# STC SA470CH

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Pegasus Innovations, LLC
- Description: Installation of 3M Scotch #8672 one inch wide polyurethane tape as gap seals for the ailerons and the stabilizer trim tabs.
- Status date: December 1, 2020
- Data sheets: 2A13, 2A13, 2A13, 2A13, 2A13, 2A13, 2A13, 2A13, 2A13, 2A13, 2A13, 2A13, 2A13, 2A13, 2A13, 2A13
- Certificate PDF: https://openairdocs.org/files/sha256/cf/31/cf31a7f758f0a5435e3f3f64b2224b95d3d41240484a3468643da9ffcc897cb4
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132056532020260428174443.0001
- Page: https://openairdocs.org/stc/SA470CH

## ADs that name it

None.

## Approved models (16)

- Piper Aircraft Inc. PA-28-140 (TCDS 2A13)
- Piper Aircraft Inc. PA-28-150 (TCDS 2A13)
- Piper Aircraft Inc. PA-28-151 (TCDS 2A13)
- Piper Aircraft Inc. PA-28-160 (TCDS 2A13)
- Piper Aircraft Inc. PA-28-161 (TCDS 2A13)
- Piper Aircraft Inc. PA-28-180 (TCDS 2A13)
- Piper Aircraft Inc. PA-28-181 (TCDS 2A13)
- Piper Aircraft Inc. PA-28-201T (TCDS 2A13)
- Piper Aircraft Inc. PA-28-235 (TCDS 2A13)
- Piper Aircraft Inc. PA-28-236 (TCDS 2A13)
- Piper Aircraft Inc. PA-28R-180 (TCDS 2A13)
- Piper Aircraft Inc. PA-28R-200 (TCDS 2A13)
- Piper Aircraft Inc. PA-28R-201 (TCDS 2A13)
- Piper Aircraft Inc. PA-28R-201T (TCDS 2A13)
- Piper Aircraft Inc. PA-28S-160 (TCDS 2A13)
- Piper Aircraft Inc. PA-28S-180 (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.

SA470CH Pegasus Innovations, LLC 45 Buttercup Loop Belton, TX 76513 Part 3 the Civil Air Regulations.

2A13 Piper Aircraft Corporation PA-28-140, PA-28-150, PA-28-151, PA-28-160, PA-28-161, PA-28-180, PA-28-181, PA-28-235, PA-28-236, PA-28S-160, PA-28S-180, PA-28R-180, PA-28R-200, PA-28R-201, PA-28R-201T, PA-28-201T

1) The installer must determine whether this design change is compatible with previously approved modifications.

2) The Never Exceed Speed (VNE) for the modification is limited to 186 knots (214 mph) Indicated Airspeed (IAS).

(Continued on Page 3) 10/21/1994 8/26/2015 12/1/2020 12/12/1995 9/24/1996 for Roy E. Boffo III Deputy Branch Manager Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 3 Installation of 3M Scotch #8672 one inch wide polyurethane tape as gap seals for the ailerons and the stabilator trim tabs according to the installation instructions titled “Aileron Gap Seal” and “Stabilator-Trim Tab Gap Seal”, no revisions, dated August 18, 1995, or later FAA approved revisions.

(See Type Certificate Data Sheet Number 2A13 for the complete certification basis.)

SA470CH 12/01/20 3

SA470CH 12/01/20 Limitations and Conditions (continued):

3) The Airplane Flight Manual Supplement, dated September 24, 1996 or later FAA approved revisions, is required with this modification.

4) If the airplane is certified with a VNE lower than 214 mph, then this lower VNE remains in effect.

5) If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission.

----------------------------------------------------------END---------------------------------------------------- 3 3 Add Page

## Every issue (2)

- December 1, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/cf/31/cf31a7f758f0a5435e3f3f64b2224b95d3d41240484a3468643da9ffcc897cb4)
- August 26, 2015: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/23/62/23625090813b1d31b6a75a3ca81d7bf709da284d4cccec9523ce275d3c643bb2)

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