What it approves
Installation of the Mid Continent MD302 Standby Attitude Module
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
Part of the
Signature
Title SR04440NY Maxcraft Avionics Ltd.
250-18799 Airport Way Pitt Meadows, British Columbia Canada, V3Y 2B4 Federal Aviation Regulations.
1. Installation of the Mid Continent MD302 Standby Attitude Module must be in accordance with Maxcraft Avionics Ltd. Master Data List MDL-34-20-62-015, Revision B, dated May 10, 2018 or later Transport Canada approved revision.
2. Operation must be in accordance with Maxcraft Avionics Ltd. Flight Manual Supplement FMS-34-20-62-015 Revision B, dated May 10, 2018 or later Transport Canada approved revision.
(See 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.
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.
(See Limitations and Conditions continued on Page 3 of 3)
Anthony E. Gallo Manager New York ACO Branch Sikorsky S-76A, S-76B, S-76C July 8, 2019 January 28, 2020 IMPORT H1NE 3
FAA Form 8110-2 (5/14) Page 2 of
To (Name and address of transferee)
From (Name and address of grantor)
3 SR04440NY
FAA Form 8110-2 (5/14) Page 3 of
3 Date of Issuance: January 28, 2020
Description of Type Design Change (continued):
3. Maintenance must be in accordance with Maxcraft Avionics Ltd. Instructions for Continued Airworthiness ICA-34-20-62-015, Revision A, dated April 6, 2016, or later Transport Canada accepted revision.
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 Sikorsky Models S-76A, S-76B, and S-76C is as follows:
a. The type certification basis for Sikorsky Models S-76A, S-76B, and S-76C as shown on Type Certificate Data Sheets (TCDS) H1NE for parts not changed or not affected by the change.
b. The type certification basis for Sikorsky Models S-76A, S-76B, and S-76C as shown on Type Certificate Data Sheets (TCDS) H1NE for parts changed or affected by the change in addition to:
Regulations at latest amendment 29-1 through 29-53
29.27, 29.29, 29.301, 29.303, 29.305, 29.307, 29.561, 29.601, 29.603, 29.605, 29.607, 29.609, 29,.610, 29.611,
29.613, 29.777, 29.863, 29.1301, 29.1303, 29.1309, 29.1316, 29.1317, 29.1321, 29.1322, 29.1325, 29.1331,
29.1333, 29.1357, 29.1381, 29.1431, 29.1529, 29.1545, 29.1581, 29.1583, 29.1585
Regulations at intermediate amendment
29.1 Amendment 29-21
29.25 Amendment 29-12
29.773 Amendment 29-3
29.1323 Amendment 29-39
29.1351 Amendment 29-40
29.1353 Amendment 29-15
29.1359 Amendment 29-0
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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.