# STC SA2650CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Advanced Aircraft Extinguishers Ltd, United States
- Description: Installation of class C cargo compartment fire extinguisher and smoke detector systems.
- Applied: March 2, 1990
- Status date: February 1, 1993
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A20EA](https://openairdocs.org/tcds/A20EA)
- Certificate PDF: https://openairdocs.org/files/sha256/f7/df/f7df6104fc54235d334b7de471b1452a3ba3b8991a0d2c30e9b7f0675f09fb8d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/30176D892B2BFD1185256CC20008C6DD.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2650CE

## ADs that name it (0)

None.

## Approved models (1)

- Bombardier-Rotax GmbH DHC-7-100 ([TCDS A20EA](https://openairdocs.org/tcds/A20EA))

## 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 Number: SA2650CE This certificate issued to: Advanced Aircraft Extinguishers, Ltd. P.O. Box 1117 Blue Springs, MO 64013-1117 Certifies that the change in the type design for the following product with the limitations and conditions Regulations. in addition to Amendments to FAR 36, SFAR 27, and special conditions shown on TCDS No. A20EA.

Original Product - Type berlificate Numben: AZOBA Make: DeHavilland Model: DHC-7-100 Series Description of Type Design Change:

Installation of Total Flood Corporation Class C Cargo Compartment Fire Extinguisher and Smoke Detector Systems in accordance with: (1) Total Flood Corporation Master Drawing TFA 10-0050, Revision none, dated August 17, 1990, and (2) FAA approved Airplane Flight Manual Supplement TFA-09-0036, dated September 11, 1990, or later FAA approved Revisions Limitations and Conditions:

This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane.

SIC SA7866SW must be completed prior to or concurrent with this installation.

Date of Application: March 2, 1990 Jule rissued: February 1, 1993 Date of Issuance: September 11, 1990 Date Amended:

EDERAL AVIATION By direlion has Send for Ronald K. Rathgeber * (Signature ) TO MINISTRATION Wichita Aircraft Certification Office Ronald K. Rathgeber, Acting Manager (Title) 47 FAA FORM 8110-2 (10-68)

## Every issue (1)

- February 1, 1993: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/f7/df/f7df6104fc54235d334b7de471b1452a3ba3b8991a0d2c30e9b7f0675f09fb8d)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.