STC SR01048DE

FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___

Part of .

SR01048DE RSG Aviation Inc.

3901 North Main St., Hangar 2S Fort Worth, TX 76106 29 Federal Aviation Regulations H4SW Bell 212, 412, 412EP (412EP SN's 36087 thru 36999) Installation of Astronautics AFI4700 Roadrunner Electronic Flight Instrument (EFI) in accordance with Document No.

RSG-MDL-001, Master Drawing List, Bell 212/412/412EP AFI4700 EFIS, Revision IR dated 5/29/2020, FAA approved 7/16/2020 or later FAA approved revision. FAA Approved Flight Manual Supplement, Document No. RSG-FMS-001, Revision IR dated 4/19/2020, FAA approved 7/16/2020 or later FAA approved revision, is required for this installation. Instructions for Continued Airworthiness (ICA), Document No. RSG-ICA-001, Revision IR dated 4/23/2020, FAA accepted 7/16/2020, or later FAA accepted revision is required to be made available at installation.

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

Continued Page 3 of 3 11/13/2019 07/16/2020 Kreg R. Voorhies, ODA Lead administrator Cert Works, LLC ODA ODA No. ODA(AIR)-833887-NM 3

FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___

SR01048DE 3

SR01048DE Limitations and Conditions Continued:

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.

3. Additional FAA approval and substantiation is required for installation of powered electrical or hydraulically driven equipment utilizing this installation.

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Bell 212/412/412EP installation of the Astronautics AFI4700 Electronic Flight Instruments is as follows:

a. The type certification basis for Bell 212/412/412EP rotorcraft is shown on TCDS H4SW for parts not changed or not affected by the change.

b. The certification basis for parts changed or affected by the change since the reference date of application, 11/13/2019, is based upon 14 CFR Part 29, effective February 1, 1965 plus Amendments 29-1 through 29-57. Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be:

Regulations at the latest amendment;

14 CFR Sections: 29.301 Amdt. - ; 29.303 Amdt. - ; 29.305(a) Amdt. - ; 29.307(a) Amdt. 29-30; 29.337

(a) Amdt. 29-30; 29.341 Amdt. - ; 29.561(a-c) Amdt. 29-38; 29.601(a) Amdt. - ; 29.603 Amdt. 29-17;

29.605 Amdt. 29-17; 29.609 Amdt. - ; 29.610 Amdt. 29-53; 29.611 Amdt. - ; 29.613 Amdt. 29-30; 29.619

(b)(1) Amdt. - ; 29.625 Amdt. 29-42; 29.771(a-c) Amdt. 29-24; 29.773(a) Amdt. 29-57; 29.777 Amdt. - ;

29.785(a) Amdt. 29-42; 29.853(a)(2-4) Amdt. 29-23; 29.1301 Amdt. - ; 29.1303(f-h) Amdt. 29-24;

29.1309(a),(b)(2)(c),(d),(e)(1,2),(3)(i),(g) Amdt. 29-53; 29.1316 Amdt. 29-53; 29.1317 Amdt. 29-49;

29.1321(a,b,f,g) Amdt. 29-21; 29.1322(a-d) Amdt. 29-12; 29.1331(a) Amdt. 29-24; 29.1333(b) Amdt.

29-24; 29.1351(a) Amdt. 29-42; 29.1353(a) Amdt. 29-15; 29.1353(b) Amdt. 29-15; 29.1357(a-d) Amdt.

29-24; 29.1359(b-c) Amdt. 29-42; 29.1381 Amdt. - ; 29.1501(a,b) Amdt. 29-15; 29.1523 Amdt. - ;

29.1525 Amdt. 29-24; 29.1529 Amdt. 29-20; 29.1541(a)(1)(2) Amdt. - ; 29.1555(a) Amdt. 29-24; 29.1581 (a,b,d) Amdt. 29-15; 29.1583(d,e) Amdt. 29-24; 29.1585(a) Amdt. 29-24; B29.8(b)(3)(4) Amdt. 29-40

Regulations at an intermediate amendment;

None

Regulations at the amendment level in TCDS H4SW;

None

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