What it approves
Installation of modified fuel injector nozzles.
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate This certificate issued to:
Number: SE09217SC General Aviation Modifications, Inc.
2800 Airport Road, Hangar A Ada, OK 74820 of Federal Aviation Regulations .
*see attached FAA Approved Model List (AML) Installation of modified fuel injector nozzles in accordance with General Aviation Modifications, Inc. “Data List”, Revision 003 dated September 24, 1996, and Installation Procedure No.
IP-96-001, “GAMIjector Installation Procedure for Continental Motors IO-550/520/470 Engines”, Revision 004, dated September 25, 1996, or later FAA approved revisions.
December 22, 1995 April 30, 1996 September 27, 1996; January 08, 1997; February 08, 2021 Jim Grigg Manager, Fort Worth ACO Branch Compliance &Airworthiness Division Aircraft Certification Service
3 Part * Continued page 3 of 3
FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SE09217SC
FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: _SE09217SC 3 3 Certification Basis:
The certification basis for this alteration is the same as the basic aircraft (shown on TCDS A67EU) except as follows: 14 CFR part 23.201, Amendment 23-62.
-END- Limitations and Conditions:
1. This STC only applies to the engine models listed on the attached FAA approved model list. This approval should not be extended to engines 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 other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that engine.
2. Compatibility of this design change with previously approved modifications must be determined by the installer.
The STC does not require any adjustment to the fuel injection control unit.
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 41
| Make | Model | Data sheet |
|---|---|---|
| Continental Aerospace Technologies Inc. | IO-470-D | 3E1 |
| Continental Aerospace Technologies Inc. | IO-470-E | 3E1 |
| Continental Aerospace Technologies Inc. | IO-470-F | 3E1 |
Every issue · 1
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| February 8, 2021 | Amended, current | CertificateAML_SE09217SC |