# STC SA02371AK

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Paul A. Woodward, United States
- Description: Installation of Lycoming O-320-B2B engine, McCauley 1A175/GM propeller and modification of airframe
- Applied: August 29, 2005
- Status date: April 22, 2010
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A-725](https://openairdocs.org/tcds/A-725)
- Certificate PDF: https://openairdocs.org/files/sha256/fa/7d/fa7ded3c1cf8c3fe4f98c37ab27b220bf74de6ad77fdfae08a19ca849aa08f29
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4B398A8E64C936BB8625771900759314.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02371AK

## ADs that name it (0)

None.

## Approved models (1)

- FS 2001 Corp. J5C ([TCDS A-725](https://openairdocs.org/tcds/A-725))

## 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 Paul A. Woodward 12201 Lady Slipper Lane Palmer, Alaska 99645

Part 4a of the Civil Air Regulations

Original Product — Type Certificate Number: A-725 Make: FS 2001 Corp. (The New Piper Aircraft, Inc.)

Model: J5C

Description of Type Design Change: Installation of Lycoming O-320-B2B engine, McCauley 1A175/GM propeller and modification of airframe in accordance with Configuration Specification, PW-J5PA12-06, Revision x1, dated November 2009.

1. Data pertaining to this modification are inadequate for duplication in other aircraft. This approval is limited to Piper J5C, Serial Number 5-1394 only. No additional modifications of this type are to be approved solely by reference to this Supplemental Type Certificate.

2. Aircraft Flight Manual Supplement No. PW-AFMS-J5PA12-01, dated April 22, 2010, or later FAA approved revision, is a required part of this modification.

3. For instructions for continued airworthiness, refer to Instructions for Continued Airworthiness, PW-ICA- J5PA12-03, Revision B, dated April 2010, or later FAA accepted revision.

4. A copy of this Certificate must be maintained as part of the permanent record of the modified aircraft.

Date of application: August 29, 2005 Date reissued:

Date of issuance: April 22, 2010 Date amended:

( Signature) August A. Asay Manager, Anchorage Aircraft Certification Office

( Title)

## Every issue (1)

- April 22, 2010: Issued, Current. [certificate](https://openairdocs.org/files/sha256/fa/7d/fa7ded3c1cf8c3fe4f98c37ab27b220bf74de6ad77fdfae08a19ca849aa08f29)

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