# STC SA2145NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Turboplus Aircraft Systems, Inc., United States
- Description: Installation of Turboplus intercooler system.
- Applied: September 12, 1983
- Status date: February 24, 2017
- Product: Aircraft, Small Airplane
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 2A13](https://openairdocs.org/tcds/2A13)
- Certificate PDF: https://openairdocs.org/files/sha256/5c/1b/5c1b0cdb607fd6bd42bb252376e35c4c731afb5944cfcc9eba441b87da495eaa
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/40738E48936EE0EB862580D5005FC112.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA2145NM

## ADs that name it (0)

None.

## Approved models (3)

- Piper Aircraft Inc. PA-28-201T ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28R-201T ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28RT-201T ([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.

United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Number SA2145NM

This certificate, issued to Turboplus Aircraft Systems, Inc.

4117 35th Ave NW Gig Harbor, WA 98335

Part 3 of the Civil Air Regulations.

2A13

Piper

PA28-201T; PA-28R-201T; PA-28RT-201T

Description of the Type Design Change: Installation of Turboplus, Inc., Intercooler System PA-28-9000-I-AD, in accordance with Turboplus, Inc., Installation Instructions No. PA28-9000-I-AD, TP-7000, dated July 24, 1985, or later FAA approved revisions.

NOTE: This installation requires the incorporation of Turboplus, Inc., modified air induction systems as per STC SA2144NM.

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 and FAA Approved Flight Manual Supplement 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: September 12, 1983 Date reissued: 07/26/85; 3/20/86; 10/26/87; 10/25/00;

8/25/05; 10/15/07; 2/24/17 Date of issuance: October 13, 1983 Date amended: 12/05/84; 07/26/85; 03/20/86;

10/25/00

(Signature) Manager, Technical and Administrative Support Staff, Los Angeles Aircraft Certification Office (Title)

Transfer the ownership of the Supplemental Type Certificate Number to (Name of transferee) (Address of transfer) (Number and street)

(City, State, and Zip code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street)

(City, State, and Zip code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

## Every issue (3)

- February 24, 2017: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/5c/1b/5c1b0cdb607fd6bd42bb252376e35c4c731afb5944cfcc9eba441b87da495eaa)
- October 15, 2007: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/b5/fe/b5fe100026aa7433659ca12a8393f726e4394aeee5c5658f9bf921f1018b77a0)
- August 25, 2005: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/5b/6f/5b6f4cea4b81ab4430ab0200242b53fa6ff407755283c6ce377a7ccec08722c1)

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