# STC SA2052WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Pacific Propeller International LLC, United States
- Description: Installation of Hartzell HC82XL-6F/8433-12 propeller(after conversion of engine to Lycoming O-320-E1A model).
- Applied: March 3, 1969
- Status date: March 25, 2004
- 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/sha256/1f/08/1f08b5c9f48bf2734f63eaf1a91379ed0f9cd31baf9967bdeebd01a4beb7c6ff
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4AF7E1A4030F918886256E780067F699.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2052WE

## ADs that name it (0)

None.

## Approved models (1)

- The New Piper Aircraft Inc. PA-28-140 ([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.

Number SA2052WE This certificate, issued to: Pacific Propeller International LLC 5802 South 228th Street Kent, WA 98032-1810

Part 3 of the Civil Air Regulations.

Original Product Type Certificate Number: 2A13 Make: Piper Model: PA-28-140

Description of the Type Design Change: Installation of Hartzell HC82XL-6F/8433-12 propeller in accordance with Pacific Propeller, Inc. Installation Instructions dated March 5, 1969.

Note: Prior to installation of this propeller, the engine must be converted to a Model 0-320-E1A in accordance with Lycoming Service Bulletin No. 1098A and Service Letter No. 164.

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 that the interrelationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate and FAA approved AFM Supplement, dated November 5, 1969, shall be maintained as part of the permanent records for the modified 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.

Date of application: March 3, 1969 Date reissued: 5/9/75; 3/25/04 Date of issuance: November 18, 1969 Date amended: March 25, 2004

(Signature)

Acting Manager, Seattle Aircraft Certification Office (Title)

**FAA FORM 8110-2(10-68**

## Every issue (1)

- March 25, 2004: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/1f/08/1f08b5c9f48bf2734f63eaf1a91379ed0f9cd31baf9967bdeebd01a4beb7c6ff)

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