STC SA03641NY

FAA Form 8110-2 (5/14) Page 1 of

Part of the

Signature

Title SA03641NY Maxcraft Avionics Ltd.

250-18799 Airport Way Pitt Meadows, British Columbia Canada V3Y 2B4 Federal Aviation Regulations.

1. Installation/Upgrade of L3 Avionics SKY899 Traffic Collision Avoidance System (TCAS I), displayed on Sandel ST3400 shall be in accordance with Maxcraft Avionics Ltd. Master Data List MDL-34-45-00-036 Revision B, dated November 19, 2015 or later Transport Canada approved revision.

2. Operation shall be in accordance with the Maxcraft Avionics Ltd. Flight Manual Supplement FMS-34-45-00-036 Revision A, dated April 15, 2015 or later Transport Canada approved revision.

(See Description of Type Design Change continued on Page 3 of 3)

1. Scope of approval does not include new penetration(s) of pressure vessel. Separate approval is required for structural installation.

2. The installer must determine whether this design is compatible with other previously approved modifications.

3. If the holder agrees to permit another person to use the certificate to alter the product, the holder must give the other person written evidence of that permission.

Raymond Reinhardt Acting Manager New York Aircraft Certification Office Beechcraft Corporation 200, 200C, B200, B200C, 300, B300, B300C June 5, 2015 December 18, 2015 IMPORT A24CE 3

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee)

From (Name and address of grantor)

3 SA03641NY

FAA Form 8110-2 (5/14) Page 3 of

3 Date of Issuance: December 18, 2015

Description of Type Design Change (continued):

3. Maintenance must be in accordance with the Maxcraft Avionics Ltd. Instructions for Continued Airworthiness ICA-34-45-00-036 Revision B, dated November 16, 2015 or later Transport Canada approved revision.

Certification Basis:

Based on 14 CFR 21.115 and 21.101, and the FAA policy for not significant changes in FAA Order 8110.48, the certification basis for this modification to the Beechcraft Corporation 200, 200C, B200, B200C, 300, B300, B300C is as follows:

a. The type certification basis for the Beechcraft Corporation 200, 200C, B200, B200C, 300, B300, B300C as shown on the TCDS A24CE for parts not changed or not affected by the change.

b. The type certification basis for the Beechcraft Corporation 200, 200C, B200, B200C, 300, B300, B300C as shown on the TCDS A24CE for parts changed or affected by the change with the following requirements:

Compliance with 14 CFR Part 23 including Amendments 23-1 through 23-34.

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