What it approves
Installation of the Garmin GTX Transponder and GTS Traffic System
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 This certificate issued to:
Part of the Original Product – Type Certificate Number: Make:
By Direction of the Administrator Signature Title SR04414NY Maxcraft Avionics Ltd 250-18799 Airport Way Pitt Meadows, British Columbia Canada V3Y 2B4 Federal Aviation Regulations.
1. Installation of the Garmin GTX Transponder and GTS Traffic System must be in accordance with Transport Canada Civil Aviation (TCCA) approved Maxcraft Avionics Ltd Master Data List MDL-34-50-20-063 Revision A, dated September 17, 2018 or later TCCA approved revisions.
(See Description of Type Design Change continued on Page 3 of 4)
1. This installation requires the aircraft to be equipped with a Garmin GTN Navigation system or other position source that has been approved by the Federal Aviation Administration (FAA) as a pairing with the Garmin GTX Transponder to provide an Automatic Dependent Surveillance - Broadcast (ADS-B) Out capability.
(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 SR04414NY
FAA Form 8110-2 (5/14) Page 3 of
4 Date of Issuance: October 17, 2019
Description of Type Design Change (continued):
2. Operation must be in accordance with Maxcraft Avionics Ltd Flight Manual Supplements as follows:
a. Garmin GTX Transponder(s); FMS-34-50-20-063 Revision A, dated March 15, 2018 or later TCCA approved revisions.
b. Garmin GTS Traffic System; FMS-34-45-00-043 Revision A, dated March 15, 2018 or later TCCA approved revisions.
3. Maintenance of the Garmin GTX Transponder and GTS Traffic System must be in accordance with TCCA accepted Maxcraft Avionics Ltd Instructions for Continued Airworthiness ICA-34-50-20-063 Revision A, dated March 15, 2018 or later TCCA accepted revisions.
2. The "Limitations" section of the Maxcraft Avionics Ltd Flight Manual Supplements are applicable as part of this installation as follows:
a. Garmin GTX Transponder(s); FMS-34-50-20-063 Revision A, TCCA approved on February 22, 2019 or later TCCA approved revisions.
b. Garmin GTS Traffic System; FMS-34-45-00-043 Revision A, TCCA approved on February 22, 2019 or later TCCA approved revisions.
3. The installer must determine whether this design change is compatible with previously approved modifications.
4. 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
(See Certification Basis continued on Page 4 of 4) SR04414NY
FAA Form 8110-2 (5/14) Page 4 of
4 SR04414NY Date of Issuance: October 17, 2019 Certification Basis (continued):
b. (continued)
• 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 § 29.1303, 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
• 14 CFR § 29.1325, amendment 29-24
• 14 CFR § 29.1331, 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
----------END----------
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.