# STC SA01269LA

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Evans & Bailey Holdings LLC, United States
- Description: Installation of replacement wing tip fairing assembly.
- Applied: March 1, 2001
- Status date: February 23, 2017
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A1CE](https://openairdocs.org/tcds/A1CE)
- Certificate PDF: https://openairdocs.org/files/sha256/c8/81/c881aa8592c0fc1684c38a87b2b09e33528949b3bab549dc92bea64f7b64173c
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6279985759FD1817862580D000615E3F.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01269LA

## ADs that name it (0)

None.

## Approved models (14)

- Beechcraft Corporation 19A ([TCDS A1CE](https://openairdocs.org/tcds/A1CE))
- Beechcraft Corporation 23 ([TCDS A1CE](https://openairdocs.org/tcds/A1CE))
- Beechcraft Corporation A23 ([TCDS A1CE](https://openairdocs.org/tcds/A1CE))
- Beechcraft Corporation A23-19 ([TCDS A1CE](https://openairdocs.org/tcds/A1CE))
- Beechcraft Corporation A23-24 ([TCDS A1CE](https://openairdocs.org/tcds/A1CE))
- Beechcraft Corporation A23A ([TCDS A1CE](https://openairdocs.org/tcds/A1CE))
- Beechcraft Corporation A24 ([TCDS A1CE](https://openairdocs.org/tcds/A1CE))
- Beechcraft Corporation A24R ([TCDS A1CE](https://openairdocs.org/tcds/A1CE))
- Beechcraft Corporation B19 ([TCDS A1CE](https://openairdocs.org/tcds/A1CE))
- Beechcraft Corporation B23 ([TCDS A1CE](https://openairdocs.org/tcds/A1CE))
- Beechcraft Corporation B24R ([TCDS A1CE](https://openairdocs.org/tcds/A1CE))
- Beechcraft Corporation C23 ([TCDS A1CE](https://openairdocs.org/tcds/A1CE))
- Beechcraft Corporation C24R ([TCDS A1CE](https://openairdocs.org/tcds/A1CE))
- Beechcraft Corporation M19A ([TCDS A1CE](https://openairdocs.org/tcds/A1CE))

## 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 SA01269LA

This Certificate issued to

Part 23 of the Civil Air or Federal Aviation Regulations.

Installation of replacement wing tip fairing assembl y in accordance with FAA approved Met -Co- Aire Controlled Drawing List, MCA2-1-02, dated October 2, 2001, or later FAA approved revision.

Limitations and Conditions: The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. The approval of this modification applies to the above noted airplane model series only. 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.

Evans & Bailey Holdings LLC 709 Airport Road Burlington, WI 53105 A1CE

Raytheon Aircraft Company (Beech)

19A, B19, M19A, 23, A23, A23A, A23-19, A23-24, B23, C23, C24, A24R, B24R and C24R Series Airplanes Original Product Type Certificate Number :

Date reissued : February 23, 2017

(Signature) Manager, Technical & Administrative Support Staff, ANM-103L

(Title)

Date of application : March 1, 2001

Date of issuance : November 21, 2001

Number (STC No.)

Limitations and Conditions continued

## Every issue (1)

- February 23, 2017: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/c8/81/c881aa8592c0fc1684c38a87b2b09e33528949b3bab549dc92bea64f7b64173c)

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