# STC SA2-213

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Staggerwing Museum Foundation Inc., United States
- Description: Installation of modified wing tips.
- Applied: May 6, 1958
- Status date: October 6, 2006
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A-2-582](https://openairdocs.org/tcds/A-2-582), [TCDS A-757](https://openairdocs.org/tcds/A-757), [TCDS A-765](https://openairdocs.org/tcds/A-765)
- Certificate PDF: https://openairdocs.org/files/sha256/e3/fa/e3fa70539817688f6cf28d54e87b5d26340b70b149c45c07bb3091c680700249
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F506696E1196E5A9862574F10063582A.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA2-213

## ADs that name it (0)

None.

## Approved models (7)

- Hawker Beechcraft Corporation Army AT-11 ([TCDS A-2-582](https://openairdocs.org/tcds/A-2-582))
- Hawker Beechcraft Corporation C-45G ([TCDS A-765](https://openairdocs.org/tcds/A-765))
- Hawker Beechcraft Corporation C-45H ([TCDS A-765](https://openairdocs.org/tcds/A-765))
- Hawker Beechcraft Corporation C18S ([TCDS A-757](https://openairdocs.org/tcds/A-757))
- Hawker Beechcraft Corporation D18S ([TCDS A-765](https://openairdocs.org/tcds/A-765))
- Hawker Beechcraft Corporation TC-45G ([TCDS A-765](https://openairdocs.org/tcds/A-765))
- Hawker Beechcraft Corporation TC-45H ([TCDS A-765](https://openairdocs.org/tcds/A-765))

## 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.

This certificate issued to: Staggerwing Museum Foundation, Inc.

560 Old Shelbyville Hwy Tullahoma, TN 37388

Part * of the Civil Air Regulations. * CAR 03 dated 11/13/45 and 3.242 of CAR 3 effective 11/01/49 as amended by 3-14.

Original Product - Type Certificate Number : 765, 757 and 2-582 Make : Beech Model : D18S, C-45G/H, TC-45G/H, Conrad 9800D/E, C18S, and AT-11

Installation of modified wing tips in accordance with Airline Training, Inc. Drawing No. 12034A dated 01/06/59, revised 04/25/60.

This modification is eligible on standard Beech Models AT-11, C18S, D18S, C-45G, TC-45G, C-45H, TC-45H, and when installed in conjunction with SA4-113 or SA4-128 Airline Training, Inc. speed up kits, and SA4-119, SA2-383, or SA2-523 Airline Training, Inc. revised horizontal stabilizer.

Airworthiness compatibility of this STC with all other major changes to the standard original model(s) shown above should be confirmed prior to installation of this STC. 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 reissued : December 9, 1966; August 15, 1968;

February 26, 1990; October 6, 2006 Date amended : July 11, 1960

Original signed by Robert D. Adamson

( Signature) Robert D. Adamson Program Manager Wichita Aircraft Certification Office (Title) Date of application : May 6, 1958 Date of issuance : January 15, 1959

## Every issue (1)

- October 6, 2006: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/e3/fa/e3fa70539817688f6cf28d54e87b5d26340b70b149c45c07bb3091c680700249)

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