechcraft Corporation | E33A | 3A15 |
| Beechcraft Corporation | E33C | 3A15 |
| Beechcraft Corporation | F33 | 3A15 |
| Beechcraft Corporation | F33A | 3A15 |
| Beechcraft Corporation | F33C | 3A15 |
| Beechcraft Corporation | G33 | 3A15 |