# STC SA1623GL

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: McCauley Propeller Systems, United States
- Description: Installation of McCauley governor model C290D3(x)/T39.
- Applied: January 24, 1991
- Status date: July 19, 2006
- Product: Aircraft, Single-Engine
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 2A13](https://openairdocs.org/tcds/2A13)
- Certificate PDF: https://openairdocs.org/files/sha256/b2/5b/b25be60846c77206ccfbf83b8207da301498e6b28317b576e8c874d163811485
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/27F2C9C0913B98E7862571CD005B5EE2.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA1623GL

## ADs that name it (0)

None.

## Approved models (4)

- The New Piper Aircraft Inc. PA-28R-180 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- The New Piper Aircraft Inc. PA-28R-200 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- The New Piper Aircraft Inc. PA-28R-201 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- The New Piper Aircraft Inc. PA-28RT-201 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

FAA FORM 8110-2(10-68) PAGE 1 of 2 PAGES Number SA1623GL This certificate issued to McCauley Propeller Systems 7751 East Pawnee Wichita, KS 67207

Part 3 of the Civil Air Regulations.

See Type Certificate Data Sheet No. 2A13 for the complete certification basis

Original Product-Type Certificate Number : 2A13 Make : The New Piper Aircraft, Inc.

Model : PA-28R-180, PA-28R-200, PA-28R-201, PA-28RT-201 Description of Type Design Change:

Installation of McCauley Governor Model C290D3(x)/T39 or DC290D1(x)/T18 in accordance with McCauley Technical Report 762, revised November 25, 1991, or later FAA-Approved revision.

1. Compatibility of this design change with previously approved modifications must be determined by the installer.

2. This approval is only applicable to the following Piper aircraft model and serial numbers and Lycoming Engine Models:

Model Serial No. Engine HP RPM PA-28R-180 All IO-360-B1E 180 2700 PA-28R-200 28R-7235001 & up IO-360-C1C6 200 2700 PA-28R-201 28R-7737002 & up IO-360-C1C6 200 2700 PA-28RT-201 28R-7918001 thru 7918267 IO-360-C1C6 200 2700 PA-28RT-201 28R-8018001 & up IO-360-C1C6 200 2700

3. 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.

…End… This certificate and the supporting data, which is the basis for approval, shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date reissued : July 19, 2006

Date amended : May 1, 1992; November 28, 1992

( Signature) Thaddeus D. Krolicki, Jr.

Manager, Propulsion Branch Chicago Aircraft Certification Office

(Title) Date of application: January 24, 1991

Date of issuance : July 2, 1991

## Every issue (1)

- July 19, 2006: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/b2/5b/b25be60846c77206ccfbf83b8207da301498e6b28317b576e8c874d163811485)

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