What it approves
Installation of S-TEC system 65 two axis automatic flight guidance system, Model ST-387.
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.
Umtrd 3tatei of ammca Bcparrmcnt of transportation -federal aoiation administration Supplemental TCpe Certificate SA6092SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 a^ 3 ^at Znt Li VI I Air ..flfaij fJr^at rui/ ijroauc/ —— •^'uJis~(ji4'p6jUca4e'iSu*rnue>r- oAlD BEECH 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E33A, E33C, F33, F33A, F33C AND G33 s/ufi* -J seAjja-r Installation of S-TEC System 65 Two Axis Automatic Flight Guidance System, Model ST-387, according to Bulletin No. 487, dated 10-06-86 and Master Drawing List No.
92397, dated 10-06-86 and/or later FAA Approved revisions of the above data (14 Volt System).
1. Only eligible on Beech Model F33A, S/N CE-315 and Below. •1 •»
2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA-.,Approved Airplane Flight Manual, P/N 89706, dated- 10-15-86 is required for Beech Models 35-33, 35-A33, 35-B33 and/or later FAA Approved revisions of the above supplement.
(See Coi»*4riuation Sheet, Page 2, a part of this STC.)*—r— fAvm*um'An'^U4c/<jvn&6A v^e^rntn^A^r^^£a^^^nervfiAf'^^£a^fi^A^a^ 10-09-86 10-15-86 (Sirnaturi) Did W.Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW (Title)
Tkii certificate may be trmsfrmj in •ccfr^ana with FAR 21AT.
»AA FOM • 110-2 (l o-A«)
tinted States of 2Uncrira Btpartment of ^transportation— .federal Station administration Supplemental H$$t Certificate(Condnuadon «Sheet) SA6092SW-D Limitations and Conditions (con't)
3. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89707, dated 10-15-86 is required for Beech Models 35-C33, 35-C33A, E33, E33A, E33C, F33, F33A, S/N CE-315 and Below F33C and G33 and/or later FAA Approved revisions of the above supplement.
4. Compatability of this modification with other previously approved modifications must be determined by the installer.
.I'n ultnntiun of this certificate is punishable by a fine of not exceeding SI,000, or imprisonment not exceeding 3 years, or /><>//•
• AA f ORM eno-2-1 (10-69) This ctrttfeatt may be transferred in accordance trtlli 1-'AI< -I ^~ PAGE 2 OF 2 PAGES
TRANSFER ENDORSEMENT Transfer the ownership of Supplemenul Type Certincate Number to (Name of transferee).
(Address of transferee). I Mumtxr tnd Oral) (City. Stall. *nd y? nJt y from (Name of grantor) (Print or type).
(Address of grantor) t Hi j itt. Slflt, Extent of Authority (if licensing agreement):.
Signature of grantor (In ink):
• it « r. » n i«««-««»-(>«>
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 |
|---|---|---|
| Raytheon Aircraft Company | 35-33 | 3A15 |
| Raytheon Aircraft Company | 35-A33 | 3A15 |
| Raytheon Aircraft Company | 35-B33 | 3A15 |
| Raytheon Aircraft Company | 35-C33 | 3A15 |
| Raytheon Aircraft Company | 35-C33A | 3A15 |
| Raytheon Aircraft Company | E33 | 3A15 |
| Raytheon Aircraft Company | E33A | 3A15 |
| Raytheon Aircraft Company | E33C | 3A15 |
| Raytheon Aircraft Company | F33 | 3A15 |
| Raytheon Aircraft Company | F33A | 3A15 |
| Raytheon Aircraft Company | F33C | 3A15 |
| Raytheon Aircraft Company | G33 | 3A15 |