What it approves
Installation of S-TEC System 60 pitch stabilization system ST-125 with optional automatic electric trim 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.
tinted &tatu of amenta Bcpartmtnt of Transportation —federal 2toiation administration Supplemental t^pe Certificate SA5147SW-D S-TEC Corporation Rt. 4, Bldg. 946 Welters Industrial Complex Mineral Wells, TX 76067 ^a* * ClVM Air aMan-nA .
Al C E BEECH C23 , A24R, B24R, C24R, 23, A23, A23A, A23-24, B23 AND A24 njz& .
Installation of S-TEC System 60 Pitch Stabilization System, Model ST-125 with Optional Automatic Electric Trim System according to Bulletin No. 225, Revision 1, dated 10-10-84 and Master Drawing List No. 92164, Revision A, dated 10-10-84 and/or later FAA Approved revisions of the above data (14 Volt System),
1. Eligible only on Beech Models 23, A23, A23A, A23-24, B23 and A24 when modified in accordance with Beech Service News Letter Volume XX, No. 11 and Beech Service Instructions No. 0253-151.
2. Optional Automatic Electric Trim System not eligible on Beech Model A24R.
(See Continuation Sheet, Page 2, a part of this STC).
12-10-82 Q)^**^^ ': 11-28-84, Revision 1 (Signature) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW _ ^^ Any alteration of this certificalr is punishable by a fine of not txettding $1,000, or imprisonment not exceeding 3 years, or '1 k.s certificate may tx transftrrid in accvrd-.nrt inith FAR ?1.47.
[O«M 81 10-2(ia-63)
linitrd £tat« of Btpartmtnt of ICransportation— federal aoiation administration supplemental IKgpe Certificate(Continuation £heet) SA5147SW-D, Revision 1 Limitations and Conditions (con't)
3. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89178, dated 3-22-83 is required for Beech Model A24R (without autotrim) and/or later FAA Approved revisions of the above supplement.
4. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89179, dated 3-22-83 is required for Beech Models B24R and C24R and/or later FAA Approved revisions of the above supplement.
5. FAA Approved Supplemental Flight Manual, P/N 89534, dated 11-28-84 is required for Beech Model C23 and Models 23, A23, A23A, A23-24, B23 and A24 when modified in accordance with Beech Service News Letter Volume XX, No. 11 and Beech Service Instructions No. 0253-151 and/or later FAA Approved revisions of the above supplement.
6. Compatabil ity of this modification with other previously approved modifications must be determined by the installer.
•:''.:n i,J this i'erlif.caif is f>:tr:; .hable by a jint nj r; .! rxitfling SI,000, nr imprisonment nut ..•- f ORM aiiy-2-i do-69) This cirtifu'att m.i> fit liamjtm,! in acc.irdiiru-t LI ilk /.I/-.' -'/ ' 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 <JP code) from (Name of grantor) (Print or type) .
(Address of grantor) (Number and street) (City, State, and <7/> code) Extent of Authority (if licensing agreement):
Signature of grantor (In ink):
U.S. GOVERNMENT PRINTING OFFICE : 1966 OF —205-579
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 10
| Make | Model | Data sheet |
|---|---|---|
| Beechcraft Corporation | 23 | A1CE |
| Beechcraft Corporation | A23 | A1CE |
| Beechcraft Corporation | A23-24 | A1CE |
| Beechcraft Corporation | A23A | A1CE |
| Beechcraft Corporation | A24 | A1CE |
| Beechcraft Corporation | A24R | A1CE |
| Beechcraft Corporation | B23 | A1CE |
| Beechcraft Corporation | B24R | A1CE |
| Beechcraft Corporation | C23 | A1CE |
| Beechcraft Corporation | C24R | A1CE |