# STC SH1030NE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Litton Special Devices, United States
- Description: Installation of Litton Special Devices Turbine Outlet Temperature (TOT) Indicator P/N s 94291001-02, -03, -04, -11 thru -15, or -31 thru -35
- Applied: November 10, 1992
- Status date: May 29, 2008
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW)
- Certificate PDF: https://openairdocs.org/files/sha256/9e/e9/9ee94270f4ac2963d175de7d2dbbac0a15d52e4d425dc0ceb182003ddd255f1f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/71A1CE9857B42AEF86257488005BBB0C.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SH1030NE

## ADs that name it (0)

None.

## Approved models (5)

- Bell Helicopter Textron (Canada) 206B ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron (Canada) 206L ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron (Canada) 206L-1 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron (Canada) 206L-3 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron (Canada) 206L-4 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))

## 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.

Number SH1030NE This certificate issued to

Part 6 the Civil Air Regulations.

Installation of Litton Special Devices Turbine Outlet Temperature (TOT) Indicator P/N’s 94291001-02, -03, -04, -11 thru -15, or -31 thru -35 in accordance with Installation Drawing 9201ER05 Rev. C dated February 20, 1996 and Drawing List No. 9201DL001 Rev.

L dated February 20, 1996.

1. The following Litton Special Devices Flight Manual Supplements are required with this installation in the following Bell Helicopters: Model 206B Supplement No.’s 9201FM001 or 9201FM002 FAA Approved 2/25/93; Model 206L Supplement No.

9201FM003 FAA Approved February 25, 1993; Model 206L-1 Supplement No. 9201FM008 FAA approved April 29, 1994; Model 206L-1 as modified per STC No.’s SH296NM or SH5695SW Supplement No. 9201FM004 FAA Approved December 8, 1992;

Model 206L-3 Supplement No.’s 9201FM005 FAA Approved December 8, 1992 or 9201FM007 FAA Approved February 15, 1994 and Model 206L-4 Supplement No. 9201FM006 FAA Approved February 15, 1994.

2. Litton Special Devices Instructions for Continued Airworthiness Report No. 9201ER004 Rev. E dated February 20, 1996, or later FAA approved revision, is required for continued airworthiness of this installation.

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 the certificate to alter a product, the holder must give the other person written evidence of that permission.

, Components Group Springfield Operations 750 West Sproul Road Springfield, PA 19064 H2SW Bell Helicopters 206B, 206L, 206L-1 206L-3, 206L-4 Date of application: November 10, 1992

Date of issuance: December 8, 1992

Date reissued: May 29, 2008

Date amended: February 25, 1993, February 15, 1994, April 29, 1994, March 21, 1996

( Signature) Anthony Socias Manager New York Aircraft Certification Office

(Title)

FAA Form 8110-2-1(10-69) Page 2 of 2

Number Date of Issuance:

## Every issue (1)

- May 29, 2008: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/9e/e9/9ee94270f4ac2963d175de7d2dbbac0a15d52e4d425dc0ceb182003ddd255f1f)

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