# STC SH574NE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Rilpa Enterprises, Ltd
- Description: Installation of environmental control system.
- Status date: September 20, 2016
- Data sheets: H2SW, H2SW
- Certificate PDF: https://openairdocs.org/files/sha256/9a/e4/9ae42556a5d1823b50c60ead62d7f11c3be011bdc05d85c74ea4fac0283da13e
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A2D55B105A42C30C8625804A0050205D.0001
- Page: https://openairdocs.org/stc/SH574NE

## ADs that name it

None.

## Approved models (2)

- Bell Helicopter Textron (Canada) 206L-3 (TCDS H2SW)
- Bell Helicopter Textron (Canada) 206L-4 (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.

FAA Form 8110-2 (5/14) Page 1 of

Part of the

Signature

Title SH574NE RILPA Enterprises Ltd.

480 Aviation Way N.E.

Calgary, Alberta T2E 7G3 Canada Civil Air Regulations.

1. Configuration A: Installation of Environmental Control System Kit No. 206-C30-A30 in accordance with DOT Approved Casey Copter Top Drawing List 206-D-038, Issue A, dated June 30, 1989, and Installation Instructions 206-S-041, Issue NC, dated December 7, 1987.

2. Configuration B: Installation of Environmental Control System P/N 206-C30-A30-2 (an improved A30 without ducting) in accordance with DOT approved CCAL Top Drawing List 206-D-038, issue B, dated February 21, 1991.

(See Description of Type Design Change continued on Page 3 of 3)

1. Configuration A to D eligible only on Helicopter Model 206L-3.

2. Configuration E to G eligible only on Helicopter Model 206L-4.

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.

Raymond H. Reinhardt Acting Manager New York Aircraft Certification Office Bell Helicopter Textron, Inc.

206 L-3, L-4 October 27, 1995, May 7, 1997, September 14, 2000, November 1, 2000, September 20, 2016 November 7, 1991, May 17, 1993 December 21, 1987 June 7, 1988 IMPORT H2SW 3

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee)

From (Name and address of grantor)

3 SH574NE

FAA Form 8110-2 (5/14) Page 3 of

3 Date Reissued: September 20, 2016

Description of Type Design Change (continued):

3. Configuration C: Installation of Environmental Control System P/N 206-C30-A30-3 (an improved A30 with ducting) in accordance with DOT approved CCAL Top Drawing List 206-D-038, issue B, dated February 21, 1991.

4. Configuration D: Installation of Environmental Control System without heater, P/N 206-C30-A30-26 in accordance with DOT approved CCAL Top Drawing List 206-D-044, issue NC, dated March 14, 1991.

5. Configuration E: Installation of Environmental Control System P/N 206-C30-A30-2 (without ducting) in accordance with DOT approved CCAL Top Drawing List 206-D-038, issue C, dated March 22, 1993.

6. Configuration F: Installation of Environmental Control System P/N 206-C30-A30-3 (with ducting) in accordance with DOT approved CCAL Top Drawing List 206-D-038, issue C, dated March 22, 1993.

7. Configuration G: Installation of Environmental Control System P/N 206-C30-A30-26 (without heater) in accordance with DOT approved CCAL Top Drawing List 206-D-044, issue A, dated March 22, 1993.

8. DOT Approved Rotorcraft Flight Manual Supplement for Bell 206 L-3 Helicopters, 206-F-040, Revision A of June 3, 1988, approved April 21, 1988 and Casey Copter Maintenance Manual Supplement 206-M-043, Issue A dated June 30, 1989, are required with Configuration A.

9. DOT approved Flight Manual Supplement, 206-F-040, Rev. B, dated June 18, 1991 and Maintenance Manual Supplement 206-M-043, issue B, dated February 19, 1991 are required with Configuration B.

10. DOT approved Flight Manual Supplement, 206-F-040, Rev. B, dated June 18, 1991 and Maintenance Manual Supplement 206-M-043, issue B, dated February 19, 1991 are required with Configuration C.

11. DOT approved Flight Manual Supplement, 206-F-048, dated June 18, 1991 and Maintenance Manual Supplement 206-M-047, issue NC, dated March 14, 1991 are required with Configuration D.

12. DOT approved Flight Manual Supplement, 206-F-041, issue NC, dated March 22, 1993 and Maintenance Manual Supplement 206-M-043, issue C, dated June 1, 1992 are required with Configuration E.

13. DOT approved Flight Manual Supplement, 206-F-041, issue NC, dated March 22, 1993 and Maintenance Manual Supplement 206-M-043, issue C, dated June 1, 1992 are required with Configuration F.

14. DOT approved Flight Manual Supplement, 206-F-049, issue NC, dated March 22, 1993 and Maintenance Manual Supplement 206-M-047, issue A, dated June 1, 1992 are required with Configuration G.

----------END---------- SH574NE

## Every issue (1)

- September 20, 2016: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/9a/e4/9ae42556a5d1823b50c60ead62d7f11c3be011bdc05d85c74ea4fac0283da13e)

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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.
