STC SH210EA

Part 6 of the Civil Air R egulations.

(See page 3 for complete certification basis).

Original Product --Type Certificate N umber :

Installation of Carson C-4 Cabin Modification Kit and co-pilot’s seat in accordance with Carson Drawing List dated 6/15/64, or later FAA approved revisions, with Franklin 6V-335-A engine installation per STC SA1-67.

Carson Helicopters, Inc. Supplement #1, approved 7/6/64, to the FAA Approved Bell 47G Rotorcraft Flight Manual is required, or later FAA approved revisions.

This certificate and the supporting data, which is the basis for approval, shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the A dministrator of the F ederal A viation A dministration.

Scott’s-Bell 47, Inc.

100 Minnesota Avenue Le Sueur, MN 56058

H-1 M ake : Bell Helicopter Textron M odel : 47G Date of application : May 18, 1964

Date of issuance : July 06, 1964 Date reissued : April 30, 2004; December 15, 2010;

August 7, 2014

B y direction of the A dministrator

Original Signed By:

Karol Mordasiewicz (Signature) Karol Mordasiewicz Manager, Airframe and Administrative Branch Chicago Aircraft Certification Office

(Title)

FAA FORM 8110-2-1(10-69) PAGE 2 of 3 PAGES

N umber SH210EA

FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES

Number SH210EA Date of Issuance: July 06, 1964 Date of Reissuance: August 7, 2014 Limitations and Conditio ns (Continued) :

Modifications described under item 3 considered structurally acceptable by EA-219 based on:

1. Report B-AN-2, revised 3/25/61, approved by Form FAA-1600 dated 11/30/61, 12/20/61, 1/17/62, 3/25/62, and 4/10/62, signed by Clyde Heaton DER 1-147 and SW-210 letter of 12/12/61 concerning the cabin modifications.

2. Report B-AN-2, Supplement 1, dated 11/5/63, approved by Form FAA-1600 dated 11/5/63, signed by Clyde E.

Heaton DER 1-147 concerning the co-pilot’s seat and its installation.

3. Satisfactory acceptance of the Franklin 6V-335-A engine per STC SA1-67.

Satisfactory conformity inspections conducted by Inspector Steinert, as evidenced by Part 1 of TIR H968EA-S dated 5/11/64, approved by Ben Rock on 6/24/64.

Satisfactory Flight Test conducted by EA-216, as evidenced by Part II of TIR H968EA-S, dated 7/6/64.

Approval basis CAR 6 of 1/15/51 and amendments 6-1 thru 6-3.

Data Located in Bell 47G STC file, Eastern Region.

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

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