STC SA5246SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Amended
Status date
October 24, 1997
Applied
September 16, 1983
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDSA1CE

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems, Model ST-215-40/50.

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.

JHmteb ^tatea of tCraitaportaitott - ^frtalmrt Qkrttftc&te SA5246SW-D S-TEC Corporation One S-TEC Way Mineral Wells Municipal Airport Mineral Wells, TX 76067-9236 J" e/Me A1CE BEECH C23, A24R, B24R, C24R, A23-19, 19A, M19A, B19, 23, A23, A23A, A23-24, B23, and A24 Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems, Model ST-215-40/50, according to Bulletin No. 315, Revision 3, dated 10-17-97 and Master Drawing List No.

92241, Revision C, dated 10-17-97 or later FAA Approved revisions of the above data (14 Volt System).

1. Eligible only on Beech Models 23-19, 19A, M19A, B19, 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.

(See Continuation Sheet, Page 2, a part of this STC.)

9-16-83 12-02-83 11-07-84, 1-31-85, 10-24-97 Revision 3 'gnaturej William J. Thomas DAS Staff Coordinator, DAS 5 SW (Title) Any dJ teration of this cert ificate is punishable by a fine of not exoepc/inc/ $1,000, or i/npr-i^on/nenfc not exceeding '3 year5, or both.

FAA Form 8110-2(10-68} Page 1 of 2 This certificate /nay be transferred in accordance1 with FAR 21.47.

Pnttcb plates ®f

•Beparfanent of ffiratwportatton - .Sfeaeral Ration <&0minf alratton Certificate Jitjeet) SA5246SW-D, Revision 3 Limitations and Conditions (con't.)

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89330, dated 12-02-83 is required for S-TEC System 40 for Beech Models A24R, B24R, and C24R 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 89331, dated 12-02-83 is required for S-TEC System 50 for Beech Models A24R, B24R, and C24R or later FAA Approved revisions of the above supplement.

4. FAA Approved Supplemental Flight Manual, P/N 89535, dated 11-07-84 is required for S-TEC System 40 in Beech Model C23 and Beech Models A23-19, 19A, M19A, B19, 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 or later FAA Approved revisions of the above supplement.

5. FAA Approved Supplemental Flight Manual, P/N 89536, dated 11-07-84 is required for S-TEC System 50 in Beech Model C23 and Beech Models A23-19, 19A, M19A, B19, 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 or later FAA Approved revisions of the above supplement.

6. FAA Approved Supplemental Flight Manual, P/N 89535-1, dated 1-31-85 is required for S-TEC System 40 in Beech Model C23 and Beech Models A23-19, 19A, M19A, B19, 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 or later FAA Approved revisions of the above supplement.

7. FAA Approved Supplemental Flight Manual, P/N 89536-1, dated 1-31-85 is required for S-TEC System 50 in Beech Model C23 and Beech Models A23-19, 19A, M19A, B19, 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 or later FAA Approved revisions of the above supplement.

8. Compatibility of this modification with other previously approved modifications must be determined by the installer.

FAA Form 811U-2-1(10-b9) Page 2 of 2

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and <7P 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):.

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 14

MakeModelData sheet
Beechcraft Corporation19AA1CE
Beechcraft Corporation23A1CE
Beechcraft CorporationA23A1CE
Beechcraft CorporationA23-19A1CE
Beechcraft CorporationA23-24A1CE
Beechcraft CorporationA23AA1CE
Beechcraft CorporationA24A1CE
Beechcraft CorporationA24RA1CE
Beechcraft CorporationB19A1CE
Beechcraft CorporationB23A1CE
Beechcraft CorporationB24RA1CE
Beechcraft CorporationC23A1CE
Beechcraft CorporationC24RA1CE
Beechcraft CorporationM19AA1CE