STC SH166GL

Part 6 of the Civil Air R egulations.

Original Product --Type Certificate N umber :

Descriptio n of Type Design Change:

Installation of Low Fuel Warning System in accordance with stamped “FAA Approved” “Low Fuel Warning Bell 47 Installations,” “Warning Light Flasher Description and Specifications,” and Lake Line Drawing Nos. 76-002-1 thru 76-002-6.

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 th e A dministrator of the F ederal A viation A dministration.

Scott’s-Bell 47, Inc.

100 Minnesota Avenue Le Sueur, MN 56058

2H3 M ake : Bell Helicopter Textron M odel : 47G-2A, G-2A-1, G-3, G-3B, G-3B-1, G-3B-2, G-3B-2A, G-4, G-4A, G-5, G-5A Date of application : February 15, 1977

Date of issuance : April 27, 1977 Date reissued : January 21, 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 3 of 3 PAGES

N umber SH166GL Date of Issuance: April 27, 1977 Date of Reissuance: August 07, 2014

Limitations and Conditions: (Continued) :

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 wr itten evidence of that permission.

A copy of this STC must be included in the permanent record of each airplane modified in accordance with this STC.

Placards The following placards are required in the locations noted:

Adjacent to the warning light: “Low Fuel”

Adjacent to the test switch: “Press to Test”

In a location in full view of the pilot: “When light flashes, approximately 5 US gallons usable at 80 knots IAS with two fuel tank configuration – varies with aircraft attitude”

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