# STC SA3-632

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Staggerwing Museum Foundation Inc., United States
- Description: Beech Kit 581-1, except angle of incidence change (Item 602) and stall strips (Item 607c) of Spec. A-765; with STC SA2-383, with or without STC's SA2-204 and SA3-409; and wing spar mod. Maximum gross weight: takeoff 9,500 lbs., landing 9,400 lbs.
- Applied: August 3, 1961
- Status date: August 12, 2005
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A-765](https://openairdocs.org/tcds/A-765)
- Certificate PDF: https://openairdocs.org/files/sha256/ff/97/ff97fca9bddb36cd38952bc1201ca2e4e43ccdae504da4122ebc888edcad4980
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A4094FD4B3E65A1F862570D1006B9E8A.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA3-632

## ADs that name it (0)

None.

## Approved models (5)

- Raytheon Aircraft Company C-45G ([TCDS A-765](https://openairdocs.org/tcds/A-765))
- Raytheon Aircraft Company C-45H ([TCDS A-765](https://openairdocs.org/tcds/A-765))
- Raytheon Aircraft Company D18S ([TCDS A-765](https://openairdocs.org/tcds/A-765))
- Raytheon Aircraft Company TC-45G ([TCDS A-765](https://openairdocs.org/tcds/A-765))
- Raytheon Aircraft Company 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 Highway Tullahoma, Tennessee 37388 Part CAR 3 of the Civil Air Regulations.

A-765 Beech C-45G, TC-45G, C-45H, TC-45H, D18S Description of Type Design Change: Combination Beech Kit No. 581-1, except angle of incidence change (Item 602) and stall strips (Item 607c); with STC SA2-383, with or without SA2-204 and SA3-409 and wing spar modification per American Turbine Engine Co. Dwg. No. B-122 dated 09/29/60. Maximum gross weight: Take-off 9500 lbs., Landing 9400 lbs.

Data Required for installation: American Turbine Engine Company Drawing No. B-122 revised July 31, 1961 and Airplane Flight Manual Revision Dated April 13, 1961.

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.

This certificate and the supporting data, which is the basis for approval, shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of application : August 3, 1961

Date of issuance : April 14, 1961

Date reissued: April 25, 2005; August 12, 2005

( Signature)

Manager, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office ( Title)

## Every issue (1)

- August 12, 2005: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/ff/97/ff97fca9bddb36cd38952bc1201ca2e4e43ccdae504da4122ebc888edcad4980)

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