STC SR04413NY

FAA Form 8110-2 (5/14) Page 1 of This certificate issued to:

Part of the Original Product – Type Certificate Number: Make:

By Direction of the Administrator Signature Title SR04413NY Maxcraft Avionics Ltd 250-18799 Airport Way Pitt Meadows, British Columbia Canada V3Y 2B4 Federal Aviation Regulations.

1. Installation of the Garmin GTN Navigator System must be in accordance with Transport Canada Civil Aviation (TCCA) approved Maxcraft Avionics Ltd Master Data List MDL-34-50-99-153 Revision A, dated February 8, 2019 or later TCCA approved revisions.

2. Operation of the Garmin GTN Navigator System must be in accordance with TCCA approved Maxcraft Avionics Ltd Flight Manual Supplement FMS-34-50-99-153 Revision A, dated March 10, 2018 or later TCCA approved revisions.

(See Description of Type Design Change continued on Page 3 of 4)

1. The "Limitations" section of Maxcraft Avionics Ltd Flight Manual Supplement FMS-34-50-99-153 Revision A, TCCA approved on February 22, 2019 or later TCCA approved revisions is applicable as part of this installation.

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

(See Limitations and Conditions continued on Page 3 of 4) Anthony E. Gallo Manager New York ACO Branch Airbus Helicopters SA-365N, SA-365N1, AS-365N2, AS 365 N3 April 12, 2019 October 17, 2019 IMPORT H10EU 4

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

To (Name and address of transferee)

From (Name and address of grantor)

4 SR04413NY

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

4 Date of Issuance: October 17, 2019

Description of Type Design Change (continued):

3. Maintenance of the Garmin GTN Navigator System must be in accordance with TCCA accepted Maxcraft Avionics Ltd Instructions for Continued Airworthiness ICA-34-50-90-153 Revision A, dated March 7, 2018 or later TCCA accepted revisions.

3. 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.

Certification Basis:

Based on title 14 Code of Federal Regulations (CFR) 21.115 and 21.101, and the Federal Aviation Administration (FAA) policy for design changes that are identified as not significant in FAA Order 8110.48, the type certification basis for Airbus Helicopters Models SA-365N, SA-365N1, AS-365N2, AS 365 N3 is as follows:

a. The type certification basis for Airbus Helicopters Models SA-365N, SA-365N1, AS-365N2, AS 365 N3 as shown on Type Certificate Data Sheets (TCDS) H10EU for parts not changed or not affected by the change.

b. The type certification basis for Airbus Helicopters Models SA-365N, SA-365N1, AS-365N2, AS 365 N3 as shown on Type Certificate Data Sheets (TCDS) H10EU for parts changed or affected by the change in addition to:

• 14 CFR § 29.1, amendment 29-39

• 14 CFR § 29.25, amendment 29-51

• 14 CFR § 29.307, amendment 29-30

• 14 CFR § 29.561, amendment 29-38

• 14 CFR § 29.603, amendment 29-17

• 14 CFR § 29.605, amendment 29-17

• 14 CFR § 29.610, amendment 29-53

• 14 CFR § 29.613, amendment 29-30

• 14 CFR § 29.771, amendment 29-24

• 14 CFR § 29.773, amendment 29-56

• 14 CFR § 29.853, amendment 29-23

• 14 CFR § 29.863, amendment 29-17

• 14 CFR § 29.1303, amendment 29-24

• 14 CFR § 29.1309, amendment 29-53

• 14 CFR § 29.1316, amendment 29-53

• 14 CFR § 29.1317, amendment 29-49

• 14 CFR § 29.1321, amendment 29-21

(See Certification Basis continued on Page 4 of 4) SR04413NY

FAA Form 8110-2 (5/14) Page 4 of

4 SR04413NY Date of Issuance: October 17, 2019 Certification Basis (continued):

b. (continued)

• 14 CFR § 29.1325, amendment 29-24

• 14 CFR § 29.1331, amendment 29-24

• 14 CFR § 29.1333, amendment 29-24

• 14 CFR § 29.1351, amendment 29-42

• 14 CFR § 29.1355, amendment 29-24

• 14 CFR § 29.1357, amendment 29-24

• 14 CFR § 29.1359, amendment 29-42

• 14 CFR § 29.1529, amendment 29-20

• 14 CFR § 29.1583, amendment 29-24

• 14 CFR § 29.1585, amendment 29-24

• 14 CFR section B29.4(f), amendment 29-21

• 14 CFR section B29.8(a) and (b), amendment 29-40

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