What it approves
Installation of S-TEC System 60 Two Axis Automatic /Flight Guidance System with Optional Autotrim System Model ST-314.
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.
Btpartmtnt of'transportation—federal atriation administration Supplemental "Cgpc Certificate iSUvmvev SA7209SW-D > S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex * Mineral Wells, Texas 76067 23 Federal Aviation : A6CE : Cessna : 337D, T337D, 337E, T337E, 337F, T337F, 337G, T337G 337H, P337H, T337H, T337H-SP Install atiofi of S-TEC Sys'tem 60 Two Axis Automatic Flight Guidance System with Optional Autotrim System Model ST-314, according to Bulletin No. 414, dated 3-14-90 and Master Drawing List No. 92503, dated 3-14-90 and/or later FAA Approved revisions of the above data (28 Volt System).
Also eligible on the above models when modified per STC SA937CE (Norton STOL Craft Conversion) .
Also eligible on the above models when modified per STC SA1627WE (Robertson STOL Conversion).
Continuation Sheet, Page 2, a part of this STC.)
SXf/rrUrn 3-16-90 4-06-90 (Signature} Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW
THis tertificale nay be transferred in aenrdance with FAR 21.17.
fAAFo*iitnO-I(l»-«t)
ttnitrd £tatu of Btpartmcnt of transportation— federal 3ttation administration ^upplcmtntal Ttgpe Certificate(Continuation Sheet) SA7209SW-D Limitations and Conditions (con't.)
3. FAA/DAS Approved Supplemental Flight Manual, P/N 89845, dated 4-06-90 is required for Cessna Models 337D, T337D, 337E, T337E, 337F, T337F, 337G, T337G, 337H, P337H, T337H and T337H-SP When Modified Per STC SA1627WE (Robertson STOL Conversion) and/or later FAA" Approved revisions of the above supplement.
4. FAA/DAS Approved Supplemental Flight Manual, P/N 89846, dated 4-06-90 is required for Cessna Models 337D, T337D, 337E, T337E, 337F, T337F, 3376, T337G, 337H, P337H, T337H and T337H-SP And The Above Models When Modified Per STC SA937CE (Horton STOL Craft Conversion) and/or later FAA Approved revisions of the above supplement.
5. Compatabi 1 ity of this modification with other previously approved modifications must be determined by the installer.
n\ alteration of this certificate is punishable by a fine of not exceeding 51,000, or imprisonment not exceeding 3 years, or bn/h.
AA FORM silo-a-l (10-69) This certificati may bi transferred in accordance with l-'AK i'J.-l?.
PAGE 2 Op 2 PAGES
INSTRUCTIONS : The transfer endorsement below may be used to notify the appropriate FAA Regional Office of the transfer of this Supplemental Type Certificate.
The FAA will reissue the certificate in the name of the transferre and forward it to him.
TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (9^ame of transferee) (Address of transferee) (y^umter and street) (City, State, andZlf cade) of grantor) (Trint or type) (Address of grantor) (tfymber and street) (City, State, and ZIP code.)
Exent of Authority (if licensing agreement) :
Signature of grantor (In inty :
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 |
|---|---|---|
| The Cessna Aircraft Company | 337D | A6CE |
| The Cessna Aircraft Company | 337E | A6CE |
| The Cessna Aircraft Company | 337F | A6CE |
| The Cessna Aircraft Company | 337G | A6CE |
| The Cessna Aircraft Company | 337H | A6CE |
| The Cessna Aircraft Company | P337H | A6CE |
| The Cessna Aircraft Company | T337D | A6CE |
| The Cessna Aircraft Company | T337E | A6CE |
| The Cessna Aircraft Company | T337F | A6CE |
| The Cessna Aircraft Company | T337G | A6CE |
| The Cessna Aircraft Company | T337H | A6CE |
| The Cessna Aircraft Company | T337H-SP | A6CE |