What it approves
Installation of a Digital Engine Monitoring system.
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.
Part 3 / 23 of the Civil Air / Federal Aviation Regulations.
Installation of a Digital Engine Monitoring System in accordance with Xerion, AuRACLE Installation Manual, *see attached AML, Document No. SA02434NY.
1. Aircraft Flight Manual Supplement for the Ultra Electronics Flightline Systems AuRACLE, Engine Management System, Revision D, FAA approved March 15, 2011, is required for this installation.
2. Ultra Electronics Flightline Systems, AuRACLE Engine Management System Pilot Guide, Revision G, dated March 15, 2011, must be carried on the aircraft at all times.
3. Xerion, Engine Management System, Instructions for Continued Airworthiness, Issue A, is required to ensure continued airworthiness of this installation.
4. This approval does not allow the AuRACLE Engine Management System to replace the approved fuel quantity indicating system.
Ultra Electronics Flightline Systems 7625 Omnitech Place Victor, NY 14564-9795
*See attached FAA Approved Model List (AML), Document No.
SA02434NY for the list of approved airplane models and applicable airworthiness regulations.
Date of application: January 27, 2006
Date of issuance: July 24, 2007 Date reissued: August 5, 2009
Date amended: February 7, 2012
( Signature) Tim Hadsall Acting Manager New York Aircraft Certification Office
( Title)
FAA Form 8110-2-1(10-69) Page 2 of 2
Number SA02434NY Date of Amendment: February 7, 2012 Date of Reissuance: August 5, 2009
Limitations and Conditions Cont’d:
5. Dual amp display not authorized for aircraft that require an instrument pressure or vacuum system.
6. The installer must determine whether this design change is compatible with previously approved modifications.
7. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.
Certification Basis:
The Certification Basis is defined as:
1. The type certification basis as shown on the TCDS (see AML, Document No. SA0243NY) for all areas not affected by the change.
2. Title 14 CFR Part 23, dated February 1, 1965, including Amendments 23-1 through 23-54 for the change and all areas affected by the change. The following lists the Federal Aviation Regulations complied with through Amendment Level 23-54.
23.301 23.303 23.305 23.307 23.337 23.561 23.601 23. 603 23.605 23.613 23.771 23.773
23.853 23.863 23.1165 23.1191 23.1301 23.1305 23.1309 23.1311 23. 1321 23.1322 23.1327 23.1331
23.1351 23.1357 23.1359 23.1365 23.1431 23.1519 23.1521 23.1527 23.1543 23.1549
3. Title 14 CFR Part 23, dated February 1, 1965, including Amendments 23-1 through 23-54 for the change and all areas affected by the change. The following lists the additional Federal Aviation Regulations complied with through Amendment Level 23-54 for pressurized aircraft.
23.365 23.571 23.627 ---END---
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 297
Every issue · 6
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| February 7, 2012 | Amended, current | CertificateApproved model list |
| February 24, 2009 | Amended, earlier issue | Certificate02434AML |
| February 24, 2009 | Amended, earlier issue | Certificate02434AML |
| July 10, 2008 | Amended, earlier issue | Certificate02434AML |
| February 25, 2008 | Amended, earlier issue | Certificate02434 |
| July 24, 2007 | Issued, earlier issue | Certificate |