# STC SA1072CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Curry Aviation LLC, United States
- Description: Installation of wing leading edge cuffs and droop tips, dorsal fin and vertical stabilizer vortex generator.
- Applied: February 4, 1974
- Status date: December 16, 2022
- Product: Aircraft, Small Airplane
- Data sheets: [TCDS 2A13](https://openairdocs.org/tcds/2A13)
- Certificate PDF: https://openairdocs.org/files/sha256/b1/85/b18543db11f343b2adcd848a893eac7c20419a30505307eb1a8b1e956bcb628a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179111759420231023184505.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA1072CE

## ADs that name it (0)

None.

## Approved models (6)

- Piper Aircraft Inc. PA-28-140 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-150 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-160 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-180 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28R-180 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28R-200 ([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 This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the proper ty of the STC holder.

FAA Form 8110-2 (5/14) Page 1 of This certificate issued to:

Part of the

Signature

Title 3 SA1072CE Curry Aviation, LLC 616 N. Palmetto Street Leesburg, FL 34748 Civil Air Regulations.3 Installation of STOL Kit (wing leading edge cuffs, droop tips, dorsal fins, and vortex generators on the vertical stabilizer).

Data required:

1. FAA Approved STOL-Craft Drawing List No. 6, dated December 5, 1974 or January 7, 1975 or November 6, 1984, or later FAA approved revision, and (continued on page 3)

1. Compatibility of this design with previously approved modification must be determined by the installer.

2. Delete all references to intentional spins from the utility category placard, and adjacent to it add a new placard which reads: "INTENTIONAL SPINS PROHIBITED."

(continued on page 3)

for Paul Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service Piper Aircraft PA-28-140, -150, -160, -180;

PA-28R-180, -200 5/26/1977, 12/16/2022 1/7/75, 2/25/75, 5/1/80, 11/6/84 February 4, 1974 December 5, 1974 2A13

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the proper ty of the STC holder.

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

3 SA1072CE

This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the proper ty of the STC holder.

FAA Form 8110-2 (5/14) Page 3 of

3 Date reissued: 12/16/2022

Type Design Description (continued from page 1):

2. Models PA-28-140, -150, -160, -180: FAA Approved Airplane Flight Manual Supplement (AFMS), dated December 5, 1974 or January 7, 1975, or later FAA approved revision, or

3. Models PA-28R-180, -200: FAA Approved Airplane Flight Manual Supplement (AFMS), dated May 1, 1980 or November 2, 1984, or later FAA approved revision.

Limitation and Conditions (continued from page 1):

3. Model PA-28-140, S/N 28-23989: AFT CG limit is 92.15 inches.

4. Model PA-28-140, S/N 28-23989: eligible for removal of the AFT CG restriction when compliance to Drawing No. 5050, Sheet No. 1, Rev. A, is accomplished.

----- END ----- SA1072CE

## Every issue (1)

- December 16, 2022: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/b1/85/b18543db11f343b2adcd848a893eac7c20419a30505307eb1a8b1e956bcb628a)

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