# STC SA3-150

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Morris J E, United States
- Description: Wright R2600-29 or -20 engines and modifications for 32,000 pound gross weight.
- Applied: December 23, 1965
- Status date: August 21, 1967
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: TCDS 785
- Certificate PDF: https://openairdocs.org/files/sha256/03/96/0396a6da6aaebbad482fd7c58b3d600d061575f068f4fe084d279b7b1479a5db
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/02CFD1973628F40A86258028006DA205.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA3-150

## ADs that name it (0)

None.

## Approved models (1)

- General Dynamics Corporation 28-5ACF (TCDS 785)

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

Federal Stiation Sigency Supplemental Type Certificate Number 513-130 This certificate issued to: J. R. Morcis #1 Lomond Delve Ferguson, Missouri 63135 Certifies that the change in the type design for the floriay fredict with the tinitativis and evrditions CAR 45 (Pover plant airplane performance and flighs characterisefce) Agulations: CAR 3 (Airplane Struccares) as rodified by portione SR405A & 407 Original Product - Typeberificate Number: 90 135 Model: 28-5402 Make: Consolidated Vuitoe Description of Type Design Change:

Femmert Wergex, Inc. Draving P5Y-01016 "p" cheage Installation of Wright 12500- 13, -20, and -29 engines and modifications for 32,000 pound gross weight.

Data Required: The above draving and AFM Suppleaene 7/14/66 or January 5, 1960 for the «20 and -29 engine models, Limitations and Conditions:

IINCOATION OF APPLICABILITY. This approval should not be extended to other specific airplanes of this rodel on which other previously approved modifications are incorporated mless it is determined that the inter-relationship betwean this change and any of those other previously approved modifications will introduce no advarse effect upon the eizworthiness of the airplane.

Date of Application: December 23, 1965 Date Reissued: Angset 22, 1967 Dates issuence: January 10, 1958 Date Amended: 3/27/58, 4/30/58, 2710/59;

By direction of 1252n9 2122167

**ORIGINAL SIGNED BY**

PAUL CLARK (Signature) DED STATES OS Chief, Engineering & Manufactueing Branch for Jobs A. Carran (Title)

FAA FORM 8110-2 (1-66; 0052-657-6000

## Every issue (1)

- August 21, 1967: Amended, Current. [certificate](https://openairdocs.org/files/sha256/03/96/0396a6da6aaebbad482fd7c58b3d600d061575f068f4fe084d279b7b1479a5db)

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