STC SR00764DE

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

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

Mode l:

By Direction of the Administrator Signature Title Peregrine 7385 S. Peoria Street, Unit C4 Englewood, CO 80112 29 3 SR00764DE Federal Aviation Regulations H1NE S-76A, S-76B, S-76C Installation of Automatic Dependent Surveillance – Broadcast (ADS-B) Out functionality using the Trig Avionics TT22 Transponder and Freeflight Systems 1201 or Accord Technology NexNav Mini 21000 Global Positioning System (GPS) with Wide Area Augmentation System (WAAS), in accordance with Master Drawing List, E-DI-13-0002, Rev. A, dated January 10, 2014, or later FAA approved revision.

1. The installer must determine if this design change is compatible with previously approved modifications.

2. The modified rotorcraft must be maintained in accordance with the ADS-B Out System Instructions for Continued Airworthiness, E-DI-13-0008 Rev. IR, dated February 13, 2014, or later FAA approved revision.

(continued on Page 3) March 28, 2014; December 19, 2018 Todd Dixon, Manager, Denver ACO Branch Compliance and Airworthiness Division Sikorsky September 5, 2013 March 13, 2014 August 8, 2019

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

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

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

Limitations and Conditions (continued)

3. The following rotorcraft flight manual supplement identified below must be maintained onboard the modified aircraft:

Rotorcraft Flight Manual Supplement to the Sikorsky Rotorcraft Model S-76A, S-76B, S-76C Rotorcraft Flight Manual, ADS-B Transmitter: Trig TT22 Transponder, Position Source: Freeflight 1201 GPS, E-DI-13-0009, Rev. IR, dated February 27, 2014, or later FAA-approved revision.

4. This STC is limited to installations where the Trig TT22 transponder is replacing a stand–alone transponder system. This STC is not applicable for rotorcraft that includes an existing remote-mount transponder that is integrated with and controlled by an electronic flight display system.

5. This installation does not include the following:

a. ADS-B In functionality

b. Heading interface

c. TCAS interface

6. A copy of this certificate, its continuation sheet, and the FAA-approved rotorcraft flight manual supplement per item number 3 above, must be maintained as part of the permanent records of the modified rotorcraft.

7. If the STC holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

8. Based on 14 CFR §21.101, §21.115, and FAA order 8110.48A, the type certification basis for parts changed or affected by the change due to this modification is the same as the regulations at the TCDS Certification Basis, amendments 29-1 through 29-11 and 29-24:

29.301(a)(b)(c), 29.303, 29.305(a)(b), 29.307(a)(b), 29.309(a)(b)(c)(d)(e)(f)(g), 29.321(a)(b), 29.337, 29.341, 29.471(a)(b), 29.561(a)(b)(d),

29.561(c), 29.601(a)(b), 29.603(a)(b), 29.605, 29.607, 29.609(a)(b), 29.611(a)(b)(c), 29.613(a)(b)(c)(d), 29.619(a)(b), 29.625(a)(b)(c),

29.671(a)(b), 29.771(a)(b), 29.773(a)(2), 29.777(a)(b), 29.1301(a)(b)(c)(d), 29.1307(e), 29.1309(a)(b)(c), 29.1325(d), 29.1351(a)(1)(2),

29.1353(a)(b), 29.1357(a)(c)(d), 29.1359(a)(b), 29.1381(a)(b), 29.1431(a)(b), 29.1519, 29.1529, 25.1581(a)(b), 29.1583(c), and 29.1585.

Note: It has been determined that this modification is a No Acoustical Change per 14 CFR 21.93 (b).

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