STC ST00046MC-D

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Original signed by Keith Johnston

United States of America Department of Transportation Federal Aviation Administration TORM STRATOS Supplemental Type Certificate Number: S100046MC-D

FEDERAL AVIATION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST00046MC-D Description of Type Design Change: (continued);

The following documents are required for MDL BAS67015003 (no dash #) configuration of this SIC:

Airplane Flight Manual Supplement BAS67045003, Revision NC, FAA Approved May 27, 2010 or later FAA approved revision.

Instructions for Continued Airworthiness, BAS67015003-ICA-1, revision (NC), dated April 16, 2010, FAA accepted May 27, 2010 or later FAA accepted revision.

The following documents are required for MDL BAS67015003-003 configuration of this STC:

Airplane Flight Manual Supplement BAS67045003, Revision A, FAA Approved September 9, 2013 or later FAA approved revision.

Instructions for Continued Airworthiness, BAS67015003-ICA-1, revision (B), dated June 7, 2013, FAA accepted September 9, 2013 or later FAA accepted revision.

The following document is required for MDL BAS67015003-005 configuration of this STC:

Instructions for Continued Airworthiness, BAS67015003-ICA-1, revision (C), dated October 18, 2013, FAA accepted January 28, 2014 or later FAA accepted revision.

Certification Basis:

Certification basis of this STC is;

Defined on T.C.D.S. T00003NY with the addition of the following later regulation:

14 CFR Part 25, $ 25.981 Amdt 25-125 for Bombardier BD-700-1A10 in the "XRS" configuration.

Defined on I.C.D.S. 100003NY for Bombardier BD-700-1A10 in the "Global 6000" configuration.

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FEDERAL AVIATION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: S100046MC-D Limitations and Conditions: (continued);

1. This approval should not be extended to aircraft of this model 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 aircraft.

2. A copy of this certificate must be maintained as part of the permanent record for the modified aircraft.

3. The installation of Rockwell Collins ARC-210 VHF/UHF Multi-mode Communication System per SIC ST00044MC-D (ARC-210 Gen 4) or ST00238MC (ARC-210 Gen 6), and the installation of structural and electrical provisions for communication equipment per STC ST00045MC-D are prior concurrent requirements.

4. The FAA has not certified the radome or the equipment for which these provisions are intended. You must get additional FAA approval to install the radome or the equipment. The FAA must evaluate the installations to ensure it complies with the applicable airworthiness standards.

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