# STC SR01079DE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Green Power Monitoring Systems, United States
- Description: Installation of the Green Power Monitoring Systems (GPMS) Foresight MX Condition Monitoring System
- Applied: August 25, 2020
- Status date: April 8, 2021
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 27
- Data sheets: [TCDS R00003RD](https://openairdocs.org/tcds/R00003RD)
- Certificate PDF: https://openairdocs.org/files/sha256/76/5f/765f24946181e018280e0ab11e9863c0d90e50a838dca9c97a74b528bf288266
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D979BC9AE70B915F862586BE007EC198.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR01079DE

## ADs that name it (0)

None.

## Approved models (1)

- Bell Textron Canada Limited 429 ([TCDS R00003RD](https://openairdocs.org/tcds/R00003RD))

## 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.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate SR01079DENumber:

This certificate issued to: Green Power Monitoring Systems 11808 Ferndale Lane Aledo, TX 76008 BB__.

Make: Bell Helicotper Textron Canada LimitedOriginal Product R00003RD7\SH&HUWLILFDWH1XPEHU Model: 429 Description of Type Design Change:

Installation of the Green Power Monitoring Systems (GPMS) Foresight MX Condition Monitoring System in accordance with Document No. B429-3130MDL001, Master Drawing List, Revision 02 dated March 24, 2021, FAA Approved April 7, 2021or later FAA approved revision. Instructions for Continued Airworthiness (ICA) Document No. B429-3130ICA001 Revision IR dated January 29, 2021, FAA accepted April 7, 2021 or later FAA accepted revision is required to be made available at the time of installation. No Flight Manual Supplement is required for this installation.

1. This STC is applicable to all serial numbers for the Bell Helicopter Textron Canada Limited 429 Continued Page 3 of 3

August 25, 2020Date of Application: Date Reissued:

Date of Issuance: April 8, 2021 Date Amended:

Kreg R. Voorhies, ODA Lead administrator Cert Works, LLC ODA Title: ODA No. ODA(AIR)-833887-NM $Q\DOWHUDWLRQRIWKLVFHUWLILFDWHLVSXQLVKDEOHE\DILQHRIQRWH[FHHGLQJRULPSULVRQPHQWQRWH[FHHGLQJ\HDUVRUERWK7KLVFHUWLILFDWHPD\EHWUDQVIHUUHGRUPDGH DYDLODEOHWRWKLUGSHUVRQVE\OLFHQVLQJDJUHHPHQWVLQDFFRUGDQFHZLWK&)53RVVHVVLRQRIWKLV6XSSOHPHQWDO7\SH&HUWLILFDWH 67& GRFXPHQWE\SHUVRQVRWKHUWKDQ WKH67&KROGHUGRHVQRWFRQVWLWXWHULJKWVWRWKHGHVLJQGDWDQRUWRDOWHUDQDLUFUDIWDLUFUDIWHQJLQHRUSURSHOOHU7KH67&¶VVXSSRUWLQJGRFXPHQWDWLRQ GUDZLQJVLQVWUXFWLRQV SURSHOOHUPXVWSURYLGHWKDWSHUVRQZLWKZULWWHQSHUPLVVLRQDFFHSWDEOHWRWKH)$$ 5HI&)5   )$$)RUP  683(56('(635(9,286(',7,21 3DJHRIBBB 3

I United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate SR01079DENumber:

Date oI transfer:

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United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SR01079DE Limitations and Conditions Continued:

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

3. 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.

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the installation of Green Power Monitoring System (GPMS) Foresight MX condition monitoring system in Bell Helicopter Textron Canada Limited 429 is as follows:

a. The type certification basis for Bell Helicopter Textron Canada Limited 429 is shown on TCDS R00003RD for parts not changed or not affected by the change.

b. The certification basis for parts changed or affected by the change since the reference date of application, 8/25/2020, is based upon 14 CFR Part 27, effective February 1, 1965 plus Amendments 27-1 through 27-44. Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be:

Regulations at latest amendment; None Regulations at an intermediate amendment; None Regulations at the amendment level in TCDS R00003RD;

14 CFR Sections: 27.301 Amdt. - ; 27.303 Amdt. - ; 27.305(a) Amdt. - ; 27.307(a) Amdt. 27-26; 27.337

(a) Amdt. 27-26; 27.341 Amdt. - ; 27.561(c) Amdt. 27-32; 27.601(a) Amdt. - ; 27.603 Amdt. 27-16; 27.605

(a) Amdt. 27-16; 27.607(a) Amdt. 27-4; 27.609(a) Amdt. - ; 27.611 Amdt. - ; 27.613(a-d) Amdt. - ; 27.619

(b)(1) Amdt. - ; 27.625(a) Amdt. 27-35; 27.853(a) Amdt. 27-37; 27.863(a),(b)(3-5) Amdt. 27-16; 27.901 (b,c) Amdt. 27-23; 27.1191(e-f) Amdt. 27-2; 27.1301 Amdt. - ; 27.1307(e) Amdt. - ; 27.1309(a),(b) Amdt.

27-21; 27.1351(a),(b)(1) Amdt. 27-13; 27.1357(a),(c) Amdt. 27-13; 27.1365 Amdt. 27-35; 27.1529 Amdt.

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## Every issue (1)

- April 8, 2021: Issued, Current. [certificate](https://openairdocs.org/files/sha256/76/5f/765f24946181e018280e0ab11e9863c0d90e50a838dca9c97a74b528bf288266)

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