# STC SA1093SO

- Type: Supplemental type certificate
- Status: Current, Surrendered
- Holder: Aeronautical Engineers, Inc, United States
- Description: Installation of class 'B' or 'E' cargo compartment.
- Applied: September 26, 1978
- Status date: June 12, 2009
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 4A27](https://openairdocs.org/tcds/4A27)
- Certificate PDF: https://openairdocs.org/files/sha256/2b/ba/2bba2c5eca3dd308227a5698aeb51816af126f0f27f7ab4a29a948b79834db0e
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6B6D0AD669EAF2138625778F0045E6C8.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1093SO

## ADs that name it (0)

None.

## Approved models (2)

- General Dynamics Corporation 22 ([TCDS 4A27](https://openairdocs.org/tcds/4A27))
- General Dynamics Corporation 22M ([TCDS 4A27](https://openairdocs.org/tcds/4A27))

## What the certificate says

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

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Added Notes at Surrender:

Future unsafe conditions existing in the product can Number SA 109350 result in an airworthiness directive requiring correction of the unsafe condition before further flight. If there is no entity to comply with 14 CFR

21.99(a), Required design changes, the existence of This certificate issued to: Aeronautical Engineers, InC. an unsafe condition might result in permanently grounding of the aircran.

2. Replacement parts might not be available in the future.

Part Air Regulationa Original Product -Typebertificate Number: 4A27 STC Surrender processed:

Make: General Dyn Model: 22 and Approval by: Melvin Taylor, ATL ACO Manager Description of Type Design Change: Insta _ai · 10. 476, Revision 6, dated "B" or "I" Make: cargo compartment 6/12/2009 in accordance with Aeronautical Eng‹ July 23, 1979, or later FAA approve STC No. ST907SO is a required part of this STC.

Limitations and Conditions: The appy oval of this change applies basically to General Dynamics Models 22, 22M only. This approval should not be extended to other airplanes of this de on which other previously approved modifications are incorporated unless determined by the installer that the interrelationship between this change nd any of those other previously approved modifications will produce no effect upon the airworthiness of that airplane. This (Continued) the supporling datu which is the bas is for approval shall remain in effect until sur rendered ded, revoked, or a termination date is otherwise established by the Adminis brater if the Federal Aviation Administration .

Date of Application: September 26, 1978 Date Reissued:

Date of Issuance: . August 14, 1979 Sateurended:

FEDERAL ION By Direction of the Administrator PRANCES C. ROCK Francis CRak Acting Chief, Eng panting TOMINISTA and Manufacturing Branch Flight Standards Division (Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA109350 Limitations and Conditions: (Continued) SURRENDER distribution such as an increase in the fixed disposable weight Aeronautical Engineers Report No. R-413, "Cargo Loading dated September 14, 1976, is a required part of this

**FAA FORM 8110-2-1 (10-69) PAGE 2 OF 2 PAGES**

## Every issue (1)

- June 12, 2009: Surrendered, Current. [certificate](https://openairdocs.org/files/sha256/2b/ba/2bba2c5eca3dd308227a5698aeb51816af126f0f27f7ab4a29a948b79834db0e)

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