What it approves
Installation of Aerospace Logic Aircraft Instruments
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.
the attached FAA AML.
Description of Type Design Change: Installation of Aerospace Logic Aircraft Instruments, identified in document No. S20 0-CPL, Rev.1.0, dated 12/02/2009 or later Transport Canad a approved revisions , as primary or secondary, new or replacement instruments. Installation must be in accordance with Aerospace Logic Document No. S200- CIL, Rev . 1.0, dated 12/02/2009, Transport Canada approved 12/14/2009, or later Transport Canada approved revisions.
Aerospace Logic Inc.
180 James Street South, Suite 205 Hamilton, Ontario Canada L8P4V1 * See attached FAA Approved Model List dated 07/28/2010 or later FAA approved revisions for the list of approved airplane models.
Date of application: January 15, 2010
Date of issuance: July 28, 2010
FAA Form 8110-2-1(10-69) Page 2 of 2
Number SA02825NY
Date of Issuance: July 28, 2010
1. Operation of instruments utilizing an intensity control module must be in accordance with Aerospace Logic - Document S200-FMS, Rev. 1.0, dated 12/02/2009, Transport Canada approved 12/14/2009, or later Transport Canada revisions.
2. Installation limitations must be observed in accordance with Aerospace Logic Installation Limitations Statement – Document No. S200-ILS, Rev. 1.0, dated 12/02/2009, Transport Canada approved 12/14/2009, or later Transport Canada approved revisions. The products are to be installed in existing panel holes and are to replace existing instrumentation. As primary replacement products it is recommended and preferred that they be placed in the same panel location as the original equipment. Their visibility and placement relative to other instruments are to be the same or similar to the existing instruments. Where they are in a different location, it is the responsibility of the installer to ensure that they are visible to the pilot under all conditions.
3. Maintenance must be in accordance with Aerospace Logic Instructions for Continued Airworthiness – Document No. S200-ICA, Rev.1.2, dated 5/04/2010 or later Transport Canada accepted revisions.
4. The installer must determine whether this design change is compatible with previously approved modifications.
5. 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.
……………………END………………………..
(Signature) Anthony Socias Manager New York Aircraft Certification Office
(Title)
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 758
| Make | Model | Data sheet |
|---|---|---|
| Aerostar Aircraft Corporation | 360 | A11WE |
| Aerostar Aircraft Corporation | 400 | A11WE |
| Aerostar Aircraft Corporation | PA-60-600 (Aerostar 600) | A17WE |
Every issue · 1
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| October 10, 2012 | Amended, current | CertificateApproved model list |