What it approves
Installation of STC-AT-141
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 Number:
IMPORT SA04595NY AIRBORNE TECHNOLOGIES GmbH VIKTOR LANG-STRASSE 8 (FLUGPLATZ WIENER NEUSTADT OST) 2700 WIENER NEUSTADT AUSTRIA 23 Title 14 Code of Federal Regulations A9EA Viking Air Limited DHC-6-400
1. Installation of STC-AT-141, DHC-6 ISR Configuration must be in accordance with Airborne Technologies GmbH Installation Instruction Document No. STC-141-G-II, Revision 0, dated June 4, 2020, or later EASA approved revisions.
(Description of Type Design Change Continued on Page 3 of 3)
1. The installer must determine whether this design change is compatible with previously approved modifications.
(See Limitations and Conditions Continued on Page 3 of 3) February 4, 2021 February 22, 2021 Anthony E. Gallo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 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:
IMPORT SA04595NY 3
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:
IMPORT SA04595NY Date of Issuance: February 22, 2021
Description of Type Design Change (continued):
2. Aircraft is to be maintained in accordance with Airborne Technologies GmbH Maintenance Manual Supplement Document No. STC-141-G-AMM, Revision 0, dated June 29, 2020, or later EASA accepted revisions.
3. Aircraft operation must be in accordance with Airborne Technologies GmbH Flight Manual Supplement STC-141-G-AFM, Revision 0, dated June 29, 2020, or later EASA approved revisions.
2. 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.
3. This STC is applicable to all serial numbers for Viking Air Limited, Model DHC-6-400 aircraft.
4. IKHANA DHC-6 Wing Payload Hard Points must be installed as per FAA STC SA02627LA.
5. Aircraft operation must be in accordance with "Limitations" section of Airborne Technologies GmbH Flight Manual Supplement STC-141-G-AFM, Revision 0, dated June 29, 2020, or later EASA approved revisions.
6. This approval integrates the installation of HD Downlink as provision.
Any function and operation of the HD Downlink will be subject to additional FAA engineering approval.
7. This approval integrates the installation of a satellite antenna as provision.
Any function and operation of the satellite antenna will be subject to additional FAA engineering approval.
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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 |
|---|---|---|
| Viking Air Limited | DHC-6-400 | A9EA |