Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Amended
Status date
January 18, 2002
Applied
April 7, 1995
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS3A15

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of S-TEC System 55/55X two axis automatic flight guidance system, Model ST-582

What the certificate saysOCR

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

- 703 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA08998 AC-D This certificate issued to: S-TEC Corporation One S-TEC Way Mineral Wells Municipal Airport Mineral Wells, TX 76067-9236 Part 3 of the Cind shin Regulations.

Original Product Type Certificate Numter: ЗА15 Make: Beech Model: 36, A36, and F33A Description of Type Design Change:

Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System, Model ST-582, according to Bulletin No. 682, Revision 4, dated 1-15-02 and Master Drawing List No. 92761, Revision D, dated 1-15-02 or later FAA Approved revisions of the above data (14 Volt System).

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

If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

Date of Application: 4-07-95 Date Reissued:

Date of Issuance: 4-13-95 Date Amended: 1-18-02 By Direction of the Administrator (Signature) TOMINISTRATO DAS Staff Coordinator, DAS 5 SW Michael Keirnan (Title) 47

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA08998AC-D Limitations and Conditions: (con't.)

Eligibility limited to Beech model F33A, S/N CE-316 and up.

Also eligible on models 36, A36, and F33A, S/N CE-316 and up when modified per STC SA153EA (tip tanks).

Also eligible on models 36 and A36 when modified per STC SA5223NM (turbo-normalizing system).

4. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891156, dated 4-13-95 is required for Beech Models 36, A36: And F33A S/N CE-316 And Up or later FAA Approved revisions of the above supplement.

5. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891156, Revision 1, dated 3-20-01 is required for Beech models 36, A36; and F33A, S/N CE-316 and up for S-TEC System 55/55X or later FAA Approved revisions of the above supplement.

FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891156, Revision 2, dated 1-18-02 is required 1. Beech models 36, A36; and F33A, S/N CE-316 and up; 2. Beech models 36, A36; and F33A, S/N CE-316 and up when modified per STC SA153EA (tip tanks); 3. Beech models 36 and A36 when modified per STC SA5223NM (turbonormalizing system) for S-TEC System 55/55X or later FAA Approved revisions of the above supplement.

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

PAA Form 8110-2-1(10-69) Page 2 of 2

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 · 3

MakeModelData sheet
Beechcraft Corporation363A15
Beechcraft CorporationA363A15
Beechcraft CorporationF33A3A15