# STC SA2422CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Curry Aviation LLC, United States
- Description: Installation of wing leading edge cuffs, drooped tips, stall panels, and aileron gap seals.
- Applied: August 26, 1988
- Status date: December 16, 2022
- Product: Aircraft, Small Airplane
- Data sheets: [TCDS A42EU](https://openairdocs.org/tcds/A42EU)
- Certificate PDF: https://openairdocs.org/files/sha256/0d/48/0d488880439ac424bde18648a8eac846a1326fb827454c75aa28a5183c794575
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187486999920231012135234.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA2422CE

## ADs that name it (0)

None.

## Approved models (3)

- Textron Aviation Inc. F182P ([TCDS A42EU](https://openairdocs.org/tcds/A42EU))
- Textron Aviation Inc. F182Q ([TCDS A42EU](https://openairdocs.org/tcds/A42EU))
- Textron Aviation Inc. FR182 ([TCDS A42EU](https://openairdocs.org/tcds/A42EU))

## 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 2 SA2422CE Curry Aviation, LLC 616 N. Palmetto Street Leesburg, FL 34748 Civil Air Regulations.3 Installation of STOL Kit (wing leading edge cuffs, drooped tips, stall fences and aileron gap seals). Data required:

1. FAA Approved STOL-Craft Drawing List No. 1, dated May 7, 1973, or later FAA approved revision, and

2. FAA Approved Airplane Flight Manual Supplement (AFMS), dated October 5, 1988, or later FAA approved revision.

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

2. FAA Approved Airplane Flight Manual Supplement (AFMS), dated October 5, 1988, is required for installation on Model F182Q S/N F18200095 and on, and Model FR182 S/N FR18200021 and on.

for Paul Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service Textron Aviation (Cessna) F182P, F182Q, FR182 12/16/2022August 26, 1988 October 5, 1988 A42EU

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):

2 SA2422CE

## Every issue (1)

- December 16, 2022: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/0d/48/0d488880439ac424bde18648a8eac846a1326fb827454c75aa28a5183c794575)

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