# STC SA02988AT

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: PowerLite LLC, United States
- Description: Change in rating of the existing Teledyne Continental Motors IO-550-G Model engine to the same as that for the IO-550-G engine installed in the Mooney M20R, 280 hp at 2500 rpm, and the installation of a Hartzell Model PHC-J3YF-1RF/F7693DF(B)-2 propeller.  Aircraft modification shall be performed in accordance with PowerLite Report AP1016-5 Installation Instructions, Revision A dated November 25, 2004, or later FAA Approved revision.
- Applied: December 16, 2003
- Status date: May 17, 2005
- Product: Aircraft, Single-Engine
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 2A3](https://openairdocs.org/tcds/2A3)
- Certificate PDF: https://openairdocs.org/files/sha256/96/ac/96ac896cfd089bfb1fdad44f6c535e0a21a12aa6843a21f43d4d665c7405df32
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A758A46BD17EA47A86257014005440AA.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02988AT

## ADs that name it (0)

None.

## Approved models (1)

- Mooney Aircraft Corporation M20S ([TCDS 2A3](https://openairdocs.org/tcds/2A3))

## 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 1 PAGES Number SA02988AT This certificate issued to PowerLite, LLC 209 River Laurel Way Woodstock, GA 30188

Part 3 of the Civil Air Regulations.

Original Product--Type Certificate Number: 2A3 Make: Mooney Model: M20S

Description of Type Design Change: STC for the change in rating of the existing Teledyne Continental Motors IO-550- G Model engine to the same as that for the IO-550-G engine installed in the Mooney M20R, 280 hp @ 2500 rpm, and the installation of a Hartzell Model PHC-J3YF-1RF/F7693DF(B)-2 propeller. Aircraft modification shall be performed in accordance with PowerLite Report AP1016-5 Installation Instructions, Revision A dated November 25, 2004, or later FAA Approved revision.

Limitations and Conditions: 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 other previously approved modifications will produce no adverse effect upon the airworthiness of that aircraft. 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. The modified aircraft shall be operated in accordance with PowerLite Report AP1016-12, Airplane Flight Manual Supplement, Revision IR dated January 10, 2005, and maintained in accordance with PowerLite Report AP1016-9, Instructions for Continued Airworthiness, Revision A dated November 25, 2004, or later FAA Approved revisions.

Date of application : December 16, 2003

Date of issuance : January 10, 2005 Date reissued : May 17, 2005

( Signature) Melvin D. Taylor Manager Atlanta Aircraft Certification Office

(Title)

## Every issue (2)

- May 17, 2005: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/96/ac/96ac896cfd089bfb1fdad44f6c535e0a21a12aa6843a21f43d4d665c7405df32)
- January 10, 2005: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/90/46/90468f321a06fc5e2eb261e1afe17cf153ee9e77dda9fc786a6bddaa02bd0637)

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