# STC SH4676SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: DeVore Aviation Corporation of America, a New Mexico Corporation, United States
- Description: Installation of Tail Rotor Floodlights on the upper surface of the horizontal stabilizer
- Applied: February 10, 1982
- Status date: April 30, 2014
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 27
- Data sheets: [TCDS H7EU](https://openairdocs.org/tcds/H7EU)
- Certificate PDF: https://openairdocs.org/files/sha256/95/e1/95e13da23ad5778bfa259502a70612c8b2b43ef6239c9d7f404d3508a48d521c
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/540C2A7950063B2986257CD3004A7718.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SH4676SW

## ADs that name it (0)

None.

## Approved models (8)

- Agusta S.p.A. A109 ([TCDS H7EU](https://openairdocs.org/tcds/H7EU))
- Agusta S.p.A. A109A ([TCDS H7EU](https://openairdocs.org/tcds/H7EU))
- Agusta S.p.A. A109A II ([TCDS H7EU](https://openairdocs.org/tcds/H7EU))
- Agusta S.p.A. A109C ([TCDS H7EU](https://openairdocs.org/tcds/H7EU))
- Agusta S.p.A. A109E ([TCDS H7EU](https://openairdocs.org/tcds/H7EU))
- Agusta S.p.A. A109K2 ([TCDS H7EU](https://openairdocs.org/tcds/H7EU))
- Agusta S.p.A. A119 ([TCDS H7EU](https://openairdocs.org/tcds/H7EU))
- Agusta S.p.A. AW119 MKII ([TCDS H7EU](https://openairdocs.org/tcds/H7EU))

## 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.

FAA FORM 8110-2(8/13) PAGE 1 of 2 PAGES

Number: SH4676SW This certificate issued to DeVore Aviation Corporation of America, a New Mexico Corporation 6104 Jefferson, N.E.

Albuquerque, NM 87109-3410 Part 27 of the Federal Aviation Regulations.

Original Product – Type Certificate Number : H7EU Make: AGUSTA S.p.A.

Model: A109, A109A, A109A II, A109C, A109K2, A109E, A119, and AW119 MKII Description of Type Design Change:

Installation of Tail Rotor Floodlights on the upper surface of the horizontal stabilizer in accordance with DeVore Aviation Corporation of America, Top Drawing, 10900001, Revision H, dated April 24, 2013, or later Federal Aviation Administration (FAA) approved revision. Rotorcraft Flight Manual Supplement (RFMS), Document No. DR-761, Revision A, dated May 22, 2013, or later FAA approved revision is required for the 10900001-5 installation only. Instructions for Continued Airworthiness (ICA), Document No. DR-760, Revision 2, dated May 16, 2013, or later FAA accepted revision is required for the 10900001-5 installation only.

The installer must determine whether this design change is compatible with previously approved modifications. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

Date of application: February 10, 1982 Date reissued: January 31, 2000; April 30, 2014 Date of issuance: May 17, 1982 Date amended: July 9, 1982; February 10, 1991; February 16, 1994; October 9, 2001; September 15, 2006; May 28, 2013

Signature Scott A. Horn Title Manager, Rotorcraft Certification Office Southwest Region P/N SA3487RC-R

**PE APG ASW-170**

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

## Every issue (2)

- April 30, 2014: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/95/e1/95e13da23ad5778bfa259502a70612c8b2b43ef6239c9d7f404d3508a48d521c)
- May 28, 2013: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/0a/e3/0ae3cf3a800b3b274bfc7d9ff79097558f3cc4ce60bc33c28d6be319ad529896)

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