Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
August 12, 1997
Applied
August 8, 1997
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS1A15

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-716.

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: SA09266AC-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 airworthiness regurements of Part 3 of the birit I i Regulations.

Original Product I ype Certifcate Number: 1A15 Make: Piper Model: PA-24 (PA-24-180), PA-24-250, PA-24-260, and PA-24-400 Description of Type Design Change:

Installation of S-TEC System 30 ALT Altitude Hold System, Model ST-716, according to Bulletin No. 816, dated 8-06-97 and Master Drawing List No. 921019, dated 8-06-97 or later FAA Approved revisions of the above data (14 Volt System).

Limitations and Conditions: enditions:

Also eligible on Models PA-24 (PA-24-180), PA-24-250, and PA-24-260 When Modified In Accordance With STC SA4-1351 or STC SA4-1235 As Applicable (Wing Tip Tanks).

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

Date of Application: 8-08-97 Date Reissued:

Date of Issuance: 8-12-97 Date Amended:

By Direction of the Administrator FEDERAL AVIATION Win Same TOMINISTRATIO William J. Thomas DAS Staff Coordinator, DAS 5 SW (hitle)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA09266AC-D Limitations and Conditions: (con't.)

2. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891489, dated 8-12-97 is required for Piper Models PA-24 (PA-24-180), PA-24-250, and PA-24-260 And The Above Models When Modified In Accordance With STC SA4-1351 or STC SA4-1235 As Applicable (Wing Tip Tanks) or later FAA Approved revisions of the above supplement.

3. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891490, dated 8-12-97 is required for Piper Model PA-24-400 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

The FAR will reissue the certificate in the name of the transferee end forward 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 2IP 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
Piper Aircraft Inc.PA-241A15
Piper Aircraft Inc.PA-24-2501A15
Piper Aircraft Inc.PA-24-2601A15
Piper Aircraft Inc.PA-24-4001A15