What it approves
Installation of S-TEC System 40/50 single and two axis automatic flight guidance system ST-223.
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.
Bepartrarnt of Transportation—Jpttoal aoiation administration Supplemental 'Cgpt Certificate SA5290SW-D S-TEC Corporation 946 Pegram Mineral Wells, TX 76067 ~AJA~/*^J ———— ——— ^ !^r «n-tn— i"firir« rrrrrr.r«mi)«^i>^r/' 3 ^s- ClVll Air 3A16 BEECH 95-55, 95-A55, 95-855, 95-B55A, 95-B55B, 95-C55, 95-C55A, D55, D55A, E55, E55A, 56TC, and A56TC Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems, Model ST-223, Bulletin No. 323, Revision 3, dated 1-23-96 and Master Drawing List No. 92251, Revision C, dated 1-23-96 or later FAA Approved revisions of the above data (28 Volt System).
1. Only eligible on Model 95-B55B When Modified Per Beech Drawing 96-002000 (Civilian Conversion).
(See Continuation Sheet, Page 2, a part of this STC.)
•<^M*<^&lX^«»t4a^<^>i4^'yt<>f><£^ ^J0tA*rvx^^A£u>6i4SiAC<!^y'JiAe< *&~: 11-28-83 3-27-84 ^-^.r_rr-fxv. 3-29-85, 9-08-93, 2-04-94, 1-31-96 Revision 4 . Thomas DAS Staff Coordinator, DAS 5 SW (TaU) Any alteration oftkit ttrtificate it punishable by a fine of not exceeding SI,OOP, or imprisonment not txttding 3 ytan, or both.
Tku ttrttjtcatt mty tr tiuujtmt m •mrdbncr talk FAR 21.47.
ttmtd £tam of 3ncnra Bqiartmtnt of transportation— f dcral atriation administration topplcmental t^gpe Certificate(Continuation Sheet) SA5290SW-D, Revision 4 Limitations and Conditions (con't.)
2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89346, dated 3-27-84 is required for Beech Models 95-55, 95-A55, 95-855, and 95-B55A for S-TEC System 40 or later FAA Approved revisions of the above supplement.
3. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89346-1, dated 9-08-93 is required for Beech Models 95-55, 95-A55, 95-B55, and 95-B55A and 95-B55B When Modified Per Beech Drawing 96-002000 for S-TEC System 40 or later FAA Approved revisions of the above supplement.
4. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 89346-2, dated 1-31-96 is required for Beech Models 95-55, 95-A55, 95-B55, and 95-B55A; and 95-B55B When Modified Per Beech Drawing 96-002000 (Civilian Conversion) for S-TEC System 40 or later FAA Approved revisions of the above supplement.
5. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89347, dated 3-27-84 is required for Beech Models 95-C55, 95-C55A, D55, D55A, E55, and E55A for S-TEC System 40 or later FAA Approved revisions of the above supplement.
6. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89348, dated 3-27-84 is required for Beech Models 95-55, 95-A55, 95-B55, and 95-B55A for S-TEC System 50 or later FAA Approved revisions of the above supplement.
7. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89348-1, dated 9-08-93 is required for Beech Models 95-55, 95-A55, 95-B55, and 95-B55A and 95-B55B When Modified Per Beech Drawing 96-002000 for S-TEC System 50 or later FAA Approved revisions of the above supplement.
8. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 89348-2, dated 1-31-96 is required for Beech Models 95-55, 95-A55, 95-B55, and 95-B55A; and 95-B55B When Modified Per Beech Drawing 96-002000 (Civilian Conversion) for S-TEC System 50 or later FAA Approved revisions of the above supplement.
.•Ifiv aitrration nf this crrtificaU is pumshabli by afint of not exceeding 11,000, or imprisonment not exceeding 3 years, or hnih.
PAA FORM »no.a-» OO.M) Tint cirttfcatt may bt trmtftrrni m attadanti with FAR .'/.•/' PAGE 2 OF 3 PAGES
&ua of Stern Bepartment of Transportation— federal 3triation Administration Supplemental HCgpe Certificate(Continuation £heet) SA5290SW-D, Revision 4 Limitations and Conditions (con't.)
9. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89349, dated 3-27-84 is required for Beech Models 95-C55, 95-C55A, D55, D55A, E55, and E55A for S-TEC System 50 or later FAA Approved revisions of the above supplement.
10. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891231, dated 1-31-96 is required for Beech Models 56TC and A56TC for S-TEC System 40 or later FAA Approved revisions of the supplement,
11. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891232, dated 1-31-96 is required for Beech Models 56TC and A56TC for S-TEC System 50 or later FAA Approved revisions of the above supplement.
12. Compatibility of this modification with other previously approved modifications must be determined by the installer.
Am alteration of this certificate is punishable by ajint of not exceeding 11,000, or imprisonment not exceeding 3 years, or bnih.
PA* FOHM ii 10.2-1 (10.M) Ttta eirhfeatt may »« lrmtfirr«i « accordant, with I'AR .•/.•/'.
TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and ^IP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and <7P 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 · 13
| Make | Model | Data sheet |
|---|---|---|
| Beechcraft Corporation | 56TC | 3A16 |
| Beechcraft Corporation | 95-55 | 3A16 |
| Beechcraft Corporation | 95-A55 | 3A16 |
| Beechcraft Corporation | 95-B55 | 3A16 |
| Beechcraft Corporation | 95-B55A | 3A16 |
| Beechcraft Corporation | 95-B55B | 3A16 |
| Beechcraft Corporation | 95-C55 | 3A16 |
| Beechcraft Corporation | 95-C55A | 3A16 |
| Beechcraft Corporation | A56TC | 3A16 |
| Beechcraft Corporation | D55 | 3A16 |
| Beechcraft Corporation | D55A | 3A16 |
| Beechcraft Corporation | E55 | 3A16 |
| Beechcraft Corporation | E55A | 3A16 |