What it approves
Installation of Low Fuel Warning Systems
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.
Part 6 of the Civil Air R egulations.
(See page 3 for complete certification basis).
Original Product --Type Certificate N umber :
Installation of Low Fuel Warning Systems in accordance with stamped “FAA Approved” “Low Fuel Warning Bell 47 Installation Instructions,” “Warning Light Flasher Description and Specifications,” and Lake Line Drawing Nos. 76-002-1 thru 76-002-6.
Limi tations and Conditions :
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 dmin istrator 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, 47G-2 Date reissued : January 21, 2004; December 15, 2010;
August 7, 2014
B y direction of the A dministrator
Original Signed By:
Gregory J. Michalik for __ (Signature) Karol Mordasiewicz Manager, Airframe and Administrative Branch Chicago Aircraft Certification Office
(Title)
Date of application : February 15, 1977
Date of issuance : April 27, 1977
FAA FORM 8110-2-1(10-69) PAGE 2 of 3 PAGES
N umber SH165GL
FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES
Number SH165GL Date of Issuance: April 27, 1977 Date of Reissuance: August 7, 2014 Limitations and Conditions:
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.
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 altitude”
------------End-----------
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 2
Every issue · 3
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| August 7, 2014 | Reissued, current | Certificate |
| December 15, 2010 | Reissued, earlier issue | Certificate |
| January 21, 2004 | Reissued, earlier issue | Certificate |