Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
May 16, 1997
Applied
May 12, 1997
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS3A12

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 30 ALT Altitude Hold System, Model ST-673.

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: SA09213 AC-D This certificate issued to: S-TEC Corporation One S-TEC Way Mineral Wells Municipal Airport Mineral Wells, TX 76067-9236 Certifies that the change in the type design for the following product with the limitations and conditions thorofor as specifed heroon meets the anorthiness reguremonts of Part 3 of the bivil dir Regulations.

Original Product I ype Certificate Number: 3A12 Make: Cesssna Model: 172M, 172N, 172P AND 172Q Description of Type Design Change: ;

Installation of S-TEC System 30 ALT Altitude Hold System, Model ST-673, according to Bulletin No. 773, dated 5-09-97 and Master Drawing List No. 92991, dated 5-09-97 or later FAA Approved revisions of the above data (28 Volt System).

Also eligible on Cessna Models 172M, 172N, and 172P When Modified By 180 H.P. Engine Conversion.

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

Date of Application: 5-12-97 Date voisued:

Date of Issuance: 5-16-97 Date Amended:

EDERAL AVIATION By Direction of the Administrator LL Signatu TOMINISTRATO William J. Thomas DAS Staff Coordinator, DAS 5 SW (Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA09213 AC-D Limitations and Conditions: (con't.)

2. FAA/DAS Approved Supplemental Flight Manual, P/N 891374, dated 5-16-97 is required for Cessna Models 172M; and 172N, S/N 17271034 And Below; and Cessna Models 172M; and 172N, S/N 17271034 and Below When Modified By 180 H.P. Engine Conversion or later FAA Approved revisions of the above supplement.

FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891375, dated 5-16-97 is required for Cessna Models 172N, S/N 17271035 And On; 172P and 172Q;

and Cessna Models 172N, S/N 17271035 And On and 172P When Modified By 180 H.P. Engine Conversion or later FAA Approved revisions of the above supplement.

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

FAA Form 8110-2-1(10-69) 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 ZIP code) from (Name of grantor) (Print or type) (Address of grantor) (Number & street) (City, State, and ZIP 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 · 4

MakeModelData sheet
Cessna Aircraft Company172M3A12
Cessna Aircraft Company172N3A12
Cessna Aircraft Company172P3A12
Cessna Aircraft Company172Q3A12