Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Amended
Status date
February 2, 2001
Applied
May 5, 1995
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDSA42EU

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-586

What the certificate saysOCR

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

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA09003 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 Ciest In Regulations.

Original Product Type Cerlificate A umber: A-42EU Make: Reims-Cessna Model: F182Q Description of Type Design Change:

Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System, Model ST-586, according to Bulletin No. 686, Revision 2, dated 2-02-01 and Master Drawing List No. 92779, Revision B, dated 2-02-01 or later FAA Approved revisions of the above data (28 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: 5-05-95 Date Reissued:

Date of Issuance: 5-15-95 Date Amended: 2-02-01 By Direction of the Administrator FEDERAL AVIATION тіля к (Signature) TOMINISTRATOF Michael Keirnan DAS Staff Coordinator, DAS 5 SW (Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA09003 AC-D Limitations and Conditions: (con't.)

1. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891167, dated 5-15-95 is required for Reims-Cessna Model F182Q or later FAA Approved revisions of the above supplement.

2. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891167, Revision 1, dated 2-02-01 is required for Reims-Cessna model F182Q 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.

PAR 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 · 1

MakeModelData sheet
Cessna Aircraft CompanyF182QA42EU