# STC SA00054WI

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: P Ponk Aviation, United States
- Description: Installation of McCauley D3A32C411/82NDA-2 propeller.
- Applied: April 1, 1993
- Status date: September 22, 2005
- Product: Aircraft, Single-Engine
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13)
- Certificate PDF: https://openairdocs.org/files/sha256/bc/52/bc52ad2422297f7c7415c352643c004e3f77bf9bc0fcec816ef26efad34732f3
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2D0CD8DB79297C68862571710051791F.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00054WI

## ADs that name it (0)

None.

## Approved models (9)

- The Cessna Aircraft Company 182E ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182F ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182G ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182H ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182J ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182K ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182L ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182M ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182P ([TCDS 3A13](https://openairdocs.org/tcds/3A13))

## 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.

This certificate issued to: P. Ponk Aviation 1212 Moore Road #2 Camano Island, WA 98282-8820

Part 3 of the Civil Air Regulations.

Original Product - Type Certificate Number : 3A13 Make : Cessna Model : 182 E, F, G, H, J, K, L, M and P Description of Type Design Change:

Installation of McCauley D3A32C411/82NDA-2 propeller as listed on the C S Industries Installation Instructions No. 411 dated April 1, 1993, or later “FAA Approved” revision.

This approval should not be extended to other specific airplanes of these models on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of the other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane. Airplanes must be equipped with a Continental 0-470-R or 0-470-S engine.

Propeller diameter not over 80” not under 78” pitch settings at 30” station low 11.0 deg high 25.6 deg McCauley D6594 spinner kit and compatible governor required. (See TCDS 3A13.) 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 reissued : September 22, 2005

Date amended : October 11, 1994

Original signed by Dan Withers

(Signature) Dan Withers Program Manager Wichita Aircraft Certification Office (Title) Date of application : April 1, 1993 Date of issuance : April 23, 1993

## Every issue (1)

- September 22, 2005: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/bc/52/bc52ad2422297f7c7415c352643c004e3f77bf9bc0fcec816ef26efad34732f3)

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