# STC SA332WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Staggerwing Museum Foundation Inc., United States
- Description: Propeller spinners and increase in maximum continuous power to 450 hp.
- Applied: January 3, 1963
- 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/sha256/57/d4/57d40562215d7394acf61b541c41fa69a9c6dddf3984ff78049922763a583a46
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/BBA0CFC5AC0ABCC3862570C9006DE8AA.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA332WE

## ADs that name it (0)

None.

## Approved models (4)

- Raytheon Aircraft Company C-45G ([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 D18S, C-45G, TC-45G, C-45, TC-45H and SNB-5 Description of Type Design Change: Installation of propeller spinners in accordance with American Turbine Engine Co. drawing No. B-185 and increase in maximum continuous power to 450 hp.

Limitations and Conditions: Prior stabilizer incidence change per STC SA2-383, SA4-554, SA4- 119 or SA2-120 and installation of modified carburetor air intakes per STC SA289WE are required. This Supplemental Type Certificate is applicable only to the noted aircraft when Pratt & Whitney R-985-AN-14B engines and Hamilton Standard Hydromantic 22D30 propellers (Item 2 of Aircraft Specification No. A-765) are installed. This approval should not be extended to other specific airplanes of these models on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those previously approved modifications will introduce no adverse (Continued on page 3)

Date of application : January 3, 1963

Date of issuance : February 6, 1963

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

Date amended : February 25, 1963

( Signature)

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

Number SA332WE

Limitations and Conditions: (Continued)

effect upon the airworthiness of that airplane.

OPERATIONAL LIMITATIONS: American Turbine Engine Company FAA Approved Airplane Flight Manual Supplement dated February 25, 1963, or American Turbine Engine Company FAA Approved Airplane Flight Manual Appendix III dated February 25, 1963, is required.

- END -

## Every issue (1)

- August 12, 2005: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/57/d4/57d40562215d7394acf61b541c41fa69a9c6dddf3984ff78049922763a583a46)

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