# STC SA00786SE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Aviation Innovations LLC, United States
- Description: Installation of Aviation Innovations fuel pump motor modification in accordance with Aviation Innovations Drawing List DLPA30, Revision G, dated August 1, 2002, or later FAA approved revision.
- Applied: August 20, 1999
- Status date: October 10, 2002
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS A1EA](https://openairdocs.org/tcds/A1EA)
- Certificate PDF: https://openairdocs.org/files/sha256/60/2e/602e5dfe75049256b28c23bee3304b79b30f2b036c882aa20741fdc2756a017a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/58B9D641F3639D6B86257995006B0D0B.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00786SE

## ADs that name it (0)

None.

## Approved models (2)

- Piper Aircraft Inc. PA-30 ([TCDS A1EA](https://openairdocs.org/tcds/A1EA))
- Piper Aircraft Inc. PA-39 ([TCDS A1EA](https://openairdocs.org/tcds/A1EA))

## 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 SA00786SE

This certificate issued to Aviation Innovations, LLC 35004 NE. 185 th Ave.

Yacolt, WA 98675 Part 3 of the Civil Air Regulations.

Original ProductType Certificate Number: A1EA Make: New Piper (Piper) Model: PA-30, PA-39

Description of the Type Design Change: Installation of Aviation Innovations fuel pump motor modification in accordance with Aviation Innovations Drawing List DLPA30, Revision G, dated August 1, 2002, or later FAA approved revision.

Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined that the relationship 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 must 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: August 20, 1999 Date reissued: February 22, 2002 Date of issuance: February 29, 2000 Date amended: December 20, 2000; October 10, 2002

(Signature) Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (1)

- October 10, 2002: Amended, Current. [certificate](https://openairdocs.org/files/sha256/60/2e/602e5dfe75049256b28c23bee3304b79b30f2b036c882aa20741fdc2756a017a)

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