# STC SH165GL

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Scott's Bell 47 Inc
- Description: Installation of Low Fuel Warning Systems
- Status date: August 7, 2014
- Data sheets: H-1, H-1
- Certificate PDF: https://openairdocs.org/files/sha256/fc/9b/fc9b583a07e63c9d2f7a80d845272b8b857a7955f20ef5ee91f04f833f6e966d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F071152C1C9D489C86257DC700515C1D.0001
- Page: https://openairdocs.org/stc/SH165GL

## ADs that name it

None.

## Approved models (2)

- Scotts-Bell 47 Inc 47G (TCDS H-1)
- Scotts-Bell 47 Inc 47G-2 (TCDS H-1)

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can 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-----------

## Every issue (3)

- August 7, 2014: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/fc/9b/fc9b583a07e63c9d2f7a80d845272b8b857a7955f20ef5ee91f04f833f6e966d)
- December 15, 2010: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/f9/36/f936326f893bba07d2213e646d652670afede25b9d98c72d169e530b37d61557)
- January 21, 2004: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/df/e3/dfe3441126568a150312a1a9f8274c933668e6791d33063db26715c54b50519d)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.