Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
June 4, 1997
Applied
May 30, 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 6, 2025.

What it approves

Installation of S-TEC System 30 ALT Altitude Hold System Model ST-686

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: SA09228AC-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 therefor as specifed hereon meets the aivorthiness regurements of Part 3 of the Civil stir Regulations.

Original Product I ype Certificate Number: 3A12 Make: Cessna Model: 172, 172A, 172B, 172C, 172D, 172E, 172F, 172G, 172H, 1721, 172K, AND 172L Descriplion of 9 ype Design Change:

Installation of S-TEC System 30 ALT Altitude Hold System, Model ST-686, according to Bulletin No. 786, dated 5-28-97 and Master Drawing List No. 92999, dated 5-28-97 or later FAA Approved revisions of the above data (14 Volt System).

Also eligible on the Above Models When Modified Per STC SA420CE (Lycoming Engine 0-360- AID, 180 H.P.)

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

Date of Application: 5-30-97 Date Reissued:

Date of Issuance: 6-04-97 Date Amended:

FEDERAL AVIATION TOMINISTRATO DAS Staff Coordinator, DAS 5 SW William J. Thomas (Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA09228 AC-D Limitations and Conditions: (con't.)

2. FAA/DAS Approved Supplemental Flight Manual, P/N 891406, dated 6-04-97 is required for Cessna Models 172, 172A, 172B, and 172C And The Above Models When Modified Per STC SA420CE (Lycoming Engine 0-360-A1D, 180 H.P.) or later FAA Approved revisions of the above supplement.

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

The FAA will reissue the certificate in the name of the transferee and fotward it to him,

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 codel Exten: 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 · 12

MakeModelData sheet
Cessna Aircraft Company1723A12
Cessna Aircraft Company172A3A12
Cessna Aircraft Company172B3A12
Cessna Aircraft Company172C3A12
Cessna Aircraft Company172D3A12
Cessna Aircraft Company172E3A12
Cessna Aircraft Company172F (USAF T-41A)3A12
Cessna Aircraft Company172G3A12
Cessna Aircraft Company172H (USAF T-41A)3A12
Cessna Aircraft Company172I3A12
Cessna Aircraft Company172K3A12
Cessna Aircraft Company172L3A12