# STC SA00001CH

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Aero Fabricators Co, United States
- Description: Install Aero Fabricators shoulder harness and seat belt assembly
- Applied: July 2, 1992
- Status date: July 6, 1995
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS 2A13](https://openairdocs.org/tcds/2A13)
- Certificate PDF: https://openairdocs.org/files/sha256/ac/4d/ac4d81c9d7e6ecec1bbac60420c49ba2d850d084d3b5e25e24bdab28d1cf5a8e
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0ECF3ED93D565BA98625836A004BAA0C.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00001CH

## ADs that name it (0)

None.

## Approved models (9)

- Piper Aircraft Inc. PA-28-140 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-150 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-151 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-160 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-161 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-180 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-235 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28R-180 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28R-200 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))

## What the certificate says

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

United States of America SA 1114CH14 Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA00001CH This certificate issued to: 1216 North Road Aero Fabricators, Inc.

Lyons, WI 53148 Part 3 of the CiVi1 Air Regulalions. (See Type Certificate Data Sheet No. 2A13 for complete certication Dasis.

Original Product -Sype bertificateAumber:2A1 Make: piper Aircraft Corp.

Model: PA-28-140, PA-28-150, PA-28-151, Description of Type Design Change: PA-28-235, PA-28R-180, PA-28R-200 PA-28-160, PA-28-161, PA-28-180, Install Aero Fabricators shoulder harness and seat belt assembly per Aero Fabricators Installation Instructions AF-44, Revision A, dated January 12, 1993, er later FAA approved revisions.

This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft.

Date of Application: July 2, 1992 Jute wissued:

Date of Issuance: . October 13, 1992 Jale unvended: July 6, 1995 + EDERAL AVIATION By Direction of the Administrator Per Charles L/ Smalley(Signature) TO MINIST RAND Manager, Airframe and Administrative Branch Chicago Aircraft Certification Office (Title)

47.

## Every issue (1)

- July 6, 1995: Amended, Current. [certificate](https://openairdocs.org/files/sha256/ac/4d/ac4d81c9d7e6ecec1bbac60420c49ba2d850d084d3b5e25e24bdab28d1cf5a8e)

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