STC SH162WE

Supplemental type certificate · Scott's Bell 47 Inc

Holder
Scott's Bell 47 Inc · United States
Status
Current · Reissued
Status date
August 7, 2014
Applied
January 14, 1974
Product
Aircraft · Rotorcraft
Certification basis
Part 21
Data sheet
TCDS2H3

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of exhaust muffler assembly.

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 :

Description of Type Des ign Change:

Installation of exhaust muffler assembly in accordance with FAA sealed Aircraft Technical Service, Inc. A & H Welding Company Drawing Summary 1446, Change “D”, or later FAA approved revision.

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 dministrat ion.

Scott’s-Bell 47, Inc.

100 Minnesota Avenue Le Sueur, MN 56058

2H3 M ake : Bell Helicopter Textron M odel : 47G-4, 47G-4A Date of application : January 14, 1974

Date of issuance : March 08, 1974 Date reissued : 12/12/95; 4/30/04; 12/15/10; 8/7/14

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 SH162WE

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

Number SH162WE Date of Issuance: March 08, 1974 Date of Reissuance: August 7, 2014 Limitations and Conditions (Continued) :

The limitations and conditions of Data Sheet 2H3 apply, except as described on page 3 of this STC. A copy of this STC must be included in the permanent records of each airplane modified in accordance with this STC.

1. The FAA approved Rotorcraft Flight Manual Supplement, dated March 8, 1974, is required with this installation.

2. The cylinder head temperature pick-up must be changed from cylinder #2 (top right looking forward) to cylinder #6 (bottom right looking forward). A description of this change must be included in the Installation Instructions.

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

4. 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.

------------End-----------

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 2

MakeModelData sheet
Scotts-Bell 47 Inc47G-42H3
Scotts-Bell 47 Inc47G-4A2H3

Every issue · 2

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
August 7, 2014Reissued, currentCertificate
December 15, 2010Reissued, earlier issueCertificate