# STC SA5298SW-D

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: S-TEC Corporation, United States
- Description: Installation of S-TEC System 60 pitch stabilization system Model ST-060.
- Applied: January 30, 1984
- Status date: March 25, 2002
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A4EU](https://openairdocs.org/tcds/A4EU)
- Certificate PDF: https://openairdocs.org/files/sha256/f6/bb/f6bb92014109a7cfabb8809141d3015f0b7755994cc4e17c51bdf9ef9e4a0518
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E22D458512B97A5A85256CC200122821.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA5298SW-D

## ADs that name it (0)

None.

## Approved models (3)

- Cessna Aircraft Company F172M ([TCDS A4EU](https://openairdocs.org/tcds/A4EU))
- Cessna Aircraft Company F172N ([TCDS A4EU](https://openairdocs.org/tcds/A4EU))
- Cessna Aircraft Company F172P ([TCDS A4EU](https://openairdocs.org/tcds/A4EU))

## What the certificate says

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: SA52985W-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 Civil dir Regulations.

Original Product I ype bertificate Number: A4EU Make: Reims Aviation S.A. Cessna Model: F172M, F172N, and F172P Description of Type Design 6 hange:

Installation of S-TEC System 60 Pitch Stabilization System, Model ST-060, according to Bulletin No.

163, Revision 6, dated 3-20-02 and Master Drawing List No. 9255, Revision F, dated 3-20-02 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: 1-30-84 Date Reissued:

Date of Issuance: 4-4-84 Date Amended: 8-19-86, 3-25-02 FEDERAL AVIATION By Direction of the Administrator milk * (Signature) TOMINSTRATO Michael Keirnan DAS Staff Coordinator, DAS 5 SW (Title) 47

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA52985W-D Limitations and Conditions: (con't.)

Also eligible on Reims Aviation S.A. Cessna models when modified by 180 H.P. engine conversion.

FAA Approved Supplemental Flight Manual, P/N 89392, dated 4-4-84 is required for Reims- Cessna model F172N or later FAA Approved revisions of the above supplement.

FAA Approved Supplemental Flight Manual, P/N 89392-1, dated 8-19-86 is required for Reims- Cessna model F172N and this model when modified by 180 H.P. Engine Conversion or later FAA Approved revisions of the above supplement.

FAA/DAS Approved Supplemental Flight Manual, P/N 89392, Revision 2, dated 3-25-02 is required for Reims Aviation S.A. Cessna models F172M, F172N, and F172P and these models when modified by 180 H.P. engine conversion or later FAA Approved revisions of the above supplement.

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 and street) (City, Stale, and ZIP code) Extent of Authority (if licensing agreement):

Date of Transfer: _ Signature of grantor (In ink):

U.S. GOVERNMENT PRINTING OFFICE: 1900 OF OF-205-S7S

## Every issue (1)

- March 25, 2002: Amended, Current. [certificate](https://openairdocs.org/files/sha256/f6/bb/f6bb92014109a7cfabb8809141d3015f0b7755994cc4e17c51bdf9ef9e4a0518)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.