What it approves
Installation of interior envelope panels
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 (5/14) Page 1 of 2
Number: SA4785SW
Part 25 of the Federal Aviation Regulations
Original Product – Type Certificate Number: A21EA Make: Canadair Model: CL-600-1A11 Description of Type Design Change:
Installation of interior envelope panels according to Report No. CH82-100R Drawing List, Revision D, dated 9/30/82, or later FAA Approved revision.
The installer must determine whether this design change is compatible with previously approved modifications. 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.
Date of Application: March 30, 1982 Date Reissued: May 16, 1989; January 5, 2016; August 1, 2016 Date of Issuance: September 30, 1982 Date Amended:
Signature
Title John Hardie Acting Manager, Fort Worth Aircraft Certification Office, Southwest Region Aero Shade Technologies, Inc.
3104-3106 Industrial Avenue Three Fort Pierce, FL 34946
FAA Form 8110-2 (5/14) Page 2 of 2
Transfer the ownership of Supplemental Type Certificate Number: SA4785SW
To (Name and address of transferee)
From (Name and address of grantor)
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST10962SC
FAA Form 8110-2 (5/14) Page 3 of 3
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Bombardier Inc. | CL-600-1A11 (CL-600) | A21EA |
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| August 1, 2016 | Reissued, current | Certificate |
| August 8, 1989 | Amended, earlier issue | Certificate |