# STC SA1244CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Cub Crafters Inc, United States
- Description: Replacement landing gear components per Flanagan Aircraft Co. Drawing No. 1-9.01, stamped "FAA Approved," with a date of July 7, 1976, or later Federal Aviation Administration (FAA) approved revision.
- Applied: February 14, 1976
- Status date: January 26, 2012
- Product: Aircraft, Single-Engine
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 1A2](https://openairdocs.org/tcds/1A2)
- Certificate PDF: https://openairdocs.org/files/sha256/16/47/16471f7242dc91a14afd9e104fd27839aaf644a9a323e1c3fb184a89b17a38b9
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/CA950284D2236F65862579A6005D9F07.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1244CE

## ADs that name it (0)

None.

## Approved models (2)

- Piper Aircraft Inc. PA-18 ([TCDS 1A2](https://openairdocs.org/tcds/1A2))
- Piper Aircraft Inc. PA-18A ([TCDS 1A2](https://openairdocs.org/tcds/1A2))

## 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 SA1244CE

This certificate, issued to Cub Crafters, Inc.

1918 South 16th Avenue Yakima, WA 98903-1212

Part 3 of the Civil Air Regulations.

Original ProductType Certificate Number: 1A2 Make: Piper Model: PA-18 and PA-18A

Description of the Type Design Change: Replacement landing gear components per Flanagan Aircraft Co.

Drawing No. 1-9.01, stamped "FAA Approved," with a date of July 7, 1976, or later Federal Aviation Administration (FAA) approved revision.

Limitations and Conditions: This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated, unless it is determined that the inter-relationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane. Parts manufactured under this STC may have been produced without an FAA-approved quality control procedure. Prior to installation, such parts must be inspected for conformity and airworthiness in accordance with Federal Aviation Regulations 21 and 43.

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: February 14, 1976 Date reissued: January 15, 1997; January 26, 2012 Date of issuance: July 7, 1976 Date amended:

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

## Every issue (1)

- January 26, 2012: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/16/47/16471f7242dc91a14afd9e104fd27839aaf644a9a323e1c3fb184a89b17a38b9)

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